Engine health monitoring and power allocation control for a turbine engine using electric generators
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-021/00
F02C-007/32
F02C-007/36
F02C-009/28
G05B-023/02
G05B-019/048
G07C-005/00
G07C-005/08
출원번호
US-0127096
(2013-11-26)
등록번호
US-9593591
(2017-03-14)
국제출원번호
PCT/US2013/071885
(2013-11-26)
국제공개번호
WO2014/143219
(2014-09-18)
발명자
/ 주소
Phillips, Steven D.
Neuman, Tom M.
Armstrong, Michael
출원인 / 주소
Rolls-Royce Corporation
대리인 / 주소
Barnes & Thornburg LLP
인용정보
피인용 횟수 :
1인용 특허 :
25
초록
A control for a turbine engine using electrical machines monitors engine health and allocates power extraction between the electrical machines.
대표청구항▼
1. A method for controlling an allocation of power extracted from a plurality of shafts of a turbine engine, the shafts having one or more electrical machines coupled thereto, the method comprising, with a controller, during operation of the turbine engine: monitoring a plurality of operating parame
1. A method for controlling an allocation of power extracted from a plurality of shafts of a turbine engine, the shafts having one or more electrical machines coupled thereto, the method comprising, with a controller, during operation of the turbine engine: monitoring a plurality of operating parameters of the turbine engine over time;assessing a health of the turbine engine over time based on the plurality of operating parameters as they are monitored, wherein the health of the turbine engine is indicative of a wear characteristic of the turbine engine; andvarying the allocation of power extraction between the plurality of electrical machines over time in response to the assessing of the health of the turbine engine by assigning a part of a total power extraction to the one or more electrical machines coupled to each of the plurality of shafts. 2. The method of claim 1, comprising obtaining, from the turbine engine, an indicator of current fuel flow to the turbine engine; and comparing the current fuel flow to a healthy turbine engine profile. 3. The method of claim 2, comprising obtaining, from one or more control units coupled to the electrical machines, data relating to a current power extraction allocation; and comparing the current power extraction allocation to the healthy turbine engine profile. 4. The method of claim 3, comprising obtaining, from the turbine engine, data relating to a current operating condition of the turbine engine; and adjusting the power extraction allocation based on the current operating condition. 5. A control for a turbine engine having a plurality of shafts and one or more electrical machines coupled to the shafts, the control comprising one or more processor-executable modules embodied in non-transitory computer memory and configured to perform the method of claim 4. 6. A system for controlling an extraction and allocation of power from a turbine engine, the system comprising: a low pressure turbine, coupled to the turbine engine via a low pressure shaft and configured to drive at least a fan of the turbine engine;a high pressure turbine, connected to the turbine engine via a high pressure shaft configured to drive at least a compressor of the turbine engine;electrical machines coupled to the low pressure shaft and the high pressure shaft, the electrical machines configured to extract rotational power from the low pressure shaft and the high pressure shaft and output electrical power;control units coupled to each of the electrical machines to control the amount of rotational power extracted by the electrical machines from the low pressure shaft and the high pressure shaft; andnon-transitory computer memory comprising a processor-executable power allocation optimizer to, during operation of the turbine engine, dynamically assess a health of the turbine engine based on a plurality of sensed operating parameters and adjust the allocation of power extraction between the low pressure shaft and the high pressure shaft based on the assessment of the health of the turbine engine, wherein the health of the turbine engine is indicative of a wear characteristic of the turbine engine. 7. The system of claim 6, wherein the non-transitory computer memory comprises a processor-executable engine health monitor in communication with the power allocation optimizer to assess turbine engine health based on turbine engine performance sensitivity to variations in shaft power extraction. 8. The system of claim 6, wherein the power allocation optimizer optimizes turbine engine cycle performance by varying electrical system controls. 9. A method for controlling an allocation of power extracted from a plurality of shafts of a turbine engine, the shafts having one or more electrical machines coupled thereto, the method comprising, with a controller, during operation of the turbine engine: receiving, via feedback control of the turbine engine, data relating to turbine engine operating conditions including one or more of a fuel flow, temperature, pressure, and speed;generating an assessment of the a health of the turbine engine based on changes in the one or more operating conditions over time;using a model-based algorithm to predict a change in the health of the turbine engine based on the operating conditions and a healthy turbine engine profile;determining an optimal power extraction allocation between the plurality of electrical machines based on the predicted change in turbine engine health, the operating conditions, and one or more optimization parameters;extracting power from the plurality of shafts; andcontrolling the electrical machines to implement the optimal power extractionwherein the plurality of electrical machines comprises a low pressure generator shaft and a high pressure generator shaft, and the method comprises increasing the power extraction from the low pressure generator shaft and decreasing the power extraction from the high pressure generator shaft. 10. The method of claim 9, comprising varying the power extraction allocation between the plurality of electrical machines in response to the predicted change in the health of the turbine engine. 11. The method of claim 10, comprising continuously varying the optimal power extraction allocation in response to power demands. 12. The method of claim 10, comprising continuously varying the optimal power extraction allocation in response to changes in the turbine engine operating conditions. 13. The method of claim 10, comprising assessing the health of the turbine engine based on changes in fuel flow over time and changes in power extraction from the plurality of electrical machines over time. 14. The method of claim 10, wherein the assessment of the turbine engine health indicates deterioration of the turbine engine health, and the method comprises adjusting the power extraction allocation to improve engine efficiency in response to the indication of turbine engine health deterioration. 15. The method of claim 9, comprising transferring power from one of the shafts to the other shaft. 16. The method of claim 9, comprising determining the optimal power extraction allocation to optimize fuel efficiency, engine performance, or engine reliability.
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이 특허에 인용된 특허 (25)
Muramatsu, Hironori; Sugitani, Yukinobu, Control system for gas-turbine engine.
Rice Robert W. (Sandy Hook CT) Sweet David H. (Tequesta FL), Engine failure monitor for a multi-engine aircraft having partial engine failure and driveshaft failure detection.
Eick, Chris D.; Gaines, Louie T.; Laidlaw, Mitchell J.; Benson, Dwayne M.; Portolese, Larry A.; Flaherty, Brian L.; Pearson, Wayne T., More electric aircraft power transfer systems and methods.
Hield Paul M. (Bristol GB2) Cundy John M. (Derby GB2) Midgley Ronald A. (Derby GB2) Newton Arnold C. (Derby GB2) Rowe Arthur L. (Derby GB2), Shaft power transfer in gas turbine engines with machines operable as generators or motors.
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