FAILSAFE PISTON PRESSURE PATH
    2.
    发明公开

    公开(公告)号:US20240003395A1

    公开(公告)日:2024-01-04

    申请号:US17856358

    申请日:2022-07-01

    IPC分类号: F16D65/84 F16D65/18 B64C25/44

    摘要: A piston assembly is disclosed herein. The piston assembly includes a piston having a first end, an opposing second end, and a sidewall extending from the first end to the second end, the piston further including a cavity at least partially defined by the sidewall, a spring guide having a first end and an opposing second end, the spring guide disposed within the cavity of the piston and adjacent the sidewall, an insulator having a first portion extending from the second end of the piston and a second portion disposed within the piston, an insulator shield disposed adjacent the first portion of the insulator, and a component coupled to the second end of the spring guide, the component being offset from the insulator shield by a distance.

    ROTOR DRIVE KEY ASSEMBLY
    5.
    发明申请

    公开(公告)号:US20210010549A1

    公开(公告)日:2021-01-14

    申请号:US16910307

    申请日:2020-06-24

    IPC分类号: F16D65/12 F16D65/84

    摘要: In some examples, an assembly includes a rotor drive key configured to fit around a wheel boss defined by a wheel of a vehicle. The rotor drive key includes a support member. The assembly further comprises a fastener configured to extend through the wheel boss and the support member in a substantially axial direction of the wheel when the rotor drive key is fit around the wheel boss. A fastening member is configured to engage with a portion of the fastener extending beyond the support member.

    Perforated heat screen for a braked aircraft wheel

    公开(公告)号:US10738849B2

    公开(公告)日:2020-08-11

    申请号:US15652342

    申请日:2017-07-18

    摘要: The invention provides a method of reducing the cooling time for disks of a brake (5) of an aircraft wheel (1) fitted with a heat screen (10) extending between the wheel and the disks of the brake, and mounted to rotate on aircraft landing gear about an axis of rotation, the method comprising making perforations (11, 12, 13) through the heat screen to allow air heated by the disks to pass through the heat screen towards the wheel, the perforations being provided with obstacles to block any radiation from passing directly from the disks towards the wheel.

    AIRCRAFT BRAKE HEAT SHIELD
    7.
    发明申请

    公开(公告)号:US20190277357A1

    公开(公告)日:2019-09-12

    申请号:US15918176

    申请日:2018-03-12

    IPC分类号: F16D65/84 B32B15/04 B32B15/18

    摘要: The present disclosure provides a heat shield. The heat shield may comprise a first shield layer defining a cylindrical inner diameter surface of the heat shield, the cylindrical inner diameter surface having a radius and an axis, an air gap layer radially outward of the first shield layer, a second shield layer radially outward of the air gap layer, a first insulation layer radially outward of the second shield layer, a foil layer radially outward of the second shield layer, a second insulation layer radially outward of the foil layer, and a third shield layer radially outward of the second insulation layer.

    Aircraft brake heat shield
    8.
    发明授权

    公开(公告)号:US10400839B1

    公开(公告)日:2019-09-03

    申请号:US15918176

    申请日:2018-03-12

    摘要: The present disclosure provides a heat shield. The heat shield may comprise a first shield layer defining a cylindrical inner diameter surface of the heat shield, the cylindrical inner diameter surface having a radius and an axis, an air gap layer radially outward of the first shield layer, a second shield layer radially outward of the air gap layer, a first insulation layer radially outward of the second shield layer, a foil layer radially outward of the second shield layer, a second insulation layer radially outward of the foil layer, and a third shield layer radially outward of the second insulation layer.