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CN115127824B - A method for troubleshooting power turbine speed control of a marine gas turbine - Google Patents

A method for troubleshooting power turbine speed control of a marine gas turbine Download PDF

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CN115127824B
CN115127824B CN202210814295.0A CN202210814295A CN115127824B CN 115127824 B CN115127824 B CN 115127824B CN 202210814295 A CN202210814295 A CN 202210814295A CN 115127824 B CN115127824 B CN 115127824B
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power turbine
speed
stop
fault
turbine speed
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CN115127824A (en
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魏昌淼
曹春荣
邹振宇
俞健
唐祖定
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703th Research Institute of CSIC Wuxi Branch
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703th Research Institute of CSIC Wuxi Branch
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00Testing of engines
    • G01M15/14Testing gas-turbine engines or jet-propulsion engines
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

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  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Turbines (AREA)

Abstract

本申请公开了一种船用燃气轮机的动力涡轮转速控制故障排查方法,涉及船用燃气轮机领域,该方法只要检测到动力涡轮的输出轴出现刹车故障时,即确定控制机动力涡轮转速的测量通道出现故障;而当确定动力涡轮出现超速故障停机,基于控制机动力涡轮转速和监测机动力涡轮转速的转速大小,根据动力涡轮转速控制故障发生的具体现象,指明了了针对性的排查方法,该方法实用,可高效排查燃气轮机动力涡轮转速控制故障,对恢复燃气轮机稳定运行具有重要意义。

The present application discloses a method for troubleshooting a power turbine speed control fault of a marine gas turbine, and relates to the field of marine gas turbines. The method determines that a fault occurs in a measurement channel of a power turbine speed control unit as long as a brake fault is detected in an output shaft of the power turbine; and when it is determined that the power turbine shuts down due to an overspeed fault, a targeted troubleshooting method is indicated based on the speed of the power turbine of the control unit and the speed of the power turbine of the monitoring unit, and according to the specific phenomenon of the power turbine speed control fault. The method is practical, can efficiently troubleshoot a power turbine speed control fault of a gas turbine, and is of great significance for restoring the stable operation of the gas turbine.

Description

Power turbine rotating speed control fault investigation method of marine gas turbine
Technical Field
The application relates to the field of marine gas turbines, in particular to a power turbine rotating speed control fault checking method of a marine gas turbine.
Background
The gas turbine is a power output device, the marine gas turbine adopts a power turbine to output kinetic energy, and the free end of the power turbine is connected with a gear box. The power turbine rotating speed control fault often occurs in the operation process of the gas turbine, the cause of the power turbine rotating speed control fault possibly is more, the current problems that the power turbine rotating speed control fault is difficult to be effectively and quickly checked and repaired are solved, on one hand, the stable operation of the gas turbine is caused to be a great hidden trouble, and on the other hand, the operation of the gas turbine cannot be recovered as soon as possible, so that the working efficiency of the gas turbine is affected.
Disclosure of Invention
The inventor provides a power turbine rotating speed control fault checking method of a marine gas turbine aiming at the problems and the technical requirements, and the technical scheme of the application is as follows:
a power turbine speed control troubleshooting method of a marine gas turbine, the method comprising:
in the running process of the marine gas turbine, when the output shaft of the power turbine has a brake fault, determining that a measuring channel for controlling the rotation speed N 3c of the power turbine has a fault;
When the power turbine is in overspeed fault shutdown, if the power turbine has overspeed fault shutdown, determining a corresponding fault detection result according to the rotation speed relation among the power turbine rotation speed N 3c of the controller, the power turbine rotation speed N 3m of the monitor and the shutdown rotation speed N 3_stop, and if the power turbine has overspeed limiter detection signals, determining a corresponding fault detection result according to the detection result of the overspeed limiter detection signals of the power turbine, and according to the rotation speed relation among the power turbine rotation speed N 3c of the controller, the power turbine rotation speed N 3m of the monitor and the shutdown rotation speed N 3_stop, wherein N 3_check is a rotation speed detection value.
According to a further technical scheme, when N 3<N3_check is adopted, the method for determining the corresponding fault detection result comprises the following steps:
When the power turbine rotating speed N 3m is inconsistent with the power turbine rotating speed N 3c, determining a collection channel of the power turbine rotating speed with faults according to the shutdown rotating speed N 3_stop;
When the monitored power turbine speed N 3m is consistent with the controller power turbine speed N 3c, determining that the power turbine overspeed limiter fails or that the power turbine speed N 3 fails according to the shutdown speed N 3_stop.
The further technical scheme is that the acquisition channel for determining the power turbine rotating speed with faults according to the shutdown rotating speed N 3_stop comprises the following steps:
When N 3c≥N3_stop and N 3m are in the corresponding working range, determining that a fault exists in the acquisition channel of the power turbine rotating speed N 3c of the controller;
When N 3m≥N3_stop and N 3c are in the corresponding working ranges, the collection channel of the power turbine rotating speed N 3m of the monitoring machine is determined to be faulty.
The further technical scheme is that when the power turbine rotation speed N 3m of the monitoring machine is consistent with the power turbine rotation speed N 3c of the control machine:
If N 3c<N3_stop、N3m<N3_stop is reached, determining that the overspeed limiter of the power turbine fails;
If N 3c≥N3_stop、N3m≥N3_stop, it is determined that the overspeed fault exists in the power turbine speed N 3.
According to a further technical scheme, when N 3≥N3_check is adopted, the method for determining the corresponding fault detection result comprises the following steps:
If the checking result of the power turbine overspeed limiter checking signal indicates that the power turbine overspeed limiter checking signal is in a normal state, determining a collection channel of the power turbine rotating speed with faults or determining that overspeed faults exist in the power turbine rotating speed N 3 according to the monitoring power turbine rotating speed N 3m, the control power turbine rotating speed N 3c and the stopping rotating speed N 3_stop;
If the checking result of the power turbine overspeed limiter checking signal indicates that the power turbine overspeed limiter checking signal is in an abnormal state, determining that the power turbine overspeed limiter fails according to the monitored power turbine rotation speed N 3m, the control power turbine rotation speed N 3c and the shutdown rotation speed N 3_stop.
The further technical proposal is that when the power turbine overspeed limiter check signal is in a normal state:
If the power turbine rotating speed N 3m is inconsistent with the power turbine rotating speed N 3c, determining a collection channel of the power turbine rotating speed with faults according to the shutdown rotating speed N 3_stop;
If the monitored power turbine speed N 3m is consistent with the controller power turbine speed N 3c and N 3c≥N3_stop、N3m≥N3_stop, then an overspeed fault is determined to exist in the power turbine speed N 3.
The further technical scheme is that the acquisition channel for determining the power turbine rotating speed with faults according to the shutdown rotating speed N 3_stop comprises the following steps:
If N 3c≥N3_stop and N 3m are in the corresponding rotating speed range, determining that a measuring channel of the power turbine rotating speed N 3c of the controller fails;
If N 3m≥N3_stop and N 3c are in the corresponding rotation speed range, determining that a measuring channel for monitoring the power turbine rotation speed N 3m fails.
The further technical proposal is that when the power turbine overspeed limiter check signal is in an abnormal state:
If the monitored power turbine speed N 3m is consistent with the controller power turbine speed N 3c and N 3c<N3_stop、N3m<N3_stop, then the power turbine overspeed limiter is determined to be faulty.
The beneficial technical effects of the application are as follows:
The application discloses a power turbine rotating speed control fault investigation method of a marine gas turbine, which is based on the rotating speed of a power turbine and the rotating speed of a power turbine, and specific phenomena of the power turbine rotating speed control fault are indicated according to the rotating speed of the power turbine.
Drawings
FIG. 1 is a graphical illustration of troubleshooting results for various parameters when a power turbine speed control failure occurs in a marine gas turbine, in accordance with one embodiment of the present application.
Detailed Description
The following describes the embodiments of the present application further with reference to the drawings.
The application discloses a power turbine rotating speed control fault checking method of a marine gas turbine, and the method is shown in a flow chart shown in FIG. 1
In the operation process of the marine gas turbine, when the output shaft of the power turbine has a brake fault, the fault of a measuring channel of the power turbine rotating speed N 3c of the controller is directly determined, and the measuring channel of the power turbine rotating speed N 3c of the controller, including a corresponding rotating speed sensor, is to be checked.
In the operation process of the marine gas turbine, when the power turbine is in overspeed fault shutdown, the power turbine is divided into the following two types according to the rotation speed N 3 of the power turbine when the fault occurs:
1. If the power turbine rotating speed N 3<N3_check is the same as the power turbine rotating speed N 3c, the power turbine rotating speed N 3m and the shutdown rotating speed N 3_stop, the corresponding fault detection result is determined according to the rotating speed relation of the power turbine rotating speed N 3c, the power turbine rotating speed N 3m and the shutdown rotating speed N 3_stop. N 3_check is a rotation speed check value. The method for determining the corresponding fault detection result comprises the following steps:
When the power turbine rotating speed N 3m is inconsistent with the power turbine rotating speed N 3c, determining a collection channel of the power turbine rotating speed with faults according to the shutdown rotating speed N 3_stop. Specific:
(1.1) when N 3c≥N3_stop and N 3m are within the corresponding operating ranges, determining that there is a fault in the collection channel of the power turbine speed N 3c of the controller, and checking the collection channel of the power turbine speed N 3c of the controller, including the corresponding speed sensor.
(1.2) When N 3m≥N3_stop and N 3c are within the corresponding operating ranges, determining that the collection channel monitoring the power turbine speed N 3m fails, the collection channel monitoring the power turbine speed N 3m should be monitored, including the corresponding speed sensor.
When the monitored power turbine speed N 3m is consistent with the controller power turbine speed N 3c, determining that the power turbine overspeed limiter fails or that the power turbine speed N 3 fails according to the shutdown speed N 3_stop. Specific:
(1.3) if N 3c<N3_stop、N3m<N3_stop, determining that the power turbine overspeed limiter fails, checking the power turbine overspeed limiter and a rotating speed acquisition channel thereof, wherein the rotating speed acquisition channel comprises a corresponding rotating speed sensor.
(1.4) If N 3c≥N3_stop、N3m≥N3_stop, determining that the actual overspeed fault exists in the power turbine rotating speed N 3, and checking mechanical facilities such as a controllable pitch propeller and the like.
2. If the power turbine rotating speed N 3≥N3_check is at fault, firstly checking the checking signal of the overspeed limiter of the power turbine, and determining the corresponding fault checking result according to the checking result of the checking signal of the overspeed limiter of the power turbine and the rotating speed relation of the power turbine rotating speed N 3c of the controller, the power turbine rotating speed N 3m of the monitor and the shutdown rotating speed N 3_stop.
If the checking result of the power turbine overspeed limiter checking signal indicates that the power turbine overspeed limiter checking signal is in a normal state, a collection channel of the power turbine rotating speed with faults is determined according to the monitoring power turbine rotating speed N 3m, the control power turbine rotating speed N 3c and the stopping rotating speed N 3_stop, or overspeed faults are determined to exist in the power turbine rotating speed N 3. Specific:
If the monitored power turbine rotating speed N 3m is inconsistent with the controller power turbine rotating speed N 3c, determining a collection channel of the power turbine rotating speed with faults according to the shutdown rotating speed N 3_stop:
(2.1) if N 3c≥N3_stop and N 3m are in the corresponding rotational speed ranges, determining that the measuring channel of the power turbine rotational speed N 3c of the controller fails.
(2.2) If N 3m≥N3_stop and N 3c are in the corresponding rotational speed ranges, determining that the measuring channel of the power turbine rotational speed N 3m of the monitor has a fault.
(2.3) If the monitored power turbine speed N 3m is consistent with the controller power turbine speed N 3c, and N 3c≥N3_stop、N3m≥N3_stop, determining that an overspeed fault exists in the power turbine speed N 3.
If the checking result of the power turbine overspeed limiter checking signal indicates that the power turbine overspeed limiter checking signal is in an abnormal state, determining that the power turbine overspeed limiter fails according to the monitored power turbine rotation speed N 3m, the control power turbine rotation speed N 3c and the shutdown rotation speed N 3_stop.
(2.4) If the monitored power turbine speed N 3m and the controller power turbine speed N 3c are consistent, and N 3c<N3_stop、N3m<N3_stop, determining that the power turbine overspeed limiter is malfunctioning.
In one example, after a certain gas turbine is successfully started, in the process of running a dry car, a sudden power turbine output shaft brake fault is caused, the power turbine rotating speed N 3c of the controller is directly checked, and through checking, the rotating speed sensor corresponding to the power turbine rotating speed N 3c of the controller is found to be loose with a signal line, and the fault is eliminated after fastening. In this example, the monitored turbine speed N 3m was determined to be 1800r/min and stable by observing the control monitoring cross section, within an empirical operating range. The power turbine speed N 3c of the controller fluctuates within a range of 1800-200 r/min, and the abnormality exists.
In another example, after a gas turbine is continuously operated for 20 hours, the power turbine is shut down at 90% rated condition in sudden overspeed. Rotational speed check value N 3_check = 2000r/min, power turbine rotational speed N 3>N3_check at the time of failure occurrence at 90% rated condition of the gas turbine. The power turbine overspeed limiter check signal is first queried for historical data when a fault occurs and is determined to be in a normal state. Meanwhile, since N 3c=N3m =3802 r/min and the shutdown speed N 3_stop =3800 r/min, because of N 3c≥N3_stop、N3m≥N3_stop, it is determined that the overspeed fault exists in the power turbine speed N 3. Through investigation, the screw pitch is reduced due to the abnormality of the hydraulic oil of the adjustable pitch propeller, so that the rotation speed N 3 of the fixed power turbine is overspeed, and the gas turbine is restored to stable operation after the fault is removed.
The above is only a preferred embodiment of the present application, and the present application is not limited to the above examples. It is to be understood that other modifications and variations which may be directly derived or contemplated by those skilled in the art without departing from the spirit and concepts of the present application are deemed to be included within the scope of the present application.

Claims (8)

1.一种船用燃气轮机的动力涡轮转速控制故障排查方法,其特征在于,所述方法包括:1. A method for troubleshooting a power turbine speed control fault of a marine gas turbine, characterized in that the method comprises: 在船用燃气轮机运行过程中,当动力涡轮的输出轴出现刹车故障时,确定控制机动力涡轮转速N3c的测量通道出现故障;During the operation of a marine gas turbine, when a brake failure occurs on the output shaft of the power turbine, it is determined that a failure occurs in the measurement channel for controlling the speed N 3c of the power turbine; 当动力涡轮出现超速故障停机时,若故障发生时的动力涡轮转速N3<N3_check,则根据控制机动力涡轮转速N3c、监测机动力涡轮转速N3m以及停机转速N3_stop的转速大小关系确定对应的故障排查结果;若故障发生时的动力涡轮转速N3≥N3_check,则先排查动力涡轮超速限制器检查信号,并根据动力涡轮超速限制器检查信号的排查结果,根据控制机动力涡轮转速N3c、监测机动力涡轮转速N3m以及停机转速N3_stop的转速大小关系确定对应的故障排查结果;其中,N3_check是转速检查值。When the power turbine shuts down due to an overspeed fault, if the power turbine speed N 3 <N 3_check when the fault occurs, the corresponding fault troubleshooting result is determined according to the speed size relationship among the control engine power turbine speed N 3c , the monitoring engine power turbine speed N 3m and the stop speed N 3_stop ; if the power turbine speed N 3 ≥N 3_check when the fault occurs, the power turbine overspeed limiter check signal is first checked, and according to the checking result of the power turbine overspeed limiter check signal, the corresponding fault troubleshooting result is determined according to the speed size relationship among the control engine power turbine speed N 3c , the monitoring engine power turbine speed N 3m and the stop speed N 3_stop ; wherein, N 3_check is the speed check value. 2.根据权利要求1所述的方法,其特征在于,当N3<N3_check时,确定对应的故障排查结果的方法包括:2. The method according to claim 1, characterized in that, when N 3 <N 3_check , the method for determining the corresponding fault troubleshooting result comprises: 当监测机动力涡轮转速N3m和控制机动力涡轮转速N3c不一致时,根据停机转速N3_stop确定存在故障的动力涡轮转速的采集通道;When the monitoring engine power turbine speed N 3m and the control engine power turbine speed N 3c are inconsistent, the acquisition channel of the power turbine speed with fault is determined according to the stop speed N 3_stop ; 当监测机动力涡轮转速N3m和控制机动力涡轮转速N3c一致时,根据停机转速N3_stop确定动力涡轮超速限制器发生故障或者动力涡轮转速N3存在超速故障。When the monitoring engine power turbine speed N 3m and the controlling engine power turbine speed N 3c are consistent, it is determined according to the stop speed N 3_stop that the power turbine overspeed limiter fails or the power turbine speed N 3 has an overspeed fault. 3.根据权利要求2所述的方法,其特征在于,所述根据停机转速N3_stop确定存在故障的动力涡轮转速的采集通道,包括:3. The method according to claim 2, characterized in that the acquisition channel for determining the speed of the power turbine with a fault according to the stop speed N 3_stop comprises: 当N3c≥N3_stop且N3m在对应的工作范围内时,确定控制机动力涡轮转速N3c的采集通道存在故障;When N 3c ≥ N 3_stop and N 3m is within the corresponding working range, it is determined that the acquisition channel for controlling the motor power turbine speed N 3c is faulty; 当N3m≥N3_stop且N3c在对应的工作范围内时,确定监测机动力涡轮转速N3m的采集通道出现故障。When N 3m ≥N 3_stop and N 3c is within the corresponding working range, it is determined that the acquisition channel for monitoring the engine power turbine speed N 3m fails. 4.根据权利要求2所述的方法,其特征在于,当监测机动力涡轮转速N3m和控制机动力涡轮转速N3c一致时:4. The method according to claim 2, characterized in that when the monitoring motor power turbine speed N 3m and the controlling motor power turbine speed N 3c are consistent: 若N3c<N3_stop、N3m<N3_stop,确定动力涡轮超速限制器发生故障;If N 3c <N 3_stop , N 3m <N 3_stop , it is determined that the power turbine overspeed limiter fails; 若N3c≥N3_stop、N3m≥N3_stop,确定动力涡轮转速N3存在超速故障。If N 3c ≥N 3_stop , N 3m ≥N 3_stop , it is determined that the power turbine speed N 3 has an overspeed fault. 5.根据权利要求1所述的方法,其特征在于,当N3≥N3_check时,确定对应的故障排查结果的方法包括:5. The method according to claim 1, characterized in that, when N 3 ≥ N 3_check , the method for determining the corresponding fault troubleshooting result comprises: 若动力涡轮超速限制器检查信号的排查结果指示动力涡轮超速限制器检查信号处于正常状态,则根据监测机动力涡轮转速N3m、控制机动力涡轮转速N3c和停机转速N3_stop确定存在故障的动力涡轮转速的采集通道或确定动力涡轮转速N3存在超速故障;If the result of the troubleshooting of the power turbine overspeed limiter check signal indicates that the power turbine overspeed limiter check signal is in a normal state, the acquisition channel of the power turbine speed with a fault is determined according to the monitoring engine power turbine speed N 3m , the control engine power turbine speed N 3c and the stop speed N 3_stop , or it is determined that the power turbine speed N 3 has an overspeed fault; 若动力涡轮超速限制器检查信号的排查结果指示动力涡轮超速限制器检查信号处于异常状态,则根据监测机动力涡轮转速N3m、控制机动力涡轮转速N3c和停机转速N3_stop确定动力涡轮超速限制器发生故障。If the checking result of the power turbine overspeed limiter check signal indicates that the power turbine overspeed limiter check signal is in an abnormal state, it is determined that the power turbine overspeed limiter fails according to the monitoring engine power turbine speed N 3m , the control engine power turbine speed N 3c and the stop speed N 3_stop . 6.根据权利要求5所述的方法,其特征在于,当动力涡轮超速限制器检查信号处于正常状态时:6. The method according to claim 5, characterized in that when the power turbine overspeed limiter check signal is in a normal state: 若监测机动力涡轮转速N3m和控制机动力涡轮转速N3c不一致,则根据停机转速N3_stop确定存在故障的动力涡轮转速的采集通道;If the monitoring engine power turbine speed N 3m and the control engine power turbine speed N 3c are inconsistent, the acquisition channel of the power turbine speed with a fault is determined according to the stop speed N 3_stop ; 若监测机动力涡轮转速N3m和控制机动力涡轮转速N3c一致,且N3c≥N3_stop、N3m≥N3_stop,则确定动力涡轮转速N3存在超速故障。If the monitoring engine power turbine speed N 3m and the controlling engine power turbine speed N 3c are consistent, and N 3c ≥ N 3_stop , N 3m ≥ N 3_stop , it is determined that the power turbine speed N 3 has an overspeed fault. 7.根据权利要求6所述的方法,其特征在于,所述根据停机转速N3_stop确定存在故障的动力涡轮转速的采集通道,包括:7. The method according to claim 6, characterized in that the acquisition channel for determining the speed of the power turbine with a fault according to the stop speed N 3_stop comprises: 若N3c≥N3_stop且N3m在对应的转速范围内,则确定控制机动力涡轮转速N3c的测量通道出现故障;If N 3c ≥ N 3_stop and N 3m is within the corresponding speed range, it is determined that the measurement channel for controlling the motor power turbine speed N 3c is faulty; 若N3m≥N3_stop且N3c在对应的转速范围内,则确定监测机动力涡轮转速N3m的测量通道出现故障。If N 3m ≥ N 3_stop and N 3c is within the corresponding speed range, it is determined that the measurement channel for monitoring the engine power turbine speed N 3m is faulty. 8.根据权利要求5所述的方法,其特征在于,当动力涡轮超速限制器检查信号处于异常状态时:8. The method according to claim 5, characterized in that when the power turbine overspeed limiter check signal is in an abnormal state: 若监测机动力涡轮转速N3m和控制机动力涡轮转速N3c一致,且N3c<N3_stop、N3m<N3_stop,则确定动力涡轮超速限制器发生故障。If the monitoring engine power turbine speed N 3m and the controlling engine power turbine speed N 3c are consistent, and N 3c <N 3_stop , N 3m <N 3_stop , it is determined that the power turbine overspeed limiter fails.
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Citations (1)

* Cited by examiner, † Cited by third party
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CN115144188A (en) * 2022-07-11 2022-10-04 中国船舶重工集团公司第七0三研究所无锡分部 Overtemperature fault shutdown troubleshooting method for marine gas turbine

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