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    ROTOR HUB FOR A ROTORCRAFT
    21.
    发明申请
    ROTOR HUB FOR A ROTORCRAFT 有权
    用于转子的转子座

    公开(公告)号：US20150175259A1

    公开(公告)日：2015-06-25

    申请号：US14135941

    申请日：2013-12-20

    Applicant: Bell Helicopter Textron Inc.

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

    IPC: B64C27/72

    CPC classification number: B64C27/72 ,  B64C27/001 ,  B64C27/35 ,  B64C27/37 ,  B64C2027/003 ,  B64C2027/004 ,  B64C2027/7216

    Abstract: A rotor hub can include a yoke, a mast, and one or more radially oriented actuators. The first radial actuator and the second radial actuator each have a piston configured to impart a translation of the yoke relative to the mast. The radial actuators are configured to attenuate in-plane whirling vibrations. The rotor hub can also have actuators coupled between the mast and the yoke for attenuating flapping and vertical vibrations.

    Abstract translation: 转子毂可以包括轭，桅杆和一个或多个径向定向的致动器。 第一径向致动器和第二径向致动器各自具有构造成赋予轭相对于桅杆平移的活塞。 径向致动器构造成衰减飞机内的旋转振动。 转子轮毂还可以具有联接在桅杆和轭架之间的致动器，用于衰减振荡和垂直振动。

    Actuation system for an active blade element of a rotor blade
    25.
    发明授权
    Actuation system for an active blade element of a rotor blade 有权
    用于转子叶片的主动叶片元件的致动系统

    公开(公告)号：US09523278B2

    公开(公告)日：2016-12-20

    申请号：US14051575

    申请日：2013-10-11

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Christopher Foskey ,  Frank B. Stamps

    IPC: F01D5/12 ,  F01D7/00 ,  B64C27/72 ,  B64C27/615

    CPC classification number: F01D5/12 ,  B64C27/615 ,  B64C27/72 ,  B64C2027/7266 ,  F01D7/00 ,  Y02T50/34

    Abstract: One example of an actuation system for an active blade element of a rotor blade includes an actuator system coupled to a linear transmission system. The actuator system attaches to a structure within a rotor blade and provides a linear motion in a direction that is spanwise to the rotor blade. The linear transmission system is coupled with the actuator system and to an active blade element attached to the rotor blade. The linear transmission system receives the linear motion provided by the actuator system, and responsively provides at least a partial rotation of the active blade element about an axis of the linear transmission system which is in the direction that is substantially parallel to the spanwise axis of the rotor blade.

    Abstract translation: 用于转子叶片的主动叶片元件的致动系统的一个实例包括耦合到线性传动系统的致动器系统。 致动器系统附接到转子叶片内的结构，并且在与转子叶片的翼展方向上的方向上提供线性运动。 线性传动系统与致动器系统和连接到转子叶片的主动叶片元件联接。 线性传动系统接收由致动器系统提供的直线运动，并且响应地提供主动叶片元件围绕线性传动系统的轴线的至少部分旋转，所述轴线基本上平行于所述线性传动系统的翼展方向轴线 转子叶片。

    Actuation System for an Active Blade Element of a Rotor Blade
    26.
    发明申请
    Actuation System for an Active Blade Element of a Rotor Blade 有权
    用于转子叶片的主动叶片元件的致动系统

    公开(公告)号：US20150104307A1

    公开(公告)日：2015-04-16

    申请号：US14051575

    申请日：2013-10-11

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Christopher Foskey ,  Frank B. Stamps

    IPC: F01D5/12

    CPC classification number: F01D5/12 ,  B64C27/615 ,  B64C27/72 ,  B64C2027/7266 ,  F01D7/00 ,  Y02T50/34

    Abstract: One example of an actuation system for an active blade element of a rotor blade includes an actuator system coupled to a linear transmission system. The actuator system attaches to a structure within a rotor blade and provides a linear motion in a direction that is spanwise to the rotor blade. The linear transmission system is coupled with the actuator system and to an active blade element attached to the rotor blade. The linear transmission system receives the linear motion provided by the actuator system, and responsively provides at least a partial rotation of the active blade element about an axis of the linear transmission system which is in the direction that is substantially parallel to the spanwise axis of the rotor blade.

    Abstract translation: 用于转子叶片的主动叶片元件的致动系统的一个实例包括耦合到线性传动系统的致动器系统。 致动器系统附接到转子叶片内的结构，并且在与转子叶片的翼展方向上的方向上提供线性运动。 线性传动系统与致动器系统和连接到转子叶片的主动叶片元件联接。 线性传动系统接收由致动器系统提供的直线运动，并且响应地提供主动叶片元件围绕线性传动系统的轴线的至少部分旋转，所述轴线基本上平行于所述线性传动系统的翼展方向轴线 转子叶片。

    Composite Flexure for Tiltrotor Rotor System
    27.
    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。

    Constant Velocity Joint with Spring Rate Control Mechanism
    28.
    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。

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