利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

8 条记录 (耗时 0.013 秒)

    Aircraft ice protection system and method
    5.
    发明授权
    Aircraft ice protection system and method 有权

    公开(公告)号：US11325713B2

    公开(公告)日：2022-05-10

    申请号：US16618663

    申请日：2018-06-04

    申请人： SHORT BROTHERS PLC

    发明人： Robert Samuel Wilson

    IPC分类号： B64D15/12 ,  B64D15/00 ,  B64D15/20 ,  B64D33/02

    摘要： Ice protection systems of aircraft and related methods are disclosed. In one embodiment of the present invention, the system includes a gas-discharge lamp and an electric power source. The gas-discharge lamp is configured to emit infrared radiation toward an inner surface of an aircraft skin. The electric power source is operatively connected to the gas-discharge lamp.

    THRUST REVERSER CASCADE AND METHOD OF MANUFACTURE
    6.
    发明公开
    THRUST REVERSER CASCADE AND METHOD OF MANUFACTURE 审中-公开

    公开(公告)号：US20240110535A1

    公开(公告)日：2024-04-04

    申请号：US18124382

    申请日：2023-03-21

    申请人： SHORT BROTHERS PLC

    发明人： Robert Samuel Wilson ,  Oran Walsh

    IPC分类号： F02K1/62 ,  B29C69/02 ,  F02K1/70

    CPC分类号： F02K1/625 ,  B29C69/02 ,  F02K1/70 ,  B29L2031/3076

    摘要： A thrust reverser cascade of an aircraft engine comprises a frame and a vane overmolded onto the frame. The frame and the vane each comprise reinforcement fibers in a thermoplastic matrix. A method is disclosed for manufacturing the thrust reverser cascade or another part comprising an aerodynamic surface configured to interact with a flow of fluid. The method comprises providing a first portion of the part and overmolding a second portion of the part onto the first portion where the second portion includes the aerodynamic surface.

    THRUST REVERSER CASCADE AND METHOD OF MANUFACTURE
    7.
    发明申请
    THRUST REVERSER CASCADE AND METHOD OF MANUFACTURE 有权

    公开(公告)号：US20220195961A1

    公开(公告)日：2022-06-23

    申请号：US17690540

    申请日：2022-03-09

    申请人： SHORT BROTHERS PLC

    发明人： Robert Samuel Wilson ,  Oran Walsh

    IPC分类号： F02K1/62 ,  F02K1/70 ,  B29C69/02

    摘要： A thrust reverser cascade of an aircraft engine comprises a frame and a vane overmolded onto the frame. The frame and the vane each comprise reinforcement fibers in a thermoplastic matrix. A method is disclosed for manufacturing the thrust reverser cascade or another part comprising an aerodynamic surface configured to interact with a flow of fluid. The method comprises providing a first portion of the part and overmolding a second portion of the part onto the first portion where the second portion includes the aerodynamic surface.

    Method for designing and fitting, via interference, an insert into an opening in a non-metallic material
    8.
    发明授权
    Method for designing and fitting, via interference, an insert into an opening in a non-metallic material 有权

    公开(公告)号：US10695985B2

    公开(公告)日：2020-06-30

    申请号：US15758801

    申请日：2016-09-09

    申请人： SHORT BROTHERS PLC

    发明人： Samuel Colin Hanna ,  Robert Samuel Wilson ,  William Christopher Campbell

    IPC分类号： B29C65/56 ,  B29C65/14 ,  B29C65/66 ,  B29C65/00 ,  F16B4/00 ,  B29C35/16 ,  B29L31/30

    摘要： A method for inserting an insert into a hole in a composite material made from a plurality of carbon fiber layers suspended in a resin material includes lowering a temperature of the insert to a reduced temperature at which a coefficient of thermal expansion of a material of the insert causes the insert to contract to a first perimeter, inserting the insert at the reduced temperature into the hole, and permitting the temperature of the insert to increase from the reduced temperature to an operational temperature. At the operational temperature, the insert expands to a second perimeter so that the insert is retained within the composite material due to an interference between the insert and the composite material. The interference transfers a structural load from the insert to the composite material and results in damage to the composite material if the insert is dislodged at the operational temperature.