Gas turbine engine and method for operating same
A gas turbine engine includes a compressor. A turbine is mechanically connected to the compressor by a shaft. An air-driven auxiliary turbine is in fluid communication with the compressor and is configured to receive pressurized air from the compressor. An auxiliary generator is operably connected to the auxiliary turbine. The auxiliary generator is configured to generate electrical energy in response to an operation of the auxiliary turbine. An energy storage device is in electrical communication with the auxiliary generator.
1. A method for operating a gas turbine engine, the method comprising:
directing pressurized air to an air-driven first auxiliary turbine of a first gas turbine engine during a first engine loading condition of the first gas turbine engine and controlling a flow rate of the pressurized air directed to the first auxiliary turbine;
generating electrical energy, during the first engine loading condition, with a first auxiliary generator of the first gas turbine engine in operable communication with the first auxiliary turbine, wherein the first gas turbine engine is electrically cross-connected with a second gas turbine engine comprising a second auxiliary generator in operable communication with a second auxiliary turbine;
storing the electrical energy in an energy storage device during the first engine loading condition; and
applying the electrical energy stored in the energy storage device to an electrical load at a second engine loading condition of the first gas turbine engine which is greater than the first engine loading condition, wherein applying the electrical energy stored in the energy storage device to the electrical load includes applying the electrical energy to the second auxiliary generator causing the second auxiliary generator to apply a rotational force to a second rotatable shaft of the second gas turbine engine, via the second auxiliary turbine, to balance loading between the first gas turbine engine and the second gas turbine engine, the second auxiliary turbine in rotational communication with the second rotatable shaft which is operably connected between a second compressor and a second turbine of the second gas turbine engine;
wherein the first auxiliary turbine is in rotational communication with a first rotatable shaft operably connected between a first compressor and a first turbine of the first gas turbine engine.
2. The method of claim 1 , wherein applying the electrical energy stored in the energy storage device to the electrical load includes applying the electrical energy to the first auxiliary generator causing the first auxiliary generator to apply a rotational force to the first rotatable shaft.
3. The method of claim 2 , further comprising selectively engaging an auxiliary shaft of the first auxiliary turbine to the first rotatable shaft with a clutch.
4. The method of claim 1 , wherein controlling the flow rate of the pressurized air directed to the first auxiliary turbine includes establishing, with a modulation device, a first flow rate of the pressurized air at the first engine loading condition and a second flow rate of the pressurized air, different than the first flow rate of the pressurized air, at the second engine loading condition.
5. The method of claim 4 , wherein the first flow rate is greater than the second flow rate.
6. The method of claim 1 , wherein the energy storage device is a battery.
7. The method of claim 1 , wherein the first engine loading condition is defined by a minimum fuel flow limit.
8. The method of claim 1 , wherein, in the first engine loading condition, the first auxiliary turbine applies a first rotational force to the first auxiliary generator for generation of the electrical energy and a second rotational force to the first rotatable shaft.
9. A method for operating a gas turbine engine, the method comprising:
directing pressurized air to an air-driven first auxiliary turbine of a first gas turbine engine and controlling a flow rate of the pressurized air directed to the first auxiliary turbine;
generating electrical energy with a first auxiliary generator of the first gas turbine engine in operable communication with the first auxiliary turbine;
wherein the first gas turbine engine is electrically cross-connected with a second gas turbine engine comprising a second auxiliary generator in operable communication with a second auxiliary turbine, the method further comprising:
applying the electrical energy generated by the first auxiliary generator to the second auxiliary generator causing the second auxiliary generator to apply a rotational force to a second rotatable shaft of the second gas turbine engine, via the second auxiliary turbine, to balance loading between the first gas turbine engine and the second gas turbine engine, the second auxiliary turbine in rotational communication with the second rotatable shaft which is operably connected between a second compressor and a second turbine of the second gas turbine engine;
wherein the first auxiliary turbine is in rotational communication with a first rotatable shaft operably connected between a first compressor and a first turbine of the first gas turbine engine.