Adjustable blade load mechanism for wiper arm assembly

    公开(公告)号:US12263816B1

    公开(公告)日:2025-04-01

    申请号:US18436638

    申请日:2024-02-08

    Abstract: A windshield wiper system for an aircraft includes a wiper drive shaft with a first end and a second end opposite the first end. The second end includes a first threaded section between the first end and the second end, a second threaded section extending axially along the wiper drive shaft between the first threaded section and the second end relative to a center axis of the wiper drive shaft, and a spline section axially between the first threaded section and the second threaded section. Further included is a first nut to thread to the first threaded section, a second nut to thread to the second threaded section, and a wiper arm assembly including an adjustment sleeve configured to interlock with the spline section, a wiper arm with a first end configured to enclose the adjustment sleeve, and a second end of the wiper arm attached to a wiper blade.

    COMPOSITE WIPER BLADE ASSEMBLY
    2.
    发明申请

    公开(公告)号:US20220289145A1

    公开(公告)日:2022-09-15

    申请号:US17408021

    申请日:2021-08-20

    Abstract: An aircraft windshield wiper system includes a wiper arm, a wiper blade coupled to a first end of the wiper arm, and an output shaft coupled to a second end of the wiper arm. The wiper blade includes a support member coupled to a blade element through a clip and a fastener extending through the blade element. The support member can be made from a composite material and the clip and fastener allow for attachment of the blade element to the support member without piercing the support member.

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