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1. 发明授权

US09234576B2 Integrated gearbox lube and control system 有权
标题翻译：集成齿轮箱润滑油和控制系统
公开(公告)号：US09234576B2
公开(公告)日：2016-01-12
申请号：US13711137
申请日：2012-12-11
申请人： Timothy P. Walgren, Jr. , Dean A. Norem , Charles L. DeGeorge , Alex Rak , Raymond N. Weyl , Ricky D. Reimers
发明人： Timothy P. Walgren, Jr. , Dean A. Norem , Charles L. DeGeorge , Alex Rak , Raymond N. Weyl , Ricky D. Reimers
IPC分类号： F16H47/00 , F16H61/00
CPC分类号： F16H57/0446 , F16H61/0009 , F16H61/0021 , F16H61/0025 , F16H61/0265 , F16H2061/0037 , Y10T74/19163
摘要： A gearbox system includes a gearbox having integrated therein a pump system, a plurality of fluid passages and a clutch control system. The pump system is in fluid communication with the clutch control system via the fluid passages to flow at least one pressurized stream. A first pressurized stream controls a first pressure-responsive device included in the clutch control system. The gearbox system further includes a hydro-mechanical control unit (HMCU) in fluid communication with the gearbox to receive a second pressurized stream and to generate at least one actuator control stream. The actuator control stream controls an actuator integrated in the gearbox.
摘要翻译：齿轮箱系统包括其中集成有泵系统，多个流体通道和离合器控制系统的变速箱。泵系统经由流体通道与离合器控制系统流体连通以流动至少一个加压流。第一加压流控制包括在离合器控制系统中的第一压力响应装置。齿轮箱系统还包括与齿轮箱流体连通以接收第二加压流并产生至少一个致动器控制流的液压 - 机械控制单元（HMCU）。致动器控制流控制集成在变速箱中的致动器。

2. 发明授权

US09038801B2 Clutch with pressure sustaining system 有权
标题翻译：离合器与压力维持系统
公开(公告)号：US09038801B2
公开(公告)日：2015-05-26
申请号：US13524538
申请日：2012-06-15
申请人： Dean A. Norem , Alex Rak , Timothy P. Walgren , Raymond N. Weyl , Ricky D. Reimers , Charles E. Long
发明人： Dean A. Norem , Alex Rak , Timothy P. Walgren , Raymond N. Weyl , Ricky D. Reimers , Charles E. Long
IPC分类号： B64C27/12 , F16D25/02 , F16D48/02 , B64D35/00
CPC分类号： F16D25/02 , B64D35/00 , F16D25/0638 , F16D2048/0218
摘要： An assembly includes an output shaft, an input shaft with an internal reservoir, and a clutch. The clutch is adapted to selectively engage and couple the input shaft to the output shaft. The clutch has a pressure chamber that communicates with the reservoir of the input shaft. The reservoir has a sufficient volume to provide the pressure chamber with a fluid pressure adequate to maintain engagement of the clutch during an interruption of a fluid supply to the input shaft and clutch.
摘要翻译：组件包括输出轴，具有内部容器的输入轴和离合器。离合器适于选择性地将输入轴接合并连接到输出轴。离合器具有与输入轴的储存器连通的压力室。储存器具有足够的体积，以在压力室向输入轴和离合器中断流体供应期间提供足够的流体压力以保持离合器的接合。

3. 发明申请

US20130334360A1 CLUTCH WITH PRESSURE SUSTAINING SYSTEM 有权
标题翻译：离合器与压力继续系统
公开(公告)号：US20130334360A1
公开(公告)日：2013-12-19
申请号：US13524538
申请日：2012-06-15
申请人： Dean A. Norem , Alex Rak , Timothy P. Walgren , Raymond N. Weyl , Ricky D. Reimers , Charles E. Long
发明人： Dean A. Norem , Alex Rak , Timothy P. Walgren , Raymond N. Weyl , Ricky D. Reimers , Charles E. Long
IPC分类号： B64C27/12 , B64D35/00 , F16D25/12
CPC分类号： F16D25/02 , B64D35/00 , F16D25/0638 , F16D2048/0218
摘要： An assembly includes an output shaft, an input shaft with an internal reservoir, and a clutch. The clutch is adapted to selectively engage and couple the input shaft to the output shaft. The clutch has a pressure chamber that communicates with the reservoir of the input shaft. The reservoir has a sufficient volume to provide the pressure chamber with a fluid pressure adequate to maintain engagement of the clutch during an interruption of a fluid supply to the input shaft and clutch.
摘要翻译：组件包括输出轴，具有内部容器的输入轴和离合器。离合器适于选择性地将输入轴接合并连接到输出轴。离合器具有与输入轴的储存器连通的压力室。储存器具有足够的体积，以在压力室向输入轴和离合器中断流体供应期间提供足够的流体压力以保持离合器的接合。

4. 发明授权

US08827204B2 Clutch system for rotary-wing aircraft with secondary thrust system 有权
标题翻译：具有二次推力系统的旋翼飞机离合器系统
公开(公告)号：US08827204B2
公开(公告)日：2014-09-09
申请号：US13349059
申请日：2012-01-12
申请人： Charles E. Long , Dean A. Norem , Raymond N. Weyl , Ricky D. Reimers
发明人： Charles E. Long , Dean A. Norem , Raymond N. Weyl , Ricky D. Reimers
IPC分类号： B64D35/00 , B64C27/22 , B64C29/00
CPC分类号： B64C27/12 , B64C27/10 , B64C27/22 , B64D35/04
摘要： An aircraft includes a powerplant system operable to power a main rotor system and a secondary thrust system, the secondary thrust system is selectively driven through operation of a clutch system, and a clutch system synchronization time corresponds to a response time of the powerplant system.
摘要翻译：飞机包括可操作以对主转子系统和次推力系统供电的动力装置系统，通过离合器系统的操作选择性地驱动二次推力系统，并且离合器系统同步时间对应于动力装置系统的响应时间。

5. 发明授权

US5265996A Regenerative pump with improved suction 失效
标题翻译：再生泵具有改进的吸力
公开(公告)号：US5265996A
公开(公告)日：1993-11-30
申请号：US850446
申请日：1992-03-10
申请人： Paul E. Westhoff , Ricky D. Reimers
发明人： Paul E. Westhoff , Ricky D. Reimers
IPC分类号： F04D5/00 , F04D29/18 , F01D1/12
CPC分类号： F04D5/002 , F04D29/188
摘要： Poor inlet suction characteristics in regenerative pumps may be avoided in a construction including a housing (10) having an impeller receiving cavity (20) with a circular impeller (22) therein. Channel-like annular grooves (32, 34) are disposed in the housing (10) and open to the cavity (20) at sides (36, 38) of the impeller (22). An outlet seal (63) is located in each of the grooves (32, 34) and outlet ports (62) opening to the grooves (32, 34) are located just upstream of the outlet seal (63). Peripheral recesses (42, 44) are located in the impeller sides (36, 38) and have radially inner extremities (59) located radially inward of the channels (32, 34). A plurality of blades (52) are mounted to the impeller (22) within the recesses (42, 44) around the periphery thereof and have radially inner edges (54) spaced from the radially inner recess extremities (59) while being isolated from recirculation within the channels ( 32, 34). An inlet port (70) is disposed in the housing (10) and is located between the radially inner extremity of the grooves (42, 44) and the radially inner edges (54) of the blades (52).
摘要翻译：在包括具有在其中具有圆形叶轮（22）的叶轮容纳腔（20）的壳体（10）的结构中，可以避免再生泵中的较差的入口抽吸特性。通道状的环形槽（32,34）设置在壳体（10）中并且在叶轮（22）的侧面（36,38）处向空腔（20）开口。出口密封件（63）位于每个凹槽（32,34）中，并且通向凹槽（32,34）的出口（62）位于出口密封件（63）的正上方。外围凹部（42,44）位于叶轮侧（36,38）中，并具有位于通道（32,34）径向内侧的径向内端（59）。多个叶片（52）围绕其周边在凹部（42,44）内安装到叶轮（22）上，并且具有与径向内凹槽末端（59）间隔开的径向内边缘（54），同时与再循环在通道（32,34）内。入口端口（70）设置在壳体（10）中并且位于凹槽（42,44）的径向内部末端和叶片（52）的径向内边缘（54）之间。

6. 发明申请

US20140157955A1 INTEGRATED GEARBOX LUBE AND CONTROL SYSTEM 有权
标题翻译：集成齿轮油和控制系统
公开(公告)号：US20140157955A1
公开(公告)日：2014-06-12
申请号：US13711137
申请日：2012-12-11
申请人： Timothy P. Walgren, JR. , Dean A. Norem , Charles L. DeGeorge , Alex Rak , Raymond N. Weyl , Ricky D. Reimers
发明人： Timothy P. Walgren, JR. , Dean A. Norem , Charles L. DeGeorge , Alex Rak , Raymond N. Weyl , Ricky D. Reimers
IPC分类号： F16H61/00
CPC分类号： F16H57/0446 , F16H61/0009 , F16H61/0021 , F16H61/0025 , F16H61/0265 , F16H2061/0037 , Y10T74/19163
摘要： A gearbox system includes a gearbox having integrated therein a pump system, a plurality of fluid passages and a clutch control system. The pump system is in fluid communication with the clutch control system via the fluid passages to flow at least one pressurized stream. A first pressurized stream controls a first pressure-responsive device included in the clutch control system. The gearbox system further includes a hydro-mechanical control unit (HMCU) in fluid communication with the gearbox to receive a second pressurized stream and to generate at least one actuator control stream. The actuator control stream controls an actuator integrated in the gearbox.
摘要翻译：齿轮箱系统包括其中集成有泵系统，多个流体通道和离合器控制系统的变速箱。泵系统经由流体通道与离合器控制系统流体连通以流动至少一个加压流。第一加压流控制包括在离合器控制系统中的第一压力响应装置。齿轮箱系统还包括与齿轮箱流体连通以接收第二加压流并产生至少一个致动器控制流的液压 - 机械控制单元（HMCU）。致动器控制流控制集成在变速箱中的致动器。

7. 发明申请

US20130181087A1 CLUTCH SYSTEM FOR ROTARY-WING AIRCRAFT WITH SECONDARY THRUST SYSTEM 有权
标题翻译：具有次级系统的旋转飞行器离合器系统
公开(公告)号：US20130181087A1
公开(公告)日：2013-07-18
申请号：US13349059
申请日：2012-01-12
申请人： Charles E. Long , Dean A. Norem , Raymond N. Weyl , Ricky D. Reimers
发明人： Charles E. Long , Dean A. Norem , Raymond N. Weyl , Ricky D. Reimers
IPC分类号： B64C27/82 , B60W10/02 , B64D35/00
CPC分类号： B64C27/12 , B64C27/10 , B64C27/22 , B64D35/04
摘要： An aircraft includes a powerplant system operable to power a main rotor system and a secondary thrust system, the secondary thrust system is selectively driven through operation of a clutch system, and a clutch system synchronization time corresponds to a response time of the powerplant system.
摘要翻译：飞机包括可操作以对主转子系统和次推力系统供电的动力装置系统，通过离合器系统的操作选择性地驱动二次推力系统，并且离合器系统同步时间对应于动力装置系统的响应时间。

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