ML18096B330: Difference between revisions
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Protection from turbine excessive overspeed is required since excessive overspeed of the turbine could generate potentially damaging missiles which could impact and damage safety-related components, equipment or structures. | Protection from turbine excessive overspeed is required since excessive overspeed of the turbine could generate potentially damaging missiles which could impact and damage safety-related components, equipment or structures. | ||
The overspeed protection instrumentation consists of five solenoid valves and one trip mechanism which can be grouped into three independent systems. These are: 1. Mechanical Overspeed Trip The mechanical overspeed trip valve will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. . SALEM -UNIT 2 B 3/4 3-3 February 11, 1993 INSTRQMimTATION | The overspeed protection instrumentation consists of five solenoid valves and one trip mechanism which can be grouped into three independent systems. These are: 1. Mechanical Overspeed Trip The mechanical overspeed trip valve will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. . SALEM -UNIT 2 B 3/4 3-3 February 11, 1993 INSTRQMimTATION | ||
*BASES 3/4.3.4 TURBINE OVERSPEED PROTECTION (continued) | *BASES 3/4.3.4 TURBINE OVERSPEED PROTECTION (continued) | ||
: 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two _solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips. The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller Either of the two overspeed protection control solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit 2 turbine is operated at full time, full arc admission. | : 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two _solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips. The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller Either of the two overspeed protection control solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit 2 turbine is operated at full time, full arc admission. | ||
To prevent excessive steam flow induced cyclic stresses of the control stage blading, perform turbine valve testing in accordance with manufacturer's recommendations. | To prevent excessive steam flow induced cyclic stresses of the control stage blading, perform turbine valve testing in accordance with manufacturer's recommendations. | ||
| Line 45: | Line 45: | ||
To prevent double shocking the turbine, perform turbine valve testing in accordance with manufacturer's recommendations. | To prevent double shocking the turbine, perform turbine valve testing in accordance with manufacturer's recommendations. | ||
SALEM -UNIT 1 B 3/4 3-4 February 11, 1993 INSTRUMENTATION BASES ============================================================================== | SALEM -UNIT 1 B 3/4 3-4 February 11, 1993 INSTRUMENTATION BASES ============================================================================== | ||
3/4.3.4 TURBINE OVERSPEED PROTECTION | 3/4.3.4 TURBINE OVERSPEED PROTECTION | ||
{continued) | {continued) | ||
During normal operation, turbine valve testing is performed at a frequency consistent with the methodology presented in WCAP-11525, "Probabilistic Evaluation of Reduction in Turbine Valve Frequency." This report evaluates the contribution of failure or unavailability of the turbine valve safety function to the probability that the turbine will overspeed and eject a missile. It concludes that extended intervals between turbine valve functional tests can be achieved without exceeding the NRC acceptance criteria for the probability of a turbine missile ejection incident. | During normal operation, turbine valve testing is performed at a frequency consistent with the methodology presented in WCAP-11525, "Probabilistic Evaluation of Reduction in Turbine Valve Frequency." This report evaluates the contribution of failure or unavailability of the turbine valve safety function to the probability that the turbine will overspeed and eject a missile. It concludes that extended intervals between turbine valve functional tests can be achieved without exceeding the NRC acceptance criteria for the probability of a turbine missile ejection incident. | ||
| Line 62: | Line 62: | ||
-... * | -... * | ||
* INSTRUMENTATION BASES ============================================================================== | * INSTRUMENTATION BASES ============================================================================== | ||
3/4.3.4 TURBINE OVERSPEED PROTECTION (continued) | 3/4.3.4 TURBINE OVERSPEED PROTECTION (continued) | ||
: 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the .oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips. The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller Either of the two overspeed protection control solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit 2 turbine is operated at full time, full arc admission. | : 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the .oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips. The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller Either of the two overspeed protection control solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit 2 turbine is operated at full time, full arc admission. | ||
To prevent excessive steam flow induced cyclic stresses of the control stage blading, perform turbine valve testing in accordance with manufacturer's recommendations. | To prevent excessive steam flow induced cyclic stresses of the control stage blading, perform turbine valve testing in accordance with manufacturer's recommendations. | ||
Revision as of 14:49, 25 April 2019
| ML18096B330 | |
| Person / Time | |
|---|---|
| Site: | Salem  |
| Issue date: | 02/25/1993 |
| From: | Public Service Enterprise Group |
| To: | |
| Shared Package | |
| ML18096B329 | List: |
| References | |
| NUDOCS 9303110421 | |
| Download: ML18096B330 (9) | |
Text
ATTACHMENT 1 TECHNICAL SPECIFICATION BASES REVISED PAGES SALEM UNITS 1 AND 2 ---------------
, 9303110421 930225 -' PDR ADOCK 05000272 p* PDR INSTRQMBNTATION BASES ==============================================================================
3/4.3.4 'I'ORBINE OVERSPEED PROTECTION This specification is provided to ensure that the turbine overspeed protection instrumentation and the turbine speed control valves are OPERABLE and will protect the turbine from excessive overspeed.
Protection from turbine excessive overspeed is required since excessive overspeed of the turbine could generate potentially damaging missiles which could impact and damage safety-related components, equipment or structures.
The overspeed protection instrumentation consists of five solenoid valves and one trip mechanism which can be grouped into three independent systems. These are: 1. Mechanical Overspeed Trip_ The mechanical overspeed trip valve will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips: The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller lither of the two overspeed protection control solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit l turbine is operated at full time, partial arc admission.
To prevent double shocking the turbine, perform turbine valve testing in accordance with manufacturer's recommendations.
SALEM -UNIT 1 B 3/4 3-4 February 11 , 19 9 3 INSTRQMBNTATION BASES ==============================================================================
3/4.3.4 TURBINE OVERSPEED PROTECTION (continued)
During normal operation, turbine valve testing is performed at a frequency consistent with the methodology presented in WCAP-11525, "Probabilistic Evaluation of Reduction in Turbine Valve Frequency." This report evaluates the contribution of failure or unavailability of the turbine valve safety function to the probability that the turbine will overspeed and eject a missile. It concludes that extended intervals between turbine valve functional tests can be achieved without exceeding the NRC acceptance criteria for the probability of a turbine missile ejection incident.
Factors which affect the selected valve test interV-al include low pressure.turbine rotor type and inspection interval; turbine valve type, arrangement and overspeed controls; and secondary side water chemistry.
SALEM -UNIT 1 B 3/4 3-5 February 11, 199!
INSTRQMENTATION BASES ==============================================================================
3/4.3.3.8 RADIOACTIVE LIQUID EFFLUENT MONITORING INSTRUMENTATION The radioactive liquid effluent instrumentation is provided to monitor and control, as applicable, the releases of radioactive materials in liquid effluents during actual or potential releases of liquid effluents.
The alarm/trip setpoints for these instruments shall be calculated and adjusted in accordance with the procedures in the ODCM to ensure that the alarm/trip will occur p.rior to exceeding the limits of 10 CFR Part 20. The OPERABILITY and use*
- of this instrumentation is consistent with the requirements of General Design Criteria 60, 63, and 64 of Appendix A to 10 CFR Part SO. The purpose of tank level indicating devices is to assure the detection and control of leaks that if not controlled could potentially result in the transport of radioactive materials to UNRESTRICTED AREAS. 3/4.3.3.9 RADIOACTIVE GASEOUS EFFLUENT MONITQRING INSTRUMENTATION The radioactive gaseous effluent instrumentation is provided to monitor and control, as applicable, the releases of radioactive materials in gaseous effluents during actual or potential releases of gaseous effluents.
The alarm/trip setpoints for these instruments shall be calculated and adjusted in accordance with the procedures in the ODCM to ensure that the alarm/trip will occur prior to exceeding the limits of 10 CFR Part 20. This instrumentation also includes provisions for monitoring (and controlling) the concentrations of potentially explosive gas mixtures in the waste gas holdup system. The OPERABILITY and use of this instrumentation is consistent with the requirements of General Design Criteria 60, 63, and 64 of Appendix A to 10 CFR Part so. 3/4.3.4 T!JRBINE OVER8PBBD PROTECTION This specification is provided to ensure that the *turbine overspeed protection instrumentation and the turbine speed control valves are OPERABLE and will protect the turbine from excessive overspeed.
Protection from turbine excessive overspeed is required since excessive overspeed of the turbine could generate potentially damaging missiles which could impact and damage safety-related components, equipment or structures.
The overspeed protection instrumentation consists of five solenoid valves and one trip mechanism which can be grouped into three independent systems. These are: 1. Mechanical Overspeed Trip The mechanical overspeed trip valve will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. . SALEM -UNIT 2 B 3/4 3-3 February 11, 1993 INSTRQMimTATION
- BASES 3/4.3.4 TURBINE OVERSPEED PROTECTION (continued)
- 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two _solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips. The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller Either of the two overspeed protection control solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit 2 turbine is operated at full time, full arc admission.
To prevent excessive steam flow induced cyclic stresses of the control stage blading, perform turbine valve testing in accordance with manufacturer's recommendations.
During normal power operation, turbine valve testing is performed at a frequency consistent with the methodology presented in WCAP-*11525, "Probabilistic Evaluation of Reduction in Turbine Valve Test Frequency." This report evaluates the contribution of failure or unavailability of the turbine valve safety function to the probability that the turbine will overspeed and eject a missile. It concludes that extended intervals between turbine valve functional tests can be achieved without exceeding_the NRC acceptance criteria for the probability of a turbine missile ejection incident.
Factors which af.fect the selected valve test interval include low pressure turbine rotor type and inspection*interval; turbine valve type, arrangement and overspeed control; and secondary side water chemistry.
SALEM -UNIT 2 B 3/4 3-4 February 11, 1993 INSTRUMENTATION BASES ============================================================================== . 3/4.3.4 TURBINE OVERSPEED PROTECTION This specification is provided to ensure that the turbine overspeed protection instrumentation and. the turbine speed control valves are OPERABLE and will protect the turbine from excessive overspeed.
Protection from turbine excessive overspeed is required since excessive overspeed of the turbine could generate potentially damaging missiles which could impact and damage safety-related components, equipment or structures.
The overspeed protection instrumentation consists of five solenoid valves and one trip mechanism which can be grouped into three independent systems. These are: 1. Mechanical Overspeed Trip The mechanical overspeed trip valve will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips. The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller Either of the two overspeed protection control. solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit 1 turbine is operated at full time, partial arc admission.
To prevent double shocking the turbine, perform turbine valve testing in accordance with manufacturer's recommendations.
SALEM -UNIT 1 B 3/4 3-4 February 11, 1993 INSTRUMENTATION BASES ==============================================================================
3/4.3.4 TURBINE OVERSPEED PROTECTION
{continued)
During normal operation, turbine valve testing is performed at a frequency consistent with the methodology presented in WCAP-11525, "Probabilistic Evaluation of Reduction in Turbine Valve Frequency." This report evaluates the contribution of failure or unavailability of the turbine valve safety function to the probability that the turbine will overspeed and eject a missile. It concludes that extended intervals between turbine valve functional tests can be achieved without exceeding the NRC acceptance criteria for the probability of a turbine missile ejection incident.
Factors which affect the selected valve test interval include low pressure turbine rotor type and inspection interval; turbine valve type, arrangement and overspeed controls; and secondary side water chemistry.
SALEM -UNIT 1 B 3/4 3-5 February 11, 1993
.. INSTRUMENTATION BASES ==============================================================================
3/4.3.3.8 RADIOACTIVE LIQUID EFFLUENT MONITORING INSTRUMENTATION The radioactive liquid effluent instrumentation is provided to monitor and control, as applicable, the releases of radioactive materials in liquid effluents during actual or potential releases of liquid effluents.
The alarm/trip setpoints for these instruments shall be calculated and adjusted in accordance with the procedures in the ODCM to ensure that the alarm/trip will occur p.rior to exceeding the limits of 10 CFR Part 20. The OPERABILITY and use of this instrumentation is consistent with the requirements of General Design Criteria 60, 63, and 64 of Appendix A to 10 CFR Part SO. The purpose of tank level indicating devices is to assure the detection and control of leaks that if not controlled could potentially result in the transport of radioactive materials to UNRESTRICTED AREAS.
RADIOACTIVE GASEOUS EFFLUENT MONITORING INSTRUMENTATION The radioactive gaseous effluent instrumentation is provided to monitor and control, as applicable, the releases of radioactive materials in gaseous. effluents during actual or potential releases of gaseous effluents.
The alarm/trip setpoints for these instruments shall be calculated and adjusted in accordance with the procedures in the ODCM to ensure that the alarm/trip will occur prior to exceeding the limits of 10 CFR Part 20. This instrumentation also includes provisions for monitoring (and controlling) the concentrations of potentially explosive gas mixtures in the waste gas holdup sys.tern.
The OPERABILITY and use of this instrumentation is consistent with the requirements of Gene.ral Design Criteria 60 63, and 64 of Appendix A to 10 CFR Part 50. 3/4.3.4 TURBINE OVERSPEED PROTECTION This specification is provided to ensure that the turbine overspeed protection instrumentation and the turbine speed control valves are OPERABLE and will protect the turbine from excessive ove*rspeed.
Protection from turbine excessive overspeed is required since excessive overspeed of the turbine could generate potentially damaging missiles which could impact and damage safety-related components, equipment or structures.
The overspeed protection instrumentation consists of five solenoid valves and orie trip mechanism which cari be grouped into three independent systems. These are: 1. Mechanical Overspeed Trip The mechanical overspeed trip valve will dump the autostop oil. The dump of the autostop oil will open the oil operated interface valve to dump the emergency electro-hydraulic trip fluid. SALEM -UNIT 2 B 3/4 3-3 February 11, 1993
-... *
- INSTRUMENTATION BASES ==============================================================================
3/4.3.4 TURBINE OVERSPEED PROTECTION (continued)
- 2. Electrical Overspeed Trip The electrically sensed overspeed will trip two solenoid valves either of which will dump the autostop oil. The dump of the autostop oil will open the .oil operated interface valve to dump the emergency electro-hydraulic trip fluid. The solenoid valves associated with the electrical overspeed are also energized by the various generator protection trips. The dump of the autostop oil will actuate a solenoid to dump the emergency electro-hydraulic trip fluid. This solenoid serves as a backup for both the mechanical and electrical overspeed trips. The backup solenoid is also energized by the various generator protection trips. 3. Overspeed Protection Controller Either of the two overspeed protection control solenoid dump valves will dump the control electro-hydraulic trip fluid from the governor and intercept valves. When turbine speed decreases, and the overspeed condition clears, the signal is removed and the governor and intercept valves reopen. Salem Unit 2 turbine is operated at full time, full arc admission.
To prevent excessive steam flow induced cyclic stresses of the control stage blading, perform turbine valve testing in accordance with manufacturer's recommendations.
During normal power turbine valve testing is performed at a frequency consistent with the methodology presented in WCAP-11525, "Probabilistic Evaluation of Reduction in Turbine Valve Test Frequency." This report evaluates the contribution of failure or unavailability of the turbine valve safety function to the probability that the turbine will overspeed and eject a missile. It concludes that extended intervals between turbine valve functional tests can be achieved without exceeding the NRC acceptance criteria for the probability of a turbine missile ejection incident.
Factors which affect the selected valve test interval include low pressure turbine rotor type and inspection interval; turbine valve type, arrangement and overspeed control; and secondary side water chemistry.
SALEM -UNIT 2 B 3/4.3-4 February 11, 1993