Aircraft engine assembly and method of generating electric energy for an aircraft power system
US-2016348589-A1 · Dec 1, 2016 · US
US9753467B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9753467-B2 |
| Application number | US-201414220858-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 20, 2014 |
| Priority date | Mar 20, 2014 |
| Publication date | Sep 5, 2017 |
| Grant date | Sep 5, 2017 |
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A tangible non-transitory computer readable medium may include instructions to analyze a first signal indicative of a speed of a turbine system and transform the first signal into a second signal. The tangible non-transitory computer-readable medium may also include instructions to transmit the second signal to control a speed of the turbine system by actuating a field device. Actuating the field device may include controlling a fluid level in a torque converter mechanically coupled to the turbine system, and the speed may be below a minimum setpoint of the turbine system.
Opening claim text (preview).
The invention claimed is: 1. A system comprising: a turbine system configured to produce power; a starting motor configured to rotate a first shaft included in the turbine system; a torque converter mechanically coupled to the first shaft and mechanically coupled to the turbine system; and a control system comprising a processor configured to determine the power of the turbine system, determine a fluid level in the torque converter based at least in part on the power of the turbine system; and control a speed of the turbine system by controlling the fluid level in the torque converter to arrive at a first turbine system speed below a minimum drive line mechanical speed of the turbine system. 2. The system of claim 1 , wherein the torque converter comprises a plurality of guide vanes, and wherein the minimum drive line mechanical speed comprises a speed of the turbine system when the guide vanes are all closed and the torque converter is filled with a fluid, and wherein controlling the fluid level in the torque converter comprises draining substantially all of the fluid in the torque converter. 3. The system of claim 1 , wherein controlling the fluid level in the torque converter comprises draining a portion of a fluid in the torque converter. 4. The system of claim 3 , wherein the processor is configured to control a drain rate of the fluid in the torque converter. 5. The system of claim 1 , wherein the control system comprises at least one of a bang/bang controller, a proportional integral derivative (PID) controller, a model based controller (MBC), a setpoint controller, or a combination thereof. 6. The system of claim 1 , wherein the turbine system comprises at least one of a gas turbine system, a steam turbine system, a hydro turbine system, a wind turbine system, a turbo expander system, or a centrifugal pump system. 7. The system of claim 1 , wherein the torque converter comprises guide vanes and a position sensor disposed on the guide vanes. 8. The system of claim 1 , wherein the starting motor comprises an electric motor, a pneumatic motor, a hydraulic motor, or a combination thereof. 9. The system of claim 1 , wherein controlling the fluid level in the torque converter comprises draining a fluid in the torque converter and subsequently refilling the torque converter with the fluid. 10. A system comprising a controller, the controller comprising a processor configured to: receive a first signal indicative of a current speed of a turbine system; transform the first signal into a second signal; transmit the second signal to control a desired speed of the turbine system by actuating an actuator; determine an output power of the turbine system; and determine the fluid level in the torque converter based on the output power of the turbine system; wherein the actuation of the actuator is configured to control a fluid level in a torque converter mechanically coupled to the turbine system to arrive at the desired speed, and wherein the desired speed comprises a first speed below a minimum drive line mechanical speed of the turbine system. 11. The system of claim 10 , wherein the processor is configured to receive a third signal indicative of an output power of the torque converter and to transform the first and third signals into the second signal to control the desired speed of the turbine system. 12. The system of claim 11 , wherein the processor is configured to receive a fourth signal indicative of an input torque of a starting motor mechanically coupled to the torque converter and to transform the first, third and fourth signals into the second signal to control the desired speed of the turbine system. 13. The system of claim 10 , wherein the actuation of the actuator is configured to drain substantially all of a fluid in the torque converter. 14. The system of claim 10 , wherein the actuation of the actuator is configured to drain a portion of a fluid in the torque converter. 15. The system of claim 10 , wherein the actuation of the actuator is configured to drain a fluid in the torque converter and subsequently refill the torque converter with the fluid. 16. A tangible non-transitory computer readable medium comprising instructions that when executed by a processor cause the processor to: analyze a first signal indicative of a current speed of a turbine system; transform the first signal into a second signal; transmit the second signal to control a desired speed of the turbine system by actuating an actuator; determine a power output of the turbine system; and determine the fluid level in the torque converter based on the power output of the turbine system, wherein the actuation of the actuator is configured to control a fluid level in a torque converter mechanically coupled to the turbine system, and wherein the desired speed comprises a first speed below a minimum drive line mechanical speed of the turbine system. 17. The tangible non-transitory computer readable medium of claim 16 , wherein the actuation of the actuator is configured to drain all of a fluid in the torque converter. 18. The tangible non-transitory computer readable medium of claim 16 , wherein the actuation of the actuator is configured to drain a portion of a fluid in the torque converter. 19. The tangible non-transitory computer readable medium of claim 16 , wherein the actuation of the actuator is configured to drain a fluid in the torque converter and subsequently refill the torque converter with the fluid.
Mechanical drives · CPC title
an electrical generator · CPC title
Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title
to control rotational speed (n) · CPC title
Spool rotational speed · CPC title
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