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 gas turbine engine assembly, comprising:
a compressor configured to increase pressure of incoming air;
a combustion chamber configured to receive a pressurized air stream from the compressor, wherein fuel is injected into the pressurized air stream and ignited so as to raise a temperature and energy level of the pressurized air;
a turbine operatively coupled to the combustion chamber so as to receive combustion products that flow from the combustion chamber;
a generator coupled to at least one of a low-pressure shaft or a high-pressure shaft of the turbine via a generator shaft;
a power bus damper configured as a battery to dampen torsional oscillations of the generator shaft of the generator by prohibiting the generator from having a constant power load at frequencies of torsional interaction;
a power converter configured to dampen torsional oscillations by reducing a power factor to increase generator losses at mechanical damping frequencies; and
a controller configured to provide a speed signal or a torque signal to the power bus damper, wherein the power bus damper is configured to prevent a power bus from having a constant power load separated from voltage control in response to the speed signal or the torque signal.
2. The gas turbine engine assembly of claim 1 , wherein the power bus damper comprises at least one of an active load, a controlled resistive load, or an energy storage device.
3. The gas turbine engine assembly of claim 1 , wherein the power bus further includes an active load to control the damping of the generator shaft of the generator by providing the speed signal or the torque signal to the active load and altering the active load in response to the speed signal or the torque signal.
4. The gas turbine engine assembly of claim 1 , wherein the power bus damper includes an active load in parallel with the battery.
5. The gas turbine engine assembly of claim 1 , wherein the power bus damper further includes an active load and a controlled resistive load each in parallel with the battery.
6. A gas turbine engine assembly, comprising:
a compressor configured to increase pressure of incoming air;
a combustion chamber configured to receive a pressurized air stream from the compressor, wherein fuel is injected into the pressurized air stream and ignited so as to raise a temperature and energy level of the pressurized air;
a turbine operatively coupled to the combustion chamber so as to receive combustion products that flow from the combustion chamber;
a generator coupled to at least one of a low-pressure shaft or a high-pressure shaft of the turbine via a generator shaft and configured to generate electric power;
a power bus damper configured to dampen torsional oscillations of the generator shaft of the generator by prohibiting 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; and
a controller configured to provide 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 a power bus from having a constant power load in response to the speed signal or the torque signal.
7. The gas turbine engine assembly of claim 6 , wherein the power bus damper comprises an active load.
8. The gas turbine engine assembly of claim 6 , wherein the power bus damper comprises a controlled resistive load.