ML051050526
| ML051050526 | |
| Person / Time | |
|---|---|
| Site: | Callaway  |
| Issue date: | 02/24/2005 |
| From: | Keith Young AmerenUE, Union Electric Co |
| To: | Document Control Desk, Office of Nuclear Reactor Regulation |
| References | |
| IN-05-001, ULNRC050121 | |
| Download: ML051050526 (42) | |
Text
AmerenUE Callaway Plant PO Box 620 Fulton, MIO 65251 February 24, 2005 U.S. Nuclear Regulatory Commission Attn: Document Control Desk Mail Stop P1-137 Washington, DC 20555-0001 ULNRC05121 Ladies and Gentlemen:
WAmeren UE DOCKET NUMBER 50-483 CALLAWAY PLANT UNIT 1 UNION ELECTRIC CO.
Transmittal of: Report on Actuation Arrangements for Halon Extinguishing System Units Ref I) NRC Event 41326, dated January 12, 2005 (Callaway)
Ref2)
NRC EventNumber41327, dated on January 12, 2005 (WolfCreek)
Ref 3)
NRC Information Notice 2005-001: Halon Fire Extinguishing System Piping Incorrectly connected.
On January 12, 2005 Callaway Plant reported a halon fire suppression system port connection error that affected five of six fire areas with halon fire suppression systems. The system was promptly restored to the qualified design configuration. In order to determine the effect on past halon system suppression capability, Chemetron Fire Systems performed testing in the as found configuration. The tests were designed to determine the impact on system function and were not used to establish qualification of the incorrect configurations. The results of the testing confirmed the system would remain functional, with a slight delay in initial system actuation. The required halon duration and concentrations would be unaffected by the actuation delay, therefore the suppression capabilities were maintained.
As other licensees have also identified similar configuration concerns, Callaway is providing the enclosed test report to facilitate generic resolution of this issue.
Application of the test results were only utilized to assess system function in the incorrect configuration.
Administrative controls lacked sufficient acceptance criteria to ensure the qualified configuration was maintained. These controls are being are being revised, in conjunction with training to ensure the halon suppression system is maintained in the original qualified configuration.
a subsidiary of Ameren Corporation
ULNRC05121 February 24, 2005 Page 2 No new commitments are identified in this correspondence.
None of the material is considered proprietary by Union Electric.
If you have any questions regarding this response, or if additional information is required, please let me know.
Sincerely, Keith D. Young Manager, Regulatory Affairs KDY/CSP/slk
Enclosure:
Chemtron Fire Systems report issued on 1/31/05: Report on Actuation Arrangements for Halon Extinguishing System Units
ULNRC05121 February 24, 2005 Page 3 Mr. Bruce S. Mallett Regional Administrator U.S. Nuclear Regulatory Commission Region IV 611 Ryan Plaza Drive, Suite 400 Arlington, TX 760114005 Senior Resident Inspector Callaway Resident Office U.S. Nuclear Regulatory Commission 8201 NRC Road Steedman, MO 65077 Mr. Jack N. Donohew (2 copies)
Licensing Project Manager, Callaway Plant Office of Nuclear Reactor Regulation U. S. Nuclear Regulatory Commission Mail Stop 7E1 Washington, DC 20555-2738 Linda J. Smith Chief, Plant Engineering Branch U.S. Nuclear Regulatory Commission Region IV 611 Ryan Plaza Drive, Suite 400 Arlington, TX 760114005 Missouri Public Service Commission Governor Office Building 200 Madison Street PO Box 360 Jefferson City, MO 65102-0360
CHEMETRon TM Fire Systems Report on Actuation Arrangements for Halon Extinguishing System Units ISSUED: 1/31/05 REVISED: N/A
Page 2 of 6 Scone The scope of this investigation is test the performance capabilities of the Manual Pneumatic Actuator (MPA) in the reverse configuration as a component in the Chemetron Fire Systems Halon Extinguishing System used in protection of the Callaway and Wolf Creek facilities and compare the results to the performance capabilities of the MPA in the standard configuration.
The standard pilot line configuration (see figure 1) utilizes a 20 in. flexible pilot hose (p/n 1-026-0267) to connect the pilot manifold to the A port of the MPA (p/n 1-061-0729). A second 20 in. flexible pilot hose (p/n 1-026-0267) is used to connect the solenoid (p/n 7-061-0006) to the B port of the MPA.
The reversed pilot configuration utilized at the Callaway and Wolf Creek facilities used a 20 in. pilot hose (p/n 1-026-0267) to connect the pilot manifold to the B port of the MPA (p/n 1-061-0729). A second 20 in. flexible pilot hose (p/n 1-026-0267) was used to connect the solenoid (p/n 7-061-0006) to the A port of the MPA.
Plan The MPA's reverse configuration will be tested and compared to the MPA's standard configuration on a simulated eight cylinder bank. Additional operation tests of the solenoid and MPA were conducted on a single cylinder to verify proper operation and compare the performance to the 8 cylinder test setup.
Equipment Eight Cylinder Test Setup The eight cylinder setup used 2 primary cylinders and 6 slave cylinders. The 2 primary cylinders were fitted with solenoids, MPA's and flexible pilot hoses. For typical installations, 2 primary cylinders are used to pressurize the pilot manifold. When the solenoids open, pressure from the cylinders enters the pilot manifold and operates the slave cylinders.
For testing purposes, the solenoid connected to the second primary cylinder was left disconnected to simulate a solenoid failure. This leaves only 1 primary bottle to fill the pilot manifold and operate the second primary and all slave cylinders.
The first primary cylinder was a 1.793 cu-ft. cylinder with a Beta discharge valve (p/n 1-061-0986). This cylinder is smaller than the 2.387 cu-ft. cylinders used in the Callaway and Wolf Creek nuclear power plants.
Note: Since the Beta uhalon' discharge valve, (p/n 1-061-0720), is no longer in production, the FM-200 version of the valve was used for testing. The FM-200 Version of the valve is identical to the halon version with the exception of the pressure rating of the safety relief disc. This change does not effect the actuation or discharge characteristics of the valves. Similarly, the solenoids, (p/n 7-061-0005), used in the Callaway and Wolfe Creek nuclear power plants are no longer available. The solenoids used in testing, (p/n 7-061-0006), are identical to the solenoids, (p/n 7-061-0005), with the exception of an upgraded coil. The solenoid flow path of the p/n 7-061-0006 solenoid is identical to the flow path of the p/n 7-061-0005 solenoid and can be considered equivalent for purposes of this report.
Super-pressurized nitrogen is the driving force for actuation and discharge. Agent vapor and super-pressurized nitrogen in the vapor space of the cylinder push the liquid agent up through the siphon tube and out through the Beta valve. For discussion sake and simplicity of explanation, we will refer to the gasses in the vapor space as super-pressurized nitrogen. Similarly, during actuation, nitrogen and agent vapor from the top of the siphon tube as well as liquid agent from the bottom of the siphon tube get pushed into the manifold. Again for discussion sake and simplicity of explanation, we will refer to the gasses and liquid in the siphon tube as super-ISSUED: 1/31/05 REVISED: N/A
Page 3 of 6 pressurized nitrogen.
Applying the ideal gas law, we can determine that using a single primary cylinder is more conservative than using two (2) primary cylinders. A system using two (2) primary cylinders would have twice the initial volume of super-pressurized nitrogen than a single primary. The volume after actuation is equal to the volume before actuation plus the volume of the MPA, hoses, and pilot manifold. Having more volume of nitrogen available for operation will result in higher pressures in the pilot manifold. Therefore, the use of a single primary cylinder is considered more conservative than the use of two (2) primary cylinders.
Again applying the ideal gas law, we can also determine that the use of a smaller cylinder is more conservative than the use of a standard cylinder. The volume before actuation is the vapor space in the primary cylinder(s).
Since the cylinder used in testing is smaller than a standard halon cylinder, the vapor space within the test cylinder is also smaller than a standard halon cylinder. The volume, after actuation, is equal to the volume before actuation plus the volume of the MPA, hoses, and pilot manifold. Again, having more volume of nitrogen available for operation will result in higher pressures in the pilot manifold. Therefore, the use of a smaller test cylinder is more conservative than the use a standard halon cylinder.
The first primary cylinder was filled with FM-200 the maximum fill density of 70 lb/cu-ft. (as allowed for halon cylinders) and super-pressurized to 540 psi with nitrogen, which corresponds to the minimum pressure allowable by surveillance procedures. Fill density is a measure of the mass of agent per unit of cylinder volume.
A cylinder at the maximum fill density will have the least volume of super-pressurized nitrogen above the liquid agent to push the most amount of agent out of that particular cylinder. The maximum fill density for FM-200 is similar to the ratio of the mass of agent to volume super-pressurizing nitrogen as seen in standard production cylinders.
FM-200 has a vapor pressure of 66.4 psia. @ 770F, while halon has a vapor pressure of 235 psia. @ 770F. A lower vapor pressure means that the liquid will convert to a gas at a lower pressure. Having a higher vapor pressure means that halon itself would actually help dispel the super-pressurized nitrogen quicker which results in a quicker activation time of the pilot line. Halon has a greater capability to produce pressure. (Vapor pressures for FM-200 and halon taken from MSDS sheets provided by Great Lakes Chemical and DuPont, respectively.)
The combination of a single, smaller, primary test cylinder and agent with a lower vapor pressure is a more conservative test setup than the actual halon cylinder banks installed at the Callaway and Wolf Creek nuclear power plants.
The second primary cylinder and all 6 slave cylinders were 0.286 cu-ft. cylinders that were pressurized with nitrogen to 600 psi.
Standard cylinder racks and a standard 8 cylinder pilot manifold were also used in testing.
Single Cylinder Test Setup The first primary cylinder from the "8 cylinder" tests was used for all "single cylinder' tests. The cylinder was filled with FM-200 the maximum fill density of 70 lb/cu-ft. (as allowed for halon cylinders) and again super-pressurized to less than the 600 psi pressure required for this type of halon cylinders.
Test 1 - 8 Cylinder Bank, Reverse Configuration - Figure 2 A 20 in. flexible pilot hose was used to connect the solenoid to the A port of the MPA for each primary cylinder.
A second 20 in. flexible pilot hose was used to connect the pilot manifold to the B port of the MPA. A 16 in.
flexible pilot hose was used to connect the pilot manifold to the top chamber of each cylinder (primary and slave).
Test 2 - 8 Cylinder Bank, Standard Configuration - Figure 3 A 20 in. flexible pilot hose was used to connect the solenoid to the B port of the MPA for each primary cylinder.
ISSUED: 1/31/05 REVISED: N/A
Page 4 of 6 A second 20 in. flexible pilot hose was used to connect the pilot manifold to the A port of the MPA. A 16 in.
flexible pilot hose was used to connect the pilot manifold to the top chamber of each cylinder (primary and slave).
Test 3 - Single Cylinder, Standard Configuration - Figure 4 A 20 in. flexible pilot hose was used to connect the solenoid to the B port of the MPA. A second 16 in. flexible pilot hose was used to connect the top chamber of the valve to the A port of the MPA.
Tests 4 to 6 - Single Cylinder, Reverse Configuration - Figure 5 A 20 in. flexible pilot hose was used to connect the solenoid to the A port of the MPA. A second 16 in. flexible pilot hose was used to connect the top chamber of the valve to the B port of the MPA.
Instrumentation 8 Cylinder Setup The discharge outlets of the first primary and last slave cylinders were fitted with caps and transducers to measure the time difference between the discharge of the first primary and last slave cylinders. All remaining valves were fitted with caps and pressure gauges to give a visual indication that proper valve actuation has occurred.
Additional pressure transducers were installed in the first primary cylinder's solenoid and the pilot manifold to determine the system initiation time and the rate of pressure increase in the manifold.
Additional pressure gauges were connected to the solenoid of the second primary cylinder and solenoid port of each slave cylinder to monitor the cylinder pressures.
All pressure gauges and transducers were calibrated using a dead weight tester prior to testing. Calibration records of the dead weight tester have been provided in Appendix A The pressure transducers and solenoid power supply were wired into a computer with Labview software for data acquisition. The sample rate for the data acquisition system was set at 10 samples per second.
Single Cylinder Setup For single cylinder tests, the test cylinder was fitted with transducers at the solenoid, the valve's top chamber and the valve's discharge port.
The pressure transducers and solenoid power supply were wired into a computer with Labview software for data acquisition. The sample rate for the data acquisition system was set at 10 samples per second.
Test Procedure Test 1 - 8 Cylinder Bank, Reverse Configuration, Electrical Operation The solenoid of the first primary cylinder was connected to a 24 vDC power supply. The power supply energized the solenoid which allowed pressure from below the cylinder valve seat to enter the pilot manifold through the MPA in the reverse configuration. The pressurized manifold operated both primary cylinders and all six (6) slave cylinders. The time difference between solenoid operation, operation of the first primary and operation of the last slave was recorded.
ISSUED: 1/31/05 REVISED: N/A
Page 5 of 6 Test 2 - 8 Cylinder Bank, Standard Configuration, Electrical Operation The solenoid of the first primary cylinder was connected to a 24 vDC power supply. The power supply energized the solenoid which allowed pressure from below the cylinder valve seat to enter the pilot manifold through the MPA in the standard configuration. The pressurized manifold operated both primary cylinders and all six (6) slave cylinders. The time difference between solenoid operation, operation of the first primary and operation of the last slave was recorded.
Test 3 - Single Cylinder, Standard Configuration, Electrical Operation The solenoid of the cylinder was connected to a 24 vDC power supply. The power supply energized the solenoid which allowed pressure from below the cylinder valve seat to enter the top chamber of the valve through the MPA. The time difference between solenoid operation and cylinder operation was recorded.
Test 4 - Single Cylinder, Reverse Configuration, Electrical Operation The solenoid of the cylinder was connected to a 24 vDC power supply. The power supply energized the solenoid which allowed pressure from below the cylinder valve seat to enter the top chamber of the valve through the MPA. The time difference between solenoid operation and cylinder operation was recorded.
Test 5 - Single Cylinder, Reverse Configuration, Manual Operation The safety pin was removed from the MPA and the lever operated to discharge the cylinder manually. The time difference between the operation of the MPA and operation of the cylinder was recorded.
Test 6 - Single Cylinder, Reverse Configuration, Manual Operation This test was identical to Test 5, except a new MPA was installed to verify repeatability of performance of production components.
Results The results are shown in the table below and graphs 1 through 6. For tests 1 and 2, all cylinders operated properly. For tests 3 through 6, the test cylinder operated properly.
Test #
Multiple Cylinder Results, Time Delay, sec.
Single Cylinder Results, Time Delay, sec.
Solenoid to 1st Solenoid to Last 16' Primary to Last Actuation to Primary Slave Slave Discharge 1
1.6 2.5 0.9 N/A 2
0.2 0.2
<0.1 N/A 3
N/A N/A N/A 0.1 4
N/A N/A N/A 0.2 5
N/A N/A N/A 0.1 6
N/A N/A N/A0.1 Summary Solenoid operation allows super-pressurized nitrogen to flow from below the cylinder valve seat into the MPA.
The MPA, in turn, increases the flow of super-pressurized nitrogen from the cylinder into the pilot manifold due to the greater flow path area. Manual actuation uses the MPA to directly pressurize the pilot manifold and will operate the system slightly faster than solenoid operation.
ISSUED: 1/31/05 REVISED: N/A
Page 6 of 6 For single cylinder operation, the reversed configuration of the MPA showed very little effect. In all cases tested, the MPA properly operated the cylinder.
For the 8 cylinder setup, the reversed configuration of the MPA successfully operated the two primary cylinders and all 6 slave cylinders. A delay of 1.6 seconds was observed between operation of the solenoid and operation of the first primary cylinder. For the standard configuration of the MPA, a 0.2 second delay was observed.
The additional delay observed in the reversed configuration is due to the asymmetrical design of the MPA's A and B ports (See figures 6 and 7). Both the A and B ports of the manual actuator supply the face of the plunger with pressure. However, the orifice on the A port has an area 4 times smaller than the B port. When pressure is introduced into the B port (standard configuration), the smaller A port chokes the flow of gas allowing super-pressurized nitrogen to build up in the volume upstream of the plunger and operate the MPA. When pressure is introduced into the A port (reverse configuration), the smaller port chokes the flow of super-pressurized nitrogen into the MPA. When in the reversed configuration, the larger B port allows this gas to continue flowing into the pilot manifold until enough pressure is built up in the manifold to operate the MPA, hence a greater time delay.
This report does not consider the radial forces applied to the MPA's plunger, nor was any additional testing performed to verify and/or quantify the application of radial forces. The testing covered in this report shows that the MPA is capable of operating in the standard and reversed configurations regardless of radial forces.
The design of the MPA (see figures 6 and 7) assures that the plunger will remain in the actuated position until complete cylinder discharge. (The surface area across the face of the plunger is much larger than the surface area of the plunger's pin.) The difference in area is an approximate 7:1 ratio. Similarly, the area above the Beta valve's piston is larger than the area below the piston. The difference in area is an approximate 3:1 ratio. As the cylinder pressure decreases, the amount of pressure required to keep the plunger (MPA) and piston (Beta valve) in place also decreases. This is true whether the MPA has been assembled in the standard or reversed configuration. The reversed configuration only effects delays the rate in which the pilot manifold is pressurized.
Once the pilot manifold is pressurized, the cylinders discharge the same as if the MPA's were in the standard configuration.
This report does not consider the spring force acting on the piston to re-seat the beta valve at the end of discharge. Testing to verify the MPA's ability to operate the discharge valve and discharge the cylinder contents within 10 seconds has already been conducted under the original Underwriters Laboratories Listing and Factory Mutual Approval for Chemetron Fire Systems Halon Extinguishing System. A drawings of the Beta valve spring has been provided (Figure 8) should further analysis be desired.
Conclusion The reversed configuration of the MPA used in the Callaway and Wolf Creek nuclear power plants validates adequate reliability as demonstrated in this report.
ISSUED: 1/31/05 REVISED: N/A
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Report on MPA Arrangements for Halon 1301 600 PSI Systems Test date:
1/2612005 2 pilot cylinders (with pneumatic operators) and 6 slave cylinders (1 pilot not electrically connected)
Electrically operated Pilot pressure into "A" and out of "B" on manual actuator (Reverse Configuration)
FM-200 superpressurized with Nitrogen In 1 pilot cylinder Nitrogen only In other 7 cylinders Pilot Cyl start pressure (Cyl 1):
Cylinders 2-8:
540 psig 600 psig Running Time Time (sec)
F 08:31.5 08:31.6 08:31.7 08:31.8 08:31.9 08:32.0 08:32.1 08:32.2 08:32.3 08:32.4 08:32.5 08:32.6 08:32.7 08:32.8 08:32.9 08:33.0 08:33.1 08:33.2 08:33.3 08:33.4 08:33.5 08:33.6 08:33.7 08:33.8 08:33.9 08:34.0 08:34.1 08:34.2 08:34.3 08:34.4 08:34.5 08:34.6 08:34.7 08:34.8 08:34.9 08:35.0 08:35.1 08:35.2 08:35.3 08:35.4 08:35.5 08:35.6 08:35.7 08:35.8 08:35.9 08:36.0 08:36.1 08:36.2 08:36.3 08:36.4
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Press (psia)
Press (psla)
Outlet Press (psla) 547.080383 23.096006 18.215384 23.096006 547.080383 23.096006 15.775072 23.096006 550.740845 13.334761 18.215384 20.655695 550.740845 13.334761 18.215384 20.655695 554.401306 15.775072 13.334761 13.334761 554.401306 15.775072 15.775072 20.655695 554.401306 18.215384 18.215384 18.215384 550.740845 15.775072 15.775072 18.215384 554.401306 23.096006 18.215384 20.655695 550.740845 18.215384 23.096006 18.215384 561.722229 13.334761 18.215384 15.775072 547.080383 18.215384 20.655695 18.215384 550.740845 18.215384 20.655695 20.655695 554.401306 13.334761 13.334761 25.536318 558.061768 18.215384 18.215384 20.655695 547.080383 18.215384 13.334761 20.655695 550.740845 18.215384 13.334761 20.655695 554.401306 13.334761 15.775072 23.096006 558.061768 8.454137 15.775072 20.655695 561.722229 25.536318 23.096006 15.775072 550.740845 10.894449 10.894449 23.096006 554.401306 15.775072 15.775072 20.655695 550.740845 15.775072 18.215384 15.775072 550.740845 18.215384 15.775072 18.215384 558.061768 18.215384 20.655695 13.334761 554.401306 15.775072 15.775072 18.215384 550.740845 13.334761 18.215384 20.655695 554.401306 13.334761 15.775072 20.655695 550.740845 15.775072 13.334761 18.215384 547.080383 18.215384 18.215384 20.655695 550.740845 15.775072 15.775072 20.655695 177.531494 15.775072 18.215384 18.215384 159.229156 23.096006 18.215384 18.215384 554.401306 27.976629 18.215384 18.215384 554.401306 37.737877 15.775072 20.655695 543.419922 47.499123 18.215384 20.655695 543.419922 57.260368 15.775072 20.655695 539.75946 62.140991 15.775072 20.655695 543.419922 64.581306 18.215384 20.655695 543.419922 67.021614 18.215384 13.334761 550.740845 84.103798 15.775072 23.096006 547.080383 101.185974 18.215384 18.215384 550.740845 118.268158 10.894449 18.215384 547.080383 142.67128 10.894449 18.215384 550.740845 157.313141 15.775072 18.215384 547.080383 176.835632 18.215384 25.536318 539.75946 193.917816 18.215384 23.096006 547.080383 211 540.442078 18.215384 532.438477 211 535.561462 18.215384 536.098999 228.082184 538.00177 18.215384 Energize Solenoid Open Pilot Cylinder Valve Opens Halon 600 psi test for nuclear plants #1 1-26-05.xls Page 1 of 4
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Time 08:36.5 08:36.6 08:36.7 08:36.8 08:36.9 08:37.0 08:37.1 08:37.2 08:37.3 08:37.4 08:37.5 08:37.6 08:37.7 08:37.8 08:37.9 08:38.0 08:38.1 08:38.2 08:38.3 08:38.4 08:38.5 08:38.6 08:38.7 08:38.8 08:38.9 08:39.0 08:39.1 08:39.2 08:39.3 08:39.4 08:39.5 08:39.6 08:39.7 08:39.8 08:39.9 08:40.0 08:40.1 08:40.2 08:40.3 08:40.4 08:40.5 08:40.6 08:40.7 08:40.8 08:40.9 08:41.0 08:41.1 08:41.2 08:41.3 08:41.4 08:41.5 08:41.6 08:41.7 08:41.8 08:41.9 08:42.0 08:42.1 08:42.2 08:42.3 08:42.4 08:42.5 08:42.6 08:42.7 08:42.8 08:42.9 08:43.0 08:43.1 Pilot Cyl Pilot Manifold Time (sec)
Press (psia)
Press (psla) 2.0 539.75946 228.082184 2.1 539.75946 225.641861 2.2 536.098999 220.761246 2.3 532.438477 240.283737 2.4 536.098999 235.403107 2.5 543.419922 230.522491 2.6 536.098999 242.724045 2.7 525.117554 242.724045 2.8 536.098999 242.724045 2.9 532.438477 252.485291 3.0 536.098999 262.246552 3.1 532.438477 274.44809 3.2 539.75946 286.649658 3.3 528.778015 296.410889 3.4 539.75946 308.612457 3.5 521.457092 320.814026 3.6 536.098999 333.015564 3.7 528.778015 337.89621 3.8 536.098999 352.538055 3.9 525.117554 362.299316 4.0 521.457092 374.500885 4.1 525.117554 374.500885 4.2 525.117554 391.583069 4.3 532.438477 396.463684 4.4 528.778015 403.784607 4.5 532.438477 418.426483 4.6 521.457092 425.747406 4.7 521.457092 433.068359 4.8 532.438477 442.82959 4.9 528.778015 447.710236 5.0 521.457092 455.031158 5.1 514.136169 464.792389 5.2 532.438477 472.113342 5.3 521.457092 476.993958 5.4 525.117554 481.874573 5.5 525.117554 486.755219 5.6 528.778015 496.516449 5.7 517.796631 498.956757 5.8 525.117554 503.837372 5.9 528.778015 508.718018 6.0 517.796631 513.598633 6.1 528.778015 511.158325 6.2 525.117554 518.479248 6.3 514.136169 520.919556 6.4 521.457092 518.479248 6.5 514.136169 520.919556 6.6 528.778015 525.800171 6.7 521.457092 523.359863 6.8 525.117554 523.359863 6.9 525.117554 525.800171 7.0 510.475708 530.680786 7.1 521.457092 528.240479 7.2 517.796631 528.240479 7.3 525.117554 530.680786 7.4 517.796631 530.680786 7.5 521.457092 530.680786 7.6 517.796631 525.800171 7.7 528.778015 525.800171 7.8 517.796631 530.680786 7.9 521.457092 530.680786 8.0 521.457092 528.240479 8.1 525.117554 530.680786 8.2 525.117554 528.240479 8.3 521.457092 533.121155 8.4 532.438477 528.240479 8.5 532.438477 528.240479 8.6 525.117554 528.240479 Pilot Cyl Outlet Final Slave Cyl Press (psia)
Outlet Press (psia) 533.121155 13.334761 533.121155 15.775072 533.121155 18.215384 535.561462 15.775072 530.680786 18.215384 533.121155 20.655695 530.680786 30.416941 Last Slave Cylinder Valve Opens 533.121155 618.532043 533.121155 608.770813 533.121155 606.330444 533.121155 611.211121 533.121155 608.770813 530.680786 608.770813 533.121155 606.330444 528.240479 603.890137 535.561462 608.770813 530.680786 611.211121 525.800171 611.211121 523.359863 603.890137 525.800171 606.330444 528.240479 608.770813 525.800171 603.890137 528.240479 608.770813 525.800171 606.330444 520.919556 606.330444 523.359863 608.770813 528.240479 606.330444 525.800171 608.770813 525.800171 606.330444 518.479248 608.770813 525.800171 608.770813 523.359863 608.770813 530.680786 608.770813 530.680786 606.330444 525.800171 608.770813 516.03894 606.330444 518.479248 608.770813 523.359863 606.330444 520.919556 606.330444 520.919556 606.330444 520.919556 613.651428 520.919556 606.330444 516.03894 603.890137 518.479248 606.330444 518.479248 611.211121 523.359863 606.330444 525.800171 611.211121 525.800171 611.211121 520.919556 611.211121 518.479248 608.770813 523.359863 606.330444 518.479248 608.770813 520.919556 606.330444 520.919556 608.770813 523.359863 608.770813 516.03894 608.770813 520.919556 608.770813 518.479248 603.890137 520.919556 603.890137 516.03894 603.890137 520.919556 608.770813 513.598633 608.770813 523.359863 608.770813 520.919556 603.890137 518.479248 603.890137 516.03894 606.330444 520.919556 608.770813 Halon 600 psi test for nuclear plants #1 1 05.xis Page 2 of 4
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Time 08:43.2 08:43.3 08:43.4 08:43.5 08:43.6 08:43.7 08:43.8 08:43.9 08:44.0 08:44.1 08:44.2 08:44.3 08:44.4 08:44.5 08:44.6 08:44.7 08:44.8 08:44.9 08:45.0 08:45.1 08:45.2 08:45.3 08:45.4 08:45.5 08:45.6 08:45.7 08:45.8 08:45.9 08:46.0 08:46.1 08:46.2 08:46.3 08:46.4 08:46.5 08:46.6 08:46.7 08:46.8 08:46.9 08:47.0 08:47.1 08:47.2 08:47.3 08:47.4 08:47.5 08:47.6 08:47.7 08:47.8 08:47.9 08:48.0 08:48.1 08:48.2 08:48.3 08:48.4 08:48.5 08:48.6 08:48.7 08:48.8 08:48.9 08:49.0 08:49.1 08:49.2 08:49.3 08:49.4 08:49.5 08:49.6 08:49.7 08:49.8 Pilot Cyl Pilot Manifold Pilot Cyl Outlet Final Slave Cyl Time (sec)
Press (psla)
Press (psla) 8.7 517.796631 533.121155 8.8 521.457092 533.121155 8.9 521.457092 533.121155 9.0 521.457092 533.121155 9.1 521.457092 528.240479 9.2 517.796631 528.240479 9.3 521.457092 528.240479 9.4 517.796631 528.240479 9.5 517.796631 530.680786 9.6 521.457092 528.240479 9.7 528.778015 528.240479 9.8 525.117554 525.800171 9.9 517.796631 525.800171 10.0 521.457092 530.680786 10.1 521.457092 530.680786 10.2 521.457092 525.800171 10.3 521.457092 525.800171 10.4 525.117554 523.359863 10.5 528.778015 525.800171 10.6 521.457092 523.359863 10.7 514.136169 525.800171 10.8 525.117554 525.800171 10.9 525.117554 525.800171 11.0 521.457092 525.800171 11.1 525.117554 523.359863 11.2 517.796631 523.359863 11.3 528.778015 530.680786 11.4 525.117554 523.359863 11.5 528.778015 525.800171 11.6 525.117554 525.800171 11.7 521.457092 530.680786 11.8 525.117554 520.919556 11.9 521.457092 518.479248 12.0 525.117554 520.919556 12.1 525.117554 520.919556 12.2 528.778015 523.359863 12.3 514.136169 520.919556 12.4 525.117554 523.359863 12.5 525.117554 523.359863 12.6 525.117554 525.800171 12.7 514.136169 528.240479 12.8 517.796631 520.919556 12.9 517.796631 518.479248 13.0 532.438477 523.359863 13.1 532.438477 516.03894 13.2 525.117554 528.240479 13.3 525.117554 525.800171 13.4 521.457092 523.359863 13.5 517.796631 523.359863 13.6 528.778015 523.359863 13.7 525.117554 520.919556 13.8 521.457092 525.800171 13.9 525.117554 525.800171 14.0 525.117554 523.359863 14.1 517.796631 520.919556 14.2 525.117554 516.03894 14.3 521.457092 518.479248 14.4 525.117554 518.479248 14.5 525.117554 528.240479 14.6 521.457092 523.359863 14.7 517.796631 523.359863 14.8 525.117554 518.479248 14.9 525.117554 516.03894 15.0 514.136169 513.598633 15.1 525.117554 518.479248 15.2 521.457092 523.359863 15.3 514.136169 518.479248 Press (psia) 523.359863 520.919556 518.479248 520.919556 520.919556 518.479248 520.919556 520.919556 518.479248 523.359863 518.479248 520.919556 520.919556 516.03894 518.479248 518.479248 523.359863 528.240479 518.479248 516.03894 520.919556 520.919556 525.800171 525.800171 513.598633 520.919556 520.919556 520.919556 523.359863 518.479248 513.598633 520.919556 520.919556 520.919556 523.359863 518.479248 516.03894 516.03894 520.919556 518.479248 518.479248 518.479248 520.919556 520.919556 523.359863 520.919556 513.598633 518.479248 516.03894 516.03894 525.800171 518.479248 518.479248 516.03894 520.919556 520.919556 518.479248 516.03894 518.479248 516.03894 513.598633 523.359863 516.03894 516.03894 516.03894 518.479248 516.03894 Outlet Press (psla) 608.770813 611.211121 608.770813 606.330444 603.890137 603.890137 601.449829 611.211121 603.890137 601.449829 606.330444 608.770813 606.330444 606.330444 603.890137 611.211121 608.770813 606.330444 608.770813 599.009521 606.330444 603.890137 608.770813 606.330444 611.211121 608.770813 606.330444 603.890137 603.890137 606.330444 608.770813 603.890137 601.449829 601.449829 599.009521 603.890137 603.890137 603.890137 603.890137 603.890137 603.890137 611.211121 606.330444 603.890137 603.890137 608.770813 603.890137 611.211121 606.330444 603.890137 606.330444 606.330444 608.770813 606.330444 608.770813 608.770813 603.890137 603.890137 608.770813 608.770813 606.330444 601.449829 603.890137 603.890137 606.330444 606.330444 606.330444 Hafon 600 psi test for nuclear plants #1 1-26-05.xls Page 3 of 4
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Time 08:49.9 08:50.0 Pilot Cyl Time (sec)
Press (psia) 15.4 521.457092 15.5 521.457092 Pilot Manifold Press (psia) 518.479248 516.03894 Pilot Cyl Outlet Press (psia) 520.919556 518.479248 Final Slave Cyl Outlet Press (psla) 603.890137 599.009521 Halon 600 psi test for nuclear plants #1 1 05.xls Page 4 of 4
Graph 2 Test 2 1-26-05 Chemetron Facility (Standard Configuration, Press into MPA port B and out ol port A, Electrically Operated) 0.7 0.
-1.0
-0.5 0.0 0.5 1.0 1.5 2.0 2.5 Time (sec) 3.0 CO2-
Report on MPA Arrangements for Halon 1301 600 PSI Systems Test date:
1/26/2005 2 pilot cylinders (with pneumatic operators) and 6 slave cylinders (1 pilot not electrically connected)
Electrically operated Pilot pressure Into "B-and out of "A' on manual actuator (Standard Configuration)
FM-200 superpressurized with Nitrogen In 1 pilot cylinder Nitrogen only In other 7 cylinders Pilot Cyl start pressure (Cyl 1):
530 psig Cylinders 2-8:
600 psig Runnino PlotiCYIPress Pilot Manifold Plot CYlIOutlet Final Slave CyI TImet Time (sec)
(DL218 Press Ivslal Press (ysla)
Outlet Press (psla) 30:04.1 43.0 554.401306 10.894449 20.655695 18.215384 30 042
-2.9 554.401306 20.655695 15.775072 23.096006 30:04.3
-2.8 550.740845 13.334761 18.215384 18.215384 30.04.4
- 2.7 550.740845 18.215384 18.215384 20.655695 30.04.5
-2.6 550.740845 18.215384 15.775072 18.215384 30.04.6
-2.5 547.080383 8.454137 15.775072 20.655695 30:04.7
.2.4 547.080383 20.655695 10.894449 20.655695 30.04.8
-2.3 554.401306 8.454137 18.215384 20.655695 30.04.9
-2.2 550.740845 20.655695 15.775072 18.215384 30:05.0
.2.1 547.080383 13.334761 13.334761 20.655695 30.05.1
-2.0 550.740845 15.775072 23.096006 15.775072 30:05.2
-1.9 554.401306 18.215384 15.775072 20.655695 30.05.3
-1.8 550.740845 13.334761 18.215384 20.655695 30:05.4
-1.7 554.401306 15.775072 23.096006 18.215384 30:05.5
-1.6 547.080383 15.775072 13.334761 18.215384 30:05.6
-1.5 554.401306 13.334761 15.775072 23.096006 30:05.7
-1.4 550.740845 15.775072 18.215384 23.096006 30:05.8
-1.3 554.401306 10.894449 15.775072 15.775072 30:05.9
-1.2 550.740845 15.775072 15.775072 18.215384 30:06.0
-1.1 550.740845 23.096006 18.215384 23.096006 30 06.1
-1.0 554.401306 23.096006 13.334761 20.655695 30:06.2
-0.9 554.401306 10.894449 15.775072 18.215384 30:06.3
-0.8 558.061768 15.775072 23.096006 18.215384 30:06.4
-0.7 558.061768 15.775072 18.215384 13.334761 30:06.5
-0.6 550.740845 13.334761 20.655695 18.215384 30:06.6
-0.5 558.061768 8.454137 18.215384 18.215384 30:06.7
-0.4 554.401306 8.454137 13.334761 13.334761 30:06.8
-0.3 550.740845 20.655695 18.215384 15.775072 30:06.9
-0.2 550.740845 10.894449 18.215384 20.655695 30:07.0
-0.1 550.740845 13.334761 15.775072 18.215384 30:07.1 0.0 550.740845 18.215384 20.655695 23.096006 30:07.2 0.1 451.908234 54.820057 15.775072 23.096006 Energize Solenoid Open 30:07.3 0.2 488.512909 145.111588 13.334761 23.096006 30:07.4 0.3 477.531494 252.485291 530.680786 606.330444 Pilot Cylinder and Last Slave Cylinder Valves Open 30:07.5 0.4 484.852417 311.052765 516.03894 603.890137 30:07.6 0.5 488.512909 411.10556 518.479248 613.651428 30:07.7 0.6 510.475708 481.874573 513.598633 611.211121 30:07.8 0.7 514.136169 520.919556 520.919556 611.211121 30:07.9 0.8 525.117554 525.800171 518.479248 606.330444 30:08.0 0.9 525.117554 530.680786 518.479248 606.330444 30:08.1 1.0 528.778015 533.121155 520.919556 616.091736 30:082 1.1 521.457092 535.561462 523.359863 603.890137 30:08.3 1.2 525.117554 533.121155 520.919556 611.211121 30:08.4 1.3 521.457092 533.121155 528.240479 613.651428 30:08.5 1.4 528.778015 538.00177 520.919556 606.330444 30:08.6 1.5 532.438477 533.121155 525.800171 611.211121 30:08.7 1.6 532.438477 535.561462 528.240479 611.211121 30:08.8 1.7 525.117554 528.240479 525.800171 611.211121 30:08.9 1.8 532.438477 538.00177 528.240479 606.330444 30:09.0 1.9 532.438477 533.121155 535.561462 608.770813 30:09.1 2.0 532.438477 535.561462 535.561462 608.770813 30:09.2 2.1 543.419922 535.561462 530.680786 601.449829 30:09.3 2.2 536.098999 530.680786 538.00177 611.211121 30.09.4 2.3 536.098999 530.680786 530.680786 611.211121 30.09.5 2.4 532.438477 533.121155 533.121155 613.651428 30:09.6 2.5 536.098999 535.561462 533.121155 608.770813 30:09.7 2.6 532.438477 535.561462 540.442078 608.770813 30:09.8 2.7 532.438477 533.121155 533.121155 608.770813 30:09.9 2.8 543.419922 535.561462 535.561462 608.770813 30:10.0 2.9 532.438477 535.561462 538.00177 611.211121 Halon 600 psi test for nuclear plants #2 1 05.xis Page 1 of 3
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Pllot Cvl Press Pilot Manifold Pilot Cvl Outlet Final Slave Cvl Time Time (sect (fsla)
Press osla)
Press (osla)
Outlet Press (psla) 30:10.1 3.0 536.098999 538.00177 528.240479 608.770813 30:10.2 3.1 543.419922 538.00177 535.561462 603.890137 30:10.3 3.2 543.419922 530.680786 538.00177 608.770813 30:10.4 3.3 543.419922 535.561462 535.561462 611.211121 30:10.5 3.4 539.75946 540.442078 535.561462 608.770813 30:10.6 3.5 539.75946 528.240479 535.561462 606.330444 30:10.7 3.6 532.438477 538.00177 535.561462 608.770813 30:10.8 3.7 536.098999 535.561462 540.442078 608.770813 30:10.9 3.8 536.098999 533.121155 533.121155 613.651428 30:11.0 3.9 536.098999 530.680786 530.680786 611.211121 30:11.1 4.0 536.098999 533.121155 538.00177 606.330444 30:112 4.1 532.438477 535.561462 535.561462 613.651428 30:11.3 4.2 536.098999 533.121155 535.561462 608.770813 30:11.4 4.3 536.098999 528.240479 530.680786 603.890137 30:11.5 4.4 536.098999 530.680786 533.121155 603.890137 30:11.6 4.5 536.098999 533.121155 535.561462 613.651428 30:11.7 4.6 539.75946 535.561462 533.121155 611.211121 30:11.8 4.7 543.419922 533.121155 533.121155 611.211121 30:11.9 4.8 539.75946 530.680786 535.561462 608.770813 30:12.0 4.9 532.438477 533.121155 533.121155 606.330444 30:12.1 5.0 539.75946 528.240479 528.240479 613.651428 30:122 5.1 532.438477 533.121155 525.800171 608.770813 30:12.3 5.2 539.75946 530.680786 535.561462 611.211121 30:12.4 5.3 539.75946 530.680786 538.00177 613.651428 30:12.5 5.4 543.419922 528.240479 533.121155 606.330444 30:12.6 5.5 539.75946 535.561462 533.121155 608.770813 30:12.7 5.6 528.778015 528.240479 535.561462 613.651428 30:12.8 5.7 536.098999 528.240479 535.561462 611.211121 30:12.9 5.8 536.098999 528.240479 533.121155 606.330444 30:13.0 5.9 543.419922 525.800171 533.121155 606.330444 30:13.1 6.0 543.419922 533.121155 528.240479 606.330444 30:13.2 6.1 536.098999 528.240479 533.121155 611.211121 30:13.3 6.2 532.438477 528.240479 533.121155 608.770813 30:13.4 6.3 536.098999 530.680786 535.561462 611.211121 30:13.5 6.4 532.438477 525.800171 533.121155 608.770813 30:13.6 6.5 528.778015 528.240479 525.800171 606.330444 30:13.7 6.6 536.098999 525.800171 530.680786 601.449829 30:13.8 6.7 532.438477 520.919556 533.121155 608.770813 30:13.9 6.8 536.098999 528.240479 528.240479 611.211121 30:14.0 6.9 536.098999 533.121155 530.680786 613.651428 30:14.1 7.0 525.117554 528.240479 528.240479 613.651428 30:14.2 7.1 532.438477 530.680786 528.240479 608.770813 30:14.3 7.2 528.778015 528.240479 528.240479 606.330444 30:14.4 7.3 539.75946 528.240479 535.561462 608.770813 30:14.5 7.4 532.438477 523.359863 530.680786 606.330444 30:14.6 7.5 536.098999 528.240479 530.680786 606.330444 30:14.7 7.6 539.75946 525.800171 528.240479 606.330444 30:14.8 7.7 532.438477 523.359863 533.121155 606.330444 30:14.9 7.8 539.75946 523.359863 530.680786 613.651428 30:15.0 7.9 536.098999 528.240479 530.680786 611.211121 30:15.1 8.0 532.438477 528.240479 530.680786 606.330444 30:152 8.1 532.438477 525.800171 533.121155 608.770813 30:15.3 8.2 532.438477 525.800171 530.680786 613.651428 30:15.4 8.3 536.098999 530.680786 528.240479 611.211121 30:15.5 8.4 543.419922 528.240479 528.240479 608.770813 30:15.6 8.5 528.778015 528.240479 528.240479 608.770813 30:15.7 8.6 532.438477 528.240479 530.680786 606.330444 30:15.8 8.7 532.438477 523.359863 533.121155 606.330444 30:15.9 8.8 536.098999 523.359863 530.680786 611.211121 30:16.0 8.9 528.778015 525.800171 530.680786 608.770813 30:16.1 9.0 528.778015 525.800171 523.359863 608.770813 30:16.2 9.1 525.117554 523.359863 525.800171 613.651428 30:16.3 9.2 532.438477 525.800171 528.240479 613.651428 30:16.4 9.3 532.438477 525.800171 533.121155 608.770813 30:16.5 9.4 532.438477 525.800171 523.359863 606.330444 30:16.6 9.5 528.778015 528.240479 525.800171 608.770813 30:16.7 9.6 528.778015 523.359863 530.680786 606.330444 30:16.8 9.7 532.438477 525.800171 528.240479 603.890137 30:16.9 9.8 528.778015 518.479248 525.800171 611.211121 30:17.0 9.9 536.098999 525.800171 525.800171 611.211121 30:17.1 10.0 536.098999 525.800171 528.240479 613.651428 30:17.2 10.1 528.778015 525.800171 528.240479 608.770813 30:17.3 10.2 528.778015 525.800171 520.919556 611.211121 30:17.4 10.3 528.778015 525.800171 523.359863 606.330444 30:17.5 10.4 525.117554 523.359863 523.359863 611.211121 30:17.6 10.5 532.438477 518.479248 525.800171 611.211121 30:17.7 10.6 536.098999 523.359863 525.800171 606.330444 Halon 600 psi test for nuclear plants #2 1-26-05.xis Page 2 of 3
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Pilot CvI Press Pilot Manifold Pilot CyI Outlet Final Slave Cvl Time Time (sect (1sia)
Press (psla)
Press (psla)
Outlet Press (Csla) 30:17.8 10.7 532.438477 525.800171 530.680786 606.330444 30:17.9 10.8 536.098999 523.359863 525.800171 608.770813 30:18.0 10.9 528.778015 525.800171 525.800171 608.770813 30:18.1 11.0 532.438477 525.800171 525.800171 613.651428 30:18.2 11.1 532.438477 520.919556 525.800171 613.651428 Halon 600 psi test for nuclear plants #2 1 26-05.xls Page 3 of 3
Graph 3 Test 3 1-26-05 Chemetron Facility 1-Cyl (Standard Configuration, Pressure into MPA B and out of A), Electrically Operated)
'A ilot Cyl Press (psia)
-Pilot Port Press (psia)
Pilot Cyl Outlet Press (psia)
-1.0
-0.5 0.0 0.5 1.0 1.5 2.0 2.5 3.0 Time (sec) coG3
Report on MPA Arrangements for Halon 1301 600 PSI Systems Test date: 1/26/2005 1 pilot cylinder only with pneumatic operator (no slave cylinders)
Electrically operated Pilot pressure into "B" and out of "A" on manual actuator (Standard Configuration)
FM-200 superpressurized with Nitrogen in 1 pilot cylinder Pilot Cyl start pressure (Cyl 1):
560 psig Running Time 42:35.3 42:35.4 42:35.5 42:35.6 42:35.7 42:35.8 42:35.9 42:36.0 42:36.1 42:36.2 42:36.3 42:36.4 42:36.5 42:36.6 42:36.7 42:36.8 42:36.9 42:37.0 42:37.1 42:37.2 42:37.3 42:37.4 42:37.5 42:37.6 42:37.7 42:37.8 42:37.9 42:38.0 42:38.1 42:38.2 42:38.3 42:38.4 42:38.5 42:38.6 42:38.7 42:38.8 42:38.9 42:39.0 Time (sec)
-3.0
-2.9
-2.8
-2.7
-2.6
-2.5
-2.4
-2.3
-2.2
-2.1
-2.0
-1.9
-1.8
-1.7
-1.6
-1.5
-1.4
-1.3
-1.2
-1.1
-1.0
-0.9
-0.8
-0.7
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 Pilot Cyl Press (psia) 583.685059 583.685059 580.024597 572.703674 576.364136 587.34552 572.703674 576.364136 580.024597 572.703674 580.024597 569.043152 576.364136 576.364136 576.364136 572.703674 576.364136 576.364136 583.685059 576.364136 572.703674 572.703674 576.364136 572.703674 576.364136 576.364136 580.024597 580.024597 576.364136 576.364136 565.38269 572.703674 451.908234 572.703674 565.38269 565.38269 561.722229 569.043152 Pilot Port Press (psla) 10.894449 18.215384 18.215384 13.334761 13.334761 13.334761 13.334761 13.334761 13.334761 15.775072 13.334761 15.775072 10.894449 18.215384 15.775072 13.334761 18.215384 8.454137 10.894449 20.655695 15.775072 15.775072 13.334761 13.334761 10.894449 13.334761 15.775072 13.334761 8.454137 13.334761 10.894449 10.894449 315.933411 555.083923 555.083923 555.083923 557.524231 557.524231 Pilot Cyl Outlet Press (psla) 18.215384 13.334761 13.334761 15.775072 13.334761 13.334761 15.775072 18.215384 15.775072 10.894449 13.334761 15.775072 13.334761 18.215384 15.775072 18.215384 15.775072 18.215384 10.894449 15.775072 15.775072 10.894449 18.215384 18.215384 18.215384 18.215384 15.775072 15.775072 10.894449 15.775072 15.775072 8.454137 559.964539 557.524231 555.083923 559.964539 564.845154 562.404846 Energize Solenoid Open Pilot Cylinder Valve Opens Halon 600 psi test for nuclear plants #3 1-26-05.xls Page 1 of 3
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Time 42:39.1 42:39.2 42:39.3 42:39.4 42:39.5 42:39.6 42:39.7 42:39.8 42:39.9 42:40.0 42:40.1 42:40.2 42:40.3 42:40.4 42:40.5 42:40.6 42:40.7 42:40.8 42:40.9 42:41.0 42:41.1 42:41.2 42:41.3 42:41.4 42:41.5 42:41.6 42:41.7 42:41.8 42:41.9 42:42.0 42:42.1 42:42.2 42:42.3 42:42.4 42:42.5 42:42.6 42:42.7 42:42.8 42:42.9 42:43.0 42:43.1 42:43.2 42:43.3 42:43.4 42:43.5 42:43.6 42:43.7 42:43.8 42:43.9 42:44.0 42:44.1 Time (sec) 0.8 0.9 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4 4.5 4.6 4.7 4.8 4.9 5.0 5.1 5.2 5.3 5.4 5.5 5.6 5.7 5.8 Pilot Cyl Press (psia) 565.38269 558.061768 561.722229 558.061768 558.061768 561.722229 554.401306 561.722229 565.38269 565.38269 550.740845 565.38269 561.722229 565.38269 554.401306 561.722229 554.401306 561.722229 558.061768 565.38269 565.38269 561.722229 558.061768 565.38269 565.38269 558.061768 550.740845 558.061768 558.061768 554.401306 558.061768 561.722229 561.722229 554.401306 561.722229 550.740845 550.740845 554.401306 554.401306 565.38269 554.401306 554.401306 554.401306 558.061768 550.740845 558.061768 561.722229 561.722229 554.401306 558.061768 547.080383 Pilot Port Press (psia) 559.964539 555.083923 557.524231 555.083923 552.643616 555.083923 550.203308 559.964539 555.083923 552.643616 559.964539 555.083923 555.083923 547.763 557.524231 550.203308 552.643616 555.083923 552.643616 552.643616 555.083923 550.203308 550.203308 555.083923 547.763 557.524231 547.763 552.643616 550.203308 550.203308 550.203308 550.203308 550.203308 552.643616 555.083923 547.763 550.203308 550.203308 550.203308 547.763 547.763 550.203308 552.643616 547.763 550.203308 542.882385 550.203308 547.763 545.322693 552.643616 547.763 Pilot Cyl Outlet Press (psia) 559.964539 557.524231 559.964539 555.083923 559.964539 559.964539 555.083923 562.404846 559.964539 559.964539 559.964539 557.524231 562.404846 555.083923 562.404846 562.404846 557.524231 557.524231 557.524231 550.203308 557.524231 557.524231 550.203308 552.643616 555.083923 552.643616 557.524231 555.083923 552.643616 555.083923 552.643616 552.643616 555.083923 552.643616 552.643616 555.083923 550.203308 555.083923 555.083923 550.203308 555.083923 552.643616 550.203308 557.524231 552.643616 550.203308 547.763 550.203308 552.643616 547.763 550.203308 Halon 600 psi test for nuclear plants #3 1-26-05.xls Page 2 of 3
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Time 42:44.2 Time (sec) 5.9 Pilot Cyl Press (psia) 554.401306 Pilot Port Press (psia) 547.763 Pilot Cyl Outlet Press (psia) 550.203308 Halon 600 psi test for nuclear plants #3 1-26-05.xls Page 3 of 3
Graph 4 Test 4 1-26-05 Chemetron Facility 1-Cyl (Reverse Configuration, Pressure into MPA A and out of B), Electrically Operated)
'uA 0
en
-1.0
-0.5 0.0 0.5 1.0 1.5 2.0 2.5 3.0 Time (sec)
C 05
Report on MPA Arrangements for Halon 1301 600 PSI Systems Test date:
112612005 1 pilot cylinder only with pneumatic operator (no slave cylinders)
Electrically operated Pilot pressure Into "A" and out of "B" on manual actuator (Reverse Configuration)
FM-200 superpressurized with Nitrogen in 1 pilot cylinder Pilot Cyl start pressure (Cyl 1):
562 psig Running Time 48:19.0 48:19.1 48:19.2 48:19.3 48:19.4 48:19.5 48:19.6 48:19.7 48:19.8 48:19.9 48:20.0 48:20.1 48:20.2 48:20.3 48:20.4 48:20.5 48:20.6 48:20.7 48:20.8 48:20.9 48:21.0 48:21.1 48:21.2 48:21.3 48:21.4 48:21.5 48:21.6 48:21.7 48:21.8 48:21.9 48:22.0 48:22.1 48:22.2 48:22.3 48:22.4 48:22.5 48:22.6 48:22.7 48:22.8 48:22.9 48:23.0 48:23.1 Time (sec)
-3.0
-2.9
-2.8
-2.7
-2.6
-2.5
-2.4
-2.3
-2.2
-2.1
-2.0
-1.9
-1.8
-1.7
-1.6
-1.5
-1.4
-1.3
-1.2
-1.1
-1.0
-0.9
-0.8
-0.7
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 Pilot Cyl Press (psia) 580.024597 583.685059 583.685059 580.024597 583.685059 587.34552 587.34552 583.685059 587.34552 576.364136 583.685059 583.685059 583.685059 583.685059 583.685059 591.005981 576.364136 587.34552 580.024597 576.364136 583.685059 580.024597 583.685059 587.34552 587.34552 583.685059 580.024597 583.685059 580.024597 580.024597 580.024597 583.685059 583.685059 580.024597 576.364136 572.703674 572.703674 569.043152 580.024597 569.043152 569.043152 565.38269 Pilot Port Press (psla) 13.334761 18.215384 13.334761 13.334761 15.775072 18.215384 20.655695 10.894449 10.894449 15.775072 18.215384 18.215384 15.775072 13.334761 18.215384 18.215384 13.334761 18.215384 13.334761 13.334761 15.775072 15.775072 13.334761 13.334761 20.655695 18.215384 13.334761 15.775072 8.454137 13.334761 15.775072 15.775072 88.984421 157.313141 181.716263 259.806244 335.455902 401.344299 462.352081 511.158325 547.763 562.404846 Pilot Cyl Outlet Press (psla) 15.775072 20.655695 18.215384 13.334761 15.775072 20.655695 18.215384 20.655695 18.215384 13.334761 18.215384 20.655695 20.655695 18.215384 20.655695 18.215384 20.655695 18.215384 15.775072 13.334761 15.775072 15.775072 18.215384 13.334761 13.334761 18.215384 15.775072 20.655695 13.334761 8.454137 13.334761 18.215384 15.775072 586.807983 567.285461 567.285461 567.285461 572.166138 569.725769 572.166138 559.964539 559.964539 Energize Solenoid Open Pilot Cylinder Valve Opens Halon 600 psi test for nuclear plants #4 1-26-05.xls Page 1 of 2
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Pilot Cyl Pilot Port Press Time Time (sec)
Press (psia)
(psia) 48:23.2 1.2 569.043152 564.845154 48:23.3 1.3 576.364136 564.845154 48:23.4 1.4 576.364136 567.285461 48:23.5 1.5 569.043152 567.285461 48:23.6 1.6 565.38269 567.285461 48:23.7 1.7 565.38269 564.845154 48:23.8 1.8 565.38269 567.285461 48:23.9 1.9 572.703674 559.964539 48:24.0 2.0 569.043152 564.845154 48:24.1 2.1 565.38269 564.845154 48:24.2 2.2 565.38269 564.845154 48:24.3 2.3 565.38269 564.845154 48:24.4 2.4 561.722229 562.404846 48:24.5 2.5 565.38269 562.404846 48:24.6 2.6 565.38269 559.964539 48:24.7 2.7 569.043152 564.845154 48:24.8 2.8 565.38269 557.524231 48:24.9 2.9 565.38269 564.845154 48:25.0 3.0 561.722229 557.524231 48:25.1 3.1 565.38269 564.845154 48:25.2 3.2 572.703674 564.845154 48:25.3 3.3 572.703674 562.404846 48:25.4 3.4 572.703674 564.845154 48:25.5 3.5 572.703674 562.404846 48:25.6 3.6 565.38269 562.404846 48:25.7 3.7 569.043152 562.404846 48:25.8 3.8 561.722229 562.404846 48:25.9 3.9 569.043152 562.404846 48:26.0 4.0 565.38269 559.964539 48:26.1 4.1 565.38269 562.404846 48:26.2 4.2 569.043152 564.845154 48:26.3 4.3 558.061768 564.845154 48:26.4 4.4 569.043152 562.404846 48:26.5 4.5 565.38269 564.845154 48:26.6 4.6 572.703674 559.964539 48:26.7 4.7 561.722229 557.524231 48:26.8 4.8 565.38269 559.964539 48:26.9 4.9 565.38269 562.404846 48:27.0 5.0 569.043152 555.083923 48:27.1 5.1 558.061768 559.964539 48:27.2 5.2 569.043152 557.524231 48:27.3 5.3 572.703674 557.524231 48:27.4 5.4 561.722229 555.083923 48:27.5 5.5 565.38269 557.524231 48:27.6 5.6 558.061768 557.524231 48:27.7 5.7 572.703674 552.643616 48:27.8 5.8 561.722229 559.964539 Pilot Cyl Outlet Press (psia) 559.964539 562.404846 569.725769 562.404846 564.845154 569.725769 562.404846 564.845154 567.285461 564.845154 562.404846 569.725769 567.285461 564.845154 562.404846 562.404846 564.845154 564.845154 564.845154 559.964539 562.404846 562.404846 562.404846 567.285461 559.964539 555.083923 562.404846 562.404846 559.964539 559.964539 559.964539 562.404846 562.404846 559.964539 564.845154 557.524231 557.524231 564.845154 564.845154 559.964539 555.083923 559.964539 555.083923 559.964539 559.964539 555.083923 557.524231 Halon 600 psi test for nuclear plants #4 1-26-05.xls Page 2 of 2
Graph 5 Test 5 1-26-05 Chemetron Facility 1-Cyl (Reverse Configuration, Pressure into MPA A and out of B), Manually operated
-1.0
-0.5 0.0 0.5 1.0 1.5 2.0 2.5 3.0
Report on MPA Arrangements for Halon 1301 600 PSI Systems Test date:
1/26/2005 1 pilot cylinder only with pneumatic operator (no slave cylinders)
Manually operated Pilot pressure into "A" and out of "B" on manual actuator (Reverse Configuration)
FM-200 superpressurized with Nitrogen in 1 pilot cylinder Pilot Cyl start pressure (Cyl 1):
560 psig Running Time 00:28.7 00:28.8 00:28.9 00:29.0 00:29.1 00:29.2 00:29.3 00:29.4 00:29.5 00:29.6 00:29.7 00:29.8 00:29.9 00:30.0 00:30.1 00:30.2 00:30.3 00:30.4 00:30.5 00:30.6 00:30.7 00:30.8 00:30.9 00:31.0 00:31.1 00:31.2 00:31.3 00:31.4 00:31.5 00:31.6 00:31.7 00:31.8 00:31.9 00:32.0 00:32.1 00:32.2 00:32.3 00:32.4 00:32.5 00:32.6 00:32.7 Time (sec)
-3.0
-2.9
-2.8
-2.7
-2.6
-2.5
-2.4
-2.3
-2.2
-2.1
-2.0
-1.9
-1.8
-1.7
-1.6
-1.5
-1.4
-1.3
-1.2
-1.1
-1.0
-0.9
-0.8
-0.7
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Pilot Cyl Press (psia) 569.043152 576.364136 572.703674 569.043152 580.024597 587.34552 580.024597 572.703674 580.024597 580.024597 576.364136 583.685059 580.024597 576.364136 587.34552 583.685059 580.024597 583.685059 576.364136 572.703674 580.024597 576.364136 576.364136 580.024597 583.685059 587.34552 576.364136 587.34552 572.703674 569.043152 576.364136 580.024597 576.364136 565.38269 572.703674 572.703674 572.703674 569.043152 576.364136 561.722229 565.38269 Pilot Port Press (psia) 13.334761 18.215384 18.215384 15.775072 15.775072 13.334761 13.334761 18.215384 13.334761 15.775072 8.454137 15.775072 13.334761 20.655695 20.655695 15.775072 8.454137 15.775072 13.334761 13.334761 13.334761 18.215384 15.775072 18.215384 13.334761 13.334761 10.894449 18.215384 18.215384 13.334761 18.215384 74.342552 223.201553 167.074387 254.925613 325.694641 398.903992 455.031158 511.158325 542.882385 559.964539 Pilot Cyl Outlet Press (psla) 15.775072 15.775072 15.775072 18.215384 18.215384 20.655695 18.215384 15.775072 15.775072 18.215384 18.215384 18.215384 15.775072 18.215384 23.096006 20.655695 20.655695 18.215384 15.775072 18.215384 20.655695 20.655695 15.775072 18.215384 20.655695 18.215384 20.655695 18.215384 18.215384 23.096006 18.215384 13.334761 574.606445 567.285461 574.606445 572.166138 572.166138 567.285461 567.285461 567.285461 569.725769 Actuated Manually Pilot Cylinder Valve Opens Halon 600 psi test for nuclear plants #5 1-26-05.xls Page 1 of 2
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Pilot Cyl Press Pilot Port Press Pilot Cyl Outlet Time Time (sec)
(psia)
(psla)
Press (psia) 00:32.8 1.1 569.043152 562.404846 567.285461 00:32.9 1.2 572.703674 567.285461 569.725769 00:33.0 1.3 576.364136 564.845154 567.285461 00:33.1 1.4 561.722229 562.404846 569.725769 00:33.2 1.5 565.38269 564.845154 572.166138 00:33.3 1.6 565.38269 559.964539 564.845154 00:33.4 1.7 569.043152 559.964539 572.166138 00:33.5 1.8 569.043152 562.404846 564.845154 00:33.6 1.9 565.38269 564.845154 567.285461 00:33.7 2.0 569.043152 562.404846 569.725769 00:33.8 2.1 569.043152 562.404846 567.285461 00:33.9 2.2 569.043152 559.964539 567.285461 00:34.0 2.3 569.043152 559.964539 562.404846 00:34.1 2.4 558.061768 562.404846 567.285461 00:34.2 2.5 569.043152 564.845154 564.845154 00:34.3 2.6 565.38269 562.404846 564.845154 00:34.4 2.7 561.722229 559.964539 567.285461 00:34.5 2.8 569.043152 564.845154 562.404846 00:34.6 2.9 554.401306 559.964539 555.083923 00:34.7 3.0 565.38269 562.404846 564.845154 00:34.8 3.1 572.703674 557.524231 567.285461 00:34.9 3.2 561.722229 559.964539 567.285461 00:35.0 3.3 561.722229 559.964539 564.845154 00:35.1 3.4 565.38269 557.524231 569.725769 00:35.2 3.5 565.38269 562.404846 567.285461 00:35.3 3.6 569.043152 562.404846 562.404846 00:35.4 3.7 561.722229 567.285461 562.404846 00:35.5 3.8 561.722229 564.845154 564.845154 00:35.6 3.9 572.703674 562.404846 559.964539 00:35.7 4.0 561.722229 559.964539 557.524231 00:35.8 4.1 565.38269 564.845154 562.404846 00:35.9 4.2 565.38269 557.524231 562.404846 00:36.0 4.3 565.38269 559.964539 562.404846 00:36.1 4.4 569.043152 559.964539 564.845154 00:36.2 4.5 561.722229 555.083923 557.524231 00:36.3 4.6 565.38269 559.964539 559.964539 00:36.4 4.7 565.38269 557.524231 564.845154 00:36.5 4.8 565.38269 557.524231 562.404846 00:36.6 4.9 565.38269 559.964539 562.404846 00:36.7 5.0 561.722229 562.404846 564.845154 00:36.8 5.1 565.38269 555.083923 562.404846 00:36.9 5.2 554.401306 557.524231 562.404846 00:37.0 5.3 565.38269 557.524231 562.404846 00:37.1 5.4 561.722229 557.524231 562.404846 00:37.2 5.5 569.043152 562.404846 564.845154 00:37.3 5.6 561.722229 552.643616 562.404846 00:37.4 5.7 561.722229 555.083923 567.285461 00:37.5 5.8 565.38269 552.643616 562.404846 Halon 600 psi test for nuclear plants #5 1-26-05.xis Page 2 of 2
Graph 6 Test 6 1-26-05 Chemetron Facility 1-Cyl (Reverse Configuration, Pressure into MPA A and out of B ), Manually operated with another MPA l-
_10-.
Time (sec)
Report on MPA Arrangements for Halon 1301 600 PSI Systems Test date:
1/2612005 1 pilot cylinder only with pneumatic operator (no slave cylinders)
Manually operated (Exact same as Test #5, but with another MPA)
Pilot pressure into "A" and out of "B" on manual actuator (Reverse Configuration)
FM-200 superpressurized with Nitrogen in 1 pilot cylinder Pilot Cyl start pressure (Cyl 1):
Running Pilot Time Time (sec) 09:26.3
-3.0 591 09:26.4
-2.9 58(
09:26.5
-2.8 591 09:26.6
-2.7 591 09:26.7
-2.6 58 09:26.8
-2.5 58' 09:26.9
-2.4 58 09:27.0
-2.3 58' 09:27.1
-2.2 58(
09:27.2
-2.1 58 09:27.3
-2.0 58 09:27.4
-1.9 58' 09:27.5
-1.8 594 09:27.6
-1.7 591 09:27.7
-1.6 58 09:27.8
-1.5 58 09:27.9
-1.4 58 09:28.0
-1.3 58 09:28.1
-1.2 58(
09:28.2
-1.1 58 09:28.3
-1.0 58' 09:28.4
-0.9 58' 09:28.5
-0.8 58' 09:28.6
-0.7 58' 09:28.7
-0.6 591 09:28.8
-0.5 591 09:28.9
-0.4 58 09:29.0
-0.3 58(
09:29.1
-0.2 57<
09:29.2
-0.1 59, 09:29.3 0.0 58' 09:29.4 0.1 58' 09:29.5 0.2 57(
09:29.6 0.3 57(
09:29.7 0.4 58' 09:29.8 0.5 56 09:29.9 0.6 57(
09:30.0 0.7 57(
09:30.1 0.8 57(
09:30.2 0.9 58(
09:30.3 1.0 57(
09:30.4 1.1 57(
09:30.5 1.2 56' 560 psig Cyl Press Pilot Port Press Pilot Cyl Outlet (psla) 1.005981
).024597 1.005981 1.005981 3.685059 3.685059 7.34552 3.685059
).024597 7.34552 7.34552 3.685059 1.666443 1.005981 7.34552 3.685059 7.34552 3.685059
).024597 3.685059 3.685059 3.685059 3.685059 3.685059 1.005981 1.005981 7.34552
).024597 2.703674 1.666443 3.685059 3.685059
'.364136 3.364136 3.685059
).043152 3.364136 3.364136
'.364136
).024597 3.364136 3.364136
).043152 (psia) 10.894449 13.334761 13.334761 18.215384 13.334761 10.894449 15.775072 20.655695 15.775072 15.775072 15.775072 15.775072 15.775072 15.775072 13.334761 10.894449 10.894449 18.215384 13.334761 15.775072 10.894449 15.775072 20.655695 10.894449 15.775072 15.775072 13.334761 18.215384 15.775072 13.334761 13.334761 30.416941 191.477509 157.313141 240.283737 320.814026 391.583069 452.590851 501.397064 535.561462 552.643616 562.404846 564.845154 Press (psla) 15.775072 10.894449 15.775072 20.655695 20.655695 18.215384 13.334761 15.775072 20.655695 10.894449 23.096006 15.775072 15.775072 18.215384 18.215384 18.215384 10.894449 20.655695 18.215384 18.215384 15.775072 20.655695 18.215384 13.334761 18.215384 15.775072 15.775072 18.215384 18.215384 18.215384 20.655695 20.655695 599.009521 569.725769 569.725769 577.046753 569.725769 567.285461 572.166138 569.725769 572.166138 569.725769 564.845154 Actuated Manually Pilot Cylinder Valve Opens Halon 600 psi test for nuclear plants #6 1-26-05.xls Page I of 2
Report on MPA Arrangements for Halon 1301 600 PSI Systems Running Pilot Cyl Press Pilot Port Press Pilot Cyl Outlet Time Time (sec)
(psia)
(psia)
Press (psia) 09:30.6 1.3 572.703674 562.404846 564.845154 09:30.7 1.4 572.703674 567.285461 564.845154 09:30.8 1.5 576.364136 559.964539 572.166138 09:30.9 1.6 569.043152 562.404846 564.845154 09:31.0 1.7 569.043152 562.404846 562.404846 09:31.1 1.8 565.38269 562.404846 564.845154 09:31.2 1.9 572.703674 559.964539 564.845154 09:31.3 2.0 572.703674 557.524231 567.285461 09:31.4 2.1 565.38269 557.524231 562.404846 09:31.5 2.2 572.703674 564.8451 54 564.845154 09:31.6 2.3 569.043152 559.964539 567.285461 09:31.7 2.4 572.703674 564.845154 562.404846 09:31.8 2.5 565.38269 557.52423 1 569.725769 09:31.9 2.6 572.703674 562.404846 562.404846 09:32.0 2.7 561.722229 559.964539 564.845154 09:32.1 2.8 576.364136 562.404846 569.725769 09:32.2 2.9 572.703674 562.404846 562.404846 09:32.3 3.0 572.703674 555.083923 564.845154 09:32.4 3.1 569.043152 562.404846 564.845154 09:32.5 3.2 569.043152 564.845154 562.404846 09:32.6 3.3 565.38269 564.845154 564.845154 09:32.7 3.4 569.043152 562.404846 564.845154 09:32.8 3.5 565.38269 559.964539 567.285461 09:32.9 3.6 565.38269 559.964539 564.8451 54 09:33.0 3.7 569.043152 559.964539 559.964539 09:33.1 3.8 565.38269 562.404846 564.8451 54 09:33.2 3.9 565.38269 557.524231 567.285461 09:33.3 4.0 561.722229 559.964539 567.285461 09:33.4 4.1 569.043152 562.404846 559.964539 09:33.5 4.2 569.043152 559.964539 564.845154 09:33.6 4.3 565.38269 562.404846 559.964539 09:33.7 4.4 569.043152 562.404846 564.8451 54 09:33.8 4.5 569.043152 557.524231 564.845154 09:33.9 4.6 561.722229 559.964539 559.964539 09:34.0 4.7 565.38269 555.083923 559.964539 09:34.1 4.8 561.722229 555.083923 562.404846 09:34.2 4.9 565.38269 557.524231 562.404846 09:34.3 5.0 565.38269 552.643616 557.524231 09:34.4 5.1 565.38269 559.964539 564.8451 54 09:34.5 5.2 569.043152 555.083923 559.964539 09:34.6 5.3 565.38269 562.404846 557.524231 09:34.7 5.4 572.703674 557.524231 559.964539 09:34.8 5.5 561.722229 559.964539 559.964539 09:34.9 5.6 565.38269 552.643616 562.404846 09:35.0 5.7 558.061 768 562.404846 557.524231 09:35.1 5.8 561.722229 559.964539 564.845154 09:35.2 5.9 565.38269 555.083923 557.524231 Halon 600 psi test for nuclear plants #6 1-26-05.xlsPae2f Page 2 of 2
Appendix A JLW INSTRUMENTS, INC./METROLOGY CONCEPTS 312.666.0595
- Fax 312.733.0009 452 N. Sangamon, Chicago, IL 60622 CEDITN E-Mall J~w~~y~rPCERT.NO.
1753O01 t l 2 E-MoJ:
l' JATION OF CALIBRATION 002744 PREPARED FOR CHEMETRON FIRE SYSTEMS CERTIFICATE NUMBER:
H2004-11 TRACKING NUMBER:
M11807-2 REFERENCE NO: PENDING QA NUMBER:
I.D. NUMBER:
JLW INSTRUMENTS, INC. CERTIFIES THAT THIS INSTRUMENT HAS BEEN CALIBRATED USING PUBLISHED AND RECOGNIZED METROLOGICAL THEORIES AND PRACTICES. THIS REPORT WAS MADE BY DIRECT COMPARISON WITH JLW STANDARDS THAT ARE TRACEABLE TO NIST (NATIONAL INSTITUTE OF STANDARDS & TECHNOLOGY).
CALIBRATIONS ARE CONDUCTED BY QUALIFIED PERSONNEL IN AN ENVIRONMENTALLY MONITORED LABORATORY.
THE CALIBRATION OF THIS INSTRUMENT MEETS APPLICABLE PROCEDURES AND REQUIREMENTS OF ISOIIEC 17025, (ANSI/NCSL Z540-1)PURSUANT TO A2LA ACCREDITATION CERTIFICATE NUMBER 1753.01.
TESTED WITH CERTIFIED STANDARDS TRACEABLE TO NIST REPORT NUMBERS:
DH 5304 SIN 3717 / 2911 CERTIFIED:/106/03 DUE DATE: 11106/05 NIST CERTIFICATE NUMBERS:
838/258930-97 & 822/259693-98.
OHAUS GT-410 S/N3886 CERTIFIED: 1-14-04 DUE DATE:1-14-05; NIST CERTIFICATE NUMBER:
822/260017-98.
A&D BALANCE GX-6100 CERTIFIED: 1-14-04 DUE DATE:1-14-05 NIST CERTIFICATE NUMBER:
822/260017-98.
WEIGHT SET, WLSB/10 CERTIFIED: 11/03/03 DUE DATE: 11/02/04 NIST CERTIFICATE NUMBERS:
822/260017-98 HYDRAULIC DEAD WEIGHT TESTER PROCEDURE JLW-002 s Certificate with data (cross-float)
El Area determination
[3 Adjustment to local gravity MFG:AMETEK MODEL:R-50 S/N 7953 ACCURACY 0.1% RDG MEDIA OIL AM PISTONS WG-89 # 12484; W/C-5 psi; RANGE 30-500 psi x 5 psi.
PISTON:
WG-92 # 28465; W/C-50 psi; RANGE: 250-5000 psi x 50 psi.
AMBIENT CONDITIONS AT JLW INSTRUMENTS DURING TEST PROCEDURE WERE AS FOLLOWS:
1-28-2004 RH: 29.4 BP:
1001 mbar TEMP: 20.6 °C GRAVITY: 9.80296 m/sA2 PRESSURE READINGS REFERENCED TO A GRAVITY OF 9.80665 m/sA2 TESTER WAS IN TOLERANCE IN THE AS FOUND CONDITION.
CERTIFIED TO AN ACCURACY OF 0.1% RDG (UNCERTAINTY: Cross Float 76.8ppm/psi.)
PRESSURE REFERENCE LINE: CALIBRATION REFERENCE LINE IS ON THE WEIGHT TUBE.
CERTIF1CATIDATl04 RECALIBiATION DATE:
1-28-2005 LEV KHODOSH, DIRECTM OP'METROLOGY WAYNE FET`MAN, DIkECTOR L3 rev.1/06/04
-This document shall not be reproduced except in full without the written approval of JLW Instruments Metrology Laboratory.-
JLW INSTRUMENTS9 INC./METROLOGY CONCEPTS 312.666.0595 v Fox 312.733.0009 452 N. Sangamon. Chicago. IL 60622 E-Mail: JlwI3lwlnstruments.com CERTIFIED TEST DATA MODEL R-50 S/N 7953 H2004-11 ACCUR WG-89 PISTON: 0.1% RDG or 0.05 psi BELOW 50 psi.
WG-92 PISTON: 0.1 % RDG or 0.5 psi. BELOW 500 psi.
UNCERTAINTY(cross-float.)76.gppm/psi.
H2744FL4 1-28-04 002744 AS FOUND AND AS LEFT ( PISTON WG-89 # 12484 TESTED WITH DH 5304FTS )
POINT 1
2 3
4 5
6 7
8 9
10 MASS LOAD kg 0.29894 0.49888 0.99883 1.04870 1.99900 2.49900 2.99919 3.99990 4.04990 4.99950 TEMP oC 19.54 19.54 19.54 19.54 19.56 19.59 19.61 19.61 19.64 19.67 PRESSURE psi 30.0217 50.0168 100.0122 104.9989 200.0293 250.0298 300.0499 400.1208 405.1208 500.0811 UUT psi 30 50 100 105 200 250 300 400 405 500 ACCURACY 0.072 0.034 0.012 0.001 0.015 0.012 0.017 0.030 0.030 0.016 WEIGHT COMBINATION W/C-5psi;5;9 W/C-5psi 5;6;9; W/C-5psi ;1 W/C-5psi:1 ;9 W/C-Spsi;1 ;2; W/C-5psi; 1-2;7-10 W/C-5psi;1 -3 W/C-5psi;1-4 W/C-5psi;1-4;9 W/C-Spsi;1-12 AS FOUND AND AS 11 2.49964 12 5.00080 13 9.99890 14 10.49890 15 20.00249 16 25.00590 17 30.00969 18 40.01450 19 40.51456 20 50.01699 LEFT ( PISTON WG-92 # 28465 TESTED 19.74 19.85 20.00 20.03 20.15 20.23 20.36 20.44 20.46 20.54 250.0897 500.2113 1000.0200 1050.0190 2000.3670 2500.6960 3001.0600 4001.4062 4052.3912 5001.6960 250 500 1000 1050 2000 2500 3000 4000 4051 5000 0.036 0.042 0.002 0.002 0.018 0.028 0.035 0.035 0.034 0.034 WITH DH 5304FTS)
W/C-50psi;5 W/C-50psi;5;6;9 W/C-50psi;1 WlC-50psi;1 ;9 W/C-50psi; 1-2 W/C-50psi;1-2;7-10 W/C-50psi;1 -3 W/C-50psi;1-4 W/C-50psi;1-4;9 WIC-50psi;1 -12
- OUT OF TOLERANCE COMMENTS:
TESTER IN TOLERANCE "AS FOUND".
PISTONS WERE TESTED IN AM OIL.
DROP TIME IN MA OIL WG-89 PISTON > 5 min. (JLWS SPEC'S = 5 min.).
DROP TIME IN MA OIL WG-92 PISTON > 3 min. (JLWS SPEC'S = 3 min.).
HEIGHT BETWEEN REFERENCE LEVEL OF UUT FOR WG-89 PISTON AND FTS= -3.9 in.
HEIGHT BETWEEN REFERENCE LEVEL OF UUT FOR WG-92 PISTON AND FTS= -3.9 in.
HYDRAULIC DEADWEIGHT MASS AND UNCERTAINTY REPORT Date 1-28-2004 Mfg AMETEK Tester Model R-50 Test# H2004-11 Tester StN 7953 Weight SIN 7953 Accuracy 0 1% RDG Gravity 9 80665 Qty Weights 12 Air Density 1*18440 ToC 206 BPmBar 1001 RH % 29.4 P.O.# PFNDING Control# on2744 Shop Order# M11807-2 Customer CHFMFTRON FIRE SYSTFMS-KlDDF-FFNWAL INC WEIGHT DESIGNATIONS AO r^Iltlr%
V AC I ~r Pi~
VJLU[4LJ O I
L.Lr I Mtg9 Weight PIN Nom. Pressure Weight
- Apparent Mass (g)
Density
- Apparent Mass g) Density 1
WG-26 95/950 psi 1
1 4308.696 6700.0 3
WG-27 100/1000 psi 2-4 2
4537.176 6700.0 4
WG-25 20/200 psi 5-8 3
4535.966 6700.0 4
WG-23 5/50 psi 9-12 4
4538.486 6700.0 5
907.719 6700.0-6 907.659 6700.0 7
907.599 6700.0 8
907.679 6700.0 9
226.872 6700.0 10 226.997 6700.0 11 226.975 6700.0
=
12 226.965 6700.0 H7953
=
WK002744.TXT
=
Balances Used:
WeightsT UncertaintyT MfgJ Model #
SN#
Range
(#s)
Ohaus GT410; # 3866; 410 g x 0.001g or 2 ppm h -12 Mettler H315; # F82572; 1 kg x 0.00019 or 0.5 ppm h A&D GX-6100; #14512835; 610Og x 0.01g or 10 ppm h 1-8 x=8nPrng MettlerPR 10003;#1117383610; 10kgx0.001g or I ppm h
Mettler PK 16MC: #40100-01; 16 kg x 0.01g or 20 ppm p Steel (st) Wt #s Zinc Alloy Wt #s 1-12 U,8 mass=2[(B/2)1+(S1,)2J'-
U,=the 95confidence uncertainty Brass (b) Wt #s Aluminum Wt#s 1_
B=the systematic uncert. of the insrument S,,= the random uncertainty.
Sub-Assy.
Quantitv MASS / UNCERTAINTY Carrier 1
112.049g Weight Tube 1
86.275 g Piston WG-89 1
8.381 g Piston WG-92 1
8.370 g Car.+W.T.+Pist.
L 5 lb 26.710 g Car.+W.T.+ Pist. H 50 lb 26.695 g Uncertainty of Piston (mass) ppm I mg 2ppm x4=8ppmlmg Mass Uncertainty at Full Range ppm I psi 96 ppmlmg=8.5ppmlpsi Uncert. DH5304 (Std) ppm I psi 76ppmlpsi Ambient Conditions Uncertainty*
ppm I psi 7.5ppmlpsi Total Combined Uncertainty" U95 76.8ppm/psi O Uncertainty (Area)
E
- (Temp;RH;BP;H Ret; Grav.)Root Sum of Squares(RSS) Performed By-Ley Khodosh.
Ml rev. 5/17/02 E Uncertainty (Cross-float)
Approved By-Waye Flman1