Method for managing a gas turbine assembly at low speed and corresponding gas turbine assembly
A method manages a gas turbine assembly during start up or shut down, the gas turbine assembly including a twin shaft gas turbine having an input shaft and an output shaft and a speed sensor for measuring a speed of the output shaft, the gas turbine assembly further having a rotor mounted on said output shaft and provided with at least a dry gas seal for preventing leakage of a process gas. The method includes monitoring the speed of the output shaft, and in parallel, reducing or increasing the speed of the input shaft after the monitored speed of the output shaft has remained above zero and below a predefined slow roll speed limit for a predefined acceptable time.
1. A method for managing a gas turbine assembly during start up or shut down, the gas turbine assembly including a twin shaft gas turbine comprising an input shaft and an output shaft and a speed sensor for measuring a speed of the output shaft, the gas turbine assembly further comprising a rotor mounted on said output shaft and provided with at least a dry gas seal for preventing leakage of a gas between the rotor and the dry gas seal, the method comprising:
monitoring the speed of the output shaft, and in parallel
reducing or increasing the speed of the input shaft after the monitored speed of the output shaft has remained above zero and below a predefined slow roll speed limit for a predefined acceptable time.
2. The method according to claim 1 ,
wherein the step of reducing or increasing the speed of the input shaft further comprises in sequence:
starting spinning the input shaft,
if after a first predefined acceptable time the speed of the output shaft remains below the predefined slow roll speed limit, then increasing the speed of the input shaft,
if the speed of the output shaft remains below the predefined slow roll speed limit, then waiting for a second predefined acceptable time before further increasing the speed of the input shaft.
3. The method according to claim 2 ,
wherein the first predefined acceptable time is 10 s to 30 s.
4. The method according to claim 2 ,
wherein the second predefined acceptable time is 60 s to 300 s.
5. The method according to claim 1 ,
wherein the step of reducing or increasing the speed of the input shaft further comprises in sequence:
waiting until the output shaft has stopped,
waiting for a predefined wait time,
spinning the input shaft at a first predefined speed,
if the speed of the output shaft remains for a third predefined acceptable time above zero but below the predefined slow roll speed limit, then increasing the speed of the input shaft up to a second predefined speed greater than the first predefined speed,
if the speed of the output shaft remains below the predefined slow roll speed limit, then stopping the input shaft, then
waiting for a time equal to the wait time, then
spinning the input shaft at a third predefined speed lower than the first predefined speed,
if the speed of the output shaft is greater than zero, then stopping the input shaft, then
waiting for a time equal to the wait time, then
periodically spinning the input shaft up to a fourth predefined speed lower than the third predefined speed and stopping the input shaft for an interval time,
if the speed of the output shaft is greater than zero, then stopping the input shaft, and
preventing the gas turbine assembly to be restarted during a resting time.
6. The method according to claim 5 ,
wherein the third predefined acceptable time is 10 s to 30 s.
7. The method according to claim 5 ,
wherein the first predefined speed is 10 to 20 percent of the nominal power turbine speed.
8. The method according to claim 5 ,
wherein the second predefined speed is 20 to 40 percent of the nominal power turbine speed.
9. The method according to claim 5 ,
wherein the third predefined speed is 5 to 10 percent of the nominal power turbine speed.
10. The method according to claim 5 ,
wherein the wait time is 2 to 3 min.
11. The method according to claim 5 ,
wherein the interval time is 2 to 3 min.
12. The method according to claim 5 ,
wherein the resting time is 10 min to 4 hours.
13. The method according to claim 1 ,
wherein the predefined slow roll speed limit is 200 to 600 rpm.
14. The method according to claim 1 ,
wherein the gas turbine assembly comprises a gas compressor including the rotor and the dry gas seal.
15. A gas turbine assembly, comprising
a twin shaft gas turbine comprising an input shaft and an output shaft,
a variable speed electrical motor connected to the input shaft,
a speed sensor for measuring a speed of the output shaft,
a controller which controls the variable speed electrical motor, and
a rotor mounted on said output shaft and provided with at least a dry gas seal for preventing leakage of a gas between the rotor and the dry gas seal,
wherein the speed sensor is configured to measure the speed of the output shaft, and
wherein the controller is configured to monitor the speed of the output shaft measured by sensor and to reduce or increase the speed of the input shaft via the variable speed electrical motor after the monitored speed of the output shaft has remained above zero and below a predefined slow roll speed limit for a predefined acceptable time.
16. The gas turbine assembly according to claim 15 ,
wherein, for reducing or increasing the speed of the input shaft, the controller is further configured to, in sequence:
start spinning the input shaft,
if after a first predefined acceptable time the speed of the output shaft remains below the predefined slow roll speed limit, then increase the speed of the input shaft,
if the speed of the output shaft remains below the predefined slow roll speed limit, then wait for a second predefined acceptable time before further increasing the speed of the input shaft.
17. The gas turbine assembly according to claim 16 ,
wherein the first predefined acceptable time is 10 s to 30 s, and/or
wherein the second predefined acceptable time is 60 s to 300 s.
18. The gas turbine assembly according to claim 15 ,
wherein, for reducing or increasing the speed of the input shaft, the controller is further configured to, in sequence:
wait until the output shaft has stopped,
wait for a predefined wait time,
spin the input shaft at a first predefined speed,
if the speed of the output shaft remains for a third predefined acceptable time above zero but below the predefined slow roll speed limit, then increase the speed of the input shaft up to a second predefined speed greater than the first predefined speed,
if the speed of the output shaft remains below the predefined slow roll speed limit, then stop the input shaft, then
wait for a time equal to the wait time, then
spin the input shaft at a third predefined speed lower than the first predefined speed,
if the speed of the output shaft is greater than zero, then stop the input shaft, then
wait for a time equal to the wait time, then
periodically spin the input shaft up to a fourth predefined speed lower than the third predefined speed and stop the input shaft for an interval time,
if the speed of the output shaft is greater than zero, then stop the input shaft, and
prevent the gas turbine assembly being restarted during a resting time.
19. The gas turbine assembly according to claim 18 ,
wherein the third predefined acceptable time is 10 s to 30 s, and/or
wherein the first predefined speed is 10 to 20 percent of the nominal power turbine speed, and/or
wherein the second predefined speed is 20 to 40 percent of the nominal power turbine speed, and/or
wherein the third predefined speed is 5 to 10 percent of the nominal power turbine speed, and/or
wherein the wait time is 2 to 3 min, and/or
wherein the interval time is 2 to 3 min, and/or
wherein the resting time is 10 min to 4 hours.
20. The gas turbine assembly according to claim 15 ,
wherein the predefined slow roll speed limit is 200 to 600 rpm.