Active stability control of compression systems utilizing electric machines

1. A turbine engine, comprising:

a compressor configured to pressurize an incoming air stream into a pressurized air stream;

a combustion chamber fluidly connected with the compressor and configured to receive the pressurized air stream from the compressor, wherein fuel is injected into the pressurized air stream and ignited in the combustion chamber so as to raise a temperature and energy level of the pressurized air stream;

a turbine fluidly connected with the combustion chamber and configured to receive combustion products that flow from the combustion chamber;

a shaft system;

an electric generator operatively coupled with the compressor via the shaft system;

one or more electrical loads electrically connectable with the electric generator via a power bus system;

a controller configured to:

receive control data indicative of a system state of the compressor, wherein the control data indicative of the system state of the compressor comprises at least one of a mass flow of the pressurized air stream through the compressor, a pressure of the pressurized air stream flowing through the compressor, and a rotational speed of the compressor;

determine a damping control command representative of instructions for adjusting a control parameter of the electric generator based at least in part on the control data, the control parameter being a voltage output of the electric generator; and

control the electric generator to adjust the control parameter based at least in part on the damping control command to change an output of the shaft system for damping instability fluctuations of the pressurized air stream within the compressor, and

wherein in controlling the electric generator to adjust the control parameter based at least in part on the damping control command to change the output of the shaft system for damping instability fluctuations of the pressurized air stream within the compressor, the controller is configured to cause a torque load placed on the shaft system by the electric generator i) that is in phase with mass flow fluctuations of the pressurized air stream within the compressor; or ii) that is out of phase with the mass flow fluctuations of the pressurized air stream within the compressor according to a phase lag offset.

2. The turbine engine of claim 1 , wherein the damping control command is determined based at least in part on a measured compressor parameter and a reference compressor parameter, wherein the reference compressor parameter is based at least in part on an operating point of the compressor.

3. The turbine engine of claim 1 , wherein in determining the damping control command, the controller is configured to:

generate a control command based at least in part on a rotational speed of the compressor;

determine an adjusted control command based at least in part on the control command and the damping control command; and

generate a command signal representative of instructions for adjusting the control parameter of the electric generator.

4. The turbine engine of claim 1 , further comprising:

one or more sensors communicatively coupled with the controller and configured for sensing one or more compressor parameters indicative of the system state of the compressor, wherein the control data is received at least in part from the one or more sensors.

5. The turbine engine of claim 1 , wherein the control data received by the controller further comprises an electrical power demand placed on the electric generator by the one or more electrical loads electrically connected with the electric generator, and wherein the electric generator is controlled to adjust the control parameter based at least in part on the electrical power demand.

6. The turbine engine of claim 1 , wherein the output of the shaft system is a shaft speed of one or more shafts of the shaft system, and wherein when the shaft speed of the shaft system is changed, a rotational speed of the compressor is changed for damping instability fluctuations of the pressurized air stream within the compressor.

7. The turbine engine of claim 1 , wherein the damping control command is representative of instructions for adjusting a control parameter of the one or more electrical loads electrically connected to the electric generator based at least in part on the control data, and

wherein the one or more electrical loads are controlled, directly or indirectly by one or more controllable sources on the power bus system, by the controller to adjust the control parameter based at least in part on the damping control command to change an output of the shaft system for damping instability fluctuations of the pressurized air stream within the compressor.

8. The turbine engine of claim 1 , wherein the compressor is a high pressure compressor, the turbine is a high pressure turbine, and the shaft system comprises a high pressure shaft operatively coupling the high pressure compressor with the high pressure turbine, and wherein the turbine engine further comprises:

a low pressure compressor positioned upstream of the high pressure compressor;

a low pressure turbine positioned downstream of the high pressure turbine, wherein the shaft system comprises a low pressure shaft operatively coupling the low pressure compressor and the low pressure turbine, and

wherein the electric generator is operatively coupled with the low pressure shaft and the control data is indicative of the system state of the high pressure compressor, and wherein the controller is configured to control the electric generator to adjust the control parameter based at least in part on the damping control command to change an output of the low pressure shaft for damping instability fluctuations of the pressurized air stream within the high pressure compressor.

9. The turbine engine of claim 1 , wherein the turbine engine is an aeroderivative gas turbine engine.

10. The turbine engine of claim 1 , wherein the turbine engine is an auxiliary power unit.

11. The turbine engine of claim 1 , wherein the compressor is a centrifugal compressor.

12. The turbine engine of claim 1 , wherein the turbine engine is a turbofan.

13. The turbine engine of claim 1 , the torque load placed on the shaft system by the electric generator is in phase with mass flow fluctuations of the pressurized air stream within the compressor.

14. The turbine engine of claim 1 , wherein the torque load placed on the shaft system by the electric generator is out of phase with mass flow fluctuations of the pressurized air stream within the compressor according to the phase lag offset.

15. A method for active stability control of a compression system operatively coupled with an electric generator via a shaft system, the method comprising:

receiving control data indicative of a system state of the compression system, wherein the control data indicative of the system state of the compressor comprises at least one of a mass flow of the pressurized air stream through the compressor, a pressure of the pressurized air stream flowing through the compressor, and a rotational speed of the compressor;

determining a damping control command representative of instructions for adjusting a control parameter of the electric generator based at least in part on the control data, the control parameter being a voltage output of the electric generator; and

adjusting the control parameter of the electric generator based at least in part on the damping control command to change an output of the shaft system for damping instability fluctuations of a fluid stream within the compression system, and wherein the electric generator is controlled to adjust the control parameter based at least in part on an electrical power demand placed on the electric generator by one or more electrical loads electrically connected with the electric generator.

16. The method of claim 15 , further comprising:

generating a control command based at least in part on a rotational speed of one or more rotational components of the compression system;

determining an adjusted control command based at least in part on the control command and the damping control command; and

generating a command signal representative of instructions for adjusting the control parameter of the electric generator.

17. The method of claim 15 , further comprising:

accessing a database that correlates the damping control command with an amount of damping remaining that is required for stabilizing the compression system at a current operating characteristic of the compression system; and

ascertaining the amount of damping remaining by correlating the damping control command at the current operating characteristic of the compression system.

18. A turbine engine, comprising:

a compressor configured to pressurize an incoming air stream into a pressurized air stream;

a combustion chamber fluidly connected with the compressor and configured to receive the pressurized air stream from the compressor, wherein fuel is injected into the pressurized air stream and ignited in the combustion chamber so as to raise a temperature and energy level of the pressurized air stream;

a turbine fluidly connected with the combustion chamber and configured to receive combustion products that flow from the combustion chamber;

a shaft system;

an electric generator operatively coupled with the compressor via the shaft system;

one or more electrical loads electrically connectable with the electric generator via a power bus system;

a controller configured to:

receive control data indicative of a system state of the compressor, wherein the control data includes an electrical power demand placed on the electric generator by the one or more electrical loads electrically connected with the electric generator, and wherein the control data indicative of the system state of the compressor comprises at least one of a mass flow of the pressurized air stream through the compressor, a pressure of the pressurized air stream flowing through the compressor, and a rotational speed of the compressor;

determine a damping control command representative of instructions for adjusting a control parameter of at least one of the electric generator and the one or more electrical loads based at least in part on the control data; and

control at least one of the electric generator and the one or more electrical loads to adjust the control parameter based at least in part on the damping control command to change an output of the shaft system for damping instability fluctuations of the pressurized air stream within the compressor, and wherein at least one of the electric generator and the one or more electrical loads are controlled to adjust the control parameter based at least in part on the electrical power demand.

19. The turbine engine of claim 18 , wherein the damping control command is representative of instructions for adjusting a control parameter of the one or more electrical loads electrically connected to the electric generator based at least in part on the control data, and

wherein the one or more electrical loads are controlled, directly or indirectly by one or more controllable sources on the power bus system, by the controller to adjust the control parameter based at least in part on the damping control command to change an output of the shaft system for damping instability fluctuations of the pressurized air stream within the compressor.

20. The turbine engine of claim 18 , wherein the turbine engine is a turbofan.