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公开(公告)号：US20120208670A1
公开(公告)日：2012-08-16
申请号：US13418179
申请日：2012-03-12
IPC分类号： B60W10/04
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.
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公开(公告)号：US08863924B2
公开(公告)日：2014-10-21
申请号：US13615711
申请日：2012-09-14
申请人： Ryan T. Ehinger , Eric S. Olson
发明人： Ryan T. Ehinger , Eric S. Olson
CPC分类号： F16D41/06 , F16D1/0858 , Y10T29/49826
摘要： A hybrid overrunning clutch includes a metal outer race and a composite outer ring that are each sized and configured such that the metal race generates a preload on the composite outer race throughout the operational temperature of the clutch. The composite outer ring significantly reduces that total weight of the clutch, as compared to a completely metal outer race. The present application further includes a method of assembling the metal outer race and composite outer ring so that thermal expansion of the metal outer race creates the preload in the composite outer ring. The present application also includes a method of designing a hybrid overrunning clutch.
摘要翻译： 混合超越离合器包括金属外圈和复合外圈，每个尺寸和构造使得金属外圈在整个离合器的操作温度下在复合外圈上产生预载。 与完全金属外圈相比，复合外环显着地减少了离合器的总重量。 本申请还包括组装金属外圈和复合外圈的方法，使得金属外圈的热膨胀在复合外圈中产生预载。 本申请还包括设计混合超越离合器的方法。
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公开(公告)号：US08454475B2
公开(公告)日：2013-06-04
申请号：US13418161
申请日：2012-03-12
IPC分类号： B60W10/04
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.
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公开(公告)号：US20110030503A1
公开(公告)日：2011-02-10
申请号：US12811937
申请日：2008-01-07
CPC分类号： F16C35/077 , F16C2326/43 , Y10T74/2186
摘要： A housing assembly for use in a rotorcraft includes a housing having an opening, a bearing configured to radially and/or axially support a shaft that is adapted to rotate, the bearing disposed within the opening of the housing, and a liner arranged between the housing and the bearing. The liner is made of a material selected from the group consisting of ceramic material, ceramic coated material, ceramic and metallic hybrid material, lightweight metallic material, lightweight metallic alloy material and lightweight metallic coated material.
摘要翻译： 用于旋翼航空器的壳体组件包括具有开口的壳体，构造成径向和/或轴向地支撑适于旋转的轴，设置在壳体的开口内的轴承以及布置在壳体之间的衬套 和轴承。 衬套由选自陶瓷材料，陶瓷涂层材料，陶瓷和金属混合材料，轻质金属材料，轻质金属合金材料和轻质金属涂层材料组成的组成。
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5.发明授权Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof 有权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
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。
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公开(公告)号：US20130117997A1
公开(公告)日：2013-05-16
申请号：US13294686
申请日：2011-11-11
申请人： Ryan T. Ehinger , Wayland Hill , Doug Mueller
发明人： Ryan T. Ehinger , Wayland Hill , Doug Mueller
CPC分类号： F16B4/004 , Y10T29/49963
摘要： A system and method for installing a fastener rod is provided. In one embodiment a fastener rod starter apparatus is provided and may include a first end for engaging a fastener rod, a second end for insertion into an insertion hole, and an elongated body of closed cell foam having sufficiently low density and high compressibility to displace fluid in the insertion hole and be compressed to allow installation of the fastener rod into the insertion hole. A method for installing a fastener rod may include lubricating an insertion hole with a fluid and inserting a starter element into the insertion hole. The starter element may have sufficiently low density and high compressibility to displace the fluid in the insertion hole and be compressed by the fastener rod inserted into the insertion hole.
摘要翻译： 提供一种用于安装拉杆的系统和方法。 在一个实施例中，提供了紧固件起动器装置，并且可以包括用于接合紧固件杆的第一端，用于插入到插入孔中的第二端和具有足够低密度和高可压缩性的细胞泡沫体的细长体以移置流体 在插入孔中并被压缩以允许将拉链安装到插入孔中。 用于安装紧固件杆的方法可以包括用流体润滑插入孔并将起动器元件插入到插入孔中。 启动器元件可以具有足够低的密度和高的可压缩性，以使插入孔中的流体移位并被插入到插入孔中的拉杆压缩。
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公开(公告)号：US20130098732A1
公开(公告)日：2013-04-25
申请号：US13615711
申请日：2012-09-14
申请人： Ryan T. Ehinger , Eric S. Olson
发明人： Ryan T. Ehinger , Eric S. Olson
CPC分类号： F16D41/06 , F16D1/0858 , Y10T29/49826
摘要： A hybrid overrunning clutch includes a metal outer race and a composite outer ring that are each sized and configured such that the metal race generates a preload on the composite outer race throughout the operational temperature of the clutch. The composite outer ring significantly reduces that total weight of the clutch, as compared to a completely metal outer race. The present application further includes a method of assembling the metal outer race and composite outer ring so that thermal expansion of the metal outer race creates the preload in the composite outer ring. The present application also includes a method of designing a hybrid overrunning clutch.
摘要翻译： 混合超越离合器包括金属外圈和复合外圈，每个尺寸和构造使得金属外圈在整个离合器的操作温度下在复合外圈上产生预载。 与完全金属外圈相比，复合外环显着地减少了离合器的总重量。 本申请还包括组装金属外圈和复合外圈的方法，使得金属外圈的热膨胀在复合外圈中产生预载。 本申请还包括设计混合超越离合器的方法。
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8.发明申请MULTI-RATIO ROTORCRAFT DRIVE SYSTEM AND A METHOD OF CHANGING GEAR RATIOS THEREOF 有权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
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。
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9.发明授权Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof 有权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
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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10.发明申请MULTI-RATIO ROTORCRAFT DRIVE SYSTEM AND A METHOD OF CHANGING GEAR RATIOS THEREOF 有权多比例转子驱动系统及其齿轮比变化方法公开(公告)号：US20110015034A1
公开(公告)日：2011-01-20
申请号：US12502596
申请日：2009-07-14
IPC分类号： B60W10/00
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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