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{{#Wiki_filter:Page 1 of I From:, Sent: To:  
{{#Wiki_filter:Page 1 of I From:,                       Halter, Mandy Sent:                       Monday, June 20, 2011 1:33 PM To:                         'pbode@entergy.com'


==Subject:==
==Subject:==
Attachments:
Part 21 - KASI MOV and AOV Software Attachments:                EN46955.pdf; KVAP-Software-for-AOV-&-MOV-design-basis-ma rgin-calculations-for-JOG-Program-Implementation-GL-96-05-Periodic-Verification-margin-improvement.pdf
Halter, Mandy Monday, June 20, 2011 1:33 PM'pbode@entergy.com' Part 21 -KASI MOV and AOV Software EN46955.pdf; KVAP-Software-for-AOV-&-MOV-design-basis-ma rgin-calculations-for-JOG-Program-Implementation-GL-96-05-Periodic-Verification-margin-improvement.pdf Paul, Attached is the Part 21 that came out of Oconee (attached above EN 46955). The defect is related to errors in the Kalsi Engineering Valve and Actuator Program (KVAP) software that provide default flow and torque coefficients for ball and plug valves which can affect margin predictions.
: Paul, Attached is the Part 21 that came out of Oconee (attached above EN 46955). The defect is related to errors in the Kalsi Engineering Valve and Actuator Program (KVAP) software that provide default flow and torque coefficients for ball and plug valves which can affect margin predictions.
Please confirm whether or not Indian Point has reviewed this issue for applicability.
Please confirm whether or not Indian Point has reviewed this issue for applicability.
Thanks and kind regards, Mandy Mandy Halter U.S. Nuclear Regulatory Commission Resident Inspector Indian Point Energy Center -Unit 3 (914) 739-8565 file://C:\Documents and Settings\lnw\Local Settings\Temporary Internet Files\Content.Outlook\OQSQO7...
Thanks and kind regards, Mandy Mandy Halter U.S. Nuclear Regulatory Commission Resident Inspector Indian Point Energy Center - Unit 3 (914) 739-8565 file://C:\Documents and Settings\lnw\Local Settings\Temporary Internet Files\Content.Outlook\OQSQO7...         7/22/2011
7/22/2011 KVAP The Leading AOV/ OV Software....
 
-~ V j...Serving the Energy Industries Kalsi Engineering, Inc.745 Park:Two Drive Sugar Land, TX 77478-2885 (281)240-6500 www;kalsi:com,.
KVAP The Leading AOV/             OV Software....
© Copyright Kalsi Engineering, Inc. 2007 All rights, resberv.ed  
                                                                  -~     V j
-.Revision Date. December 17, 2007 KVAP, The AO V/MO V Software with Technology Table of Contents Page Introduction to KVAP 2 Background of Kalsi Engineering Flow Loop Testing and Validated Model Development Program for KVAP 6 KVAP Software Capabilities 8 KVAP Scope of Valves and Actuators 9 Typical KVAP Screens 13 Company Background and Experience Relevant to AOVs, MOVs, and Check Valves 20 Key Personnel 28 KVAP References and Other Significant Documents Developed by Kalsi Engineering, Inc. 33 KVAP Development/Enhancement/History 38 KVAP Training Seminar Outline 41 Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 2 Introduction to KVAP The AOV/MOV Software with Technology KVAP, the Kalsi Valve & Actuator Program, is a state-of-the-art software for performing reliable design basis calculations for all common types of globe, gate, diaphragm, butterfly, ball, and plug valves.The KVAP software represents a significant advancement over all other design basis calculation software packages (e.g. EPRI MOV PPM, ACE, AirBase, etc.) available in the industry for it incorporates validated models that the industry was lacking for many different types of valves commonly used in AOV/MOV applications (see Tables I(A) through I(D)). These validated models are the outcome of a very comprehensive flow loop testing program conducted by Kalsi Engineering, Inc., (KEI) to overcome the limitations of valve manufacturers' data, and the new database of torque/flow coefficients in KVAP, based upon four years of extensive flow loop testing on a wide range of valve designs, provides more accurate, position dependent bounding predictions, while eliminating excessive conservatism, as well as, non-conservatism found in the EPRI MOV PPM software (see the Part 21 and EPRI Error Notices below).KVAP was developed by the same KEI valve specialists who previously developed the EPRI MOV PPM and software modules. All testing, analytical model development, software development, and verification and validation activities were performed under the Kalsi Engineering, Inc., quality assurance program, which meets IOCFR50 Appendix B requirements.
                                          ... Serving the Energy Industries Kalsi Engineering, Inc.
KVAP Benefits Key advantages offered by KVAP to it's over 50 current users are:* KVAP is the only software that includes validated valve models with position dependent accuracy (necessary for AOV evaluations) that the industry was lacking; these enable reliable design basis calculations for accurately quantifying AOV/MOV margins, not possible with previous industry models" KVAP models are based upon/validated against a comprehensive database of 1OCFR50 Appendix B test results for incompressible flow and compressible flow tests performed on all common types of quarter-turn valves (over 2500 tests), that provide reliable predictions while eliminating excessive conservatism in earlier models (e.g., EPRI MOV PPM).KVAP models provide more accurate, bounding predictions that typically result in larger margins in AOVs/MOVs* The larger margins in AOVs/MOVs provided by KVAP eliminate unnecessary equipment modifications, especially those, resulting from excessively conservative methodologies (e.g., EPRI MOV PPM) in many applications
745 Park:Two Drive Sugar Land, TX 77478-2885 (281)240-6500 www;kalsi:com,.
                                © Copyright Kalsi Engineering, Inc. 2007 All rights, resberv.ed .    -
Revision Date. December 17, 2007
 
KVAP, The AO V/MO V Software with Technology Table of Contents Page Introduction to KVAP                                             2 Background of Kalsi Engineering Flow Loop Testing and Validated Model Development Program for KVAP                               6 KVAP Software Capabilities                                       8 KVAP Scope of Valves and Actuators                               9 Typical KVAP Screens                                             13 Company Background and Experience Relevant to AOVs, MOVs, and Check Valves                                                     20 Key Personnel                                                   28 KVAP References and Other Significant Documents Developed by Kalsi Engineering, Inc.                                         33 KVAP Development/Enhancement/History                             38 KVAP Training Seminar Outline                                   41 Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology                                                       2 Introduction to KVAP The AOV/MOV Software with Technology KVAP, the Kalsi Valve & Actuator Program, is a state-of-the-art software for performing reliable design basis calculations for all common types of globe, gate, diaphragm, butterfly, ball, and plug valves.
The KVAP software represents a significant advancement over all other design basis calculation software packages (e.g. EPRI MOV PPM, ACE, AirBase, etc.) available in the industry for it incorporates validated models that the industry was lacking for many different types of valves commonly used in AOV/MOV applications (see Tables I(A) through I(D)). These validated models are the outcome of a very comprehensive flow loop testing program conducted by Kalsi Engineering, Inc., (KEI) to overcome the limitations of valve manufacturers' data, and the new database of torque/flow coefficients in KVAP, based upon four years of extensive flow loop testing on a wide range of valve designs, provides more accurate, position dependent bounding predictions, while eliminating excessive conservatism, as well as, non-conservatism found in the EPRI MOV PPM software (see the Part 21 and EPRI Error Notices below).
KVAP was developed by the same KEI valve specialists who previously developed the EPRI MOV PPM and software modules. All testing, analytical model development, software development, and verification and validation activities were performed under the Kalsi Engineering, Inc., quality assurance program, which meets IOCFR50 Appendix B requirements.
KVAP Benefits Key advantages offered by KVAP to it's over 50 current users are:
* KVAP is the only software that includes validated valve models with position dependent accuracy (necessary for AOV evaluations) that the industry was lacking; these enable reliable design basis calculations for accurately quantifying AOV/MOV margins, not possible with previous industry models
    " KVAP models are based upon/validated against a comprehensive database of 10CFR50 Appendix B test results for incompressible flow and compressible flow tests performed on all common types of quarter-turn valves (over 2500 tests), that provide reliablepredictions while eliminating excessive conservatism in earlier models (e.g., EPRI MOV PPM).
KVAP models provide more accurate, bounding predictions that typically result in larger margins in AOVs/MOVs
* The larger margins in AOVs/MOVs provided by KVAP eliminate unnecessary equipment modifications, especially those, resulting from excessively conservative methodologies (e.g.,
EPRI MOV PPM) in many applications
* The larger margins in AOVs/MOVs provided by KVAP reduce the frequency of periodic verification testing required to meet the Joint Owners Groups recommendations
* The larger margins in AOVs/MOVs provided by KVAP reduce the frequency of periodic verification testing required to meet the Joint Owners Groups recommendations
* KVAP validated models eliminate the need for expensive in-situ dynamic testing, resulting in savings of thousands of dollars per valve" The user-friendly graphic interface eliminates potential errors commonly made during calculations, enabling a more efficient completion of evaluations" KVAP does not have the non-conservatism found, and limitations imposed in the use of the EPRI MOV PPM models as identified in the following Part 21 and Error Notices: Revision Date.- December 17, 2007 KVAP, The AOV/MO V Software with Technology 3 o 10CFR21 Notification by EPRI Regarding Potential Non-Conservatism of EPRI's MOV Performance Prediction Methodology (PPM) Butterfly Valve Model under Compressible Flow Conditions, 13-April-07 o PPM Software Error Notice 2007-1 (Potential Non-Conservatism in Butterfly Valve Model Predictions under Compressible Flow Conditions) 12-Mar-07 o PPM Software Error Notice 2005-1 (Minimum Required Thrust Unconservative in Self Actuating Portion of Stroke)o PPM Software Error Notice 2004-2 (Potential Non-Conservatism in Butterfly Valve Model Predictions under Compressible Flow Conditions) 22-Oct-04 o PPM Software Error Notice 2003-2 (Required Adjustments to Butterfly Valve Disc Angle Dependent Torque Predictions) 19-Dec-03 o PPM Software Error Notice 2003-1 Version 3.0 (Build 3.0.50) and Version 3.1 (Build 3.1.8) (Proximity of Upstream Disturbances) 9-Apr-03 o PPM Software Information Notice 2002-1 (Prediction of Butterfly Valve Design Basis Required Torque as a Function of Disk Position) 6-May-02 o PPM Version 3.0 (Build 3.0.50) Software Error Notice 2001-1 (Butterfly Valve Stem Orientation) 6-Nov-01 Cost Savings, Stability and Continuity Many KVAP users have reported savings in excess of $500,000 achieved by avoiding unwarranted equipment replacement in valves previously determined to have negative or low margins, ALARA savings and elimination of dynamic testing requirements.
* KVAP validated models eliminate the need for expensive in-situ dynamic testing, resulting in savings of thousands of dollars per valve
The enhanced models in KVAP can also potentially yield increased MOV margins that can help extend static periodic verification test intervals.
    " The user-friendly graphic interface eliminates potential errors commonly made during calculations, enabling a more efficient completion of evaluations
KVAP software was developed by a team of Kalsi specialists who are recognized as leaders in the industry for technological advances in AOVs and MOVs, and for providing stability and continuity of service to our clients. The software is backed by comprehensive training and technical support offered by this highly capable KVAP team.Revision Date. December 17, 2007 KVAP, The AOV/MO V Software with Technology' 4 Table 1(A)Quarter-Turn 1zJah'es Validated Methodologies/Software Available For AOVs & MOVs Valve Types Prevalent in AOV Population NRC/INEL Cont. Purge*EPRI MOV PPM**Ace, AirBase KVAP 1 Symmetric Butterfly NteNone V ,N6n' V 2 Single-Offset Butterfly Nolte 3 Double-Offset Butterfly None None 4 Segmented V-Ball N None /5 Spherical Ball Nonte None Non6kre V 6 Eccentric Plug =,None n Nofe> V 7 Tapered/Cylinder Plug Nolte 'Nole NoeV* No software was provided by NRC/INEL** No Compressible flow testing was performed by EPRI*** EPRI Models found to be non-conservative for certain applications as described in NRC Part 21 and EPRI Error Notices (see previous page for a listing)Table I(B)Linear Vadves Validated or First Principles Based Methodologies/Software Available for AOVs & MOVs EPRI Ace, KVAP Valve Type MOV PPM AirBase 1 Globe-Unbalanced V V 2 Globe-Balanced, Cage V V 3 Globe-Balanced, Double Disc V V 4 Globe-Balanced, Pilot Non V V 5 Globe-3-way Converging, Single Disc Non> ... None V 6 Globe-3-way Converging, Double Disc None 'Nolte.7 Globe-3-way Diverging, Single Disc Nolt 8 Globe-3-way Diverging, Double Disc Nn II 9 Diaphragm Nolne , 10 Gate-Solid or Flexible V V V Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 5 Table I(C)Linear and Quarter- Turn / ctualor Models/Software Available for AOVs & MOVs EPRI Ace, KVAP Actuator Type MOV PPM AirBase A 0 Vs Cylinder Noi Diaphragm I F-N eV'Scotch Yoke Nonei V Rack & Pinion Nn V Cylinder with Linkage (Type 1) V Cylinder with Linkage (Type 2) None Nollje , Diaphragm with Lever N Vn M1O Vs Limitorque V V Rotork KiNone Otiler User Defined ~7 No7 I VC Table I(D)M in Evaluation and 0 01 Set Point Control Features Feature EPRI Ace, KVAP MOV PPM AirBase Margin Evaluation None AOV Setup Box for Set Point Control e V*For linear valves, mid stroke margins are not calculated in Ace or AirBase Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 6 Background of Kalsi Engineering.
    " KVAP does not have the non-conservatism found, and limitations imposed in the use of the EPRI MOV PPM models as identified in the following Part 21 and Error Notices:
Flow Loop Testing and Validated Model Development Program for KVAP As summarized in USNRC Regulatory Issue Summary 2000-03, problems with power-operated valves have resulted in an increased emphasis by USNRC on improving the performance reliability and predictability of AOVs. In response, the Joint Owners Group for Air-Operated Valves (JOG AOV) developed a document to provide guidance and define minimum requirements to the utilities for implementing AOV programs.
Revision Date.-December 17, 2007
Additionally, four utilities performed design basis calculations under EPRI's AOV pilot programs.
 
This resulted in a calculation methodology for AOVs, which is documented in the EPRI AOV Evaluation Guide (TR107322).
KVAP, The AOV/MO V Software with Technology                                                   3 o   10CFR21 Notification by EPRI Regarding Potential Non-Conservatism of EPRI's MOV Performance Prediction Methodology (PPM) Butterfly Valve Model under Compressible Flow Conditions, 13-April-07 o   PPM Software Error Notice 2007-1 (Potential Non-Conservatism in Butterfly Valve Model Predictions under Compressible Flow Conditions) 12-Mar-07 o   PPM Software Error Notice 2005-1 (Minimum Required Thrust Unconservative in Self Actuating Portion of Stroke) o   PPM Software Error Notice 2004-2 (Potential Non-Conservatism in Butterfly Valve Model Predictions under Compressible Flow Conditions) 22-Oct-04 o   PPM Software Error Notice 2003-2 (Required Adjustments to Butterfly Valve Disc Angle Dependent Torque Predictions) 19-Dec-03 o   PPM Software Error Notice 2003-1 Version 3.0 (Build 3.0.50) and Version 3.1 (Build 3.1.8) (Proximity of Upstream Disturbances) 9-Apr-03 o   PPM Software Information Notice 2002-1 (Prediction of Butterfly Valve Design Basis Required Torque as a Function of Disk Position) 6-May-02 o   PPM Version 3.0 (Build 3.0.50) Software Error Notice 2001-1 (Butterfly Valve Stem Orientation) 6-Nov-01 Cost Savings, Stability and Continuity Many KVAP users have reported savings in excess of $500,000 achieved by avoiding unwarranted equipment replacement in valves previously determined to have negative or low margins, ALARA savings and elimination of dynamic testing requirements. The enhanced models in KVAP can also potentially yield increased MOV margins that can help extend static periodic verification test intervals. KVAP software was developed by a team of Kalsi specialists who are recognized as leaders in the industry for technological advances in AOVs and MOVs, and for providing stability and continuity of service to our clients. The software is backed by comprehensive training and technical support offered by this highly capable KVAP team.
These EPRI AOV pilot plant programs, and the implementation of the AOV Evaluation Guide methodologies at other plants revealed three key problems:* There are no validated models for several types of quarter-turn valves (e.g., spherical ball, V-notch ball, eccentric plug) that constitute a large AOV population; unvalidated approaches had to be used for design basis calculations.
Revision Date. December 17, 2007
This can lead to unreliable AOV performance, based on industry experience and lessons learned from MOVs.* EPRI MOV PPP methodology for symmetric and many single-offset butterfly valves was found to provide negative margin for AOVs. The original PPM models were based on a very limited amount of butterfly valve tests in incompressible flow applications.
 
To cover valve applications that were not tested and uncertainties, additional conservatism was added in the PPM. This excessive conservatism caused the EPRI methodology to predict low or negative margins for AOVs that, in fact, have larger margins and capability to operate under design basis conditions." Subsequent compressible flow testing performed by Kalsi Engineering revealed that the EPRI MOV PPP methodology was non-conservative in compressible flow applications (See Part 21 and EPRI Error Notices on page 3).This testing led to improved and validated methodologies that accurately predict torque requirements for all types of quarter-turn valves prevalent in AOV applications.
KVAP, The AOV/MO V Software with Technology'                                                 4 Table 1(A)
A comprehensive matrix of flow loop testing was performed to develop more accurate validated models for AOVs incorporated in KVAP.Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 7 Valve Orientation Configuration Group Tests Valve Orientation Confi uration Quarter-turn Valve Test Matrix Incompressible:
Quarter-Turn 1zJah'es Validated Methodologies/Software Available For AOVs & MOVs Valve Types Prevalent in AOV       NRC/INEL           EPRI              Ace, KVAP Population              Cont. Purge*   MOV PPM**           AirBase 1   Symmetric Butterfly                   NteNone
15 Valve Designs, 71 Configurations, 1,272 Tests Compressible:
* V         ,N6n'             V 2   Single-Offset Butterfly                                                 Nolte 3   Double-Offset Butterfly         *NoleNone                              None 4   Segmented V-Ball                     'N*one          N               None           /
9 Valve Designs., 84 Configurations, 1,1 16 Tests The KVAP software and its extensive database capabilities incorporate the new validated models for quarter-turn valves developed under this program. KVAP also includes validated/first principles based industry established models for all other common types of globe, gate, and diaphragm valves and actuators to offer a complete software package for reliable and efficient calculations.
5   Spherical Ball                         Nonte         None               Non6kre       V 6   Eccentric Plug                   =,None             N**oe n             Nofe>         V 7   Tapered/Cylinder Plug                 Nolte         'Nole             NoeV
KVAP software development, analytical models, flow loop test program, and verification and validation meet the requirements of IOCFR50 Appendix B.KVAP includes models for all common types of linear (globe, gate, diaphragm) and quarter-turn (butterfly, ball, plug) valves & actuators.
* No software was provided by NRC/INEL
Revision Date. December 17, 2007 KVAP, The AOV/MO V Software with Technology 8 KVAP Software Capabilities The Kalsi Valve & Actuator Program is a state-of-the-art software that efficiently performs reliable design basis calculations for all common types of globe, gate, diaphragm, butterfly, ball, and plug valves as well as linear and quarter-turn actuators used in POV applications.
        ** No Compressible flow testing was performed by EPRI
KVAP is the only POV software in the industry that includes a number of new validated valve models based on first principles supported by extensive CFD analyses and 1OCFR50 Appendix B testing. These new models are applicable to several types of valves that are common to AOV applications which had not been addressed by the EPRI MOV PPM, JOG AOV, NSSS Owners Groups, valve manufacturers, or other organizations marketing competing software.KVAP includes a comprehensive database of lOCFRR5O Appendix B test results to accurately predict torque/thrust requirements for various types of POVs under design basis conditions.
        *** EPRI Models found to be non-conservative for certain applications as described in NRC Part 21 and EPRI Error Notices (see previous page for a listing)
The flow loop test matrix to support KVAP development and validation included over 2,000 static and dynamic tests to cover variations in valve/disc geometry, elbow orientation, elbow distance, flow direction, flow rates, and maximum AP. KVAP provides geometry-specific torque and flow coefficients for baseline conditions and for elbow effects.In many POV applications, the new KVAP models for quarter-turn valves provide a substantial increase in margin between valve requirements and actuator capabilities, thus eliminating unnecessary equipment modifications.
Table I(B)
The KVAP database and the more accurate models have already demonstrated substantial cost savings for the plants.From inception, KVAP software development was planned with a well-structured modular approach to minimize the cost and time associated with the V&V effort for upgrades and revisions.
Linear Vadves Validated or First Principles Based Methodologies/Software Available for AOVs & MOVs EPRI               Ace,       KVAP Valve Type                     MOV PPM         AirBase 1   Globe-Unbalanced                                   V               V 2   Globe-Balanced, Cage                               V               V 3   Globe-Balanced, Double Disc                       V                 V 4   Globe-Balanced, Pilot                             Non               V           V 5   Globe-3-way Converging, Single Disc               Non> ...         None           V 6   Globe-3-way Converging, Double Disc               None             'Nolte.
This ensures that new data and improvements to address emerging industry issues for POVs can be efficiently incorporated, verified, and validated in KVAP.The KVAP software input and output screens are heavily supported by graphics that illustrate critical features and dimensions of the valve being analyzed, valve orientation, flow direction, elbow orientation, required valve thrust/torque throughout the stroke, minimum and maximum actuator capability throughout the stroke, and margin throughout the stroke. This user-friendly graphic interface eliminates mistakes and errors commonly made during PO V calculations.
7   Globe-3-way Diverging, Single Disc               Nolt 8   Globe-3-way Diverging, Double Disc               Nn                 II 9   Diaphragm                                         Nolne               ,
KVAP was developed by a team of Kalsi senior specialists who are recognized as leaders in the industry for technological advances in AOV, MOV, HOV, SOV and check valves. Our specialists have more than 20 years of continuous involvement in R&D to develop validated first principles models and software for valves and actuators to address generic industry-wide issues, including the EPRI MOV Performance Prediction Program and MOV guides. This experience is supplemented by performing design basis calculations and implementing MOV, AOV and Check Valve programs at more than 25 power plants.Revision Date: December 17, 2007 KVAP, The AOV/MOV Software with Technology 9 KVAP Scope of Valves and Actuators KVAP software is capable of evaluating all common types of AOV/MOV valves and actuators:
10   Gate-Solid or Flexible                             V               V           V Revision Date: December 17, 2007
Valve Types Linear (dirtect & reverse acting, (isapplcbe~
 
* Gate-Solid, Flexible, Parallel Slide* Globe-Unbalanced
KVAP, The AOV/MO V Software with Technology                                       5 Table I(C)
* Globe-Balanced, Cage* Globe-Balanced, Double Disc* Globe-Balanced, Pilot* Globe-3-way Converging, Single Disc* Globe-3-way Converging, Double Disc* Globe-3-way Diverging, Single Disc* Globe-3-way Diverging, Double Disc* Diaphragm Quarter-Turn
Linear and Quarter-Turn / ctualor Models/Software Available for AOVs & MOVs EPRI           Ace,       KVAP Actuator Type                 MOV PPM         AirBase A 0 Vs Cylinder                                   Noi Diaphragm                           IF-N         eV' Scotch Yoke                                 Nonei           V Rack & Pinion                               Nn                           V Cylinder with Linkage (Type 1)
* Symmetric Butterfly* Single-Offset Butterfly* Double-Offset Butterfly* Segmented V-Ball* Spherical Ball 9 floating and trunnion mounted* Eccentric Plug* Tapered/Cylinder Plug* User Defined Actuator Types" Cylinder* Single acting w/spring" Double acting* Double acting, double ended* Double acting w/spring" Diaphragm* Single acting w/spring Quarter-Turn" Scotch Yoke" Single acting w/spring" Double acting* Rack & Pinion" Single acting w/spring" Double acting" Cylinder with Linkage (2 types)" Single acting w/spring" Double acting* Diaphragm with Lever 9 Single acting w/spring Ele'c'tric_
* None*                        V Cylinder with Linkage (Type 2)             None         , Nollje Diaphragm with Lever                       N                           Vn M1O Vs Limitorque                                                 V           V Rotork                                   KiNone Otiler 7
M__o-t-or* Limitorque" Rotork Other 9 User Defined* any air, hydraulic, or electric motor actuator with defined output vs. stroke Revision Date.- December 17, 2007 KVAP, The AOV/MOV Software with Technology 10 Other KVAP Features/Capabilities
User Defined             ~                 No7 I                       VC Table I(D)
* Analyzes incompressible, compressible, choking, flashing flow* Includes valve geometry-specific upstream elbow effect coefficients for butterfly, ball, and plug valves* Evaluates mid-stroke margins* Provides extremely user-friendly, intuitive graphical user interface and comprehensive database capabilities
M   in Evaluation and   001 Set Point Control Features Feature                         EPRI         Ace,   KVAP MOV PPM       AirBase Margin Evaluation                                 None AOV Setup Box for Set Point Control         ;*;None  **      No* e     V
    *For linear valves, mid stroke margins are not calculated in Ace or AirBase Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology                                                       6 Background of Kalsi Engineering. Flow Loop Testing and Validated Model Development Program for KVAP As summarized in USNRC Regulatory Issue Summary 2000-03, problems with power-operated valves have resulted in an increased emphasis by USNRC on improving the performance reliability and predictability of AOVs. In response, the Joint Owners Group for Air-Operated Valves (JOG AOV) developed a document to provide guidance and define minimum requirements to the utilities for implementing AOV programs. Additionally, four utilities performed design basis calculations under EPRI's AOV pilot programs. This resulted in a calculation methodology for AOVs, which is documented in the EPRI AOV Evaluation Guide (TR107322).
These EPRI AOV pilot plant programs, and the implementation of the AOV Evaluation Guide methodologies at other plants revealed three key problems:
* There are no validated models for several types of quarter-turn valves (e.g., spherical ball, V-notch ball, eccentric plug) that constitute a large AOV population; unvalidated approaches had to be used for design basis calculations. This can lead to unreliable AOV performance, based on industry experience and lessons learned from MOVs.
* EPRI MOV PPP methodology for symmetric and many single-offset butterfly valves was found to provide negative margin for AOVs. The original PPM models were based on a very limited amount of butterfly valve tests in incompressible flow applications. To cover valve applications that were not tested and uncertainties, additional conservatism was added in the PPM. This excessive conservatism caused the EPRI methodology to predict low or negative margins for AOVs that, in fact, have larger margins and capability to operate under design basis conditions.
    "   Subsequent compressible flow testing performed by Kalsi Engineering revealed that the EPRI MOV PPP methodology was non-conservative in compressible flow applications (See Part 21 and EPRI Error Notices on page 3).
This testing led to improved and validated methodologies that accurately predict torque requirements for all types of quarter-turn valves prevalent in AOV applications.
A comprehensive matrix of flow loop testing was performed to develop more accurate validated models for AOVs incorporated in KVAP.
Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology                                                   7 Valve     Orientation     Configuration   Group Tests Valve     Orientation   Confi uration Quarter-turn Valve Test Matrix Incompressible: 15 Valve Designs, 71 Configurations, 1,272 Tests Compressible: 9 Valve Designs., 84 Configurations, 1,1 16 Tests The KVAP software and its extensive database capabilities incorporate the new validated models for quarter-turn valves developed under this program. KVAP also includes validated/first principles based industry established models for all other common types of globe, gate, and diaphragm valves and actuators to offer a complete software package for reliable and efficient calculations. KVAP software development, analytical models, flow loop test program, and verification and validation meet the requirements of IOCFR50 Appendix B.
KVAP includes models for all common types of linear (globe, gate, diaphragm) and quarter-turn (butterfly, ball, plug) valves & actuators.
Revision Date. December 17, 2007
 
KVAP, The AOV/MO V Software with Technology                                                     8 KVAP Software Capabilities The Kalsi Valve & Actuator Program is a state-of-the-art software that efficiently performs reliable design basis calculations for all common types of globe, gate, diaphragm, butterfly, ball, and plug valves as well as linear and quarter-turn actuators used in POV applications.
KVAP is the only POV software in the industry that includes a number of new validated valve models based on first principles supported by extensive CFD analyses and 10CFR50 Appendix B testing. These new models are applicable to several types of valves that are common to AOV applications which had not been addressed by the EPRI MOV PPM, JOG AOV, NSSS Owners Groups, valve manufacturers, or other organizations marketing competing software.
KVAP includes a comprehensive database of 10CFRR5O Appendix B test results to accurately predict torque/thrust requirements for various types of POVs under design basis conditions. The flow loop test matrix to support KVAP development and validation included over 2,000 static and dynamic tests to cover variations in valve/disc geometry, elbow orientation, elbow distance, flow direction, flow rates, and maximum AP. KVAP provides geometry-specific torque and flow coefficients for baseline conditions and for elbow effects.
In many POV applications, the new KVAP models for quarter-turn valves provide a substantial increase in margin between valve requirements and actuator capabilities, thus eliminating unnecessary equipment modifications. The KVAP databaseand the more accurate models have already demonstratedsubstantialcost savingsfor the plants.
From inception, KVAP software development was planned with a well-structured modular approach to minimize the cost and time associated with the V&V effort for upgrades and revisions. This ensures that new data and improvements to address emerging industry issues for POVs can be efficiently incorporated,verified, and validated in KVAP.
The KVAP software input and output screens are heavily supported by graphics that illustrate critical features and dimensions of the valve being analyzed, valve orientation, flow direction, elbow orientation, required valve thrust/torque throughout the stroke, minimum and maximum actuator capability throughout the stroke, and margin throughout the stroke. This user-friendly graphicinterface eliminates mistakes and errors commonly made during PO V calculations.
KVAP was developed by a team of Kalsi senior specialists who are recognized as leaders in the industry for technological advances in AOV, MOV, HOV, SOV and check valves. Our specialists have more than 20 years of continuous involvement in R&D to develop validated first principles models and software for valves and actuators to address generic industry-wide issues, including the EPRI MOV Performance Prediction Program and MOV guides. This experience is supplemented by performing design basis calculations and implementing MOV, AOV and Check Valve programs at more than 25 power plants.
Revision Date: December 17, 2007
 
KVAP, The AOV/MOV Software with Technology                                                       9 KVAP Scope of Valves and Actuators KVAP software is capable of evaluating all common types of AOV/MOV valves and actuators:
Valve Types                                    Actuator Types Linear (dirtect & reverse acting, (isapplcbe~
* Gate-Solid, Flexible, Parallel Slide           " Cylinder
* Globe-Unbalanced
* Single acting w/spring
* Globe-Balanced, Cage                                 " Double acting
* Globe-Balanced, Double Disc
* Double acting, double ended
* Globe-Balanced, Pilot
* Double acting w/spring
* Globe-3-way Converging, Single Disc           " Diaphragm
* Globe-3-way Converging, Double Disc
* Single acting w/spring
* Globe-3-way Diverging, Single Disc           Quarter-Turn
* Globe-3-way Diverging, Double Disc             " Scotch Yoke
* Diaphragm                                             " Single acting w/spring Quarter-Turn                                             " Double acting
* Symmetric Butterfly
* Rack & Pinion
* Single-Offset Butterfly                               " Single acting w/spring
* Double-Offset Butterfly                               " Double acting
* Segmented V-Ball                               " Cylinder with Linkage (2 types)
* Spherical Ball                                       " Single acting w/spring 9 floating and trunnion mounted                     " Double acting
* Eccentric Plug
* Diaphragm with Lever
* Tapered/Cylinder Plug                                 9 Single acting w/spring Ele'c'tric_ M__o-t-or
* User Defined
* Limitorque
                                                    " Rotork Other 9 User Defined
* any air, hydraulic, or electric motor actuator with defined output vs. stroke Revision Date.-December 17, 2007
 
KVAP, The AOV/MOV Software with Technology                                                        10 Other KVAP Features/Capabilities
* Analyzes incompressible, compressible, choking, flashing flow
* Includes valve geometry-specific upstream elbow effect coefficients for butterfly, ball, and plug valves
* Evaluates mid-stroke margins
* Provides extremely user-friendly, intuitive graphical user interface and comprehensive database capabilities
* Well planned modular structure for efficient V&V to support upgrades/new capabilities
* Well planned modular structure for efficient V&V to support upgrades/new capabilities
* Operates on Windows operating systems Applications, Advantages, and Benefits* Performs reliable POV design basis calculations, including minimum required thrust/torque, actuator capabilities and margin* Eliminates the need for dynamic AP testing, saving tens of thousands of dollars per valve* Provides models for double-offset butterfly, full ball, segmented ball, and plug valves, for which no validated models were available in the industry* Eliminates excessive conservatism in EPRI PPM models; increases margin* Eliminates unnecessary equipment modifications and/or repeat calculations to address low/negative margins* Extremely intuitive, user-friendly graphical interface improves efficiency and eliminates errors* Troubleshoots valve performance problems Continuous Enhancements Based on User/Industry Feedback KVAP is being actively expanded/enhanced and supported to address industry wide emerging issues and requirements and feedback from its 50+ current users. Some of the recent enhancements include the AOV Setup Box and set point data sheets for efficient implementation and verification of the design basis calculations in the field, efficient implementation of the Joint Owners Group MOV Periodic Verification recommendations.
* Operates on Windows operating systems Applications, Advantages, and Benefits
Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 11 A 0 V Setup Box and Set Point Data Sheets for Field Implementation The component level calculations provide an assessment of actuator margin based on valve requirements and actuator output. Changes in valve set points (e.g. regulator, air pressure and spring preload) and packing adjustments may affect the actuator output and invalidate values calculated prior to performing valve setup tests. Additionally, adjustments of the set points in one direction may affect the required set point in the opposite direction.
* Performs reliable POV design basis calculations,           including   minimum required thrust/torque, actuator capabilities and margin
To facilitate the addressing of these issues, a setup module has been incorporated into KVAP that graphically displays the required and allowable spring preload (i.e. minimum and maximum allowable lower bench set) as a function of regulated air pressure and regulator settings using two different approaches.
* Eliminates the need for dynamic AP testing, saving tens of thousands of dollars per valve
This setup box also accounts for all AOV uncertainties in various parameters.
* Provides models for double-offset butterfly, full ball, segmented ball, and plug valves, for which no validated models were available in the industry
The set point datasheet defines the setup parameters and allows adjustments to be made without revisiting the margin calculations.
* Eliminates excessive conservatism in EPRI PPM models; increases margin
The following figure shows a typical AOV setup box and an alternative approach of displaying static thrust trace predicted by KVAP and the allowable bench set window.AOV Setup Box AOV Setup Window -Static Stroke-- TnnBt hsneRaenn  
* Eliminates unnecessary equipment modifications and/or repeat calculations to address low/negative margins
.co...... A n4ed StIcSflc~e  
* Extremely intuitive, user-friendly graphical interface improves efficiency and eliminates errors
-- Lo..,etBnhnOeoRn Sl* o-e ch~t See 5 -iL Re S tr Se -Regu -piel.e ROte htn. LoweM L nnchent II Ai Rqu- P- r~e , ~ nua tmDsi et*- -- -Mm Ongolnini ffnen;-Of-atOn n 32 34 33 30 *o n6 1e 'm 60a o e n n e n n Approach (A) Approach (B)Setup Box Showing Allowable Spring Preload Setup Window for Allowable Lower Bench Set Range as a Function of Regulated Air Supply Range for a Given Regulated Air Supply Pressure Pressure Displayed on KVAP Static Thrust Stroke Predictions Graphical Approaches in KVAP for Field Implementation of AOV Setup Parameters Rev KVAP, The A 0 V/MO V Software with Technology 12 MO VActuator Module The KVAP MOV Actuator Module is developed to calculate torque and thrust capabilities for motor operated valve actuators and quarter-turn units based on "Application Guide for Motor-Operated Valves in Nuclear Power Plants" prepared by Kalsi Engineering, Inc. It features a user-friendly graphical interface that reduces mistakes and errors commonly made during calculations, thus enabling a more efficient completion of evaluations.
* Troubleshoots valve performance problems ContinuousEnhancements Based on User/Industry Feedback KVAP is being actively expanded/enhanced and supported to address industry wide emerging issues and requirements and feedback from its 50+ current users. Some of the recent enhancements include the AOV Setup Box and set point data sheets for efficient implementation and verification of the design basis calculations in the field, efficient implementation of the Joint Owners Group MOV Periodic Verification recommendations.
The module includes Limitorque SMB/SB/SBD actuators, Rotork Actuator, and quarter turn gear operators.
Revision Date: December 17, 2007
This module can augment calculations performed during the implementation of the GL-96-05 MOV JOG Periodic Verification program.The Limitorque actuator module enables the calculation of SMB/SB/SBD for: " Pullout torque/thrust,* Stall torque/thrust," Running torque/thrust and* Stem speed Inputs include: the overall gear ratio, stem thread characteristics (as applicable), application factors, efficiency, reduced voltage, and temperature effects (as applicable).
 
The model comprises equations, and built-in manufacturers' default values for actuator efficiency, application factors, motor ratings, and temperature effects. The model also provides inputs for using enhanced electric motor models such as ComEd.The Rotork actuator module uses torque and thrust output capability values published in the Rotork catalog for "A" type actuators.
KVAP, The AOV/MO V Software with Technology                                                                                                           11 A 0 V Setup Box and Set PointData Sheets for FieldImplementation The component level calculations provide an assessment of actuator margin based on valve requirements and actuator output. Changes in valve set points (e.g. regulator, air pressure and spring preload) and packing adjustments may affect the actuator output and invalidate values calculated prior to performing valve setup tests. Additionally, adjustments of the set points in one direction may affect the required set point in the opposite direction. To facilitate the addressing of these issues, a setup module has been incorporated into KVAP that graphically displays the required and allowable spring preload (i.e. minimum and maximum allowable lower bench set) as a function of regulated air pressure and regulator settings using two different approaches. This setup box also accounts for all AOV uncertainties in various parameters. The set point datasheet defines the setup parameters and allows adjustments to be made without revisiting the margin calculations. The following figure shows a typical AOV setup box and an alternative approach of displaying static thrust trace predicted by KVAP and the allowable bench set window.
The user selects the gearbox size and stem nut RPM, and enters stem diameter, stem lead, stem pitch, and coefficient of friction between the stem and stem nut. The model selects the corresponding values of torque rating and thrust rating and calculates the thrust output. The value for torque output is the same as the torque rating. The values returned are applicable to type "A" 60 Hz 3 phase Rotork actuators.
AOV Setup Box                                                         AOV Setup Window - Static Stroke
The quarter turn gear operator can be coupled to Limitorque or Rotork actuators.
                                                                          --   TnnBt hsneRaenn   . Aco......
The inputs allow for any generic actuator definition which defines the actuator by gear ratio and efficiency.
n4ed StIcSflc~e -- Lo..,etBnhnOeoRn o-e     ch~t           See5          -iL     Re         Str Se           -Regu-piel.e ROte Sl*
Revision Date.: December 17, 2007 KVAP, The AOVMO V Software with Technology 13 Typical KVAP Screens The KVAP software input and output screens are heavily supported by graphics that illustrate critical featuresand dimensions of the valve being analyzed, valve orientation, flow direction,.elbow orientation, required valve thrust/torque throughout the stroke, minimum and maximum actuator capability throughout the stroke, and margin throughout the stroke. This user-friendly graphic interface eliminates the potential for errors commonly made during POV calculations.
htn. LoweML nnchent
Some examples of input and output screens follow: KVAP Main Menu Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology , 14 Globe Valve Configuration Fil. T-Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 15 Flow Inputs for Globe Valve Fjile Tos~~ ja~Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 16 Valve Design File Tools H -lo Analysis I Revision Date. December 17, 2007 KVAP, The AOV/MO V Software with Technooigy Valve Installation 17 HEji ol ep ay Revision Date. December 17, 2007 KVAP, The AOV/MO V Software with Technology 18 Valve Results Eile Tools Helk Aalysis Reports VALVE RESULTS
      *-        -- -                                                  II MmOngolnini Rqu-P-Air~e , ~ ffnen;-Of-nua  tmDsi        et atOn     n       32       34         33         30               *o   n6                               o 1e     e      n
                                                                                                                              'm n     e       n   n 60a Approach (A)                                                                   Approach (B)
Setup Box Showing Allowable Spring Preload                               Setup Window for Allowable Lower Bench Set Range as a Function of Regulated Air Supply                           Range for a Given Regulated Air Supply Pressure Pressure Displayed on KVAP Static Thrust Stroke Predictions Graphical Approaches in KVAP for Field Implementation of AOV Setup Parameters Rev
 
KVAP, The A 0 V/MO V Software with Technology                                                       12 MO VActuator Module The KVAP MOV Actuator Module is developed to calculate torque and thrust capabilities for motor operated valve actuators and quarter-turn units based on "Application Guide for Motor-Operated Valves in Nuclear Power Plants" prepared by Kalsi Engineering, Inc. It features a user-friendly graphical interface that reduces mistakes and errors commonly made during calculations, thus enabling a more efficient completion of evaluations. The module includes Limitorque SMB/SB/SBD actuators, Rotork Actuator, and quarter turn gear operators. This module can augment calculations performed during the implementation of the GL-96-05 MOV JOG Periodic Verification program.
The Limitorque actuator module enables the calculation of SMB/SB/SBD for:
        "   Pullout torque/thrust,
* Stall torque/thrust,
        "   Running torque/thrust and
* Stem speed Inputs include: the overall gear ratio, stem thread characteristics (as applicable), application factors, efficiency, reduced voltage, and temperature effects (as applicable). The model comprises equations, and built-in manufacturers' default values for actuator efficiency, application factors, motor ratings, and temperature effects. The model also provides inputs for using enhanced electric motor models such as ComEd.
The Rotork actuator module uses torque and thrust output capability values published in the Rotork catalog for "A" type actuators. The user selects the gearbox size and stem nut RPM, and enters stem diameter, stem lead, stem pitch, and coefficient of friction between the stem and stem nut. The model selects the corresponding values of torque rating and thrust rating and calculates the thrust output. The value for torque output is the same as the torque rating. The values returned are applicable to type "A" 60 Hz 3 phase Rotork actuators.
The quarter turn gear operator can be coupled to Limitorque or Rotork actuators. The inputs allow for any generic actuator definition which defines the actuator by gear ratio and efficiency.
Revision Date.: December 17, 2007
 
KVAP, The AOVMO V Software with Technology                                                   13 Typical KVAP Screens The KVAP software input and output screens are heavily supported by graphics that illustrate critical featuresand dimensions of the valve being analyzed, valve orientation, flow direction,
.elbow orientation, required valve thrust/torque throughout the stroke, minimum and maximum actuator capability throughout the stroke, and margin throughout the stroke. This user-friendly graphic interface eliminates the potentialfor errorscommonly made during POV calculations.
Some examples of input and output screens follow:
KVAP Main Menu Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology             , 14 Globe Valve Configuration Fil. T-Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology               15 Flow Inputs for Globe Valve Fjile Tos~~ ja~
Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology     16 Valve Design File Tools H Analysis
                  -lo I Revision Date. December 17, 2007
 
KVAP, The AOV/MO V Software with Technooigy         17 Valve Installation HEji ol ep ay Revision Date. December 17, 2007
 
KVAP, The AOV/MO V Software with Technology                                             18 Valve Results Eile Tools Helk Aalysis Reports VALVERESULTS


==SUMMARY==
==SUMMARY==
, 1 11 -.I I I ..OTHER CALCULATED DAM, " ., .-10 1 1 ýj Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 19 Margin Plot I I.Eile Tools Helo Analysis ReosIs Revision Date: December 17, 2007 KVAP, The AOV/MO V Software with Technology 20 Company Background and Experience Relevant to AOVs, MOVs, and Check Valves Valve design, analysis, testing, model development,
,
1 11-    . I II    . . OTHER CALCULATED DAM, " ., . - 10 1 1ýj Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology        19 Margin Plot I I.
Eile Tools Helo Analysis ReosIs Revision Date: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology                                                      20 Company Background and Experience Relevant to AOVs, MOVs, and Check Valves Valve design, analysis, testing, model development, application, and problem solving are areas of special competence at Kalsi Engineering.
KVAP Software Development, Verification and Validation
KVAP Software Development, Verification and Validation
: 1. KEI Document No. 2092C, KVAP Software Version 1.2." Software Quality Assurance Plan.2. KEI Document No. 2093C, KVAP Software.
: 1. KEI Document No. 2092C, KVAP Software Version 1.2." Software Quality Assurance Plan.
Software Requirements Specification.
: 2. KEI Document No. 2093C, KVAP Software. Software Requirements Specification.
: 3. KEI Document No. 2094C, KVAP Software.
: 3. KEI Document No. 2094C, KVAP Software. Software Design Specification
Software Design Specification
: 4. KEI Document No. 2094C, Attachment 1: KVAP Software Version 2.0.: Software Design Specification - User Interface Module.
: 4. KEI Document No. 2094C, Attachment 1: KVAP Software Version 2.0.: Software Design Specification  
: 5. KEI Document No. 2094C, Attachment 2: KVAP Software. Software Design Specification - System Flow Module.
-User Interface Module.5. KEI Document No. 2094C, Attachment 2: KVAP Software.
: 6. KEI Document No. 2094C, Attachment 3: KVAP Software: Software Design Specification - Air- OperatedActuator Module.
Software Design Specification  
: 7. KEI Document No. 2094C, Attachment 4: KVAP Software: Software Design Specification - Gate Valve, Module.
-System Flow Module.6. KEI Document No. 2094C, Attachment 3: KVAP Software:
: 8. KEI Document No. 2094C, Attachment 5: KVAP Software: Software Design Specification - Globe Valve Module.
Software Design Specification  
: 9. KEI Document No. 2094C, Attachment 6: KVAP Software. Software Design Specification - Diaphragm Valve Module.
-Air- Operated Actuator Module.7. KEI Document No. 2094C, Attachment 4: KVAP Software:
: 10. KEI Document No. 2094C, Attachment 7: KVAP Software: Software Design Specification - Butterfly Valve Module.
Software Design Specification  
1]. KEI Document No. 2094C, Attachment           8: KVAP Software: Software Design Specification - Ball/Plug Valve Module.
-Gate Valve, Module.8. KEI Document No. 2094C, Attachment 5: KVAP Software:
: 12. KEI Document No. 2094C, Attachment 9: KVAP Software: Software Design Specification - KVAP Global Module.
Software Design Specification  
: 13. KEI Document No. 2094C, Attachment 10: KVAP Software: Software Design Specification - Margin Module.
-Globe Valve Module.9. KEI Document No. 2094C, Attachment 6: KVAP Software.
: 14. KEI Document No. 2094C, Attachment 11: KVAP Software Version 2.0." Software Design Specification - Default Flow and Torque Coefficients Module for Butterfly.
Software Design Specification  
: 15. KEI Document No. 2094C, Attachment 12: KVAP Software Version 2.0.: Software Design Specification- Motor Operator.
-Diaphragm Valve Module.10. KEI Document No. 2094C, Attachment 7: KVAP Software:
: 16. KEI Document No. 2095C: KVAP Software Version 2.0. Program Code Listing:
Software Design Specification  
: 17. KEI Document No. 2096C: KVAP Software Version 2.0." Verfication and Validation Plan.
-Butterfly Valve Module.1]. KEI Document No. 2094C, Attachment 8: KVAP Software:
Revision Date: December 17, 2007
Software Design Specification  
 
-Ball/Plug Valve Module.12. KEI Document No. 2094C, Attachment 9: KVAP Software:
KVAP, The AO V/MO V Software with Technology                                           34
Software Design Specification  
: 18. KEI Document No. 2097C: KVAP Software Version 1.2.: V& V Report: Attachments 1 through 11.
-KVAP Global Module.13. KEI Document No. 2094C, Attachment 10: KVAP Software:
KVAP Models & Methodologies
Software Design Specification  
: 19. KEI Document No. 2098C, Attachment 1: KVAP Software: Model DescriptionReport -
-Margin Module.14. KEI Document No. 2094C, Attachment 11: KVAP Software Version 2.0." Software Design Specification  
User Interface Module.
-Default Flow and Torque Coefficients Module for Butterfly.
: 20. KEI Document No. 2098C, Attachment 2: KVAP Software: Model Description Report -
: 15. KEI Document No. 2094C, Attachment 12: KVAP Software Version 2.0.: Software Design Specification  
System Flow Module.
-Motor Operator.16. KEI Document No. 2095C: KVAP Software Version 2. 0. Program Code Listing: 17. KEI Document No. 2096C: KVAP Software Version 2.0." Verfication and Validation Plan.Revision Date: December 17, 2007 KVAP, The AO V/MO V Software with Technology 34 18. KEI Document No. 2097C: KVAP Software Version 1.2.: V& V Report: Attachments 1 through 11.KVAP Models & Methodologies
: 21. KEI Document No. 2098C, Attachment 3: KVAP Software. Model DescriptionReport -
: 19. KEI Document No. 2098C, Attachment 1: KVAP Software:
Air-OperatedActuator Module.
Model Description Report -User Interface Module.20. KEI Document No. 2098C, Attachment 2: KVAP Software:
: 22. KEI Document No. 2098C, Attachment 4: KVAP Software. Model DescriptionReport -
Model Description Report -System Flow Module.21. KEI Document No. 2098C, Attachment 3: KVAP Software.
Gate Valve Module.
Model Description Report -Air-Operated Actuator Module.22. KEI Document No. 2098C, Attachment 4: KVAP Software.
: 23. KEI Document No. 2098C, Attachment 5: KVAP Software: Model DescriptionReport -
Model Description Report -Gate Valve Module.23. KEI Document No. 2098C, Attachment 5: KVAP Software:
Globe Valve Module.
Model Description Report -Globe Valve Module.24. KEI Document No. 2098C, Attachment 6: KVAP Software:
: 24. KEI Document No. 2098C, Attachment 6: KVAP Software: Model DescriptionReport -
Model Description Report -Diaphragm Valve Module.25. KEI Document No. 2098C, Attachment 7: KVAP Software:
Diaphragm Valve Module.
Model Description Report -Butterfly Valve Module 26. KEI Document No. 2098C, Attachment 8: KVAP Software:
: 25. KEI Document No. 2098C, Attachment 7: KVAP Software: Model DescriptionReport -
Model Description Report -Ball/Plug Valve Module.27. KEI Document No. 2098C, Attachment 10: KVAP Software Version 2.0: Model Description Report: Margin Module.28. KEI Document No. 2098C, Attachment 11: Model Description Report: Default Coefficient Module -Butterfly Valves.29. KEI Document No. 2098C, Attachment 12: Model Description Report: Motor Operator Module.30. KEI Document No. 2111 C, CFD Modeling Methodology Validation for Quarter- Turn Valves.31. KEI Document No. 2122C, Verification and Validation Plan for ANSYS/FLOTRAN 5-5 CFD Elements.32. KEI Document No. 2121C, Verification and Validation Report for ANSYS/ FLOTRAN 5-5 CFD Elements.KVAP Flow Loop Test Program 33. KEI Document No. 2101C, Procedure for Kalsi AOV/MOV Validation Testing.34. KEI Document No. 2118C, Kalsi AOV/MOV Model Validation Test Data Report.35. KEI Document No. 2119C, Kalsi A OV/MO V Test Data.36. KEI Document No. 2119C, Attachment 1: Spherical Ball Valve (Assembly 1).37. KEI Document No. 2119C, Attachment 2: Segmented Ball Valve (Assembly 2).38. KEI Document No. 2119C, Attachment 3: Double Offset Butterfly Valve (Assembly 3).39. KEI Document No. 2119C, Attachment 4: Kalsi Test Fixture (Assembly
Butterfly Valve Module
: 4) Symmetric Disc 0.15 Aspect Ratio.Revision Date: December 17, 2007 KVAP, The A 0 V/MO V Software with Technology 35 40. KEI Document No. 2119C, Attachment 5: Kalsi Test Fixture (Assembly 5)Nonsymmetric Disc 0.15 Aspect Ratio.41. KEI Document No. 2119C, Attachment 6: Kalsi Test Fixture (Assembly 6)Nonsymmetric Disc 0.25 Aspect Ratio.42. KEI Document No. 2119C, Attachment 7: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 7). Double Offset: 0.090" Lateral (Stem), 40% axial (Seat).43. KEI Document No. 2119C, Attachment 8: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 8). Double Offset: 0.090" Lateral (Stem), 60% axial (Seat).44. KEI Document No. 2119C, Attachment 9: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 9). Double Offset: 0.045" Lateral (Stem), 40% axial (Seat).45. KEI Document No. 2119C, Attachment 10: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 10). Double Offset: 0.045" Lateral (Stem), 60% axial (Seat).46. KEI Document No. 2119C, Attachment 11: Spherical Q-Ball Valve with QOM Insert (Assembly 12).47. KEI Document No. 2119C, Attachment 12: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.24 Aspect Ratio (Assembly 13). Triple Offset: 0.364" Lateral, 59% axial, 16-deg cone.48. KEI Document No. 2119C, Attachment 13: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.30 Aspect Ratio (Assembly 14). Triple Offset: 0.632" Lateral (Stem), 67% axial (Seat).49. KEI Document No. 2205C, Procedure for Kalsi AOV/MOV Model Validation Testing, July 2000.50. KEI Document No. 2120C, Kalsi AOV/MOV Model Validation Testing- Lab Notebooks, Volumes 1-14.51. KEI Document No. 2221C, Kalsi AOV/MOV Model Validation Testing- Lab Notebooks, Volumes 1-11.52. KEI Document No. 2222C, Kalsi AOV/MO V Compressible Flow Testing Report.53. KEI Document No. 2222C, Attachment 1: Ball Valve: Full Ball, Trunnion Mounted 6" Valve (Assembly 1).54. KEI Document No. 2222C, Attachment 2: Jamesbury 6" Butterfly Valve Double Disc (Assembly 3).55. KEI Document No. 2222C, Attachment 3: Kalsi Butterfly Valve Test Fixture with Single Offset Disc 0.15 Aspect Ratio (Assembly 5).56. KEI Document No. 2222C, Attachment 4: Kalsi Butterfly Valve Test Fixture with Single Offset Disc 0.25 Aspect Ratio (Assembly 6).57. KEI Document No.. 2222C, Attachment 5: Kalsi Butterfly Valve Double Offset Disc with 0.25 Aspect Ratio (Assembly 8).Revision Date: December 17, 2007 KVAP, The AO V/MO V Software with Technology 36 58. KEI Document No. 2222C, Attachment 6: Jamesbury 6" Valve Double Offset with Steamline Disc (Assembly 11).59. KEI Document No. 2222C, Attachment 7: 6" Model of a 48" Henry Pratt Butterfly Valve (Assembly 16).60. KEI Document No. 2222C, Attachment 8: 6" Scale Model of an 18" Jamesbury Butterfly Valve (Assembly 18).61. KEI Document No. 2222C, Attachment 9: Kalsi Butterfly Valve Test Fixture Symmetric Disc with 0.25 Aspect Ratio (Assembly 19).62. M. S. Kalsi, B. H. Eldiwany, V. Sharma, D. Somogyi. "Dynamic Torque Models for Quarter-Tum Air-Operated Valves," Proceedings of the Sixth NRC/ASME Symposium on Valve & Pump Testing, NUREG/CP-0152, Vol. 3, July 2000.63. M. S. Kalsi, Bahir Eldiwany, Vinod Sharma, Ryan Sicking, "Flow Loop Testing to Validate Improved Models for Single, Double & Triple Offset Disk Butterfly Valves," Abstract for EPRI/NMAC Eighth Valve Technology Symposium, August 2001.64. J. K. Wang, Desi Somogyi, P. Daniel Alvarez, M. S. Kalsi, John Hosler (EPRI), "Flow Loop Testing and Validation of Thermal Binding Model for Wedge Gate Valves," Proceedings of the EPRI/NMAC Eighth Valve Technology Symposium, August 2001.65. M. S. Kalsi, B. E. Eldiwany, V. Sharma, "Butterfly Valve Model Improvements Based on Compressible Flow Testing Benefit Industry AOV Programs, Proceedings of the Seventh NRC/ASME Symposium on Valve and Pump Testing, July 2002.66. M. S. Kalsi, B. E. Eldiwany, V. Sharma, "Butterfly Valve Model Improvements Based on Compressible Flow Testing Benefit Industry AOV Programs, Proceedings of the Seventh NRC/ASME Symposium on Valve and Pump Testing, July 2002.67. M. S. Kalsi, B. Eldiwany, "Plant Experience Based Upon Application of New Validated Models for Air-Operated Valves, Proceedings of the 9th EPRI Valve Technology Symposium, August 2003.68. M. S. Kalsi, B. Eldiwany, Vinod Sharma, Aaron Richie, "Effect of Butterfly Valve Disc Shape Variations on Torque Requirements for Power Plant Applications, Proceedings of the Eighth NRC/ASME Symposium on Valve and Pump Testing, July 2004.69. KEI Document No. 2099C, KVAP User's Manual.EPRI MOV Performance Prediction Program &EPRI/NMAC Guides developed by Kalsi Engineering, Inc.70. EPRI MOV Performance Prediction Program: Guide for the Application and Use of Valves in Power Plant Systems, Electric Power Research Institute, EPRI NP-6516, Rev.0.71. EPRI MOV Performance Prediction Program: Guide for the Application, Use, and Maintenance of Valves in Power Plants, Electric Power Research Institute, EPRI TR-105852-V1.
: 26. KEI Document No. 2098C, Attachment 8: KVAP Software: Model DescriptionReport -
: 72. EPRI MOV Performance Prediction Program: Butterfly Valve Model Description Report, Electric Power Research Institute, EPRI TR- 103224.73. EPRI MOV Performance Prediction Program: Butterfly Valve Design, Elbow, and Scaling Effects Test Report, Electric Power Research Institute, EPRI TR-1 03257.Revision Date.- December 17, 2007 KVAP, The A 0 V/MO V Software with Technology 37 74. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Butterfly Valves in Nuclear Power Plants, Electric Power Research Institute, EPRI NP-7501.75. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Butterfly Valves in Nuclear Power Plants, Rev. 1, Electric Power Research Institute, EPRI TR-106563 V2.76. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Gate and Globe Valves in Nuclear Power Plants, Rev. 1, Electric Power Research Institute, EPRI TR-106563 VI.77. EPRI MOV Performance Prediction Program: Gate Valve Model Report, Electric Power Research Institute, EPRI TR-103229.
Ball/Plug Valve Module.
: 27. KEI Document No. 2098C, Attachment 10: KVAP Software Version 2.0: Model DescriptionReport: Margin Module.
: 28. KEI Document No. 2098C, Attachment 11: Model Description Report: Default Coefficient Module - Butterfly Valves.
: 29. KEI Document No. 2098C, Attachment 12: Model DescriptionReport: Motor Operator Module.
: 30. KEI Document No. 2111 C, CFD Modeling Methodology Validationfor Quarter-Turn Valves.
: 31. KEI Document No. 2122C, Verification and Validation Planfor ANSYS/FLOTRAN 5-5 CFD Elements.
: 32. KEI Document No. 2121C, Verification and Validation Report for ANSYS/ FLOTRAN 5-5 CFD Elements.
KVAP Flow Loop Test Program
: 33. KEI Document No. 2101C, Procedurefor Kalsi AOV/MOV Validation Testing.
: 34. KEI Document No. 2118C, Kalsi AOV/MOV Model Validation Test Data Report.
: 35. KEI Document No. 2119C, Kalsi AOV/MO V Test Data.
: 36. KEI Document No. 2119C, Attachment 1: Spherical Ball Valve (Assembly 1).
: 37. KEI Document No. 2119C, Attachment 2: Segmented Ball Valve (Assembly 2).
: 38. KEI Document No. 2119C, Attachment 3: Double Offset Butterfly Valve (Assembly 3).
: 39. KEI Document No. 2119C, Attachment 4: Kalsi Test Fixture (Assembly 4) Symmetric Disc 0.15 Aspect Ratio.
Revision Date: December 17, 2007
 
KVAP, The A 0 V/MO V Software with Technology                                         35
: 40. KEI Document No. 2119C, Attachment 5: Kalsi Test Fixture           (Assembly 5)
Nonsymmetric Disc 0.15 Aspect Ratio.
: 41. KEI Document No. 2119C, Attachment 6: Kalsi Test Fixture           (Assembly 6)
Nonsymmetric Disc 0.25 Aspect Ratio.
: 42. KEI Document No. 2119C, Attachment 7: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 7). Double Offset: 0.090" Lateral (Stem), 40% axial (Seat).
: 43. KEI Document No. 2119C, Attachment 8: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 8). Double Offset: 0.090" Lateral (Stem), 60% axial (Seat).
: 44. KEI Document No. 2119C, Attachment 9: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 9). Double Offset: 0.045" Lateral (Stem), 40% axial (Seat).
: 45. KEI Document No. 2119C, Attachment 10: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 10). Double Offset: 0.045" Lateral (Stem), 60% axial (Seat).
: 46. KEI Document No. 2119C, Attachment 11: Spherical Q-Ball Valve with QOM Insert (Assembly 12).
: 47. KEI Document No. 2119C, Attachment 12: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.24 Aspect Ratio (Assembly 13). Triple Offset: 0.364" Lateral, 59% axial, 16-deg cone.
: 48. KEI Document No. 2119C, Attachment 13: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.30 Aspect Ratio (Assembly 14). Triple Offset: 0.632" Lateral (Stem), 67% axial (Seat).
: 49. KEI Document No. 2205C, Procedurefor Kalsi AOV/MOV Model Validation Testing, July 2000.
: 50. KEI Document No. 2120C, Kalsi AOV/MOV Model Validation Testing- Lab Notebooks, Volumes 1-14.
: 51. KEI Document No. 2221C, Kalsi AOV/MOV Model Validation Testing- Lab Notebooks, Volumes 1-11.
: 52. KEI Document No. 2222C, Kalsi AOV/MO V CompressibleFlow Testing Report.
: 53. KEI Document No. 2222C, Attachment 1: Ball Valve: Full Ball, Trunnion Mounted 6" Valve (Assembly 1).
: 54. KEI Document No. 2222C, Attachment 2: Jamesbury 6" Butterfly Valve Double Disc (Assembly 3).
: 55. KEI Document No. 2222C, Attachment 3: Kalsi Butterfly Valve Test Fixture with Single Offset Disc 0.15 Aspect Ratio (Assembly 5).
: 56. KEI Document No. 2222C, Attachment 4: Kalsi Butterfly Valve Test Fixture with Single Offset Disc 0.25 Aspect Ratio (Assembly 6).
: 57. KEI Document No.. 2222C, Attachment 5: Kalsi Butterfly Valve Double Offset Disc with 0.25 Aspect Ratio (Assembly 8).
Revision Date: December 17, 2007
 
KVAP, The AO V/MO V Software with Technology                                               36
: 58. KEI Document No. 2222C, Attachment 6: Jamesbury 6" Valve Double Offset with Steamline Disc (Assembly 11).
: 59. KEI Document No. 2222C, Attachment 7: 6" Model of a 48" Henry Pratt Butterfly Valve (Assembly 16).
: 60. KEI Document No. 2222C, Attachment 8:           6" Scale Model of an 18" Jamesbury Butterfly Valve (Assembly 18).
: 61. KEI Document No. 2222C, Attachment 9: Kalsi Butterfly Valve Test Fixture Symmetric Disc with 0.25 Aspect Ratio (Assembly 19).
: 62. M. S. Kalsi, B. H. Eldiwany, V. Sharma, D. Somogyi. "Dynamic Torque Models for Quarter-Tum Air-Operated Valves," Proceedings of the Sixth NRC/ASME Symposium on Valve & Pump Testing, NUREG/CP-0152, Vol. 3, July 2000.
: 63. M. S. Kalsi, Bahir Eldiwany, Vinod Sharma, Ryan Sicking, "Flow Loop Testing to Validate Improved Models for Single, Double & Triple Offset Disk Butterfly Valves,"
Abstract for EPRI/NMAC Eighth Valve Technology Symposium, August 2001.
: 64. J. K. Wang, Desi Somogyi, P. Daniel Alvarez, M. S. Kalsi, John Hosler (EPRI), "Flow Loop Testing and Validation of Thermal Binding Model for Wedge Gate Valves,"
Proceedings of the EPRI/NMAC Eighth Valve Technology Symposium, August 2001.
: 65. M. S. Kalsi, B. E. Eldiwany, V. Sharma, "Butterfly Valve Model Improvements Based on Compressible Flow Testing Benefit Industry AOV Programs, Proceedings of the Seventh NRC/ASME Symposium on Valve and Pump Testing, July 2002.
: 66. M. S. Kalsi, B. E. Eldiwany, V. Sharma, "Butterfly Valve Model Improvements Based on Compressible Flow Testing Benefit Industry AOV Programs, Proceedings of the Seventh NRC/ASME Symposium on Valve and Pump Testing, July 2002.
: 67. M. S. Kalsi, B. Eldiwany, "Plant Experience Based Upon Application of New Validated Models for Air-Operated Valves, Proceedings of the 9th EPRI Valve Technology Symposium, August 2003.
: 68. M. S. Kalsi, B. Eldiwany, Vinod Sharma, Aaron Richie, "Effect of Butterfly Valve Disc Shape Variations on Torque Requirements for Power Plant Applications, Proceedings of the Eighth NRC/ASME Symposium on Valve and Pump Testing, July 2004.
: 69.     KEI Document No. 2099C, KVAP User's Manual.
EPRI MOV Performance Prediction Program &
EPRI/NMAC Guides developed by Kalsi Engineering, Inc.
: 70. EPRI MOV Performance Prediction Program: Guide for the Application and Use of Valves in Power Plant Systems, Electric Power Research Institute, EPRI NP-6516, Rev.
0.
: 71. EPRI MOV Performance Prediction Program: Guide for the Application, Use, and Maintenance of Valves in Power Plants, Electric Power Research Institute, EPRI TR-105852-V1.
: 72. EPRI MOV Performance Prediction Program: Butterfly Valve Model Description Report, Electric Power Research Institute, EPRI TR- 103224.
: 73. EPRI MOV Performance Prediction Program: Butterfly Valve Design, Elbow, and Scaling Effects Test Report, Electric Power Research Institute, EPRI TR-1 03257.
Revision Date.-December 17, 2007
 
KVAP, The A 0 V/MO V Software with Technology                                               37
: 74. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Butterfly Valves in Nuclear Power Plants, Electric Power Research Institute, EPRI NP-7501.
: 75. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Butterfly Valves in Nuclear Power Plants, Rev. 1, Electric Power Research Institute, EPRI TR-106563 V2.
: 76. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Gate and Globe Valves in Nuclear Power Plants, Rev. 1, Electric Power Research Institute, EPRI TR-106563 VI.
: 77. EPRI MOV Performance Prediction Program: Gate Valve Model Report, Electric Power Research Institute, EPRI TR-103229.
: 78. EPRI MOV Performance Prediction Program: Gate Valve Design Effects Testing Results, Electric Power Research Institute, EPRI TR-103255.
: 78. EPRI MOV Performance Prediction Program: Gate Valve Design Effects Testing Results, Electric Power Research Institute, EPRI TR-103255.
: 79. EPRI MOV Performance Prediction Program: Gate Valve Thermal Binding Methodology, Electric Power Research Institute, EPRI GC- 110301.80. EPRI MOV Performance Prediction Program: Stem Thrust Prediction Method for Westinghouse Flexible Wedge Gate Valves, Electric Power Research Institute, EPRI TR-103233.
: 79. EPRI MOV Performance Prediction Program: Gate Valve Thermal                   Binding Methodology, Electric Power Research Institute, EPRI GC- 110301.
: 81. EPRI MOV Performance Prediction Program: Stem Thrust Prediction Method for W-K-M Parallel Expanding Gate Valves, Electric Power Research Institute, EPRI TR-103236.82. EPRI MOV Performance Prediction Program: Motor-Operated Valve Margin Improvement Guide, Electric Power Research Institute, EPRI TR-100449.
: 80. EPRI MOV Performance Prediction Program: Stem Thrust Prediction Method for Westinghouse Flexible Wedge Gate Valves, Electric Power Research Institute, EPRI TR-103233.
: 83. EPRI MOV Performance Prediction Program: Application Guide for Check Valves in Nuclear Power Plants, Electric Power Research Institute, EPRI NP-5479, Rev. 0 and Rev. 1.Revision Date.: December 17, 2007 KVAP, The AOV/MO V Software with Technology 38 KVAP Development/Enhancement KVAP is actively being developed and technically enhanced to ensure that the software is up-to-date and is responsive to emergent industry issues. The following summary illustrates the upgrades performed on KVAP since its release in November 2000. The software has since been revised to incorporate new features, address error reports, and fix non-technical format problems.Subscribers to the software annual maintenance receive free upgrades and electronic database migration services.KVAP 1.0 Released November 2000 Initial Modules Globe Butterfly Gate Air operators Margin Flow Default butterfly coefficients User interface KVAP 1.1 Released March 2001 Corrected problems identified in Error Reports: 2000-1 through 2000-22, except 2000-18 Revised code to address 12 formatting/enhancement type non-technical issues KVAP 1.2 Released February 2002 New features: Ball and plug valves module Default incompressible flow coefficients for full spherical ball and segmented ball Rotary diaphragm with linkage Reverse acting piston actuator"Other" actuator for defining out of scope actuators Correct problem identified in Error Report 2000-18, and 2001-1 Added saturation temperature information calculation for steam and water Added safe spring load data field Revised code to address 19 formatting/enhancement type non-technical issues KVAP 1.3 Released January 2003 Correct problem identified in Error Reports 2002-2, 2002-4, 2002-6, 2002-7, Revised code to address 42 formatting/enhancement type non-technical issues KVAP 2.0 Released May 2004 Significantly upgraded KVAP capabilities to analyze quarter-turn valves in compressible flow application including at low-pressure coefficients for butterfly valves. This effort was supported Revision Date.: December 17, 2007 KVAP, The AOV/MO V Software with Technology 39 by an additional 1100 compressible flow tests on 9 different valve designs tested in 84 configurations. (KVAP 1.3 models were based on over 1250 incompressible flow tests on 15 valves designs in 71 configurations).
: 81. EPRI MOV Performance Prediction Program: Stem Thrust Prediction Method for W-K-M Parallel Expanding Gate Valves, Electric Power Research Institute, EPRI TR-103236.
New features included: Additional incompressible flow torque coefficients for cylindrical and tapered plug valves and Camflex valves Default compressible flow coefficients for ball, plug, and eccentric plug valves Butterfly valve compressible flow coefficient for very low pressures and vacuum Optional bounding torque coefficients for butterfly valves Added Reverse acting pilot balanced valve Added Three way converging globe, valve"User" valve to permit manually defining thrust/torque valve requirements Torque predictions for 1/4 turn valves under incompressible blowdown conditions Ability to analyze valve and actuator, valve only, or actuator only Ability to change actuator type after beginning analysis Ability to define piston actuator using area or diameters Customization of AOV categories Component thrust/torque rating input Ability to selectively calculate and plot margin calculations New input screen for defining margin calculation options Added valve thrust plot capability to all linear valves New optional MOV actuator sizing module for Limitorque and Rotork actuators Numerous new illustrations Expanded numerous help menu definitions Corrected problem identified in Error Reports 2001-1, 2002-1, 2002-2, 2003-1 through 2003-7rl, and K2004-1 Redesigned input screens for added flexibility and user-friendliness Redesigned reports for added flexibility and user-friendliness Redesigned report header wizard Query feature for sorting the database KVAP 2.1 Released August 2004 Corrected problem identified in Error Report 2004-2 Revision Date.- December 17, 2007 KVAP, The AOV/MOV Software with Technology 40 KVAP 2.2 Released October 2005 Add AOV setup parameter window and set-up datasheet Provide user with options for addressing uncertainties Add open and close stroke in same analysis Provide alternate "valve factor" input for gate valves in addition to coefficient of friction Refined pilot globe valve seating-thrust calculations Enhanced effective diaphragm area model Refined Sigma-F methodology Improved application of benchset parameters Included additional combinations of actuator and linkage types KVAP 3.0 to be released in 2008 JOG MOV PV predictions SQL server database Force equations in reports Packing friction force calculator Parallel slide gate valve model Butterfly valve disc weight equations Data import & export features SI units MOV setup window to account for margin and uncertainty values Autotork and AUMA actuator capability tables Spring characteristics for bellows sealed valves Nested spring equations for air operators Potential Enhancements for Future Revisions PPM equivalent predictions Westinghouse valve model Split wedge gate valve model Anchor-Darling double disc gate valve model Revision Date: December 17, 2007 KVAP, The AO V/MO V Software with Technology 41 Comprehensive KVAP Training Seminar Outline 1. Thrust Requirements for Globe Valves" Required Stem Thrust for Globe valves" Model Applicability and Limitations" Approach* Assumptions
: 82. EPRI MOV Performance Prediction Program: Motor-Operated Valve                   Margin Improvement Guide, Electric Power Research Institute, EPRI TR-100449.
* Required Thrust for Unbalanced Disc Globe Valves* Required Thrust for Balanced Disc Globe Valves* Required Thrust for Other Types of Globe Valves* Criteria for Determining whether a Globe Valve is Seat Based or Guide Based 2. Evaluation of Air Operators" Scope" Model Description" Assumptions" Rising Stem Actuators-Double-Acting Air Cylinder, Single Ended-Double-Acting Air Cylinder, Double Ended-Double-Acting Air Cylinder, Direct Acting (Spring to Retract)-Double-Acting Air Cylinder, Reverse Acting (Spring to Extend)-Direct-Acting Diaphragm (Spring to Retract)-Reverse-Acting Diaphragm (Spring to Extend)-Direct-Acting Diaphragm with Mechanical Advantage-Reverse-Acting Diaphragm with Mechanical Advantage" Quarter-Tum Stem Actuators-Scotch Yoke, Double-Acting Air Cylinder-Scotch Yoke, Single-Acting Air Cylinder with Spring to Retract-Rotary Diaphragm Actuator-Rack and Pinion, Double-Acting Air Cylinder-Rack and Pinion, Single-Acting Air Cylinder with Spring Return-Double-Acting Air Cylinder with Linkage-Single-Acting Air Cylinder with Spring Return and Linkage 3. Torque Requirements for Butterfly Valves: KVAP-Improved Models" Torque Requirements for Butterfly Valves-References
: 83. EPRI MOV Performance Prediction Program: Application Guide for Check Valves in Nuclear Power Plants, Electric Power Research Institute, EPRI NP-5479, Rev. 0 and Rev. 1.
-Butterfly Valve Design-KVAP Butterfly Valve Model* Model Applicability and Limitations" Assumptions" Effect of Flow Disturbances on Hydrodynamic Torque (Upstream Elbow Model)* Maximum Transmitted Torque, TTR" KVAP Butterfly Model Validation Revision Date.: December 17, 2007 KVAP, The AOV/MOV Software with Technology 42 4. Torque Requirements for Ball/Plug Valves KVAP Improved Models-Ball/Plug Valve Model-Assumptions
Revision Date.: December 17, 2007
-Required Actuation Torque 5. Thrust Requirements for Solid and Flexible Wedge Gate Valves" Scope" Model Applicability and Limitations" Assumptions" Application of Thrust Equations for Steam Flow Conditions" Opening Stroke Equations" Closing Stroke Equations" Force Component Calculations" Bounding Friction Coefficients" Obtaining Disc-to-Seat Friction Coefficient through In-Situ Testing" Relationship between Valve Factor and Coefficient of Friction for Gate Valves-Exact Relationship between the Valve Factor and the Disc-to-Seat Coefficient of Friction 6. Thrust Requirements for Diaphragm Valves" Required Stem Thrust* Definitions and Units" Assumptions" Opening Stroke Equations" Closing Stroke Equations" Force Component Calculations
 
: 7. Case Studies -Plant Examples Provided by Students OPTIONAL TOPICS 8. Overview of AOV Problems, Testing Control, & Accessories" Major Causes of AOV Failure" Corrective Actions" Overview of AOV Diagnostic Devices* Bench Set Point Control* Functions of AOV Accessories
KVAP, The AOV/MO V Software with Technology                                                       38 KVAP Development/Enhancement KVAP is actively being developed and technically enhanced to ensure that the software is up-to-date and is responsive to emergent industry issues. The following summary illustrates the upgrades performed on KVAP since its release in November 2000. The software has since been revised to incorporate new features, address error reports, and fix non-technical format problems.
: 9. Margins" Margin Definitions" Uncertainties" Degradation" Margin Improvement Revision Date: December 17, 2007}}
Subscribers to the software annual maintenance receive free upgrades and electronic database migration services.
KVAP 1.0 Released November 2000 Initial Modules Globe Butterfly Gate Air operators Margin Flow Default butterfly coefficients User interface KVAP 1.1 Released March 2001 Corrected problems identified in Error Reports:
2000-1 through 2000-22, except 2000-18 Revised code to address 12 formatting/enhancement type non-technical issues KVAP 1.2 Released February 2002 New features:
Ball and plug valves module Default incompressible flow coefficients for full spherical ball and segmented ball Rotary diaphragm with linkage Reverse acting piston actuator "Other" actuator for defining out of scope actuators Correct problem identified in Error Report 2000-18, and 2001-1 Added saturation temperature information calculation for steam and water Added safe spring load data field Revised code to address 19 formatting/enhancement type non-technical issues KVAP 1.3 Released January 2003 Correct problem identified in Error Reports 2002-2, 2002-4, 2002-6, 2002-7, Revised code to address 42 formatting/enhancement type non-technical issues KVAP 2.0 Released May 2004 Significantly upgraded KVAP capabilities to analyze quarter-turn valves in compressible flow application including at low-pressure coefficients for butterfly valves. This effort was supported Revision Date.: December 17, 2007
 
KVAP, The AOV/MO V Software with Technology                                                   39 by an additional 1100 compressible flow tests on 9 different valve designs tested in 84 configurations. (KVAP 1.3 models were based on over 1250 incompressible flow tests on 15 valves designs in 71 configurations). New features included:
Additional incompressible flow torque coefficients for cylindrical and tapered plug valves and Camflex valves Default compressible flow coefficients for ball, plug, and eccentric plug valves Butterfly valve compressible flow coefficient for very low pressures and vacuum Optional bounding torque coefficients for butterfly valves Added Reverse acting pilot balanced valve Added Three way converging globe, valve "User" valve to permit manually defining thrust/torque valve requirements Torque predictions for 1/4 turn valves under incompressible blowdown conditions Ability to analyze valve and actuator, valve only, or actuator only Ability to change actuator type after beginning analysis Ability to define piston actuator using area or diameters Customization of AOV categories Component thrust/torque rating input Ability to selectively calculate and plot margin calculations New input screen for defining margin calculation options Added valve thrust plot capability to all linear valves New optional MOV actuator sizing module for Limitorque and Rotork actuators Numerous new illustrations Expanded numerous help menu definitions Corrected problem identified in Error Reports 2001-1, 2002-1, 2002-2, 2003-1 through 2003-7rl, and K2004-1 Redesigned input screens for added flexibility and user-friendliness Redesigned reports for added flexibility and user-friendliness Redesigned report header wizard Query feature for sorting the database KVAP 2.1 Released August 2004 Corrected problem identified in Error Report 2004-2 Revision Date.-December 17, 2007
 
KVAP, The AOV/MOV Software with Technology                                                   40 KVAP 2.2 Released October 2005 Add AOV setup parameter window and set-up datasheet Provide user with options for addressing uncertainties Add open and close stroke in same analysis Provide alternate "valve factor" input for gate valves in addition to coefficient of friction Refined pilot globe valve seating-thrust calculations Enhanced effective diaphragm area model Refined Sigma-F methodology Improved application of benchset parameters Included additional combinations of actuator and linkage types KVAP 3.0 to be released in 2008 JOG MOV PV predictions SQL server database Force equations in reports Packing friction force calculator Parallel slide gate valve model Butterfly valve disc weight equations Data import & export features SI units MOV setup window to account for margin and uncertainty values Autotork and AUMA actuator capability tables Spring characteristics for bellows sealed valves Nested spring equations for air operators Potential Enhancements for Future Revisions PPM equivalent predictions Westinghouse valve model Split wedge gate valve model Anchor-Darling double disc gate valve model Revision Date: December 17, 2007
 
KVAP, The AO V/MO V Software with Technology                                         41 Comprehensive KVAP Training Seminar Outline
: 1. Thrust Requirements for Globe Valves
      " Required Stem Thrust for Globe valves
      " Model Applicability and Limitations
      " Approach
* Assumptions
* Required Thrust for Unbalanced Disc Globe Valves
* Required Thrust for Balanced Disc Globe Valves
* Required Thrust for Other Types of Globe Valves
* Criteria for Determining whether a Globe Valve is Seat Based or Guide Based
: 2. Evaluation of Air Operators
      " Scope
      " Model Description
      " Assumptions
      " Rising Stem Actuators
        - Double-Acting Air Cylinder, Single Ended
        - Double-Acting Air Cylinder, Double Ended
        - Double-Acting Air Cylinder, Direct Acting (Spring to Retract)
        - Double-Acting Air Cylinder, Reverse Acting (Spring to Extend)
        - Direct-Acting Diaphragm (Spring to Retract)
        - Reverse-Acting Diaphragm (Spring to Extend)
        - Direct-Acting Diaphragm with Mechanical Advantage
        - Reverse-Acting Diaphragm with Mechanical Advantage
      " Quarter-Tum Stem Actuators
        - Scotch Yoke, Double-Acting Air Cylinder
        - Scotch Yoke, Single-Acting Air Cylinder with Spring to Retract
        - Rotary Diaphragm Actuator
        - Rack and Pinion, Double-Acting Air Cylinder
        - Rack and Pinion, Single-Acting Air Cylinder with Spring Return
        - Double-Acting Air Cylinder with Linkage
        - Single-Acting Air Cylinder with Spring Return and Linkage
: 3. Torque Requirements for Butterfly Valves: KVAP-Improved Models
      " Torque Requirements for Butterfly Valves
        - References
        - Butterfly Valve Design
        - KVAP Butterfly Valve Model
* Model Applicability and Limitations
      " Assumptions
      " Effect of Flow Disturbances on Hydrodynamic Torque (Upstream Elbow Model)
* Maximum Transmitted Torque, TTR
      " KVAP Butterfly Model Validation Revision Date.: December 17, 2007
 
KVAP, The AOV/MOV Software with Technology                                                 42
: 4. Torque Requirements for Ball/Plug Valves KVAP Improved Models
        - Ball/Plug Valve Model
        - Assumptions
        - Required Actuation Torque
: 5. Thrust Requirements for Solid and Flexible Wedge Gate Valves
      " Scope
      " Model Applicability and Limitations
      " Assumptions
      " Application of Thrust Equations for Steam Flow Conditions
      " Opening Stroke Equations
      " Closing Stroke Equations
      " Force Component Calculations
      " Bounding Friction Coefficients
      " Obtaining Disc-to-Seat Friction Coefficient through In-Situ Testing
      " Relationship between Valve Factor and Coefficient of Friction for Gate Valves
        - Exact Relationship between the Valve Factor and the Disc-to-Seat Coefficient of Friction
: 6. Thrust Requirements for Diaphragm Valves
      " Required Stem Thrust
* Definitions and Units
      " Assumptions
      " Opening Stroke Equations
      " Closing Stroke Equations
      " Force Component Calculations
: 7. Case Studies - Plant Examples Provided by Students OPTIONAL TOPICS
: 8. Overview of AOV Problems, Testing Control, & Accessories
      " Major Causes of AOV Failure
      " Corrective Actions
      " Overview of AOV Diagnostic Devices
* Bench Set Point Control
* Functions of AOV Accessories
: 9. Margins
      " Margin Definitions
      " Uncertainties
      " Degradation
      " Margin Improvement Revision Date: December 17, 2007}}

Revision as of 15:42, 12 November 2019

Email from M. Halter, Subj: Part 21 - Kasi MOV and AOV Software, (44 Pages)
ML11258A116
Person / Time
Site: Indian Point Entergy icon.png
Issue date: 06/20/2011
From: Halter M
Reactor Projects Branch 2
To: Bode P
Entergy Nuclear Operations
References
FOIA/PA-2011-0272
Download: ML11258A116 (44)


Text

Page 1 of I From:, Halter, Mandy Sent: Monday, June 20, 2011 1:33 PM To: 'pbode@entergy.com'

Subject:

Part 21 - KASI MOV and AOV Software Attachments: EN46955.pdf; KVAP-Software-for-AOV-&-MOV-design-basis-ma rgin-calculations-for-JOG-Program-Implementation-GL-96-05-Periodic-Verification-margin-improvement.pdf

Paul, Attached is the Part 21 that came out of Oconee (attached above EN 46955). The defect is related to errors in the Kalsi Engineering Valve and Actuator Program (KVAP) software that provide default flow and torque coefficients for ball and plug valves which can affect margin predictions.

Please confirm whether or not Indian Point has reviewed this issue for applicability.

Thanks and kind regards, Mandy Mandy Halter U.S. Nuclear Regulatory Commission Resident Inspector Indian Point Energy Center - Unit 3 (914) 739-8565 file://C:\Documents and Settings\lnw\Local Settings\Temporary Internet Files\Content.Outlook\OQSQO7... 7/22/2011

KVAP The Leading AOV/ OV Software....

-~ V j

... Serving the Energy Industries Kalsi Engineering, Inc.

745 Park:Two Drive Sugar Land, TX 77478-2885 (281)240-6500 www;kalsi:com,.

© Copyright Kalsi Engineering, Inc. 2007 All rights, resberv.ed . -

Revision Date. December 17, 2007

KVAP, The AO V/MO V Software with Technology Table of Contents Page Introduction to KVAP 2 Background of Kalsi Engineering Flow Loop Testing and Validated Model Development Program for KVAP 6 KVAP Software Capabilities 8 KVAP Scope of Valves and Actuators 9 Typical KVAP Screens 13 Company Background and Experience Relevant to AOVs, MOVs, and Check Valves 20 Key Personnel 28 KVAP References and Other Significant Documents Developed by Kalsi Engineering, Inc. 33 KVAP Development/Enhancement/History 38 KVAP Training Seminar Outline 41 Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 2 Introduction to KVAP The AOV/MOV Software with Technology KVAP, the Kalsi Valve & Actuator Program, is a state-of-the-art software for performing reliable design basis calculations for all common types of globe, gate, diaphragm, butterfly, ball, and plug valves.

The KVAP software represents a significant advancement over all other design basis calculation software packages (e.g. EPRI MOV PPM, ACE, AirBase, etc.) available in the industry for it incorporates validated models that the industry was lacking for many different types of valves commonly used in AOV/MOV applications (see Tables I(A) through I(D)). These validated models are the outcome of a very comprehensive flow loop testing program conducted by Kalsi Engineering, Inc., (KEI) to overcome the limitations of valve manufacturers' data, and the new database of torque/flow coefficients in KVAP, based upon four years of extensive flow loop testing on a wide range of valve designs, provides more accurate, position dependent bounding predictions, while eliminating excessive conservatism, as well as, non-conservatism found in the EPRI MOV PPM software (see the Part 21 and EPRI Error Notices below).

KVAP was developed by the same KEI valve specialists who previously developed the EPRI MOV PPM and software modules. All testing, analytical model development, software development, and verification and validation activities were performed under the Kalsi Engineering, Inc., quality assurance program, which meets IOCFR50 Appendix B requirements.

KVAP Benefits Key advantages offered by KVAP to it's over 50 current users are:

  • KVAP is the only software that includes validated valve models with position dependent accuracy (necessary for AOV evaluations) that the industry was lacking; these enable reliable design basis calculations for accurately quantifying AOV/MOV margins, not possible with previous industry models

" KVAP models are based upon/validated against a comprehensive database of 10CFR50 Appendix B test results for incompressible flow and compressible flow tests performed on all common types of quarter-turn valves (over 2500 tests), that provide reliablepredictions while eliminating excessive conservatism in earlier models (e.g., EPRI MOV PPM).

KVAP models provide more accurate, bounding predictions that typically result in larger margins in AOVs/MOVs

  • The larger margins in AOVs/MOVs provided by KVAP eliminate unnecessary equipment modifications, especially those, resulting from excessively conservative methodologies (e.g.,

EPRI MOV PPM) in many applications

  • The larger margins in AOVs/MOVs provided by KVAP reduce the frequency of periodic verification testing required to meet the Joint Owners Groups recommendations
  • KVAP validated models eliminate the need for expensive in-situ dynamic testing, resulting in savings of thousands of dollars per valve

" The user-friendly graphic interface eliminates potential errors commonly made during calculations, enabling a more efficient completion of evaluations

" KVAP does not have the non-conservatism found, and limitations imposed in the use of the EPRI MOV PPM models as identified in the following Part 21 and Error Notices:

Revision Date.-December 17, 2007

KVAP, The AOV/MO V Software with Technology 3 o 10CFR21 Notification by EPRI Regarding Potential Non-Conservatism of EPRI's MOV Performance Prediction Methodology (PPM) Butterfly Valve Model under Compressible Flow Conditions, 13-April-07 o PPM Software Error Notice 2007-1 (Potential Non-Conservatism in Butterfly Valve Model Predictions under Compressible Flow Conditions) 12-Mar-07 o PPM Software Error Notice 2005-1 (Minimum Required Thrust Unconservative in Self Actuating Portion of Stroke) o PPM Software Error Notice 2004-2 (Potential Non-Conservatism in Butterfly Valve Model Predictions under Compressible Flow Conditions) 22-Oct-04 o PPM Software Error Notice 2003-2 (Required Adjustments to Butterfly Valve Disc Angle Dependent Torque Predictions) 19-Dec-03 o PPM Software Error Notice 2003-1 Version 3.0 (Build 3.0.50) and Version 3.1 (Build 3.1.8) (Proximity of Upstream Disturbances) 9-Apr-03 o PPM Software Information Notice 2002-1 (Prediction of Butterfly Valve Design Basis Required Torque as a Function of Disk Position) 6-May-02 o PPM Version 3.0 (Build 3.0.50) Software Error Notice 2001-1 (Butterfly Valve Stem Orientation) 6-Nov-01 Cost Savings, Stability and Continuity Many KVAP users have reported savings in excess of $500,000 achieved by avoiding unwarranted equipment replacement in valves previously determined to have negative or low margins, ALARA savings and elimination of dynamic testing requirements. The enhanced models in KVAP can also potentially yield increased MOV margins that can help extend static periodic verification test intervals. KVAP software was developed by a team of Kalsi specialists who are recognized as leaders in the industry for technological advances in AOVs and MOVs, and for providing stability and continuity of service to our clients. The software is backed by comprehensive training and technical support offered by this highly capable KVAP team.

Revision Date. December 17, 2007

KVAP, The AOV/MO V Software with Technology' 4 Table 1(A)

Quarter-Turn 1zJah'es Validated Methodologies/Software Available For AOVs & MOVs Valve Types Prevalent in AOV NRC/INEL EPRI Ace, KVAP Population Cont. Purge* MOV PPM** AirBase 1 Symmetric Butterfly NteNone

  • V ,N6n' V 2 Single-Offset Butterfly Nolte 3 Double-Offset Butterfly *NoleNone None 4 Segmented V-Ball 'N*one N None /

5 Spherical Ball Nonte None Non6kre V 6 Eccentric Plug =,None N**oe n Nofe> V 7 Tapered/Cylinder Plug Nolte 'Nole NoeV

  • No software was provided by NRC/INEL
    • No Compressible flow testing was performed by EPRI
      • EPRI Models found to be non-conservative for certain applications as described in NRC Part 21 and EPRI Error Notices (see previous page for a listing)

Table I(B)

Linear Vadves Validated or First Principles Based Methodologies/Software Available for AOVs & MOVs EPRI Ace, KVAP Valve Type MOV PPM AirBase 1 Globe-Unbalanced V V 2 Globe-Balanced, Cage V V 3 Globe-Balanced, Double Disc V V 4 Globe-Balanced, Pilot Non V V 5 Globe-3-way Converging, Single Disc Non> ... None V 6 Globe-3-way Converging, Double Disc None 'Nolte.

7 Globe-3-way Diverging, Single Disc Nolt 8 Globe-3-way Diverging, Double Disc Nn II 9 Diaphragm Nolne ,

10 Gate-Solid or Flexible V V V Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 5 Table I(C)

Linear and Quarter-Turn / ctualor Models/Software Available for AOVs & MOVs EPRI Ace, KVAP Actuator Type MOV PPM AirBase A 0 Vs Cylinder Noi Diaphragm IF-N eV' Scotch Yoke Nonei V Rack & Pinion Nn V Cylinder with Linkage (Type 1)

  • None* V Cylinder with Linkage (Type 2) None , Nollje Diaphragm with Lever N Vn M1O Vs Limitorque V V Rotork KiNone Otiler 7

User Defined ~ No7 I VC Table I(D)

M in Evaluation and 001 Set Point Control Features Feature EPRI Ace, KVAP MOV PPM AirBase Margin Evaluation None AOV Setup Box for Set Point Control  ;*;None ** No* e V

  • For linear valves, mid stroke margins are not calculated in Ace or AirBase Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 6 Background of Kalsi Engineering. Flow Loop Testing and Validated Model Development Program for KVAP As summarized in USNRC Regulatory Issue Summary 2000-03, problems with power-operated valves have resulted in an increased emphasis by USNRC on improving the performance reliability and predictability of AOVs. In response, the Joint Owners Group for Air-Operated Valves (JOG AOV) developed a document to provide guidance and define minimum requirements to the utilities for implementing AOV programs. Additionally, four utilities performed design basis calculations under EPRI's AOV pilot programs. This resulted in a calculation methodology for AOVs, which is documented in the EPRI AOV Evaluation Guide (TR107322).

These EPRI AOV pilot plant programs, and the implementation of the AOV Evaluation Guide methodologies at other plants revealed three key problems:

  • There are no validated models for several types of quarter-turn valves (e.g., spherical ball, V-notch ball, eccentric plug) that constitute a large AOV population; unvalidated approaches had to be used for design basis calculations. This can lead to unreliable AOV performance, based on industry experience and lessons learned from MOVs.
  • EPRI MOV PPP methodology for symmetric and many single-offset butterfly valves was found to provide negative margin for AOVs. The original PPM models were based on a very limited amount of butterfly valve tests in incompressible flow applications. To cover valve applications that were not tested and uncertainties, additional conservatism was added in the PPM. This excessive conservatism caused the EPRI methodology to predict low or negative margins for AOVs that, in fact, have larger margins and capability to operate under design basis conditions.

" Subsequent compressible flow testing performed by Kalsi Engineering revealed that the EPRI MOV PPP methodology was non-conservative in compressible flow applications (See Part 21 and EPRI Error Notices on page 3).

This testing led to improved and validated methodologies that accurately predict torque requirements for all types of quarter-turn valves prevalent in AOV applications.

A comprehensive matrix of flow loop testing was performed to develop more accurate validated models for AOVs incorporated in KVAP.

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 7 Valve Orientation Configuration Group Tests Valve Orientation Confi uration Quarter-turn Valve Test Matrix Incompressible: 15 Valve Designs, 71 Configurations, 1,272 Tests Compressible: 9 Valve Designs., 84 Configurations, 1,1 16 Tests The KVAP software and its extensive database capabilities incorporate the new validated models for quarter-turn valves developed under this program. KVAP also includes validated/first principles based industry established models for all other common types of globe, gate, and diaphragm valves and actuators to offer a complete software package for reliable and efficient calculations. KVAP software development, analytical models, flow loop test program, and verification and validation meet the requirements of IOCFR50 Appendix B.

KVAP includes models for all common types of linear (globe, gate, diaphragm) and quarter-turn (butterfly, ball, plug) valves & actuators.

Revision Date. December 17, 2007

KVAP, The AOV/MO V Software with Technology 8 KVAP Software Capabilities The Kalsi Valve & Actuator Program is a state-of-the-art software that efficiently performs reliable design basis calculations for all common types of globe, gate, diaphragm, butterfly, ball, and plug valves as well as linear and quarter-turn actuators used in POV applications.

KVAP is the only POV software in the industry that includes a number of new validated valve models based on first principles supported by extensive CFD analyses and 10CFR50 Appendix B testing. These new models are applicable to several types of valves that are common to AOV applications which had not been addressed by the EPRI MOV PPM, JOG AOV, NSSS Owners Groups, valve manufacturers, or other organizations marketing competing software.

KVAP includes a comprehensive database of 10CFRR5O Appendix B test results to accurately predict torque/thrust requirements for various types of POVs under design basis conditions. The flow loop test matrix to support KVAP development and validation included over 2,000 static and dynamic tests to cover variations in valve/disc geometry, elbow orientation, elbow distance, flow direction, flow rates, and maximum AP. KVAP provides geometry-specific torque and flow coefficients for baseline conditions and for elbow effects.

In many POV applications, the new KVAP models for quarter-turn valves provide a substantial increase in margin between valve requirements and actuator capabilities, thus eliminating unnecessary equipment modifications. The KVAP databaseand the more accurate models have already demonstratedsubstantialcost savingsfor the plants.

From inception, KVAP software development was planned with a well-structured modular approach to minimize the cost and time associated with the V&V effort for upgrades and revisions. This ensures that new data and improvements to address emerging industry issues for POVs can be efficiently incorporated,verified, and validated in KVAP.

The KVAP software input and output screens are heavily supported by graphics that illustrate critical features and dimensions of the valve being analyzed, valve orientation, flow direction, elbow orientation, required valve thrust/torque throughout the stroke, minimum and maximum actuator capability throughout the stroke, and margin throughout the stroke. This user-friendly graphicinterface eliminates mistakes and errors commonly made during PO V calculations.

KVAP was developed by a team of Kalsi senior specialists who are recognized as leaders in the industry for technological advances in AOV, MOV, HOV, SOV and check valves. Our specialists have more than 20 years of continuous involvement in R&D to develop validated first principles models and software for valves and actuators to address generic industry-wide issues, including the EPRI MOV Performance Prediction Program and MOV guides. This experience is supplemented by performing design basis calculations and implementing MOV, AOV and Check Valve programs at more than 25 power plants.

Revision Date: December 17, 2007

KVAP, The AOV/MOV Software with Technology 9 KVAP Scope of Valves and Actuators KVAP software is capable of evaluating all common types of AOV/MOV valves and actuators:

Valve Types Actuator Types Linear (dirtect & reverse acting, (isapplcbe~

  • Gate-Solid, Flexible, Parallel Slide " Cylinder
  • Globe-Unbalanced
  • Single acting w/spring
  • Globe-Balanced, Cage " Double acting
  • Globe-Balanced, Double Disc
  • Double acting, double ended
  • Globe-Balanced, Pilot
  • Double acting w/spring
  • Globe-3-way Converging, Single Disc " Diaphragm
  • Globe-3-way Converging, Double Disc
  • Single acting w/spring
  • Globe-3-way Diverging, Single Disc Quarter-Turn
  • Globe-3-way Diverging, Double Disc " Scotch Yoke
  • Diaphragm " Single acting w/spring Quarter-Turn " Double acting
  • Symmetric Butterfly
  • Rack & Pinion
  • Single-Offset Butterfly " Single acting w/spring
  • Double-Offset Butterfly " Double acting
  • Segmented V-Ball " Cylinder with Linkage (2 types)
  • Spherical Ball " Single acting w/spring 9 floating and trunnion mounted " Double acting
  • Eccentric Plug
  • Tapered/Cylinder Plug 9 Single acting w/spring Ele'c'tric_ M__o-t-or
  • User Defined
  • Limitorque

" Rotork Other 9 User Defined

  • any air, hydraulic, or electric motor actuator with defined output vs. stroke Revision Date.-December 17, 2007

KVAP, The AOV/MOV Software with Technology 10 Other KVAP Features/Capabilities

  • Analyzes incompressible, compressible, choking, flashing flow
  • Includes valve geometry-specific upstream elbow effect coefficients for butterfly, ball, and plug valves
  • Evaluates mid-stroke margins
  • Provides extremely user-friendly, intuitive graphical user interface and comprehensive database capabilities
  • Well planned modular structure for efficient V&V to support upgrades/new capabilities
  • Operates on Windows operating systems Applications, Advantages, and Benefits
  • Performs reliable POV design basis calculations, including minimum required thrust/torque, actuator capabilities and margin
  • Eliminates the need for dynamic AP testing, saving tens of thousands of dollars per valve
  • Provides models for double-offset butterfly, full ball, segmented ball, and plug valves, for which no validated models were available in the industry
  • Eliminates excessive conservatism in EPRI PPM models; increases margin
  • Eliminates unnecessary equipment modifications and/or repeat calculations to address low/negative margins
  • Extremely intuitive, user-friendly graphical interface improves efficiency and eliminates errors
  • Troubleshoots valve performance problems ContinuousEnhancements Based on User/Industry Feedback KVAP is being actively expanded/enhanced and supported to address industry wide emerging issues and requirements and feedback from its 50+ current users. Some of the recent enhancements include the AOV Setup Box and set point data sheets for efficient implementation and verification of the design basis calculations in the field, efficient implementation of the Joint Owners Group MOV Periodic Verification recommendations.

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 11 A 0 V Setup Box and Set PointData Sheets for FieldImplementation The component level calculations provide an assessment of actuator margin based on valve requirements and actuator output. Changes in valve set points (e.g. regulator, air pressure and spring preload) and packing adjustments may affect the actuator output and invalidate values calculated prior to performing valve setup tests. Additionally, adjustments of the set points in one direction may affect the required set point in the opposite direction. To facilitate the addressing of these issues, a setup module has been incorporated into KVAP that graphically displays the required and allowable spring preload (i.e. minimum and maximum allowable lower bench set) as a function of regulated air pressure and regulator settings using two different approaches. This setup box also accounts for all AOV uncertainties in various parameters. The set point datasheet defines the setup parameters and allows adjustments to be made without revisiting the margin calculations. The following figure shows a typical AOV setup box and an alternative approach of displaying static thrust trace predicted by KVAP and the allowable bench set window.

AOV Setup Box AOV Setup Window - Static Stroke

-- TnnBt hsneRaenn . Aco......

n4ed StIcSflc~e -- Lo..,etBnhnOeoRn o-e ch~t See5 -iL Re Str Se -Regu-piel.e ROte Sl*

htn. LoweML nnchent

  • - -- - II MmOngolnini Rqu-P-Air~e , ~ ffnen;-Of-nua tmDsi et atOn n 32 34 33 30 *o n6 o 1e e n

'm n e n n 60a Approach (A) Approach (B)

Setup Box Showing Allowable Spring Preload Setup Window for Allowable Lower Bench Set Range as a Function of Regulated Air Supply Range for a Given Regulated Air Supply Pressure Pressure Displayed on KVAP Static Thrust Stroke Predictions Graphical Approaches in KVAP for Field Implementation of AOV Setup Parameters Rev

KVAP, The A 0 V/MO V Software with Technology 12 MO VActuator Module The KVAP MOV Actuator Module is developed to calculate torque and thrust capabilities for motor operated valve actuators and quarter-turn units based on "Application Guide for Motor-Operated Valves in Nuclear Power Plants" prepared by Kalsi Engineering, Inc. It features a user-friendly graphical interface that reduces mistakes and errors commonly made during calculations, thus enabling a more efficient completion of evaluations. The module includes Limitorque SMB/SB/SBD actuators, Rotork Actuator, and quarter turn gear operators. This module can augment calculations performed during the implementation of the GL-96-05 MOV JOG Periodic Verification program.

The Limitorque actuator module enables the calculation of SMB/SB/SBD for:

" Pullout torque/thrust,

  • Stall torque/thrust,

" Running torque/thrust and

  • Stem speed Inputs include: the overall gear ratio, stem thread characteristics (as applicable), application factors, efficiency, reduced voltage, and temperature effects (as applicable). The model comprises equations, and built-in manufacturers' default values for actuator efficiency, application factors, motor ratings, and temperature effects. The model also provides inputs for using enhanced electric motor models such as ComEd.

The Rotork actuator module uses torque and thrust output capability values published in the Rotork catalog for "A" type actuators. The user selects the gearbox size and stem nut RPM, and enters stem diameter, stem lead, stem pitch, and coefficient of friction between the stem and stem nut. The model selects the corresponding values of torque rating and thrust rating and calculates the thrust output. The value for torque output is the same as the torque rating. The values returned are applicable to type "A" 60 Hz 3 phase Rotork actuators.

The quarter turn gear operator can be coupled to Limitorque or Rotork actuators. The inputs allow for any generic actuator definition which defines the actuator by gear ratio and efficiency.

Revision Date.: December 17, 2007

KVAP, The AOVMO V Software with Technology 13 Typical KVAP Screens The KVAP software input and output screens are heavily supported by graphics that illustrate critical featuresand dimensions of the valve being analyzed, valve orientation, flow direction,

.elbow orientation, required valve thrust/torque throughout the stroke, minimum and maximum actuator capability throughout the stroke, and margin throughout the stroke. This user-friendly graphic interface eliminates the potentialfor errorscommonly made during POV calculations.

Some examples of input and output screens follow:

KVAP Main Menu Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology , 14 Globe Valve Configuration Fil. T-Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 15 Flow Inputs for Globe Valve Fjile Tos~~ ja~

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 16 Valve Design File Tools H Analysis

-lo I Revision Date. December 17, 2007

KVAP, The AOV/MO V Software with Technooigy 17 Valve Installation HEji ol ep ay Revision Date. December 17, 2007

KVAP, The AOV/MO V Software with Technology 18 Valve Results Eile Tools Helk Aalysis Reports VALVERESULTS

SUMMARY

,

1 11- . I II . . OTHER CALCULATED DAM, " ., . - 10 1 1ýj Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 19 Margin Plot I I.

Eile Tools Helo Analysis ReosIs Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 20 Company Background and Experience Relevant to AOVs, MOVs, and Check Valves Valve design, analysis, testing, model development, application, and problem solving are areas of special competence at Kalsi Engineering. Our personnel have in-depth knowledge, extensive experience, and an established track record of supporting all US and Canadian nuclear power utilities, and contributing to EPRI, and NSSS Owners' Groups in developing generic models/methodologies to address industry-wide issues; performing design basis reviews; and implementing plant-wide programs related to MOVs, AOVs, and check valves.

The depth, diversity, and continuity of our experience in addressing AOV, MOV, and check valve issues for nuclear power utilities over the last 25 years is unique in the industry. The insight and expertise of our personnel benefit our clients by identifying and implementing the most technically sound and cost-effective approach that can be fully justified to the regulatory authorities.

Our consulting engineering offices as well as the testing laboratories are located at the same facility in the Houston metropolitan area. This environment facilitates the development of the most optimum approach based on the appropriate combination of analysis and testing.

The following factors make Kalsi Engineering the most capable organization to efficiently support your valve-related projects:

" Personnel with Strong Technical Background, Experience, and Continuity. Our key personnel have more than 25 years of experience directly related to solving problems with all types of valves, and the average tenure of our senior staff is 19 years. Their continuity and depth of experience makes them immediately productive on your project.

  • EPRI MOV Performance Prediction Program (PPP) Models/Software and NMAC Guides. Based upon our unique background, Kalsi Engineering was selected by EPRI/NMAC to develop validated models, software, and testing for the EPRI MOV PPP methodologies and guides for gate, globe, and butterfly valves that are widely used by all nuclear utilities (see Table 2).

The same KEI senior specialists who developed the EPRI MOV PPM models are responsible for the development of new and more accurate models for POVs to meet industry needs.

" Validated Models for Quarter-Turn Valves. Recognizing that the industry was lacking validated models for a wide variety of quarter-turn valves, KEI undertook a very comprehensive program to develop such models to accurately quantify the torque requirements for all common types of ball, butterfly, and plug valves used in nuclear power plants. The program also focused on developing more accurate, validated models for symmetric and single offset butterfly valves to eliminate the excessive conservatism in the EPRI MOV PPP models that were developed specifically for MOVs. The new models provide a substantial increase in margins between valve requirements and actuator capabilities, thus eliminating unnecessary equipment modifications.

Revision Date.-December 17, 2007

KVAP, The AOV/MO V Software with Technology 21 The test program was conducted under IOCFR50 Appendix B QA requirements to develop the torque and flow coefficients, including the effect of elbows. The test matrix included over 2,500 static and dynamic tests to cover variations in disc geometry, elbow orientation, elbow distance, flow direction, flow rates, and maximum AP. The validated methodologies as well as torque coefficients, flow coefficients, and elbow influence factors are incorporated in KVAP, the Kalsi Valve & Actuator Program.

Design Basis Reviews, Analyses, and Implementation of MOV, AOV, and Check Valve Programs. Kalsi Engineering personnel have worked with over 50 U.S. nuclear power utilities in performing design basis calculations and reviews of MOV, AOV, and check valves to improve margins and address NRC GL 89-10, GL 95-07, GL 96-05, NRC lE Bulletin 85-03, and INPO SOER 86-03, and JOG AOV program guidelines. Many of these projects have employed advanced analytical methods (e.g., CFD and FEA) or special tests to qualify valves that cannot be tested in-situ.

" Credibility with USNRC. Due to our strong technical background and rigorous approach in supporting utilities and industry-wide technical programs, Kalsi Engineering has established an excellent credibility with the NRC over the years. This has been a significant factor in obtaining NRC approval on a number of critical industry-wide programs and individual utility issues. Kalsi Engineering has successfully supported numerous utilities in NRC closures, inspections, and enforcement conferences.

  • Root Cause Analysis and Problem Solving Experience. In our root cause analyses and problem-solving experiences at nuclear power plants and petrochemical plants, we have performed in-depth investigations of valves and actuators made by all the major manufacturers. This has provided our personnel with significant insight into the critical differences between similar-looking designs made by different manufacturers that can have a major impact on valve performance. Kalsi Engineering can provide complete design modification support to solve valve/actuator problems.

Revision Date: December 17, 2007

KVAP, The A 0 V/MO V Software with Technology 22 Table 2: Kalsi Engineering EPRI Projects Kalsi Engineering EPRI Report Title Report No. Principal Investigators Gate Valve Model Report TR-103229 Wang, Kalsi Butterfly Valve Model Description Report TR-103224 Eldiwany, Kalsi Stem Thrust Prediction Method for TR-103233 Wang, Kalsi Westinghouse Flexible Wedge Gate Valves Stem Thrust Prediction Method for TR-103236 Eldiwany, Alvarez W-K-M Parallel Expanding Gate Valves Gate Valve Design Effects Testing Results TR-103255 Alvarez, Kalsi Butterfly Valve Design, Elbow, and Scaling TR-103257 Sharma, Kalsi Effects Test Report Motor-Operated Valve Margin Improvement TR-100449 Alvarez, Kalsi Guide Application Guide for Motor-Operated Gate and 1015396 Volume I Kalsi, Wang, Globe Valves in Nuclear Power Plants, Rev. 2 Alvarez, Eldiwany Application Guide for Motor-Operated Butterfly 1015396 Volume 2 Eldiwany, Kalsi Valves in Nuclear Power Plants, Rev. 2 Guide for the Application, Use, and TR-105852-V1 Eldiwany, Alvarez Maintenance of Valves in Power Plants Guide for the Application and Use of Valves in NP-6516, Rev 0 Kalsi, Alvarez Power Plant Systems Application Guide for Check Valves in Nuclear NP-5479, Rev 0 and Kalsi, Wang, Sharma Power Plants Rev. 1 U.S. Nuclear Industry Approaches to Address TR- 114051 Eldiwany, Kalsi Gate Valve Pressure Locking, Thermal Binding, and Related Issues Gate Valve Thermal Binding Unwedging Thrust E210203 Volumes 1-4 Kalsi, Wang, Alvarez, Methodology Somogyi Non-Metallic Bearing Friction Test Program for 1003151, 1007285, Alvarez, Sicking Quarter-Turn Valves 1007286, 1007287 1007288 Limitorque Actuator Fatigue Life Extension 1013464 Estep, Alvarez, Kalsi Table Updated on August 21, 2007 Revision Date. December 17, 2007

KVAP, The AOV/MO V Software with Technology 23

" Independent Assessment of Utilities' MOV, AOV, and Check Valve Programs. Kalsi Engineering personnel have performed independent assessments of valve programs to address NRC Generic Letters 89-10, 95-07, and 96-05 concerns, check valve programs to address INPO SOER 86-03 issues, and AOV programs to address JOG AOV program recommendations and INPO SER 1-99 recommendations for several utilities.

  • AOV Actuator Sizing/Stability Criteria and Modifications. AOV instabilities that are often unrecognized create premature degradation of packings and fatigue failure of AOV components, resulting in substantial cost penalties due to unscheduled downtime and maintenance. Based on AOV actuator stability problems encountered in various plants with balanced and unbalanced design globe valves, Kalsi Engineering has developed technical criteria to ensure stability of the AOV actuators. These criteria are based on first principle models verified by laboratory testing and in-situ plant performance. Kalsi Engineering personnel have performed tests on diaphragm actuators to determine effective diaphragm area from the actuator output versus stroke curves. KEI has implemented modifications in diaphragm actuators, including unique tandem configurations, to meet higher thrust requirements while eliminating instability (see Attachment 2 papers).
  • Limitorque Actuator Rating Increase Program and Software. Under multiple-utility and NSSS Owners' Group sponsorship, Kalsi Engineering conducted the Limitorque Actuator Rating Increase Program, which has been recognized as one of the most valuable and cost effective program by all participating utilities. Recognizing the benefits offered by this program, virtually all U.S. nuclear power utilities joined in the program. The program results permitted the utilities to technically evaluate and continue to use their existing actuators at thrust and torque ratings well above Limitorque's standard published ratings without any safety concerns. The LTAFLA software was developed and validated to determine allowable cycles in operation under over-torque conditions in MOVs, thus eliminating the need for actuator modifications.

" MOV, AOV, and Check Valve Training Seminars for Utilities and NMAC. Kalsi Engineering has presented numerous seminars to provide basic and advanced MOV, AOV, and check valve training to utilities and the EPRI/NMAC organization. Seminars can be custom tailored and scheduled to meet the individual utility's needs, including needs arising from reorganization or new personnel being assigned to the valve projects. Seminars can be conducted at either the plant or the Kalsi Engineering facility. Our facility offers the advantage of hands-on experience/testing at our flow loop, including the use of diagnostic tools and the opportunity to discuss your plant's problems with several of our senior specialists who are recognized as leading industry experts.

" Improved Model for Gate Valve Unwedging Thrust, including Pressure Locking and Pressure-Induced Binding. Under the sponsorship of selected utilities from the BWR Owners' Group, Kalsi Engineering developed a validated methodology to accurately predict gate valve unwedging thrust performance under traditional pressure locking and even under pressure-induced binding conditions as reported in INPO OE 10318 dated October 13, 1999.

KEI's methodology eliminates potentially large uncertainties associated with other industry methodologies and is particularly valuable for predicting unwedging thrust requirements for AOV gate valves that typically have small margins.

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 24

" Thermal Binding Methodology. Under the sponsorship of EPRI, Kalsi Engineering has developed a comprehensive, first-principles model for thermal binding of gate valves.

Under Phase I, the first principles model was released in March 1998 as EPRI Report No.

GC- 110301. Phase II is in progress to validate the methodology by flow loop testing under a variety of thermal binding scenarios.

" Development of EPRI Check Valve Application Guidelines (EPRI NP-5479). Kalsi Engineering was contracted by NSSS Joint Owners' Group and EPRI to develop a comprehensive guide for the application and use of check valves in the industry. This guide was the first such publication to fully address problems/failures related to check valves. It also included guidance regarding how to systematically review and improve the design, application, installation, inspection, testing, and maintenance practices to prevent check valve failures. A large matrix of tests was performed to quantify the effect of variations in design, upstream flow disturbances, and flow conditions on the check valve performance and life. The guide was revised to include results from extensive wear and fatigue tests performed at Kalsi Engineering's flow loop and application experience gained at more than 20 plants.

  • Condition Monitoring/Preventive Maintenance Based on Check Valve Analyses and Prioritization (CVAP) Program. We have developed the Check Valve Analysis and Prioritization (CVAP) program, which is based upon extensive data from the EPRI Check Valve Guidelines developed by Kalsi Engineering; our root cause analyses from many failures; and our continuing, systematic wear and fatigue testing on check valves at our flow test facility. CVAP allows us to perform a thorough, efficient, and very cost-effective analysis of various types of valves and provide quantitative information regarding relative degradation trends. This methodology has proven to be very useful in prioritizing valves from the standpoint of their adverse effect on safety and reliability as well as in developing a condition monitoring-based preventive maintenance program with suitable maintenance/

inspection intervals for each valve. This methodology referred to by INPO as a "model for the industry" has been used to analyze over 3,000 check valves at more than 20 US nuclear power plants. It is a valuable resource for fulfilling the requirements for condition monitoring (ASME OMa Code 1996, ISTC 4.5.5, and Appendix II).

  • Improved Gate Valve Design. Kalsi Engineering developed an improved gate valve product line for GE Nuclear Energy for critical service applications in nuclear power plants. The new designs have been proven to repeatedly withstand severe blowdown conditions without any degradation of performance. Several patents were awarded for proprietary features of this design. The valves have been installed at several U.S. and foreign utilities, including Boston Edison/Pilgrim Nuclear Power Station, which was the lead utility that cooperated with KEI and GE in the development, testing, and installation of the improved gate valve.

The new designs have accumulated a history of excellent performance for more than six years and have been implemented at several US and international plants.

  • Teaming Arrangements to Provide Best Expertise to the Client. Kalsi Engineering has an established relationship with other internationally recognized organizations and, when required, can team up to provide the optimum combination of talent to meet a client's technical goals and schedule requirements efficiently.

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 25

  • Special Valve Test Facilitiesand Flow Loops. Kalsi Engineering has a variety of unique test fixtures and flow loops to perform special tests on valves and actuators. A gate valve design effects test fixture capable of faithfully simulating -the performance of gate valves under specified AP and flow conditions was developed to cost-effectively support the development of EPRI models. This fixture is available for characterizing the performance of gate valve discs, seats, and guides, and is particularly suited for qualifying non-testable gate valves. Additionally, a number of actuator thrust, torque, and cyclic fatigue test fixtures are available to determine the performance characteristics and life of actuator components. A water flow loop capable of pressures up to 300 psi and flow rates up to 3,000 gpm is available at KEI test facilities. Kalsi Engineering has access to two additional flow loops in close proximity that permit flow testing with water up to 2,000 psi and 450 gpm and with steam up to 650'F.
  • Development of Innovations Related to Valves and Seals. Over 35 patents have been granted to Kalsi Engineering personnel, most of which are related to valves and seals.

Several of these patents are assigned to valve manufacturers and are in commercial use.

Patents relating to seals are in commercial use in harsh, abrasive fluid media, high differential pressure rotary seal applications.

" Expert Witness Experience in Legal Testimony. Kalsi Engineering has provided expert witness support and testimony for legal issues related to valves, seals, rotating equipment, and other mechanical equipment. Based on our strong background, experience, and insight in valves and actuators, we have established an impeccable record of supporting our clients and bringing each lawsuit to a favorable conclusion to date. This has covered a wide range of valve and actuator designs made by different manufacturers and used in different industries, including petrochemical and manufacturing plants.

" Intimate Familiaritywith Design of Valves. Kalsi Engineering has in-depth experience in the detail design, typical tolerances, materials, manufacturing, and development of complete product lines of gate, globe, butterfly, ball, check, and safety relief valves. These product lines have included:

- Motor operated gate valves for nuclear service

- Main steam and feedwater isolation gate valves for nuclear service

- Motor- or air-operated globe valves

- End-entry ball valves, both trunnion mounted and floating ball designs

- Rectangular body gate valves of fabricated design for high temperature cyclic service in petrochemical plant applications

- Trunnion mounted top entry ball valves for high pressure (5,000 psi) gathering manifolds in oil and gas production

- High performance fire-safe butterfly valves for power generation and industrial applications

- High-pressure gate valves for 30,000 psi sour gas critical service in oil field wellhead applications

- Geothermal gate valves for 600'F steam service Revision Date.-December 17, 2007

KVAP, The AOV/MOV Software with Technology 26

- Catalytic cracker slide valves used in petrochemical plants for temperatures up to 1,1 00°F

- Quarter-turn tapered plug valves capable of withstanding pressure transients without taper-locking problems typically encountered with conventional plug valves under water hammer conditions.

Extensive Design, Analysis, and Testing Experience. In supporting the development of various valve product lines, Kalsi Engineering personnel have utilized systematic design, advanced analyses, and testing approaches for many years. Some of the more important accomplishments are described below:

- Detailed stress and deflection analysis of the major components of many types and sizes of valves under pressure, external pipe loads, thermal transients, seismic, and pipe rupture loads. Finite element analysis techniques were widely employed to gain a thorough under-standing of valve distortions and stresses under combined loads and to quantify their effect on operability.

- Instrumented bending moment tests on several types of gate, globe, and ball valves.

Internal seat distortions and changes in clearances were measured to quantify and provide adequate design clearances and operating thrust margins under worst combination of loads.

- Sliding friction tests between several seat/gate material combinations to determine coefficient of friction threshold of galling stress and wear rates, which cause degradation of the seating faces. These tests were conducted on standard friction test machines using standard specimens as well as by sliding prototypical valve components.

- Flow Tests for various shapes and sizes of valves to develop and refine flow resistance and scaling methods, and quantify torque coefficients, and upstream flow disturbance effects.

- Performanceprediction of butterfly valves: Developed analytical methods to account for the effect of piping installations, upstream and downstream resistance, and flow conditions including pump flow, pipe rupture, and parallel branches on butterfly valve performance.

- Development offlexible metal-to-metal seats and wedge discs to accommodate anticipated seat distortions and displacements under pressure and thermal transients without significantly increasing operating thrusts and degrading the shut-off characteristics.

- Seismic qualification of several actuators and valve product lines using combined finite element dynamic analysis and testing techniques.

- Strain gage instrumented tests to determine impact stresses during fast-closing operation of MSIVs and FWIVs.

- Operating thrust measurements by instrumented cycle testing on gate valves using nitrogen (up to 1,000°F), water, and steam (up to 600'F) under various differential pressures.

- Water slug impact tests on control valve plugs; design improvements to make them resistant to impact stresses caused by slug-type water hammer.

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 27

- Cavitation, noise, and flashing tests on high pressure drop control valves. Developed noise prediction methods for control valves in both incompressible and compressible fluid service. Developed a low noise, high pressure drop trim design.

- Stability analysis of air-operated control valves; developed techniques to predict and avoid instabilities caused by negative stem force gradients encountered in high AP applications. A hydraulic force test simulator was developed to faithfully duplicate many complex stem force curves observed in actual plant conditions on different types of control valves/actuator assemblies.

- Check valve wear andfatigue research. We continue to be involved in and at the forefront of the development and refinement of methodology to predict degradation of check valve internals. An extensive matrix of long-term wear and fatigue tests was performed to refine the predictive models for hinge pin wear and disc stud fatigue.

- Cyclic overloadqualification of Limitorque actuators has been done by applying fracture mechanics and fatigue analysis techniques and by testing with specially instrumented test fixtures capable of simulating different valve stiffnesses.

Revision Date: December 17, 2007

KVAP, The AOV/MOV Software with Technology 28 Key Personnel Kalsi Engineering, Inc. has a staff of over 20 personnel. Qualifications of our key personnel are summarized below.

Dr. M. S. Kalsi holds a B.S., M.S., and Ph.D. degrees in mechanical engineering. He is the president of Kalsi Engineering Inc. and has 30 years of experience in valve design, analysis, and testing. Prior to starting Kalsi Engineering, he was manager of research and development at a major U.S.

valve manufacturing company. He has been awarded 25 patents, eight of which pertain to valve design improvements, and has published more than 60 technical papers related to valves. He has provided management and technical guidance to his staff in implementing valve programs and performing design basis reviews for MOVs, AOVs, and check valves at 25 nuclear power plants. He has served as a project manager as well as a principal investigator in many large scale, industry-wide valve programs for EPRI (including EPRI's MOV PPP), nuclear power utilities, NSSS Owners Groups, and Small Business Innovation Research Phase I and II projects awarded to Kalsi Engineering, Inc. by NRC, DOD, DOE, and NASA.

Dr. Kalsi has worked with more than 40 nuclear power plants as well as all major valve manufacturers in resolving valve issues for gate, check, safety relief, plug, control, butterfly, and ball valves. Dr. Kalsi has worked extensively in all aspects of valves: detail design, prototype fabrication, testing, research and development, structural and operability analysis, valve instability analysis, fluid-induced vibration, tribology and quantitative wear prediction, response of valve disc or plug to pressure transients, water hammer analysis, flow characteristics and pressure drop across valves, life cycle testing to determine performance degradation, establishing surveillance testing requirements to ensure operability, and root cause analysis of failures. With an equally strong background in analysis, testing, and project management, Dr. Kalsi has the expertise to plan and develop the best technical approach to meet the project objectives at a minimum cost.

Mr. P. D. Alvarez holds a Bachelor Degree in Mechanical Technology. He is a vice president and principal consultant at Kalsi Engineering, and has over 31 years of experience in performing valve calculations, design basis reviews, operability evaluations, and providing recommendations to solve valve problems. Prior to joining Kalsi Engineering, he worked at a major valve manufacturing company. He has performed extensive work in the design, analysis, and testing, of valves of all types. He currently holds six patents, five pertaining to valve improvements.

He was the project leader responsible for developing a very sophisticated Gate Valve Design Effects Test Fixture under the EPRI MOV Performance Prediction Program. Mr. Alvarez conducted an extensive matrix of tests to evaluate the effect of variations in design features present in different manufacturer's valves on the performance under a range of LP and flow conditions. He was the lead engineer in the Limitorque Actuator Thrust Rating Increase study Revision Date.-December 17, 2007

KVAP, The AOV/MO V Software with Technology 29 performed by Kalsi Engineering for a consortium of nuclear utilities. He was also a principal contributor to the development of the GE Improved Gate Valve. He was responsible for overall project coordination of the Kalsi Valve Analysis Program (KVAP) and development of validated models for POV quarter-turn valves at Kalsi Engineering.

Mr. Alvarez was a principal contributor to the preparation of Application Guidelinesfor Valves in Nuclear Power Plants that was published in 1990 and updated in 1998 under EPRI sponsorship.

He has worked on several projects relating to MOV actuator sizing and thrust requirements over a range of operating conditions for ten major utilities; analyzed operability problems in different types of valves in power plants, pipelines, petrochemical, and oil field applications; and developed modifications to overcome operability problems. He has performed stress analyses to determine maximum stresses at critical areas of the drive train from the actuator to the final inner valve element and identified problem areas to allow the correct settings for limit switches. He has designed several test fixtures and performed instrumented tests on valves under conditions simulating various combinations of piping loads, flows, pressures, and temperatures. Mr. Alvarez was project leader in performing MOV design basis reviews related to torque/thrust requirements, determination, and improvements. He was the principal investigator for the EPRI MOV Margin Improvement Guide and Gate Valve Design Effects Testing.

Dr. Bahir Eldiwany holds a B.S., M.S., and Ph.D. degrees in mechanical engineering. He is a senior consultant with 20 years of experience with Kalsi Engineering in mechanical equipment design and analysis, including MOVs, AOVs, and check valves. His analysis experience includes first principles model development, design basis reviews, and recommending solutions for valve problems. He has performed analyses to determine operating thrust/torque requirements and stresses in various types of gate valves, butterfly valves, and globe valves and has developed many in-house and commercial software packages to perform valve calculations. Dr. Eldiwany has performed root cause investigations of valve failures and has been instrumental in proposing design modifications and solutions for MOV, AOV, and check valve problems. Dr. Eldiwany was the principal investigator in developing the Butterfly Valve Model and the W-K-M Parallel Expanding Gate Valve Model of the EPRI MOV PPM. He also developed the Butterfly MOV Guide for EPRI/NMAC. Recently he was the lead engineer for developing the quarter-turn butterfly, ball, and plug valve models for the Kalsi Valve and Actuator analysis Program (KVAP) to more accurately predict torque requirements.

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 30 Dr. J. K. Wang holds B.S., M.S. and Ph.D. degrees in mechanical engineering.

He has been a vice president and principal consultant at Kalsi Engineering for 25 years, and has 28 years of experience in performing valve calculations, model development, component level design basis reviews, operability evaluations, and providing recommendations to solve valve problems for more than 35 nuclear power plants. Prior to joining Kalsi Engineering, he worked at a major valve manufacturing company. His background includes detailed analysis, design, and testing of valve body structures and internal components such as seats, gates, stems, and packing to accommodate external piping loads, pressures, and temperatures to ensure valve operability and structural integrity. Dr. Wang was the principal investigator in developing the Flexible and Solid Gate Valve Model and Westinghouse Gate Valve Model of the EPRI MOV Performance Prediction Program. He was also the principal investigator for the development of Kalsi Engineering's Generalized Pressure Locking Methodology and EPRI's Gate Valve Thermal Binding Methodology. He was the lead engineer for developing the first principles model for gate valves, globe valves, diaphragm valves, and all linear and quarter-turn actuators used in the Kalsi Valve and Actuator Program (KVAP) software.

Mr. Neal Estep holds a B.S. and M.S. in mechanical engineering and is a licensed PE. He is a Senior Specialist and Project Manager with over 25 years of mechanical equipment experience. He served as the corporate lead for implementation of the GL 89-10 MOV program at Duke Power (Oconee, McGuire and Catawba). In this position he participated in the development of M

T MOV diagnostic test equipment (MOVATS and Liberty VOTESTM systems), and developed program documents and engineering standards for actuator maintenance, testing, data review and performing design basis sizing calculations. In addition, he performed and reviewed design basis sizing calculations, performed in-situ and flow loop testing of valves using diagnostic test equipment, and analyzed and interpreted test data. He was also involved in developing the KEI actuator torque test stands for Duke Power.

Mr. Estep also served as the co-chairman for the EPRI MOV Performance Prediction Program, with specific focus on the flow loop testing portion of the program. He also served on the ASME O&M committee for MOVs, was active in the MOV User's Group and served on the NEI committee to address industry resolution of NRC MOV concerns.

His background also includes resolution of valve problems at fossil and hydro power plants, and he served as rotating equipment engineer at Catawba Nuclear Station, engineering supervisor at Catawba Nuclear Station over the valve area, and held project management and equipment support positions at a refinery and chemical plant.

Revision Date: December 17, 2007

KVAP, The AOV/MOV Software with Technology 31 Mr. Steven Averitt holds a B.S. degree in mechanical engineering. He is a consulting engineer \ with more than nine years of experience in analysis, modeling, and capability evaluations of MOVs, AOVs, and check valves. Mr.

Averitt has supported project leaders by reducing data obtained from analysis and testing, and by evaluating MOVs in safety and non-safety nuclear power plant applications using in-situ test data. He has been responsible for developing a user-friendly input interface for the Kalsi Engineering model used to analyze gate valves in support of NRC GL89-10 programs. He was responsible for the development of valve body and disc stiffness models used in the enhanced pressure locking and thermal binding methodologies developed by Kalsi Engineering. He is the software lead engineer for the development, maintenance and enhancements of Kalsi Engineering's KVAP software.

Mr. Ryan Sicking holds a B.S. degree in mechanical engineering. He is a consulting engineer with nine years of experience in analysis, design, testing, and capability evaluations of MOVs, AOVs, and check valves. Mr. Sicking has been a project leader on numerous high-volume AOV, MOV, and check valve evaluations, and is knowledgeable and fluent in the use of Kalsi Engineering software such as KVAP, CVAP, LiFE, and KEI's pressure locking and thermal binding software. He has also assisted in developing the user-friendly input interfaces for many of the Kalsi Engineering software models. Mr. Sicking is the principal engineer responsible for actuator test stands used in performing quality control testing at nuclear power plants and at Limitorque Corporation. He has also supported several cases in expert witness litigation related to valve incidents Mr. Zachary Leutwyler holds a B.S. and M.S. in mechanical engineering. He has special expertise in Computational Fluid Dynamics (CFD). and Thermal-Fluid Sciences. His graduate work includes a computational study of the compressible flow field and the flow-induced resultant force and torque on various butterfly disc geometries using two- and three-dimensional computational models. His graduate course work emphasized studies in computational, thermal, and fluid sciences. His thermal science background includes conduction, convection, and radiation heat transfer. His background in fluid mechanics includes gas dynamics (theoretical and computational), boundary-layer theory, turbulent flow, potential flow, viscous flow, and fundamental fluid mechanics.

Mr. Leutwyler has been a part the Kalsi Engineering research and development team for several years (both working directly and in partnership with the University of Houston). He has had a significant role in the KEI AOV quarter-turn valve test program (including incompressible and compressible fluid media), computational modeling and methodology development and application. Mr. Leutwyler also has had an active role in developing the Kalsi Valve and Actuator Analysis Program (KVAP) software. Prior to joining Kalsi Engineering, Mr. Leutwyler worked for a major valve manufacture and has a fundamental understanding of valve and actuator assembly, positioner calibration and seat-leak, hydrostatic, and valve diagnostic testing. His valve experience also includes pneumatic, I/P, and digital positioners.

Revision Date: December 17, 2007

KVAP, The AOV/MO V Software with Technology 32 Mr. Aaron Richie holds a B.S: degree in mechanical engineering. He is a consulting engineer \ with more than five years of experience in analysis, modeling, and capability evaluations of MOVs, AOVs, and check valves. Mr.

Richie was the test engineer for the KEI AOV/MOV compressible flow testing program. He has performed numerous flow loop tests on a variety of check valves. He supports Steven Averitt in the development, maintenance and enhancement of the Kalsi Valve and Actuator Program (KVAP) software.

Revision Date: December 17, 2007

KVAP, The A 0 V/MO V Software with Technology 33 KVAP References and Other Significant Documents Developed by Kalsi Engineering, Inc.

The following is a list of references supporting the development of KVAP, EPRI MOV Performance Prediction Program models and EPRI/NMAC Guides developed by Kalsi Engineering, and other related references.

KVAP Software Development, Verification and Validation

1. KEI Document No. 2092C, KVAP Software Version 1.2." Software Quality Assurance Plan.
2. KEI Document No. 2093C, KVAP Software. Software Requirements Specification.
3. KEI Document No. 2094C, KVAP Software. Software Design Specification
4. KEI Document No. 2094C, Attachment 1: KVAP Software Version 2.0.: Software Design Specification - User Interface Module.
5. KEI Document No. 2094C, Attachment 2: KVAP Software. Software Design Specification - System Flow Module.
6. KEI Document No. 2094C, Attachment 3: KVAP Software: Software Design Specification - Air- OperatedActuator Module.
7. KEI Document No. 2094C, Attachment 4: KVAP Software: Software Design Specification - Gate Valve, Module.
8. KEI Document No. 2094C, Attachment 5: KVAP Software: Software Design Specification - Globe Valve Module.
9. KEI Document No. 2094C, Attachment 6: KVAP Software. Software Design Specification - Diaphragm Valve Module.
10. KEI Document No. 2094C, Attachment 7: KVAP Software: Software Design Specification - Butterfly Valve Module.

1]. KEI Document No. 2094C, Attachment 8: KVAP Software: Software Design Specification - Ball/Plug Valve Module.

12. KEI Document No. 2094C, Attachment 9: KVAP Software: Software Design Specification - KVAP Global Module.
13. KEI Document No. 2094C, Attachment 10: KVAP Software: Software Design Specification - Margin Module.
14. KEI Document No. 2094C, Attachment 11: KVAP Software Version 2.0." Software Design Specification - Default Flow and Torque Coefficients Module for Butterfly.
15. KEI Document No. 2094C, Attachment 12: KVAP Software Version 2.0.: Software Design Specification- Motor Operator.
16. KEI Document No. 2095C: KVAP Software Version 2.0. Program Code Listing:
17. KEI Document No. 2096C: KVAP Software Version 2.0." Verfication and Validation Plan.

Revision Date: December 17, 2007

KVAP, The AO V/MO V Software with Technology 34

18. KEI Document No. 2097C: KVAP Software Version 1.2.: V& V Report: Attachments 1 through 11.

KVAP Models & Methodologies

19. KEI Document No. 2098C, Attachment 1: KVAP Software: Model DescriptionReport -

User Interface Module.

20. KEI Document No. 2098C, Attachment 2: KVAP Software: Model Description Report -

System Flow Module.

21. KEI Document No. 2098C, Attachment 3: KVAP Software. Model DescriptionReport -

Air-OperatedActuator Module.

22. KEI Document No. 2098C, Attachment 4: KVAP Software. Model DescriptionReport -

Gate Valve Module.

23. KEI Document No. 2098C, Attachment 5: KVAP Software: Model DescriptionReport -

Globe Valve Module.

24. KEI Document No. 2098C, Attachment 6: KVAP Software: Model DescriptionReport -

Diaphragm Valve Module.

25. KEI Document No. 2098C, Attachment 7: KVAP Software: Model DescriptionReport -

Butterfly Valve Module

26. KEI Document No. 2098C, Attachment 8: KVAP Software: Model DescriptionReport -

Ball/Plug Valve Module.

27. KEI Document No. 2098C, Attachment 10: KVAP Software Version 2.0: Model DescriptionReport: Margin Module.
28. KEI Document No. 2098C, Attachment 11: Model Description Report: Default Coefficient Module - Butterfly Valves.
29. KEI Document No. 2098C, Attachment 12: Model DescriptionReport: Motor Operator Module.
30. KEI Document No. 2111 C, CFD Modeling Methodology Validationfor Quarter-Turn Valves.
31. KEI Document No. 2122C, Verification and Validation Planfor ANSYS/FLOTRAN 5-5 CFD Elements.
32. KEI Document No. 2121C, Verification and Validation Report for ANSYS/ FLOTRAN 5-5 CFD Elements.

KVAP Flow Loop Test Program

33. KEI Document No. 2101C, Procedurefor Kalsi AOV/MOV Validation Testing.
34. KEI Document No. 2118C, Kalsi AOV/MOV Model Validation Test Data Report.
35. KEI Document No. 2119C, Kalsi AOV/MO V Test Data.
36. KEI Document No. 2119C, Attachment 1: Spherical Ball Valve (Assembly 1).
37. KEI Document No. 2119C, Attachment 2: Segmented Ball Valve (Assembly 2).
38. KEI Document No. 2119C, Attachment 3: Double Offset Butterfly Valve (Assembly 3).
39. KEI Document No. 2119C, Attachment 4: Kalsi Test Fixture (Assembly 4) Symmetric Disc 0.15 Aspect Ratio.

Revision Date: December 17, 2007

KVAP, The A 0 V/MO V Software with Technology 35

40. KEI Document No. 2119C, Attachment 5: Kalsi Test Fixture (Assembly 5)

Nonsymmetric Disc 0.15 Aspect Ratio.

41. KEI Document No. 2119C, Attachment 6: Kalsi Test Fixture (Assembly 6)

Nonsymmetric Disc 0.25 Aspect Ratio.

42. KEI Document No. 2119C, Attachment 7: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 7). Double Offset: 0.090" Lateral (Stem), 40% axial (Seat).
43. KEI Document No. 2119C, Attachment 8: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 8). Double Offset: 0.090" Lateral (Stem), 60% axial (Seat).
44. KEI Document No. 2119C, Attachment 9: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 9). Double Offset: 0.045" Lateral (Stem), 40% axial (Seat).
45. KEI Document No. 2119C, Attachment 10: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.25 Aspect Ratio (Assembly 10). Double Offset: 0.045" Lateral (Stem), 60% axial (Seat).
46. KEI Document No. 2119C, Attachment 11: Spherical Q-Ball Valve with QOM Insert (Assembly 12).
47. KEI Document No. 2119C, Attachment 12: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.24 Aspect Ratio (Assembly 13). Triple Offset: 0.364" Lateral, 59% axial, 16-deg cone.
48. KEI Document No. 2119C, Attachment 13: Kalsi Butterfly Valve Test Fixture Nonsymmetric Disc 0.30 Aspect Ratio (Assembly 14). Triple Offset: 0.632" Lateral (Stem), 67% axial (Seat).
49. KEI Document No. 2205C, Procedurefor Kalsi AOV/MOV Model Validation Testing, July 2000.
50. KEI Document No. 2120C, Kalsi AOV/MOV Model Validation Testing- Lab Notebooks, Volumes 1-14.
51. KEI Document No. 2221C, Kalsi AOV/MOV Model Validation Testing- Lab Notebooks, Volumes 1-11.
52. KEI Document No. 2222C, Kalsi AOV/MO V CompressibleFlow Testing Report.
53. KEI Document No. 2222C, Attachment 1: Ball Valve: Full Ball, Trunnion Mounted 6" Valve (Assembly 1).
54. KEI Document No. 2222C, Attachment 2: Jamesbury 6" Butterfly Valve Double Disc (Assembly 3).
55. KEI Document No. 2222C, Attachment 3: Kalsi Butterfly Valve Test Fixture with Single Offset Disc 0.15 Aspect Ratio (Assembly 5).
56. KEI Document No. 2222C, Attachment 4: Kalsi Butterfly Valve Test Fixture with Single Offset Disc 0.25 Aspect Ratio (Assembly 6).
57. KEI Document No.. 2222C, Attachment 5: Kalsi Butterfly Valve Double Offset Disc with 0.25 Aspect Ratio (Assembly 8).

Revision Date: December 17, 2007

KVAP, The AO V/MO V Software with Technology 36

58. KEI Document No. 2222C, Attachment 6: Jamesbury 6" Valve Double Offset with Steamline Disc (Assembly 11).
59. KEI Document No. 2222C, Attachment 7: 6" Model of a 48" Henry Pratt Butterfly Valve (Assembly 16).
60. KEI Document No. 2222C, Attachment 8: 6" Scale Model of an 18" Jamesbury Butterfly Valve (Assembly 18).
61. KEI Document No. 2222C, Attachment 9: Kalsi Butterfly Valve Test Fixture Symmetric Disc with 0.25 Aspect Ratio (Assembly 19).
62. M. S. Kalsi, B. H. Eldiwany, V. Sharma, D. Somogyi. "Dynamic Torque Models for Quarter-Tum Air-Operated Valves," Proceedings of the Sixth NRC/ASME Symposium on Valve & Pump Testing, NUREG/CP-0152, Vol. 3, July 2000.
63. M. S. Kalsi, Bahir Eldiwany, Vinod Sharma, Ryan Sicking, "Flow Loop Testing to Validate Improved Models for Single, Double & Triple Offset Disk Butterfly Valves,"

Abstract for EPRI/NMAC Eighth Valve Technology Symposium, August 2001.

64. J. K. Wang, Desi Somogyi, P. Daniel Alvarez, M. S. Kalsi, John Hosler (EPRI), "Flow Loop Testing and Validation of Thermal Binding Model for Wedge Gate Valves,"

Proceedings of the EPRI/NMAC Eighth Valve Technology Symposium, August 2001.

65. M. S. Kalsi, B. E. Eldiwany, V. Sharma, "Butterfly Valve Model Improvements Based on Compressible Flow Testing Benefit Industry AOV Programs, Proceedings of the Seventh NRC/ASME Symposium on Valve and Pump Testing, July 2002.
66. M. S. Kalsi, B. E. Eldiwany, V. Sharma, "Butterfly Valve Model Improvements Based on Compressible Flow Testing Benefit Industry AOV Programs, Proceedings of the Seventh NRC/ASME Symposium on Valve and Pump Testing, July 2002.
67. M. S. Kalsi, B. Eldiwany, "Plant Experience Based Upon Application of New Validated Models for Air-Operated Valves, Proceedings of the 9th EPRI Valve Technology Symposium, August 2003.
68. M. S. Kalsi, B. Eldiwany, Vinod Sharma, Aaron Richie, "Effect of Butterfly Valve Disc Shape Variations on Torque Requirements for Power Plant Applications, Proceedings of the Eighth NRC/ASME Symposium on Valve and Pump Testing, July 2004.
69. KEI Document No. 2099C, KVAP User's Manual.

EPRI MOV Performance Prediction Program &

EPRI/NMAC Guides developed by Kalsi Engineering, Inc.

70. EPRI MOV Performance Prediction Program: Guide for the Application and Use of Valves in Power Plant Systems, Electric Power Research Institute, EPRI NP-6516, Rev.

0.

71. EPRI MOV Performance Prediction Program: Guide for the Application, Use, and Maintenance of Valves in Power Plants, Electric Power Research Institute, EPRI TR-105852-V1.
72. EPRI MOV Performance Prediction Program: Butterfly Valve Model Description Report, Electric Power Research Institute, EPRI TR- 103224.
73. EPRI MOV Performance Prediction Program: Butterfly Valve Design, Elbow, and Scaling Effects Test Report, Electric Power Research Institute, EPRI TR-1 03257.

Revision Date.-December 17, 2007

KVAP, The A 0 V/MO V Software with Technology 37

74. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Butterfly Valves in Nuclear Power Plants, Electric Power Research Institute, EPRI NP-7501.
75. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Butterfly Valves in Nuclear Power Plants, Rev. 1, Electric Power Research Institute, EPRI TR-106563 V2.
76. EPRI MOV Performance Prediction Program: Application Guide for Motor-Operated Gate and Globe Valves in Nuclear Power Plants, Rev. 1, Electric Power Research Institute, EPRI TR-106563 VI.
77. EPRI MOV Performance Prediction Program: Gate Valve Model Report, Electric Power Research Institute, EPRI TR-103229.
78. EPRI MOV Performance Prediction Program: Gate Valve Design Effects Testing Results, Electric Power Research Institute, EPRI TR-103255.
79. EPRI MOV Performance Prediction Program: Gate Valve Thermal Binding Methodology, Electric Power Research Institute, EPRI GC- 110301.
80. EPRI MOV Performance Prediction Program: Stem Thrust Prediction Method for Westinghouse Flexible Wedge Gate Valves, Electric Power Research Institute, EPRI TR-103233.
81. EPRI MOV Performance Prediction Program: Stem Thrust Prediction Method for W-K-M Parallel Expanding Gate Valves, Electric Power Research Institute, EPRI TR-103236.
82. EPRI MOV Performance Prediction Program: Motor-Operated Valve Margin Improvement Guide, Electric Power Research Institute, EPRI TR-100449.
83. EPRI MOV Performance Prediction Program: Application Guide for Check Valves in Nuclear Power Plants, Electric Power Research Institute, EPRI NP-5479, Rev. 0 and Rev. 1.

Revision Date.: December 17, 2007

KVAP, The AOV/MO V Software with Technology 38 KVAP Development/Enhancement KVAP is actively being developed and technically enhanced to ensure that the software is up-to-date and is responsive to emergent industry issues. The following summary illustrates the upgrades performed on KVAP since its release in November 2000. The software has since been revised to incorporate new features, address error reports, and fix non-technical format problems.

Subscribers to the software annual maintenance receive free upgrades and electronic database migration services.

KVAP 1.0 Released November 2000 Initial Modules Globe Butterfly Gate Air operators Margin Flow Default butterfly coefficients User interface KVAP 1.1 Released March 2001 Corrected problems identified in Error Reports:

2000-1 through 2000-22, except 2000-18 Revised code to address 12 formatting/enhancement type non-technical issues KVAP 1.2 Released February 2002 New features:

Ball and plug valves module Default incompressible flow coefficients for full spherical ball and segmented ball Rotary diaphragm with linkage Reverse acting piston actuator "Other" actuator for defining out of scope actuators Correct problem identified in Error Report 2000-18, and 2001-1 Added saturation temperature information calculation for steam and water Added safe spring load data field Revised code to address 19 formatting/enhancement type non-technical issues KVAP 1.3 Released January 2003 Correct problem identified in Error Reports 2002-2, 2002-4, 2002-6, 2002-7, Revised code to address 42 formatting/enhancement type non-technical issues KVAP 2.0 Released May 2004 Significantly upgraded KVAP capabilities to analyze quarter-turn valves in compressible flow application including at low-pressure coefficients for butterfly valves. This effort was supported Revision Date.: December 17, 2007

KVAP, The AOV/MO V Software with Technology 39 by an additional 1100 compressible flow tests on 9 different valve designs tested in 84 configurations. (KVAP 1.3 models were based on over 1250 incompressible flow tests on 15 valves designs in 71 configurations). New features included:

Additional incompressible flow torque coefficients for cylindrical and tapered plug valves and Camflex valves Default compressible flow coefficients for ball, plug, and eccentric plug valves Butterfly valve compressible flow coefficient for very low pressures and vacuum Optional bounding torque coefficients for butterfly valves Added Reverse acting pilot balanced valve Added Three way converging globe, valve "User" valve to permit manually defining thrust/torque valve requirements Torque predictions for 1/4 turn valves under incompressible blowdown conditions Ability to analyze valve and actuator, valve only, or actuator only Ability to change actuator type after beginning analysis Ability to define piston actuator using area or diameters Customization of AOV categories Component thrust/torque rating input Ability to selectively calculate and plot margin calculations New input screen for defining margin calculation options Added valve thrust plot capability to all linear valves New optional MOV actuator sizing module for Limitorque and Rotork actuators Numerous new illustrations Expanded numerous help menu definitions Corrected problem identified in Error Reports 2001-1, 2002-1, 2002-2, 2003-1 through 2003-7rl, and K2004-1 Redesigned input screens for added flexibility and user-friendliness Redesigned reports for added flexibility and user-friendliness Redesigned report header wizard Query feature for sorting the database KVAP 2.1 Released August 2004 Corrected problem identified in Error Report 2004-2 Revision Date.-December 17, 2007

KVAP, The AOV/MOV Software with Technology 40 KVAP 2.2 Released October 2005 Add AOV setup parameter window and set-up datasheet Provide user with options for addressing uncertainties Add open and close stroke in same analysis Provide alternate "valve factor" input for gate valves in addition to coefficient of friction Refined pilot globe valve seating-thrust calculations Enhanced effective diaphragm area model Refined Sigma-F methodology Improved application of benchset parameters Included additional combinations of actuator and linkage types KVAP 3.0 to be released in 2008 JOG MOV PV predictions SQL server database Force equations in reports Packing friction force calculator Parallel slide gate valve model Butterfly valve disc weight equations Data import & export features SI units MOV setup window to account for margin and uncertainty values Autotork and AUMA actuator capability tables Spring characteristics for bellows sealed valves Nested spring equations for air operators Potential Enhancements for Future Revisions PPM equivalent predictions Westinghouse valve model Split wedge gate valve model Anchor-Darling double disc gate valve model Revision Date: December 17, 2007

KVAP, The AO V/MO V Software with Technology 41 Comprehensive KVAP Training Seminar Outline

1. Thrust Requirements for Globe Valves

" Required Stem Thrust for Globe valves

" Model Applicability and Limitations

" Approach

  • Assumptions
  • Criteria for Determining whether a Globe Valve is Seat Based or Guide Based
2. Evaluation of Air Operators

" Scope

" Model Description

" Assumptions

" Rising Stem Actuators

- Double-Acting Air Cylinder, Single Ended

- Double-Acting Air Cylinder, Double Ended

- Double-Acting Air Cylinder, Direct Acting (Spring to Retract)

- Double-Acting Air Cylinder, Reverse Acting (Spring to Extend)

- Direct-Acting Diaphragm (Spring to Retract)

- Reverse-Acting Diaphragm (Spring to Extend)

- Direct-Acting Diaphragm with Mechanical Advantage

- Reverse-Acting Diaphragm with Mechanical Advantage

" Quarter-Tum Stem Actuators

- Scotch Yoke, Double-Acting Air Cylinder

- Scotch Yoke, Single-Acting Air Cylinder with Spring to Retract

- Rotary Diaphragm Actuator

- Rack and Pinion, Double-Acting Air Cylinder

- Rack and Pinion, Single-Acting Air Cylinder with Spring Return

- Double-Acting Air Cylinder with Linkage

- Single-Acting Air Cylinder with Spring Return and Linkage

3. Torque Requirements for Butterfly Valves: KVAP-Improved Models

" Torque Requirements for Butterfly Valves

- References

- Butterfly Valve Design

- KVAP Butterfly Valve Model

  • Model Applicability and Limitations

" Assumptions

" Effect of Flow Disturbances on Hydrodynamic Torque (Upstream Elbow Model)

" KVAP Butterfly Model Validation Revision Date.: December 17, 2007

KVAP, The AOV/MOV Software with Technology 42

4. Torque Requirements for Ball/Plug Valves KVAP Improved Models

- Ball/Plug Valve Model

- Assumptions

- Required Actuation Torque

5. Thrust Requirements for Solid and Flexible Wedge Gate Valves

" Scope

" Model Applicability and Limitations

" Assumptions

" Application of Thrust Equations for Steam Flow Conditions

" Opening Stroke Equations

" Closing Stroke Equations

" Force Component Calculations

" Bounding Friction Coefficients

" Obtaining Disc-to-Seat Friction Coefficient through In-Situ Testing

" Relationship between Valve Factor and Coefficient of Friction for Gate Valves

- Exact Relationship between the Valve Factor and the Disc-to-Seat Coefficient of Friction

6. Thrust Requirements for Diaphragm Valves

" Required Stem Thrust

  • Definitions and Units

" Assumptions

" Opening Stroke Equations

" Closing Stroke Equations

" Force Component Calculations

7. Case Studies - Plant Examples Provided by Students OPTIONAL TOPICS
8. Overview of AOV Problems, Testing Control, & Accessories

" Major Causes of AOV Failure

" Corrective Actions

" Overview of AOV Diagnostic Devices

  • Bench Set Point Control
  • Functions of AOV Accessories
9. Margins

" Margin Definitions

" Uncertainties

" Degradation

" Margin Improvement Revision Date: December 17, 2007