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    Yoke and bearing fitting assembly for rotors
    2.
    发明授权
    Yoke and bearing fitting assembly for rotors 有权
    用于转子的轭和轴承配件组件

    公开(公告)号：US08360727B2

    公开(公告)日：2013-01-29

    申请号：US13144510

    申请日：2009-01-19

    申请人： Frank B. Stamps ,  Patrick R. Tisdale ,  Thomas C. Campbell ,  Richard E. Rauber ,  James L. Braswell, Jr.

    发明人： Frank B. Stamps ,  Patrick R. Tisdale ,  Thomas C. Campbell ,  Richard E. Rauber ,  James L. Braswell, Jr.

    IPC分类号： B64C27/37

    CPC分类号： B64C27/33 ,  B64C27/32

    摘要： A yoke and bearing fitting assembly for a multi-blade aircraft rotor is disclosed. The assembly has a yoke having arms extending generally radially from a central portion of the yoke, the arms each having opposing surfaces. An aperture is formed in each arm and extends between the surfaces. A bearing fitting has a body configured for insertion into the aperture of the yoke and has two rims protruding from a periphery of the body, the body also having a bearing mount adapted for mounting a pitch change bearing assembly to the yoke. Each rim abuts one of the surfaces of the associated yoke arm when the bearing fitting is installed within the aperture, so as to create clamping forces between the rims and the arm and the arm. The bearing fitting transmits forces from the pitch bearing assembly into the yoke.

    摘要翻译： 公开了一种用于多叶片飞行器转子的轭和轴承配件组件。 组件具有轭，其具有从轭的中心部分大致径向延伸的臂，每个臂具有相对的表面。 在每个臂中形成一个孔，并在表面之间延伸。 轴承配件具有构造成用于插入轭的孔中的主体，并且具有从主体的周边突出的两个轮缘，该主体还具有适于将变桨轴承组件安装到轭的轴承座。 当轴承配件安装在孔内时，每个轮辋邻接相关联的轭臂的一个表面，以便在轮辋与臂和臂之间产生夹紧力。 轴承配件将变桨轴承组件的力传递到轭架中。

    Yoke and Bearing Fitting Assembly for Rotors
    7.
    发明申请
    Yoke and Bearing Fitting Assembly for Rotors 有权
    转子的轭和轴承配件组件

    公开(公告)号：US20110274550A1

    公开(公告)日：2011-11-10

    申请号：US13144510

    申请日：2009-01-19

    申请人： Frank B. Stamps ,  Patrick R. Tisdale ,  Thomas C. Campbell ,  Richard E. Rauber ,  James L. Braswell

    发明人： Frank B. Stamps ,  Patrick R. Tisdale ,  Thomas C. Campbell ,  Richard E. Rauber ,  James L. Braswell

    IPC分类号： B64C11/04

    CPC分类号： B64C27/33 ,  B64C27/32

    摘要： A yoke and bearing fitting assembly for a multi-blade aircraft rotor is disclosed. The assembly has a yoke having arms extending generally radially from a central portion of the yoke, the arms each having opposing surfaces. An aperture is formed in each arm and extends between the surfaces. A bearing fitting has a body configured for insertion into the aperture of the yoke and has two rims protruding from a periphery of the body, the body also having a bearing mount adapted for mounting a pitch change bearing assembly to the yoke. Each rim abuts one of the surfaces of the associated yoke arm when the bearing fitting is installed within the aperture, so as to create clamping forces between the rims and the arm and the arm. The bearing fitting transmits forces from the pitch bearing assembly into the yoke.

    摘要翻译： 公开了一种用于多叶片飞行器转子的轭和轴承配件组件。 组件具有轭，其具有从轭的中心部分大致径向延伸的臂，每个臂具有相对的表面。 在每个臂中形成一个孔，并在表面之间延伸。 轴承配件具有构造成用于插入轭的孔中并具有从主体的周边突出的两个轮缘的主体，该主体还具有适于将变桨轴承组件安装到轭的轴承座。 当轴承配件安装在孔内时，每个轮辋邻接相关联的轭臂的一个表面，以便在轮辋与臂和臂之间产生夹紧力。 轴承配件将变桨轴承组件的力传递到轭架中。

    Multiple-Yoke Main Rotor Assembly
    8.
    发明申请
    Multiple-Yoke Main Rotor Assembly 有权
    多重主转子总成

    公开(公告)号：US20130149151A1

    公开(公告)日：2013-06-13

    申请号：US13324363

    申请日：2011-12-13

    申请人： Richard E. Rauber ,  Frank B. Stamps ,  David A. Popelka ,  Patrick R. Tisdale ,  Tommie L. Wood

    发明人： Richard E. Rauber ,  Frank B. Stamps ,  David A. Popelka ,  Patrick R. Tisdale ,  Tommie L. Wood

    IPC分类号： B64C27/43 ,  B64C27/39

    CPC分类号： B64C27/43 ,  B64C29/0033

    摘要： The present application includes a main rotor assembly for an aircraft. The rotor assembly has a main rotor mast configured for rotation about a mast axis and two yokes pivotally connected to the mast for rotation therewith about the mast axis. Each yoke is independently pivotable relative to the mast about at least one flap axis that is generally perpendicular to the mast axis. In at least one embodiment, a torque splitter connects the yokes and allows for limited rotation of the yokes relative to each other about the mast axis. Each yoke is configured for the attachment of rotor blades extending generally radially relative to the mast axis.

    摘要翻译： 本申请包括用于飞机的主转子组件。 转子组件具有构造成围绕桅杆轴线旋转的主转子桅杆和两个枢转地连接到桅杆的轭架，用于围绕桅杆轴线旋转。 每个轭体可相对于桅杆独立地枢转，围绕大体上垂直于桅杆轴线的至少一个翼片轴线。 在至少一个实施例中，扭矩分配器连接轭，并且允许轭围绕桅杆轴线相对于彼此受到有限的旋转。 每个轭被构造成用于附接相对于桅杆轴线大致径向延伸的转子叶片。

    Aircraft rotor with discrete flap hinge
    9.
    发明授权
    Aircraft rotor with discrete flap hinge 有权
    具有离散翼片铰链的飞机转子

    公开(公告)号：US09352830B2

    公开(公告)日：2016-05-31

    申请号：US13455814

    申请日：2012-04-25

    申请人： Frank B. Stamps ,  David A. Popelka ,  Tom Donovan ,  Patrick R. Tisdale ,  Richard E. Rauber

    发明人： Frank B. Stamps ,  David A. Popelka ,  Tom Donovan ,  Patrick R. Tisdale ,  Richard E. Rauber

    IPC分类号： B64C27/39 ,  B64C27/48

    CPC分类号： B64C27/39 ,  B64C27/48

    摘要： An aircraft rotor assembly has upper and lower hub plates adapted to be mounted to a central rotor mast for rotation therewith. A plurality of radial arms is connected to at least two flap bearings mounted between the hub plates and forming a discrete flap hinge, each flap hinge defining a flap axis and allowing rotation of the associated arm relative to the hub plates and about the corresponding flap axis. Each of a plurality of blade grips is rotatably connected to one of the arms for rotation about a pitch axis and adapted for mounting of a blade to each blade grip, such that each blade is capable of rotation with the grip about the pitch axis and capable of rotation together with the corresponding arm relative to the hub plates and about the corresponding flap axis.

    摘要翻译： 飞机转子组件具有适于安装到中心转子桅杆上的上和下毂板，以与其一起旋转。 多个径向臂连接到安装在轮毂板之间并形成离散的翼片铰链的至少两个翼片轴承，每个翼片铰链限定翼片轴线并允许相关联的臂相对于轮毂板和相应翼片轴线的旋转 。 多个叶片夹具中的每一个可旋转地连接到一个臂上，用于围绕俯仰轴线旋转，并适于将叶片安装到每个叶片手柄上，使得每个叶片能够围绕俯仰轴线旋转，并且能够 与相应的臂相对于轮毂板和围绕相应的翼片轴线旋转。

    Stiff-in-plane rotor configuration
    10.
    发明授权
    Stiff-in-plane rotor configuration 有权
    刚体平面转子配置

    公开(公告)号：US08956117B2

    公开(公告)日：2015-02-17

    申请号：US13144448

    申请日：2009-01-19

    申请人： Frank B. Stamps ,  Patrick R. Tisdale ,  Tom Donovan ,  Richard E. Rauber

    发明人： Frank B. Stamps ,  Patrick R. Tisdale ,  Tom Donovan ,  Richard E. Rauber

    IPC分类号： B64C27/33 ,  B64C27/32

    CPC分类号： B64C27/35 ,  B64C27/32 ,  B64C27/33 ,  B64C27/39 ,  B64C27/48

    摘要： A rotor assembly for a rotary-wing aircraft, the rotor having a central hub assembly with a flexure-type, twist-shank yoke with multiple arms, each arm being adapted for a rotor blade to be mounted thereto. The arms provide for pitch changes of blades attached to the yoke through twisting of portions of the arms about a corresponding pitch axis. An inboard pitch bearing associated with each arm is attached to the hub assembly and allows for rotation of the attached blade about the pitch axis, the inboard pitch bearing also allowing for out-of-plane motion of the arm relative to the hub assembly about a flapping axis. An outboard pitch bearing associated with each arm is attached to the associated arm a selected distance from the inboard pitch bearing and allows for rotation of the attached blade about the pitch axis.

    摘要翻译： 一种用于旋转翼飞行器的转子组件，该转子具有中心轮毂组件，其具有带有多个臂的挠曲型扭转柄轭，每个臂适于安装在其上的转子叶片。 臂通过扭转相应的俯仰轴线的臂的部分来提供附接到轭的叶片的桨距变化。 与每个臂相关联的内侧变桨轴承附接到轮毂组件并且允许所附接的叶片围绕俯仰轴线旋转，内侧变桨轴承还允许臂相对于轮毂组件的平面外运动绕一个 拍动轴。 与每个臂相关联的外侧变桨轴承从相对于内侧变桨轴承的选定距离附接到相关联的臂，并且允许所附接的叶片围绕桨距轴线旋转。