Detection of bearing carbonization failure in turbine systems
A method of detecting a bearing carbonization failure in a turbine system, the turbine system has a bearing, a turbine rotational speed sensor, and a bearing displacement acceleration sensor. The method includes obtaining individual measurement values from each of the turbine rotational speed sensor and the bearing displacement acceleration sensor, determining, as a first condition, whether the measurement values from the rotational speed sensor exceed or equal a first threshold value during a first period of time, calculating a characteristic value based on the measurement values from the bearing displacement acceleration sensor corresponding to a second period of time, the second period of time being part of the first period of time, determining, as a second condition, whether the calculated characteristic value exceeds a second threshold value, and determining that a bearing carbonization failure has occurred if both the first condition and the second condition are fulfilled.
1. A method of detecting a bearing carbonization failure in a turbine system, the turbine system comprising a bearing, a turbine rotational speed sensor, and a bearing displacement acceleration sensor, the method comprising:
obtaining individual measurement values from each of the turbine rotational speed sensor and the bearing displacement acceleration sensor,
determining, as a first condition, whether the measurement values from the rotational speed sensor exceed or equal a first threshold value during a first period of time,
calculating a characteristic value based on the measurement values from the bearing displacement acceleration sensor corresponding to a second period of time, the second period of time being part of the first period of time,
determining, as a second condition, whether the calculated characteristic value exceeds a second threshold value, and
determining that a bearing carbonization failure has occurred if both the first condition and the second condition are fulfilled.
2. The method according to claim 1 ,
wherein the characteristic value is calculated by applying a predetermined function to the measurement values from the bearing displacement acceleration sensor corresponding to the second period of time.
3. The method according to claim 2 ,
wherein the predetermined function is selected from the group consisting of a standard deviation of the measurement values during the second period of time, an average of the measurement values during the second period of time, an exponential average of the measurement values during the second period of time, and an integral of the measurement values during the second period of time.
4. The method according to claim 2 ,
wherein the predetermined function is a difference between the largest measurement value and the smallest measurement value from the bearing displacement acceleration sensor during the second period of time.
5. The method according to claim 1 , wherein the turbine system further comprises a further bearing displacement acceleration sensor, the method further comprising:
obtaining measurement values from the further bearing displacement acceleration sensor,
calculating a further characteristic value based on the measurement values from the further bearing displacement acceleration sensor corresponding to the second period of time,
determining, as a third condition, whether the calculated characteristic value exceeds a third threshold value, and
determining that a bearing carbonization failure has occurred if both the first condition and the third condition are fulfilled.
6. The method according to claim 5 ,
wherein the bearing displacement acceleration sensor and the further bearing displacement acceleration sensor measure displacement acceleration of the bearing in respective orthogonal directions.
7. The method according to claim 5 ,
wherein the turbine system comprises a further bearing, wherein the bearing displacement acceleration sensor measures displacement acceleration of the bearing, and wherein the further bearing displacement acceleration sensor measures displacement acceleration of the further bearing.
8. The method according to claim 1 ,
wherein the duration of the first period of time is at least 30 minutes, and wherein the duration of the second period of time is at least 10 minutes.
9. The method according to claim 1 ,
wherein the first period of time and the second period of time end at the same time.
10. A system for monitoring a plurality of turbine systems, each turbine system comprising a bearing, a turbine rotational speed sensor, and a bearing displacement acceleration sensor, the system comprising:
a communication unit for receiving measurement values from the turbine rotational speed sensor and bearing displacement acceleration sensor of each turbine system,
a storage unit for storing the received measurement values, and
a processing unit for performing the method according to claim 1 on the stored data for each turbine system.
11. The system according to claim 10 , further comprising:
a notification unit transmitting a notification message to an operator of a turbine system if the processing unit has detected a bearing carbonization failure in the turbine system.
12. A non-transitory computer readable medium, comprising
computer executable instructions stored thereon, which, when executed by a computer, causes the computer to perform the steps of the method according to claim 1 .
13. A computer program product comprising:
a non-transitory computer readable medium loaded with computer executable instructions, which, when executed by a computer, causes the computer to perform the steps of the method according to claim 1 .
14. The method according to claim 1 , further comprising:
transmitting a notification to an operator of a turbine system based on the detected bearing carbonization failure.
15. The method according to claim 1 , further comprising:
eliminating a root cause of the bearing carbonization failure in the turbine system.
16. The method according to claim 1 , further comprising:
cleaning the carbonized bearing in the turbine system based on the detected bearing carbonization failure.
17. The method according to claim 1 , further comprising:
detecting an abnormal turbine shutdown;
eliminating a root cause of the bearing carbonization failure in the turbine system; and
restarting the turbine system after the abnormal turbine shutdown.
18. The method according to claim 1 , further comprising:
stopping the turbine for maintenance; and
eliminating a root cause of the bearing carbonization failure in the turbine system.
19. A device for detecting a bearing carbonization failure in a turbine system, the turbine system comprising a bearing, a turbine rotational speed sensor, and a bearing displacement acceleration sensor, the device comprising:
a unit for obtaining individual measurement values from each of the turbine rotational speed sensor and the bearing displacement acceleration sensor,
a unit for determining, as a first condition, whether the measurement values from the rotational speed sensor exceed or equal a first threshold value during a first period of time,
a unit for calculating a characteristic value based on the measurement values from the bearing displacement acceleration sensor corresponding to a second period of time, the second period of time being part of the first period of time,
a unit for determining, as a second condition, whether the calculated characteristic value exceeds a second threshold value, and
a unit for determining that a bearing carbonization failure has occurred if both the first condition and the second condition are fulfilled.