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    Rotor System with Torque-Splitter Assembly
    101.
    发明申请
    Rotor System with Torque-Splitter Assembly 有权
    带转矩分配器的转子系统

    公开(公告)号：US20150053814A1

    公开(公告)日：2015-02-26

    申请号：US13975830

    申请日：2013-08-26

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Frank B. Stamps

    IPC: B64C27/37 ,  F16D3/30 ,  B64C27/12

    CPC classification number: B64C27/41 ,  F16D3/42

    Abstract: According to one embodiment, a rotor head includes a yoke, a torque-splitter assembly, and a joint assembly. The torque-splitter assembly includes a spine assembly, a first trunion, and a second trunion. The spline assembly is configured to receive the drive shaft through a first opening. The spline assembly has a first plurality of outer splines oriented in a first direction and a second plurality of outer splines oriented in a second direction different from the first direction. The first trunion is disposed about the first plurality of outer splines. The second trunion is disposed about the second plurality of outer splines.

    Abstract translation: 根据一个实施例，转子头包括轭，扭矩分配器组件和接头组件。 扭矩分配器组件包括脊柱组件，第一组合和第二组合。 花键组件构造成通过第一开口接收驱动轴。 花键组件具有沿第一方向定向的第一多个外花键和沿与第一方向不同的第二方向定向的第二多个外花键。 第一组合围绕第一多个外花键设置。 第二组合围绕第二多个外花键设置。

    Composite Flexure for Tiltrotor Rotor System
    102.
    发明申请
    Composite Flexure for Tiltrotor Rotor System 有权
    用于倾斜转子转子系统的复合挠曲

    公开(公告)号：US20150034772A1

    公开(公告)日：2015-02-05

    申请号：US13958192

    申请日：2013-08-02

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Christopher Foskey ,  Frank B. Stamps ,  Joel McIntyre ,  Gary Miller

    IPC: B64C27/33 ,  B64C27/52 ,  B64C27/28

    CPC classification number: B64C27/33 ,  B64C27/48 ,  B64C29/0033

    Abstract: According to one embodiment, a composite flexure may secure a rotor blade to a yoke in a tiltrotor rotor system. The composite flexure includes a composite body, a first end configured to couple the composite member to the yoke, and a second end configured to couple the composite member to the rotor blade.

    Abstract translation: 根据一个实施例，复合挠曲件可将转子叶片固定在倾斜转子转子系统中的轭。 复合挠曲件包括复合体，构造成将复合构件耦合到轭的第一端，以及构造成将复合构件耦合到转子叶片的第二端。

    Tiltrotor Control System With Two Rise/Fall Actuators
    103.
    发明申请
    Tiltrotor Control System With Two Rise/Fall Actuators 有权
    具有两个上升/下降执行器的倾翻机控制系统

    公开(公告)号：US20140271204A1

    公开(公告)日：2014-09-18

    申请号：US13835705

    申请日：2013-03-15

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Ken Shundo ,  Carlos A. Fenny ,  Frank B. Stamps

    IPC: B64C29/00 ,  B64C11/32

    CPC classification number: B64C29/0033 ,  B64C11/32 ,  B64C27/605

    Abstract: A rotor system for rotor aircraft comprises a rotor hub comprising a plurality of rotor blades, a rotatable rotor mast coupled to the rotor hub, a swashplate assembly comprising a non-rotating ring engaged with a rotatable ring, a plurality of pitch links mechanically coupling the rotatable ring to the plurality of rotor blades, and a swashplate actuator system. The rotatable ring is configured to rotate with the rotor mast, and the non-rotating ring is configured to engage and guide the rotatable ring. The pitch links are configured to control the pitch angle of each rotor blade. The swashplate actuator system consists of: a first actuator and a second actuator, where the first actuator and the second actuator are mechanically coupled to a stationary surface and the non-rotating ring.

    Abstract translation: 用于转子飞行器的转子系统包括转子毂，该转子毂包括多个转子叶片，连接到转子毂的可旋转转子柱塞，包括与可旋转环接合的非旋转环的斜盘组件，多个螺距连杆， 可旋转环到多个转子叶片，以及斜盘致动器系统。 可旋转环被构造成与转子桅杆一起旋转，并且非旋转环被构造成接合和引导可旋转环。 俯仰连杆构造成控制每个转子叶片的俯仰角。 斜盘致动器系统包括：第一致动器和第二致动器，其中第一致动器和第二致动器机械地联接到固定表面和非旋转环。

    Flexing Clevis Arrangement Bolted Joint Attachment For Flexible Rotor Hub With High Offset And High Flapping
    104.
    发明申请
    Flexing Clevis Arrangement Bolted Joint Attachment For Flexible Rotor Hub With High Offset And High Flapping 有权
    弯曲夹具布置螺栓接头附件适用于具有高偏移和高颤动的柔性转子毂

    公开(公告)号：US20140271200A1

    公开(公告)日：2014-09-18

    申请号：US13801965

    申请日：2013-03-13

    Applicant: BELL HELICOPTER TEXTRON INC.

    Inventor： Drew Sutton ,  Frank B. Stamps ,  Patrick Ryan Tisdale ,  Paul Oldroyd

    IPC: F01D5/02

    CPC classification number: B64C27/33 ,  B64C11/02 ,  B64C27/32 ,  B64C27/48 ,  Y10T29/49316

    Abstract: A flexible joint assembly for providing flexure to a rotor blade comprising an upper hub plate and a lower hub plate configured to secure a rotor blade yoke via a bolted joint located radially outward of a mast; and an upper flexure assembly connected to the upper hub plate and a lower flexure assembly connected to the lower hub plate, wherein the upper flexure assembly and lower flexure assembly are configured to promote flapping of the rotor blade yoke about a flapping hinge located radially outward of the bolted joint.

    Abstract translation: 一种用于向转子叶片提供挠曲的柔性接头组件，包括上轮毂板和下轮毂板，所述上轮毂板和下轮毂板被构造成通过位于桅杆的径向外侧的螺栓接头固定转子叶片翼片; 以及连接到上轮毂板的上挠性组件和连接到下轮毂板的下挠曲组件，其中上弯曲组件和下挠曲组件构造成促使转子叶片轭绕着位于径向向外的振动铰链 螺栓接头。

    Constant Velocity Joint with Spring Rate Control Mechanism
    105.
    发明申请
    Constant Velocity Joint with Spring Rate Control Mechanism 有权
    具有弹簧速率控制机构的恒速接头

    公开(公告)号：US20140248150A1

    公开(公告)日：2014-09-04

    申请号：US14258187

    申请日：2014-04-22

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Drew Sutton ,  Frank B. Stamps ,  Christopher Foskey

    IPC: B64C27/41 ,  F16D3/16

    CPC classification number: B64C27/41 ,  B64C27/32 ,  F16D3/28 ,  F16D3/30 ,  F16D3/33

    Abstract: According to one embodiment, a constant velocity (CV) joint includes a first yoke, a second yoke, and three bearings. The first yoke is configured to be rotatably coupled to an input device about a first axis and configured to receive the input device through a first opening. The second yoke is rotatably coupled to the first yoke about a second axis and rotatably coupled to an output device about a third axis. The first bearing is disposed about the first axis adjacent to the first yoke, the second bearing is disposed about the second axis adjacent to the first yoke or the second yoke, and the third bearing disposed about the third axis adjacent to the second yoke. The first and third bearings torsionally constrain movement the first yoke and the second yoke so as to achieve a substantially CV characteristic between the input device and the output device.

    Abstract translation: 根据一个实施例，等速（CV）接头包括第一磁轭，第二磁轭和三个轴承。 第一磁轭被配置成围绕第一轴线可旋转地联接到输入装置，并且被配置成通过第一开口接收输入装置。 第二轭被围绕第二轴可旋转地联接到第一轭，并且围绕第三轴可旋转地联接到输出装置。 所述第一轴承围绕所述第一轴线邻近所述第一磁轭设置，所述第二轴承围绕所述第二轴线邻近所述第一磁轭或所述第二磁轭设置，所述第三轴承围绕所述第三轴线邻近所述第二磁轭设置。 第一和第三轴承扭转约束运动第一轭和第二轭，以便在输入装置和输出装置之间实现基本的CV特性。

    Adjustable pitch link
    107.
    发明授权
    Adjustable pitch link 有权

    公开(公告)号：US10377477B2

    公开(公告)日：2019-08-13

    申请号：US13669212

    申请日：2012-11-05

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Joseph Biser ,  Clifton B. Day ,  Frank B. Stamps ,  Daniel Spivey

    IPC: B64C27/605 ,  F16C7/06

    Abstract: According to one embodiment, a pitch link includes a first link, a second link coupled to a first end of the first link, a third link coupled to a second end of the first link opposite the first end, and a first bearing housing having a first bearing and a second bearing housing having a second bearing. The first bearing housing is removably coupled to the second link. The second link separates the first bearing housing from the first link. The second bearing housing is removably coupled to the third link. The third link separates the second bearing housing from the first link.

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