[특허]Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof

Bell Helicopter Textron Inc.

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특허 상세정보

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Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F16H-059/30
미국특허분류(USC)	477/124;
출원번호	US-0502596 (2009-07-14)
등록번호	US-8133155 (2012-03-13)
발명자 / 주소	Ehinger, Ryan T. Fenny, Carlos A. Kilmain, Charles J. Sinusas, Eric A. Worrell, Kevin
출원인 / 주소	Bell Helicopter Textron Inc.
대리인 / 주소	Orrick, Herrington & Sutcliffe LLP
인용정보	피인용 횟수 : 8 인용 특허 : 13

초록
▼

A multi-ratio rotorcraft drive system and a method of changing gear ratios thereof are disclosed. According to one embodiment, the multi-ratio rotorcraft drive system comprises a rotor system comprising one or more rotors and one or more engines. Each engine of the one or more engines is coupled to the rotor system through a multi-ratio transmission. The multi-ratio transmission comprises an output shaft coupled to the rotor system, an input shaft coupled to a respective engine of the one or more engines, a high speed clutch integrated into a high speed gear train, and a low speed clutch integrated into a low speed gear train. The high speed clutch and the low speed clutch are freewheeling clutches without a friction plate and are capable of disconnecting the output shaft and the input shaft in an overrunning condition when the output shaft spins faster than the input shaft. The multi-ratio transmission shifts between the high speed gear train and the low speed gear train by engaging or disengaging the high speed clutch and modulating speed of the coupled engine.

대표
청구항
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1. A rotorcraft drive system comprising: a rotor system comprising one or more rotors;one or more engines, each engine of the one or more engines being coupled to the rotor system through a multi-ratio transmission, the multi-ratio transmission comprising: an output shaft coupled to the rotor system;an input shaft coupled to a respective engine of the one or more engines;a high speed clutch integrated into a high speed gear train; anda low speed clutch integrated into a low speed gear train,wherein the high speed clutch and the low speed clutch are freewheeling clutches without a friction plate and are capable of disconnecting the output shaft and the input shaft in an overrunning condition when the output shaft spins faster than the input shaft; andwherein the multi-ratio transmission shifts between the high speed gear train and the low speed gear train by engaging or disengaging the high speed clutch and modulating speed of the coupled engine. 2. The rotorcraft drive system of claim 1, wherein the low speed clutch is permanently engaged. 3. The rotorcraft drive system of claim 1, wherein the output shaft of the multi-ratio transmission is coupled to the rotor system either through gears or an interconnect driveshaft system. 4. The rotorcraft drive system of claim 1, wherein the high speed clutch is selectively disengaged and engaged for respective lowering and increasing the speed of the rotor system. 5. The rotorcraft drive system of claim 1, wherein the high speed clutch and the low speed clutch are self-energizing freewheeling clutches with an overrunning capability. 6. The rotorcraft drive system of claim 1, where the rotor system does not transmit torque to the one or more engines via the high speed clutch or the low speed clutch in the overrunning condition. 7. A method of reducing the speed of a rotor system driven by one or more engines from a high speed to a low speed, the method comprising: lowering the speed of the rotor system from the high speed to a transitional speed;shifting a first multi-ratio transmission coupled to a first engine of the one or more engines from a high gear train integrating a high speed clutch to a low gear train integrating a low speed clutch while the speed of the rotor system is maintained at or near the transitional speed;shifting a second multi-ratio transmission coupled to a second engine of the one or more engines from a high gear train integrating a high speed clutch to a low gear train integrating a low speed clutch while the speed of the rotor system is maintained at or near the transitional speed; andrestoring the speed of the first engine and second engine to an optimum engine speed, causing the speed of the rotor system to be reduced to the low speed. 8. The method of claim 7, wherein the lowering the speed of the rotor system from the high speed to a transitional speed further comprising: lowering the speed of the first engine just below the transitional speed of the rotor system;disengaging the high speed clutch of the first multi-ratio transmission; andramping the speed of the first engine to match the transitional speed of the rotor system. 9. The method of claim 7, wherein the lowering the speed of the rotor system from the high speed to a transitional speed further comprising: lowering the speed of the second engine just below the transitional speed of the rotor system;disengaging the high speed clutch of the second multi-ratio transmission; andramping the speed of the second engine to the transitional speed of the rotor system. 10. The method of claim 7, wherein the low speed clutch of the first multi-ratio transmission and the low speed clutch of second multi-ratio transmission are permanently engaged. 11. The method of claim 7, wherein the high speed clutch of the first multi-ratio transmission and the high speed clutch of second multi-ratio transmission are selectively disengaged and engaged for respective lowering and increasing the speed of the rotor system. 12. The method of claim 7, wherein the high speed clutch and the low speed clutch of the first multi-ratio transmission and second multi-ratio transmission are self-energizing freewheeling clutches with an overrunning capability. 13. A method of increasing the speed of a rotor system driven by one or more engines from a low speed to a high speed, the method comprising: increasing the speed of the rotor system from the low speed to a transitional speed;shilling a first multi-ratio transmission coupled to a first engine of the one or more engines from a low gear train integrating a low speed clutch to a high gear train integrating a high speed clutch while the speed of the rotor system is maintained at or near the transitional speed;shifting a second multi-ratio transmission coupled to a second engine of the one or more engines from a low gear train integrating a low speed clutch to a high gear train integrating a high speed clutch while the speed of the rotor system is maintained at or near the transitional speed; andrestoring the speed of the first engine and second engine to an optimum engine speed, causing the speed of the rotor system to be increased to the high speed. 14. The method of claim 13, wherein the increasing the speed of the rotor system from the low speed to a transitional speed further comprising: lowering the speed of the first engine just below the transitional speed of the rotor system;engaging the high speed clutch of the first multi-ratio transmission; andramping the speed of the first engine to match the transitional speed of the rotor system. 15. The method of claim 13, wherein the increasing the speed of the rotor system from the low speed to a transitional speed further comprising: lowering the speed of the second engine just below the transitional speed of the rotor system;engaging the high speed clutch of the second multi-ratio transmission; andramping the speed of the second engine to the transitional speed of the rotor system. 16. The method of claim 13, wherein the low speed clutch of the first multi-ratio transmission and the low speed clutch of second multi-ratio transmission are permanently engaged. 17. The method of claim 13, wherein the high speed clutch of the first multi-ratio transmission and the high speed clutch of second multi-ratio transmission are selectively disengaged and engaged for respective lowering and increasing the speed of the rotor system. 18. The method of claim 13, wherein the high speed clutch and the low speed clutch of the first multi-ratio transmission and second multi-ratio transmission are self-energizing freewheeling clutches with an overrunning capability.

이 특허에 인용된 특허 (13)

이 특허를 인용한 특허 피인용횟수: 8

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특허 상세정보

Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof

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이 특허에 인용된 특허 (13)

이 특허를 인용한 특허 피인용횟수: 8

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Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof

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이 특허에 인용된 특허 (13)

이 특허를 인용한 특허 피인용횟수: 8

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