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11. 发明授权

US07668627B2 Mechanical flight control auxiliary power assist system 有权
标题翻译：机械飞行辅助辅助辅助系统
公开(公告)号：US07668627B2
公开(公告)日：2010-02-23
申请号：US11664664
申请日：2005-10-13
申请人： Peter M. Shultz , Carlos A. Fenny , Todd Walker , Sam Arjunan
发明人： Peter M. Shultz , Carlos A. Fenny , Todd Walker , Sam Arjunan
IPC分类号： G01C23/00
CPC分类号： B64C13/24
摘要： A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and a booster means for connecting the upstream portion to the downstream portion. The booster means may comprise dual concentric valve actuators and/or a variety of system load limiting features.
摘要翻译：公开了一种用于旋翼飞机的机械飞行控制系统。飞行控制系统包括上游部分，下游部分和用于将上游部分连接到下游部分的升压装置。增压装置可以包括双同心阀致动器和/或各种系统负载限制特征。

12. 发明授权

US07461812B2 Rotorcraft control system with stepped mixing linkage 有权
标题翻译：旋翼机控制系统采用阶梯式混合联动
公开(公告)号：US07461812B2
公开(公告)日：2008-12-09
申请号：US10528906
申请日：2003-09-19
申请人： Carlos A. Fenny , Duane Hicks
发明人： Carlos A. Fenny , Duane Hicks
IPC分类号： B64C27/52
CPC分类号： B64C27/56 , B64C13/24
摘要： A control system for a rotorcraft is disclosed. The control system includes a stepped mixing linkage, such that a selected amount of right-left lateral cyclic output is generated for certain amounts of forward-aft cyclic input. The stepped mixing linkage includes two supporting links and a floating link pivotally coupled between the two supporting links. The ratio of the lengths of the two supporting links to the length of the floating link is small, thereby generating a selected lateral sinusoidal output, a selected rotation of the sinusoidal output, and a selected ramped output in response to each forward-aft pilot input command.
摘要翻译：公开了一种用于旋翼飞机的控制系统。控制系统包括阶梯式混合连杆，使得针对一定量的前后循环输入产生选定量的左右横向循环输出。阶梯式混合联动装置包括两个支撑连杆和枢转地联接在两个支撑连杆之间的浮动连杆。两个支撑链节的长度与浮动连杆的长度之比小，从而产生选定的横向正弦输出，正弦输出的选定旋转以及响应于每个前后导频输入的选定斜坡输出命令。

13. 发明授权

US07165950B2 Two-stage pressure relief valve 有权
标题翻译：两级减压阀
公开(公告)号：US07165950B2
公开(公告)日：2007-01-23
申请号：US10736161
申请日：2003-12-15
申请人： Carlos A. Fenny , Darrel B. Bryan , David P. Schultz
发明人： Carlos A. Fenny , Darrel B. Bryan , David P. Schultz
IPC分类号： F04B1/26 , F04B49/24 , F15B21/02 , F16D31/02 , F04F1/00
CPC分类号： F15B13/024 , F04B1/2042 , F04B3/006 , F15B20/007 , F15B2211/20546 , F15B2211/50518 , F15B2211/511 , F15B2211/5157 , F15B2211/528 , F15B2211/8752 , Y10T137/2761
摘要： A two-stage pressure relief valve for use with hydraulic systems is disclosed. The two-stage pressure relief valve has a first stage that relieves increases in hydraulic system pressure over the normal operating pressure and up to a selected threshold pressure level, and a second stage that brings the hydraulic system pressure down to a selected reduced operating pressure that is below the normal operating pressure in response to increases in the operating pressure over the threshold pressure level.
摘要翻译：公开了一种用于液压系统的两级减压阀。两级减压阀具有第一级，其减轻液压系统压力在正常工作压力和高达所选阀值压力水平之上的增加，以及将液压系统压力降低至所选择的降低的操作压力的第二级，响应于超过阈值压力水平的操作压力的增加而低于正常工作压力。

14. 发明授权

US08857757B2 Independent blade control system with hydraulic pitch link 有权
标题翻译：具有液压节距连接的独立叶片控制系统
公开(公告)号：US08857757B2
公开(公告)日：2014-10-14
申请号：US13565554
申请日：2012-08-02
申请人： Carlos A. Fenny
发明人： Carlos A. Fenny
IPC分类号： B64C27/64 , B64C27/72
CPC分类号： B64C27/605 , B64C27/72 , B64C2027/7216 , F15B15/261 , Y02T50/34
摘要： According to one embodiment, a rotorcraft pitch link includes a housing and a piston assembly. The housing comprises a first chamber and a second chamber. A first housing opening allows a first fluid to flow into the first chamber, and a second housing allows a second fluid to flow into the second chamber. The piston assembly is at least partially disposed within the housing and comprises a piston head and a piston rod coupled to the piston head. The piston head separates the first chamber from the second chamber.
摘要翻译：根据一个实施例，旋翼航空桨距连杆包括壳体和活塞组件。壳体包括第一室和第二室。第一壳体开口允许第一流体流入第一腔室，而第二壳体允许第二流体流入第二腔室。活塞组件至少部分地设置在壳体内，并且包括联接到活塞头的活塞头和活塞杆。活塞头将第一室与第二室分开。

15. 发明申请

US20140234102A1 RADIAL FLUID DEVICE WITH VARIABLE PHASE AND AMPLITUDE 有权
标题翻译：具有可变相和放大器的径向流体装置
公开(公告)号：US20140234102A1
公开(公告)日：2014-08-21
申请号：US13565496
申请日：2012-08-02
申请人： Carlos A. Fenny
发明人： Carlos A. Fenny
IPC分类号： B64C27/64 , B64C27/605
CPC分类号： B64C27/64 , B64C27/605 , B64C27/72 , B64C2027/7216 , F15B7/001 , F15B7/003 , Y02T50/34
摘要： According to one embodiment, a radial fluid device comprises a cylinder block, first and second pluralities of pistons, a first cam disposed about the first plurality of radially extending cylinders, and a second cam disposed about the second plurality of radially extending cylinders. The direction of rotation of the second cam is independent of the direction of rotation of the first cam.
摘要翻译：根据一个实施例，径向流体装置包括气缸体，第一和第二多个活塞，围绕第一多个径向延伸的气缸设置的第一凸轮和围绕第二多个径向延伸的气缸设置的第二凸轮。第二凸轮的旋转方向与第一凸轮的旋转方向无关。

16. 发明申请

US20140231579A1 RADIAL FLUID DEVICE WITH MULTI-HARMONIC OUTPUT 有权
标题翻译：具有多谐波输出的径向流体装置
公开(公告)号：US20140231579A1
公开(公告)日：2014-08-21
申请号：US13565526
申请日：2012-08-02
申请人： Carlos A. Fenny
发明人： Carlos A. Fenny
IPC分类号： B64C27/64 , B64C27/06 , B64C27/12 , B64C27/605
CPC分类号： B64C27/64 , B64C27/06 , B64C27/12 , B64C27/605 , B64C27/72 , B64C2027/7216 , F04B1/047 , F04B1/0474 , F15B7/00 , F15B7/001 , F15B7/003 , Y02T50/34
摘要： According to one embodiment, a radial fluid device comprises a cylinder block, first and second pluralities of pistons, a first cam disposed about the first plurality of radially extending cylinders, and a second cam disposed about the second plurality of radially extending cylinders. The second cam has at least one more lobe than the first cam.
摘要翻译：根据一个实施例，径向流体装置包括气缸体，第一和第二多个活塞，围绕第一多个径向延伸的气缸设置的第一凸轮和围绕第二多个径向延伸的气缸设置的第二凸轮。第二凸轮具有比第一凸轮至少多一个凸角。

17. 发明申请

US20140034777A1 INDEPENDENT BLADE CONTROL SYSTEM WITH HYDRAULIC PITCH LINK 有权
标题翻译：独立叶片控制系统与液压连接
公开(公告)号：US20140034777A1
公开(公告)日：2014-02-06
申请号：US13565554
申请日：2012-08-02
申请人： Carlos A. Fenny
发明人： Carlos A. Fenny
IPC分类号： B64C27/64 , F01D7/00
CPC分类号： B64C27/605 , B64C27/72 , B64C2027/7216 , F15B15/261 , Y02T50/34
摘要： According to one embodiment, a rotorcraft pitch link includes a housing and a piston assembly. The housing comprises a first chamber and a second chamber. A first housing opening allows a first fluid to flow into the first chamber, and a second housing allows a second fluid to flow into the second chamber. The piston assembly is at least partially disposed within the housing and comprises a piston head and a piston rod coupled to the piston head. The piston head separates the first chamber from the second chamber.
摘要翻译：根据一个实施例，旋翼航空桨距连杆包括壳体和活塞组件。壳体包括第一室和第二室。第一壳体开口允许第一流体流入第一腔室，而第二壳体允许第二流体流入第二腔室。活塞组件至少部分地设置在壳体内，并且包括联接到活塞头的活塞头和活塞杆。活塞头将第一室与第二室分开。

18. 发明授权

US08500597B2 Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof 有权
标题翻译：多比旋翼航空器驱动系统及其变速比的改变方法
公开(公告)号：US08500597B2
公开(公告)日：2013-08-06
申请号：US13418179
申请日：2012-03-12
申请人： Ryan T. Ehinger , Carlos A. Fenny , Charles J. Kilmain , Eric A. Sinusas , Kevin Worrell
发明人： Ryan T. Ehinger , Carlos A. Fenny , Charles J. Kilmain , Eric A. Sinusas , Kevin Worrell
IPC分类号： B60K5/08
CPC分类号： B64C27/08 , B64C27/12 , Y10T477/20 , Y10T477/27 , Y10T477/638 , Y10T477/6414 , Y10T477/6422 , Y10T477/69335
摘要： 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.
摘要翻译：公开了一种多比例旋翼航空器驱动系统及其变速比的改变方法。根据一个实施例，多比例旋翼航空器驱动系统包括包括一个或多个转子和一个或多个发动机的转子系统。一个或多个发动机的每个发动机通过多比率变速器联接到转子系统。多比率变速器包括联接到转子系统的输出轴，联接到一个或多个发动机的相应发动机的输入轴，集成到高速齿轮系中的高速离合器和集成在其中的低速离合器低速齿轮系。高速离合器和低速离合器是没有摩擦板的续流离合器，当输出轴旋转速度高于输入轴时，能够以超越状态将输出轴和输入轴断开。

19. 发明申请

US20120214642A1 MULTI-RATIO ROTORCRAFT DRIVE SYSTEM AND A METHOD OF CHANGING GEAR RATIOS THEREOF 有权
标题翻译：多比例转子驱动系统及其齿轮比变化方法
公开(公告)号：US20120214642A1
公开(公告)日：2012-08-23
申请号：US13418161
申请日：2012-03-12
申请人： RYAN T. EHINGER , Carlos A. Fenny , Charles J. Kilmain , Eric A. Sinusas , Kevin Worrell
发明人： RYAN T. EHINGER , Carlos A. Fenny , Charles J. Kilmain , Eric A. Sinusas , Kevin Worrell
IPC分类号： B60W10/02
CPC分类号： B64C27/08 , B64C27/12 , Y10T477/20 , Y10T477/27 , Y10T477/638 , Y10T477/6414 , Y10T477/6422 , Y10T477/69335
摘要： 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.
摘要翻译：公开了一种多比例旋翼航空器驱动系统及其变速比的改变方法。根据一个实施例，多比例旋翼航空器驱动系统包括包括一个或多个转子和一个或多个发动机的转子系统。一个或多个发动机的每个发动机通过多比率变速器联接到转子系统。多比率变速器包括联接到转子系统的输出轴，联接到一个或多个发动机的相应发动机的输入轴，集成到高速齿轮系中的高速离合器和集成在其中的低速离合器低速齿轮系。高速离合器和低速离合器是没有摩擦板的续流离合器，当输出轴旋转速度高于输入轴时，能够以超越状态将输出轴和输入轴断开。

20. 发明授权

US08133155B2 Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof 有权
标题翻译：多比旋翼航空器驱动系统及其变速比的改变方法
公开(公告)号：US08133155B2
公开(公告)日：2012-03-13
申请号：US12502596
申请日：2009-07-14
申请人： Ryan T. Ehinger , Carlos A. Fenny , Charles J. Kilmain , Eric A. Sinusas , Kevin Worrell
发明人： Ryan T. Ehinger , Carlos A. Fenny , Charles J. Kilmain , Eric A. Sinusas , Kevin Worrell
IPC分类号： F16H59/30
CPC分类号： B64C27/08 , B64C27/12 , Y10T477/20 , Y10T477/27 , Y10T477/638 , Y10T477/6414 , Y10T477/6422 , Y10T477/69335
摘要： 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.
摘要翻译：公开了一种多比例旋翼航空器驱动系统及其变速比的改变方法。根据一个实施例，多比例旋翼航空器驱动系统包括包括一个或多个转子和一个或多个发动机的转子系统。一个或多个发动机的每个发动机通过多比率变速器联接到转子系统。多比率变速器包括联接到转子系统的输出轴，联接到一个或多个发动机的相应发动机的输入轴，集成到高速齿轮系中的高速离合器和集成在其中的低速离合器低速齿轮系。高速离合器和低速离合器是没有摩擦板的续流离合器，当输出轴旋转速度比输入轴快时，能够以超越状态将输出轴和输入轴断开。高速齿轮系和低速齿轮系之间的多比率传动通过使高速离合器接合或分离并调节联接的发动机的速度而移动。

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