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24 条记录 (耗时 0.015 秒)

    Integrated assymmetry brake mechanism
    13.
    发明授权
    Integrated assymmetry brake mechanism 有权

    公开(公告)号：US11794877B2

    公开(公告)日：2023-10-24

    申请号：US17128373

    申请日：2020-12-21

    申请人： Hamilton Sundstrand Corporation

    发明人： Victor Barger

    IPC分类号： B64C13/28 ,  B64D45/00

    CPC分类号： B64C13/341 ,  B64D2045/0085

    摘要： An integrated asymmetric brake system for an aircraft includes a housing and a control surface actuator arranged in the housing. The control surface actuator includes a torque limiter output member and is operable to selectively deploy and retract a control surface. An asymmetry brake system is arranged in the housing and is operably connected to the control surface actuator and the torque limiter output member. The asymmetry brake system is selectively operable to prevent deployment of the control surface by activating the torque limiter output member upon detecting an asymmetry event. An asymmetry brake test monitor switch is mounted in the housing and operably coupled to the asymmetry brake system. The asymmetry brake test monitor switch is monitored to confirm functionality of the asymmetry brake system prior to flight.

    AXIAL LOAD CAPABLE TORQUE TUBE ASSEMBLY & MANUFACTURING METHODS THEREOF
    14.
    发明申请
    AXIAL LOAD CAPABLE TORQUE TUBE ASSEMBLY & MANUFACTURING METHODS THEREOF 有权

    公开(公告)号：US20210147067A1

    公开(公告)日：2021-05-20

    申请号：US17075933

    申请日：2020-10-21

    申请人： Hamilton Sundstrand Corporation

    发明人： Victor Barger ,  Joseph M. Bielefeldt ,  Jude C. Lai ,  Eric W. Karlen

    IPC分类号： B64C13/28 ,  B21D39/04

    摘要： An assembly and a method for manufacturing an assembly for transmitting torque to an aircraft actuator. The assembly and method include a torque tube having a longitudinal axis and an end fitting. The ending fitting includes a connector portion and an engagement portion that is inserted into the torque tube. The engagement portion includes a first end adjacent the connector portion, a second end opposite the first end, and a coupling region between the first and second end that includes an outer coupling surface having an outer diameter and a continuous groove formed thereon. The continuous groove includes two axial grooves that extend along the outer coupling surface along the longitudinal axis and a first parallel groove that extends circumferentially about the longitudinal axis along the outer coupling surface that joins the two axial grooves.

    Aerodynamic control surface movement monitoring system
    15.
    发明授权
    Aerodynamic control surface movement monitoring system 有权

    公开(公告)号：US10780977B2

    公开(公告)日：2020-09-22

    申请号：US15433021

    申请日：2017-02-15

    申请人： Hamilton Sundstrand Corporation

    发明人： Andrew N. Baines ,  Cory M. Crandall-Seibert ,  Victor Barger ,  William E. Leden ,  David K. Boe

    IPC分类号： B64C13/28 ,  B64C9/16 ,  B64C9/02 ,  B64C9/18 ,  B64C13/40 ,  B64D45/00 ,  B64C9/14

    摘要： An actuator system for controlling a flight surface of an aircraft includes a first actuator having a first actuator input and a first linear translation element that moves based on rotational motion received at the first actuator input and a first sensor coupled to the first linear translation element that generates a first output based on a displacement of the first linear translation element. The system also includes a second actuator having a second actuator input and a second linear translation element that moves based on rotational motion received at the second actuator input and a second sensor coupled to the second linear translation element that generates a second output based on a displacement of the second linear translation element. The system also includes a control unit that receives the first and second outputs and determines if an error condition exists for the system based on first and second output.

    Direct position measurement for aircraft flight control surfaces
    17.
    发明授权
    Direct position measurement for aircraft flight control surfaces 有权

    公开(公告)号：US10048090B2

    公开(公告)日：2018-08-14

    申请号：US14300853

    申请日：2014-06-10

    申请人： HAMILTON SUNDSTRAND CORPORATION

    发明人： Victor Barger

    IPC分类号： B64D45/00 ,  G01D5/14 ,  B64C27/00

    摘要： A method and apparatus for determining a discrete position of a first surface of an aircraft is disclosed. The first surface and a second surface movable relative to the first surface are provided. A sensor is disposed on one of the first surface and a second surface and a magnetic field source disposed on the other of the first surface and the second surface. The sensor detects a local magnetic field related to the magnetic field source and generates a voltage indicative of strength of the local magnetic field. The strength of the local magnetic field and therefore the generated voltage is related to a relative position between the sensor and the magnetic field source. The relative distance between the first surface and the second surface is determined from the generated voltage.

    AIRCRAFT COMPONENT ROTARY DEVICE
    18.
    发明申请
    AIRCRAFT COMPONENT ROTARY DEVICE 有权
    飞机组件旋转装置

    公开(公告)号：US20160016653A1

    公开(公告)日：2016-01-21

    申请号：US14486443

    申请日：2014-09-15

    申请人： HAMILTON SUNDSTRAND CORPORATION

    发明人： Victor Barger

    IPC分类号： B64C9/30 ,  F16H57/00 ,  F16H13/04 ,  F16D59/00 ,  B64C13/28

    CPC分类号： B64C9/30 ,  B64C9/16 ,  B64C9/22 ,  B64C13/28 ,  F16D43/206 ,  F16D43/218 ,  F16D59/00 ,  F16D65/18 ,  F16D2125/36 ,  F16H13/04 ,  F16H57/0006

    摘要： A rotary device assembly is provided and includes an input shaft coupled to a torque generating device, an output shaft and a rotary device disposed to transmit first torque from the input shaft to the output shaft and configured with no-back capability to prevent second torque applied to the output shaft from being transmitted to the input shaft in an event the second torque deceeds a torque-limiting threshold and the no-back capability and torsional lock-up capability to prevent an overload of the torque generating device in an event the second torque exceeds the torque-limiting threshold.

    摘要翻译： 提供了一种旋转装置组件，其包括联接到转矩产生装置的输入轴，输出轴和旋转装置，其被设置为将第一扭矩从输入轴传递到输出轴，并且被配置为具有不反转能力以防止施加第二扭矩 在第二扭矩变为扭矩限制阈值和无返回能力和扭转锁定能力的情况下，输出轴传递到输入轴，以防止在第二扭矩的情况下扭矩产生装置的过载 超过扭矩限制阈值。