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    ROTOR HUB VIBRATION ATTENUATOR
    1.
    发明申请
    ROTOR HUB VIBRATION ATTENUATOR 审中-公开
    转子毂振动衰减器

    公开(公告)号：WO2017209827A2

    公开(公告)日：2017-12-07

    申请号：PCT/US2017/022380

    申请日：2017-03-14

    Applicant: BELL HELICOPTER TEXTRON INC.

    Inventor： CHOI, Jouyoung, Jason ,  HEVERLY, David ,  KIZHAKKEPAT, Amarjit, O. ,  PARHAM, Thomas ,  SEIFERT, Michael ,  SMITH, Michael ,  STAMPS, Frank, B. ,  GAY, Frederick, S.

    IPC: B64C27/00

    Abstract: A vibration attenuation system for attenuating vibrations in a mast of an aircraft includes a weight attached to the mast but free to orbit about the mast. The weight can be comprised of one or more weight assemblies. Embodiments can include a single weight, or plural weight assemblies wherein each weight assembly can include a mechanical interconnecting mechanism so that each weight assembly receives feedback regarding the position and movement of one or more other weight assemblies. Each weight can be associated with a spring that urges the weight towards a neutral position. Rotation of the mast can cause the weight to orbit about the mast and self-excite such that the weight acts against the urging of the spring towards an attenuating position.

    Abstract translation: 用于衰减飞机的桅杆中的振动的减振系统包括附接到桅杆但可围绕桅杆自由绕轨道运动的重物。 重量可以由一个或多个重量组件组成。 实施例可以包括单个重量或多个重量组件，其中每个重量组件可以包括机械互连机构，使得每个重量组件接收关于一个或多个其他重量组件的位置和移动的反馈。 每个重量都可以与一个弹簧联系起来，这个弹簧将重量推向中立位置。 桅杆的转动可能导致重物在桅杆上绕轨道运动并自行激励，使得重物抵抗弹簧朝向衰减位置的推动而起作用。

    METHOD AND APPARATUS FOR ACTIVELY MANIPULATING AERODYNAMIC SURFACES
    3.
    发明申请
    METHOD AND APPARATUS FOR ACTIVELY MANIPULATING AERODYNAMIC SURFACES 审中-公开
    用于动态操纵气动表面的方法和装置

    公开(公告)号：WO2012060806A1

    公开(公告)日：2012-05-10

    申请号：PCT/US2010/054910

    申请日：2010-11-01

    Applicant: BELL HELICOPTER TEXTRON INC. ,  SCHANK, Troy, C. ,  KINTZINGER, Peter, H. ,  SHERRILL, Paul, B. ,  PARHAM, Thomas

    Inventor： SCHANK, Troy, C. ,  KINTZINGER, Peter, H. ,  SHERRILL, Paul, B. ,  PARHAM, Thomas

    IPC: B64C27/615

    CPC classification number: B64C13/26 ,  B64C13/30 ,  B64C27/00 ,  B64C27/001 ,  B64C27/615 ,  B64C2027/7266 ,  F16H21/44 ,  Y02T50/34 ,  Y02T50/44

    Abstract: A method and apparatus is provided, including an actuator system that may be connected to a wing frame for controlling an active element. The actuator system may include sliding elements movable along an axis parallel to the span-wise axis of the wing. The sliding elements may be connected to fixed elements and a crank element, the crank element generally comprising a beam element and a pivot element. The beam element may be offset from the pivot element so that the crank element is rotatable about the pivot element with a negative stiffness under an external force that tends to pull the sliding elements away from the fixed elements.

    Abstract translation: 提供了一种方法和装置，其包括致动器系统，该致动器系统可以连接到用于控制有源元件的机翼框架。 致动器系统可以包括可沿着平行于机翼的跨度轴线的轴线移动的滑动元件。 滑动元件可以连接到固定元件和曲柄元件，曲柄元件通常包括梁元件和枢轴元件。 梁元件可以从枢转元件偏移，使得曲柄元件可以在外力作用下具有负刚度的枢转元件旋转，其倾向于将滑动元件拉离固定元件。

    DAMPER
    4.
    发明公开
    DAMPER 审中-公开

    公开(公告)号：EP3705744A1

    公开(公告)日：2020-09-09

    申请号：EP19180627.2

    申请日：2019-06-17

    Applicant: Bell Helicopter Textron Inc.

    Inventor： SEIFERT, Michael Scott ,  ROMANO, Peter Quinn ,  PARHAM, Thomas

    IPC: F16F7/14 ,  F16F7/116

    Abstract: The present invention includes a damper assembly (306), method and kit to provide dampening to an airframe comprising: a mass (310) to dampen the vibration of the airframe; one or more wire rope isolators (312a, 312b) having a first and a second portion, wherein the mass (310) is attached to the one or more wire rope isolators (312a, 312b) and the mass (310) is isolated from the airframe by the one or more wire rope isolators (312a, 312b); and a first fastener (314a) and a second fastener (316a), wherein the first fasteners (314a) attaches to the first portion of the wire rope isolator (312a) to the mass (310), and the second fastener (316a) attaches the second portion of the wire rope isolator (312a) to the airframe to dampen vibration of the airframe.

    METHOD AND APPARATUS FOR ACTIVELY MANIPULATING AERODYNAMIC SURFACES
    9.
    发明公开
    METHOD AND APPARATUS FOR ACTIVELY MANIPULATING AERODYNAMIC SURFACES 有权
    用于有效地操纵空气动力学表面的方法和设备

    公开(公告)号：EP2616334A1

    公开(公告)日：2013-07-24

    申请号：EP10859345.0

    申请日：2010-11-01

    Applicant: Bell Helicopter Textron Inc.

    Inventor： SCHANK, Troy, C. ,  KINTZINGER, Peter, H. ,  SHERRILL, Paul, B. ,  PARHAM, Thomas

    IPC: B64C27/615

    CPC classification number: B64C13/26 ,  B64C13/30 ,  B64C27/00 ,  B64C27/001 ,  B64C27/615 ,  B64C2027/7266 ,  F16H21/44 ,  Y02T50/34 ,  Y02T50/44

    Abstract: A method and apparatus is provided, including an actuator system that may be connected to a wing frame for controlling an active element. The actuator system may include sliding elements movable along an axis parallel to the span-wise axis of the wing. The sliding elements may be connected to fixed elements and a crank element, the crank element generally comprising a beam element and a pivot element. The beam element may be offset from the pivot element so that the crank element is rotatable about the pivot element with a negative stiffness under an external force that tends to pull the sliding elements away from the fixed elements.

    Abstract translation: 提供了一种方法和设备，其包括可连接到机翼框架以用于控制有源元件的致动器系统。 致动器系统可以包括滑动元件，该滑动元件可以沿着平行于机翼的翼展轴线的轴线移动。 滑动元件可以连接到固定元件和曲柄元件，曲柄元件通常包括梁元件和枢转元件。 横梁元件可以偏离枢转元件，使得曲柄元件在倾向于将滑动元件拉离固定元件的外力的作用下以负刚度围绕枢转元件旋转。

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