Method of operating a gas turbine engine
A method of operating a gas turbine engine having a rotatable turbine shaft with an electric machine mounted to the shaft. The method includes providing supplemental acceleration and/or deceleration of the turbine shaft of the gas turbine engine through the use of the electric machine operated as an electric motor and/or an electric generator, in order to avoid an undesirable engine speed range during engine operation.
1. A method of operating a gas turbine engine, the engine having at least one rotatable turbine shaft with an electric motor/generator mounted thereto, the method comprising the steps of accelerating a speed of said shaft by providing a fuel flow to the engine, operating the electric motor/generator to momentarily further increase shaft acceleration through at least one shaft speed range to be avoided, and determining a minimum time required for development of a resonant response associated with the at least one speed range to be avoided, wherein said operation of the electric motor/generator causes the shaft to accelerate through the at least one shaft speed range to be avoided in less than said minimum time so that resonant response is substantially avoided.
2. The method of claim 1 wherein the electric motor/generator is operated as a motor to add kinetic energy to the shaft to effect said increased shaft acceleration.
3. The method of claim 2 wherein operation of the electric motor/generator as a motor is substantially ceased when said shaft speed is substantially above the at least one shaft speed range to be avoided.
4. The method of claim 1 wherein acceleration of the shaft is momentarily restrained by operating the electric motor/generator as a generator/brake, and then such operation as a generator/brake is substantially ceased to allow said increased acceleration through the at least one shaft speed range to be avoided.
5. The method of claim 1 wherein the increased shaft acceleration occurs at a rate at which shaft speed accelerates through said at least one shaft speed range to be avoided more quickly than a time required for resonant response of a component associated with said at least one speed range to be avoided.
6. A method of operating a gas turbine engine having at least one rotatable shaft with a turbine and an electric motor/generator mounted thereto, the method comprising the steps of:
changing a rate of fuel flow provided to the gas turbine engine to change a rotational shaft speed of the at least one rotatable shaft at a fuel-flow-driven rate of change; and
upon reaching a threshold condition representative of a boundary condition of at least one speed range of said rotational shaft speed to be avoided, operating the electric motor/generator to provide a second rate of change of the rotational shaft speed having an absolute value greater than an absolute value of the fuel-flow-driven rate of change, including determining a minimum time required for development of a resonant response associated with the speed range to be avoided, and wherein said operation of the electric motor/generator causes the at least one rotatable shaft to accelerate through the at least one speed range to be avoided in less then said minimum time so that resonant response is substantially avoided.
7. The method of claim 6 wherein the motor/generator is operated as a motor to accelerate to said second rate of change.
8. The method of claim 6 wherein the motor/generator is operated as a generator/brake and then released to thereby allow the at least one rotatable shaft to momentarily accelerate to said second rate of change.