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12 条记录 (耗时 0.064 秒)

    Rotary-Wing Aircraft Torque Coupling with Pad Bearings
    3.
    发明申请
    Rotary-Wing Aircraft Torque Coupling with Pad Bearings 有权
    旋转翼飞机扭矩耦合与垫轴承

    公开(公告)号：US20100009764A1

    公开(公告)日：2010-01-14

    申请号：US12376979

    申请日：2006-08-17

    申请人： Frank B. Stamps ,  Richard Rauber ,  David Popelka ,  Pat Tisdale ,  Tom Campbell ,  James Lee Braswell, JR.

    发明人： Frank B. Stamps ,  Richard Rauber ,  David Popelka ,  Pat Tisdale ,  Tom Campbell ,  James Lee Braswell, JR.

    IPC分类号： F16D3/18

    CPC分类号： B64C27/32 ,  B64C27/35

    摘要： A torque coupling for a rotor head of a rotary-wing aircraft is configured for rotation with a mast and for causing rotation of an attached yoke. The coupling has trunnions that rotate with the mast and extend generally radially. Pad-bearing assemblies each have a central member coupled to one of the trunnions with a laminated spherical bearing and have laminated pad bearings affixed to opposing sides of the central member. The laminated bearings have alternating rigid and elastomeric layers. A bearing mount is affixed to each pad bearing and is connected to a yoke for rotating the yoke with the mast. The pad-bearing assemblies allow for relative motion between each central member and the associated trunnion and between each central member and the bearing mounts through elastic shear deformation, and this allows for gimballing of the attached yoke relative to the mast.

    摘要翻译： 用于旋转翼飞行器的转子头的扭矩联接器构造成用桅杆旋转并且用于使附接的轭的旋转。 联轴器具有与桅杆一起旋转并且径向延伸的耳轴。 垫轴承组件各自具有与层叠的球面轴承联接到其中一个耳轴的中心构件，并且具有固定到中心构件的相对侧的层压垫轴承。 层压轴承具有交替的刚性和弹性层。 轴承座固定到每个垫轴承上，并连接到轭架上，用于使桅杆旋转。 垫片轴承组件允许在每个中心构件和相关联的耳轴之间以及通过弹性剪切变形在每个中心构件和轴承座之间进行相对运动，并且这允许相对于桅杆对附接的轭进行槌球。

    Rotary-wing aircraft torque coupling with pad bearings
    4.
    发明授权
    Rotary-wing aircraft torque coupling with pad bearings 有权
    旋翼飞机扭矩联轴器与垫轴承

    公开(公告)号：US08029371B2

    公开(公告)日：2011-10-04

    申请号：US12376979

    申请日：2006-08-17

    申请人： Frank B. Stamps ,  Richard Rauber ,  David Popelka ,  Pat Tisdale ,  Tom Campbell ,  James Lee Braswell, Jr.

    发明人： Frank B. Stamps ,  Richard Rauber ,  David Popelka ,  Pat Tisdale ,  Tom Campbell ,  James Lee Braswell, Jr.

    IPC分类号： F16D3/00

    CPC分类号： B64C27/32 ,  B64C27/35

    摘要： A torque coupling for a rotor head of a rotary-wing aircraft is configured for rotation with a mast and for causing rotation of an attached yoke. The coupling has trunnions that rotate with the mast and extend generally radially. Pad-bearing assemblies each have a central member coupled to one of the trunnions with a laminated spherical bearing and have laminated pad bearings affixed to opposing sides of the central member. The laminated bearings have alternating rigid and elastomeric layers. A bearing mount is affixed to each pad bearing and is connected to a yoke for rotating the yoke with the mast. The pad-bearing assemblies allow for relative motion between each central member and the associated trunnion and between each central member and the bearing mounts through elastic shear deformation, and this allows for gimballing of the attached yoke relative to the mast.

    摘要翻译： 用于旋转翼飞行器的转子头的扭矩联接器构造成用桅杆旋转并且用于使附接的轭的旋转。 联轴器具有与桅杆一起旋转并且径向延伸的耳轴。 垫轴承组件各自具有与层叠的球面轴承联接到其中一个耳轴的中心构件，并且具有固定到中心构件的相对侧的层压垫轴承。 层压轴承具有交替的刚性和弹性层。 轴承座固定到每个垫轴承上，并连接到轭架上，用于使桅杆旋转。 垫片轴承组件允许在每个中心构件和相关联的耳轴之间以及通过弹性剪切变形在每个中心构件和轴承座之间进行相对运动，并且这允许相对于桅杆对附接的轭架进行槌球。

    Hub Assembly with Grease Lubricated Roller Bearing and Tension-Torsion Strap
    7.
    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

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

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

    IPC分类号： B64C27/59

    CPC分类号： B64C27/33 ,  B64C11/04 ,  B64C27/35 ,  B64C29/0033

    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。

    Torque coupling for rotary-wing aircraft
    9.
    发明授权
    Torque coupling for rotary-wing aircraft 有权
    旋翼飞机的扭矩联轴器

    公开(公告)号：US08226355B2

    公开(公告)日：2012-07-24

    申请号：US11629027

    申请日：2006-04-19

    申请人： Frank B. Stamps ,  Richard Rauber

    发明人： Frank B. Stamps ,  Richard Rauber

    IPC分类号： B64C27/32

    CPC分类号： B64C27/32

    摘要： A torque coupling (13) for a rotor head (11) of a rotary-wing aircraft has upper and lower plates (29, 31) configured for rotation with a rotor mast (19). Drive links (33) pivotally connected to the upper and lower plates (29, 31) pivot about a pivot axis generally parallel to and radially offset from an axis of rotation of the plates. Each link (33) is engaged with adjacent drive links (33) to form a continuous ring of links, such that motion of one link (33) about its pivot axis causes motion in an opposite direction of each adjacent link (33) about its pivot axis. Drive elements (25) connect the drive links (33) to an assembly configured to receive rotor blades. The drive elements (25) may be components of a universal joint, a multiple trailing-link configuration, a pad-bearing configuration, or another type of articulating assembly.

    摘要翻译： 用于转翼飞行器的转子头（11）的扭矩联接器（13）具有被配置为与转子桅杆（19）一起旋转的上板和下板（29,31）。 枢转地连接到上板和下板（29,31）的驱动连杆（33）围绕大致平行于板的旋转轴线并径向偏移的枢转轴线枢转。 每个连杆（33）与相邻的驱动连杆（33）接合以形成连续的环形环，使得一个连杆（33）围绕其枢转轴线的运动引起每个相邻连杆（33）围绕其枢轴的相反方向的运动 枢轴。 驱动元件（25）将驱动连杆（33）连接到被配置为接收转子叶片的组件。 驱动元件（25）可以是万向接头，多拖尾构造，衬垫承载构型或另一类型的铰接组件的组件。

    Torque Coupling for Rotary-Wing Aircraft
    10.
    发明申请
    Torque Coupling for Rotary-Wing Aircraft 有权
    旋翼机的扭矩耦合

    公开(公告)号：US20080267778A1

    公开(公告)日：2008-10-30

    申请号：US11629027

    申请日：2006-04-19

    申请人： Frank B. Stamps ,  Richard Rauber

    发明人： Frank B. Stamps ,  Richard Rauber

    IPC分类号： F01D7/00

    CPC分类号： B64C27/32

    摘要： A torque coupling (13) for a rotor head (11) of a rotary-wing aircraft has upper and lower plates (29, 31) configured for rotation with a rotor mast (19). Drive links (33) pivotally connected to the upper and lower plates (29, 31) pivot about a pivot axis generally parallel to and radially offset from an axis of rotation of the plates. Each link (33) is engaged with adjacent drive links (33) to form a continuous ring of links, such that motion of one link (33) about its pivot axis causes motion in an opposite direction of each adjacent link (33) about its pivot axis. Drive elements (25) connect the drive links (33) to an assembly configured to receive rotor blades. The drive elements (25) may be components of a universal joint, a multiple trailing-link configuration, a pad-bearing configuration, or another type of articulating assembly.

    摘要翻译： 用于转翼飞行器的转子头（11）的扭矩联接器（13）具有被配置为与转子桅杆（19）一起旋转的上板和下板（29,31）。 枢转地连接到上板和下板（29,31）的驱动连杆（33）围绕大致平行于板的旋转轴线并径向偏移的枢转轴线枢转。 每个连杆（33）与相邻的驱动连杆（33）接合以形成连续的环形环，使得一个连杆（33）围绕其枢转轴线的运动引起每个相邻连杆（33）围绕其枢轴的相反方向的运动 枢轴。 驱动元件（25）将驱动连杆（33）连接到被配置为接收转子叶片的组件。 驱动元件（25）可以是万向接头，多拖尾构造，衬垫承载构型或另一类型的铰接组件的组件。