Torsional damping for gas turbine engines
The present disclosure is directed to a gas turbine engine assembly having a compressor configured to increase pressure of incoming air, a combustion chamber, at least one turbine coupled to a generator, a torsional damper, and a controller. The combustion chamber is configured to receive a pressurized air stream from the compressor. Further, fuel is injected into the pressurized air in the combustion chamber and ignited so as to raise a temperature and energy level of the pressurized air. The turbine is operatively coupled to the combustion chamber so as to receive combustion products that flow from the combustion chamber. The generator is coupled to the turbine via a shaft. Thus, the torsional damper is configured to dampen torsional oscillations of the generator. Moreover, the controller is configured to provide additional damping control to the generator.
1. A method of operating a gas turbine engine assembly, comprising:
pressurizing air via a compressor of the gas turbine engine assembly;
providing the pressurized air from the compressor to a combustion chamber;
injecting fuel into the pressurized air within the combustion chamber and igniting the fuel so as to raise a temperature and energy level of the pressurized air;
providing combustion products from the combustion chamber to a turbine coupled to a generator; and
damping torsional oscillations of a shaft system of the generator via a controller providing a speed signal or a torque signal to at least one of a battery and a load in parallel to prohibit the generator from having a constant power load at frequencies of torsional interaction.
2. The method of claim 1 , wherein each of the battery and the load are configured to prevent a power bus from having a constant power load in response to the speed signal or the torque signal.
3. The method of claim 1 , wherein the controller controls a power bus damper to prohibit the generator from having a constant power load at frequencies of torsional interaction.
4. The method of claim 3 , wherein the load comprises at least one of an active load or a controlled resistive load.
5. The method of claim 4 , wherein the power bus damper comprises at least one of the active load, the controlled resistive load, or an energy storage device.
6. The method of claim 1 , further comprising:
converting, via a power converter operably coupled with the controller, AC voltage into DC voltage, wherein the power converter is configured to dampen torsional oscillations by reducing a power factor to increase generator losses at mechanical damping frequencies.
7. A method of operating a gas turbine engine assembly, comprising:
providing combustion products from a combustion chamber to a turbine coupled to a generator; and
damping torsional oscillations of a shaft system of the generator via a power bus damper operably coupled with the shaft system of the generator through a power bus and configured to prohibit the generator from having a constant power load at frequencies of torsional interaction, wherein the power bus damper includes a battery and an active load in parallel.
8. The method of claim 7 , further comprising:
providing a speed signal or a torque signal to the power bus damper, wherein each of the battery and the active load are configured to prevent the power bus from having a constant power load in response to the speed signal or the torque signal.
9. The method of claim 8 , further comprising converting, via a power converter, AC voltage into DC voltage, wherein the power converter is configured to dampen torsional oscillations by reducing a power factor to increase generator losses at mechanical damping frequencies.
10. The method of claim 7 , wherein the power bus damper further controls a controlled resistive load of a resistor to prohibit the generator from having a constant power load at frequencies of torsional interaction.