Gas turbine engine with an engine rotor element turning device
A turbine engine has a core with a compressor, combustor, and turbine sections in axial flow arrangement and with corresponding rotating elements mounted to a shaft defining engine rotor elements. The turbine engine has a rotary driver operably coupled to the engine rotor elements. The turbine engine has at least one thermoelectric generator in thermal communication with the core and in electrical communication with the rotary driver to provide power to the rotary driver to turn the engine rotor elements.
1. A turbine engine comprising;
a core having compressor, combustor, and turbine sections in axial flow arrangement, with corresponding rotating elements, including a spinner mounted to a shaft to define engine rotor elements;
a rotary driver including a friction driver attached to and turning the spinner of the engine rotor elements; and
at least one thermoelectric generator in thermal communication with the core and in electrical communication with the rotary driver to provide power to the rotary driver to turn the engine rotor elements.
2. The turbine engine of claim 1 further comprising an inner core cowl surrounding the core, and the at least one thermoelectric generator is secured to the inner core cowl.
3. The turbine engine of claim 2 wherein the inner core cowl further comprises an upper bifurcation area and the at least one thermoelectric generator is secured in the upper bifurication area.
4. The turbine engine of claim 3 wherein the at least one thermoelectric generator is removably secured in the upper bifurication area of the inner core cowl.
5. The turbine engine of claim 1 further comprising an accessory gear box operably coupled to the shaft, and the rotary driver connects to and drives the accessory gear box to rotate the shaft.
6. The turbine engine of claim 1 further comprising a fan wherein the rotary driver connects to and drives the fan operably connected to the engine rotor elements.
7. The turbine engine of claim 1 wherein the at least one thermoelectric generator is in thermal communication with one of the combustor or turbine sections.
8. The turbine engine of claim 7 wherein the at least one thermoelectric generator is a plurality of thermoelectric generators arranged in electrical communication with a boost converter to provide output voltage sufficient to drive an electric motor.
9. A turbine engine rotation device comprising;
a rotary driver including a friction driver attached to and turning a spinner of engine rotor elements on the turbine engine;
at least one thermoelectric generator positioned above at least a portion of a heat source on the turbine engine and in electrical communication with the rotary driver to provide power to the rotary driver to turn the engine rotor elements.
10. The turbine engine rotation device of claim 9 further comprising an accessory gear box operably coupled to the engine rotor elements, and the rotary driver connects to and drives the accessory gear box to rotate the engine rotor elements.
11. The turbine engine rotation device of claim 9 further comprising a fan wherein the rotary driver connects to and drives the fan operably connected to the engine rotor elements.
12. The turbine engine rotation device of claim 9 wherein the at least one thermoelectric generator is in thermal communication and positioned above one of a combustor or turbine sections of the turbine engine.
13. A method of turning engine rotor elements including a spinner of a turbine engine with a rotary driver including a friction driver, the method comprising the step of converting heat from the engine into electricity and supplying the electricity to the rotary driver to power the rotary driver and the friction driver to turn the spinner of the engine rotor elements.
14. The method of claim 13 wherein converting heat from the engine into electricity comprises generating the electricity from a thermoelectric generator.
15. The method of claim 14 wherein the method further comprises the step of transferring rotational energy from the rotary driver to an accessory gear box operably coupled to engine rotor elements.
16. The method of claim 14 wherein the method further comprises the step of transferring rotational energy from the rotary driver to a fan operably coupled to engine rotor elements.
17. The method of claim 13 further comprising the step of turning the engine rotor elements after engine shutdown.
18. The method of claim 17 wherein the engine rotor elements are turned in a range of about 1-5 RPM.
19. The method of claim 18 further comprising the step of securing at least one thermoelectric generator to an inner core cowl of the turbine engine.
20. The method of claim 19 further comprising the step of positioning the at least one thermoelectric generator to an upper bifurication area of the inner core cowl.