Compact rotorcraft dual-element spherical elastomeric centrifugal-force bearing assembly
    1.
    发明授权
    Compact rotorcraft dual-element spherical elastomeric centrifugal-force bearing assembly 有权
    紧凑型旋翼飞机双元件球形弹性离心力轴承总成

    公开(公告)号:US08926281B2

    公开(公告)日:2015-01-06

    申请号:US13401203

    申请日:2012-02-21

    IPC分类号: F01D25/16

    CPC分类号: B64C27/35

    摘要: A rotary system includes a retention member and a flexible yoke having an opening forming a bridge. The rotary system is further provided with two bearing assemblies, a first bearing assembly extending through the opening of the yoke and configured to secure a rotor blade to the retention member and a second bearing assembly extending through the opening of the flexible yoke and configured to secure the rotor blade to the bridge. The second bearing element includes a bearing element having a first surface forming a spherical contouring and an opposing integral second surface forming a conical contouring.

    摘要翻译: 旋转系统包括保持构件和具有形成桥的开口的柔性轭。 旋转系统还设置有两个轴承组件,第一轴承组件延伸穿过轭的开口并且构造成将转子叶片固定到保持构件,以及延伸穿过柔性轭的开口的第二轴承组件, 转子叶片到桥。 第二轴承元件包括具有形成球形轮廓的第一表面和形成锥形轮廓的相对的整体第二表面的轴承元件。

    Compact Rotorcraft Dual-Element Spherical Elastomeric Centrifugal-Force Bearing Assembly
    2.
    发明申请
    Compact Rotorcraft Dual-Element Spherical Elastomeric Centrifugal-Force Bearing Assembly 有权
    紧凑型Rotorcraft双元件球形弹性离心力轴承组件

    公开(公告)号:US20130216384A1

    公开(公告)日:2013-08-22

    申请号:US13401203

    申请日:2012-02-21

    IPC分类号: B64C27/00

    CPC分类号: B64C27/35

    摘要: A rotary system includes a retention member and a flexible yoke having an opening forming a bridge. The rotary system is further provided with two bearing assemblies, a first bearing assembly extending through the opening of the yoke and configured to secure a rotor blade to the retention member and a second bearing assembly extending through the opening of the flexible yoke and configured to secure the rotor blade to the bridge. The second bearing element includes a bearing element having a first surface forming a spherical contouring and an opposing integral second surface forming a conical contouring.

    摘要翻译: 旋转系统包括保持构件和具有形成桥的开口的柔性轭。 旋转系统还设置有两个轴承组件,第一轴承组件延伸穿过轭的开口并且构造成将转子叶片固定到保持构件,以及延伸穿过柔性轭的开口的第二轴承组件, 转子叶片到桥。 第二轴承元件包括具有形成球形轮廓的第一表面和形成锥形轮廓的相对的整体第二表面的轴承元件。

    Hub Assembly with Grease Lubricated Roller Bearing and Tension-Torsion Strap
    4.
    发明申请
    Hub Assembly with Grease Lubricated Roller Bearing and Tension-Torsion Strap 审中-公开
    带润滑脂润滑滚子轴承和张力扭力带的轮毂组件

    公开(公告)号:US20130164129A1

    公开(公告)日:2013-06-27

    申请号:US13337215

    申请日:2011-12-26

    IPC分类号: B64C27/59

    摘要: A rotary system and method to control feathering and centrifugal forces of a rotor blade during flight. The rotary system having a hub assembly, which includes a hollow yoke arm to receive a spindle section of the rotor blade. A tension-torsion strap extends through the hollow yoke arm and couples the rotor blade and the hub assembly. The method includes allowing the spindle section of the rotor blade to pivot within the hollow yoke arm and controlling rotational and centrifugal movement of the rotor blade with the tension-torsion strap.

    摘要翻译: 一种用于在飞行中控制转子叶片的羽化和离心力的旋转系统和方法。 旋转系统具有轮毂组件,其包括用于接收转子叶片的心轴部分的中空轭臂。 张力扭力带延伸穿过中空的轭臂并联接转子叶片和轮毂组件。 该方法包括允许转子叶片的主轴部分在中空轭臂内枢转并且控制转子叶片与拉力扭力带的旋转和离心运动。

    Dual mode rotor hub assembly
    5.
    发明授权
    Dual mode rotor hub assembly 有权
    双模转子轮毂总成

    公开(公告)号:US09126680B2

    公开(公告)日:2015-09-08

    申请号:US13298033

    申请日:2011-11-16

    摘要: A rotor hub assembly and method for controlling movement of a rotor blade relative to a swashplate. The hub assembly having an attachment device operably associated with the rotor blade and the swashplate. The attachment device provides pivot and rotational blade movement relative to the swashplate. A dual spring-rate damper is operably associated with the attachment device. The damper switches between a first spring rate and a second spring rate during flight to control movement of the rotor blade. The method includes the process of switching the damper between the first spring rate and the second spring rate during flight.

    摘要翻译: 用于控制转子叶片相对于斜盘的运动的转子轮毂组件和方法。 轮毂组件具有可操作地与转子叶片和旋转斜盘相关联的附接装置。 附接装置提供相对于斜盘的枢转和旋转刀片移动。 双弹簧阻尼器与附接装置可操作地相关联。 减速器在飞行期间在第一弹簧速率和第二弹簧刚度之间切换以控制转子叶片的运动。 该方法包括在飞行期间在第一弹簧刚度和第二弹簧刚度之间切换阻尼器的过程。

    Dual Mode Rotor Hub Assembly
    6.
    发明申请
    Dual Mode Rotor Hub Assembly 有权
    双模转子毂总成

    公开(公告)号:US20130121827A1

    公开(公告)日:2013-05-16

    申请号:US13298033

    申请日:2011-11-16

    IPC分类号: B64C27/51 B21D53/78 B64C11/04

    摘要: A rotor hub assembly and method for controlling movement of a rotor blade relative to a swashplate. The hub assembly having an attachment device operably associated with the rotor blade and the swashplate. The attachment device provides pivot and rotational blade movement relative to the swashplate. A dual spring-rate damper is operably associated with the attachment device. The damper switches between a first spring rate and a second spring rate during flight to control movement of the rotor blade. The method includes the process of switching the damper between the first spring rate and the second spring rate during flight.

    摘要翻译: 用于控制转子叶片相对于斜盘的运动的转子轮毂组件和方法。 轮毂组件具有可操作地与转子叶片和旋转斜盘相关联的附接装置。 附接装置提供相对于斜盘的枢转和旋转刀片运动。 双弹簧阻尼器与附接装置可操作地相关联。 减速器在飞行期间在第一弹簧速率和第二弹簧刚度之间切换以控制转子叶片的运动。 该方法包括在飞行期间在第一弹簧刚度和第二弹簧刚度之间切换阻尼器的过程。