Enclosure for contacts of aircraft wing heater blanket

    公开(公告)号:US11939067B2

    公开(公告)日:2024-03-26

    申请号:US17897344

    申请日:2022-08-29

    CPC classification number: B64D15/12 B64D2221/00 H01R2201/26 H05B2203/016

    Abstract: Briefly, the disclosure relates to apparatuses and methods to enclose electrical contacts for de-icing equipment utilized on fixed-wing aircraft and rotary-wing aircraft, such as helicopters and tiltrotor aircraft. In some implementations, enclosing electrical contacts for a de-ice heater blanket may ensure that high-quality electrical connections are made between conductors of one or more de-icing cables and the electrical contacts of the de-ice heater blanket. Such high-quality electrical connections may be maintained even during aircraft operations conducted in below-freezing ambient environments, rainy and/or wet environments, dusty desert environments, and so forth.

    ROTOR BLADE WEIGHT SYSTEM
    2.
    发明公开

    公开(公告)号:US20240300641A1

    公开(公告)日:2024-09-12

    申请号:US18178897

    申请日:2023-03-06

    CPC classification number: B64C27/008 B64C27/001 B64C27/473

    Abstract: A rotorcraft has a rotor blade having a spar comprising an internal space. A weight system is disposed within the spar and the weight system includes a weight tray having an open top, a weight guide rod connected to the weight tray. The weight guide rod extends in a spanwise direction through an interior of the weight tray and a weight is disposed on the weight guide rod and vertically captured by at least one side wall of the weight tray. The weight guide rod is insertable into the weight tray from a location above the weight tray to restrict longitudinal movement of the weight guide rod relative to the weight tray.

    Rotor blade weight system
    3.
    发明授权

    公开(公告)号:US12110101B2

    公开(公告)日:2024-10-08

    申请号:US18178897

    申请日:2023-03-06

    CPC classification number: B64C27/008 B64C27/001 B64C27/473

    Abstract: A rotorcraft has a rotor blade having a spar comprising an internal space. A weight system is disposed within the spar and the weight system includes a weight tray having an open top, a weight guide rod connected to the weight tray. The weight guide rod extends in a spanwise direction through an interior of the weight tray and a weight is disposed on the weight guide rod and vertically captured by at least one side wall of the weight tray. The weight guide rod is insertable into the weight tray from a location above the weight tray to restrict longitudinal movement of the weight guide rod relative to the weight tray.

    ENCLOSURE FOR CONTACTS OF AIRCRAFT WING HEATER BLANKET

    公开(公告)号:US20220411078A1

    公开(公告)日:2022-12-29

    申请号:US17897344

    申请日:2022-08-29

    Abstract: Briefly, the disclosure relates to apparatuses and methods to enclose electrical contacts for de-icing equipment utilized on fixed-wing aircraft and rotary-wing aircraft, such as helicopters and tiltrotor aircraft. In some implementations, enclosing electrical contacts for a de-ice heater blanket may ensure that high-quality electrical connections are made between conductors of one or more de-icing cables and the electrical contacts of the de-ice heater blanket. Such high-quality electrical connections may be maintained even during aircraft operations conducted in below-freezing ambient environments, rainy and/or wet environments, dusty desert environments, and so forth.

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