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 assembly and method of assembling same

    公开(公告)号:US12012200B2

    公开(公告)日:2024-06-18

    申请号:US17462546

    申请日:2021-08-31

    CPC classification number: B64C11/06 B64C11/30 F01D7/00

    Abstract: A rotor assembly has a rotor hub having a unitary structure. The rotor assembly further includes a unitary crosshead having a first upper tab and a first lower tab located vertically below the first upper tab. The first upper tab and the first lower tab define a slot therebetween to accept a first pin of the first rotor blade. A second upper tab and a second lower tab located vertically below the second upper tab define a slot therebetween to accept a second pin of the second rotor blade. A first recess is provided between the first lower tab and the second lower tab so that the crosshead comprises no material directly between at least a portion of the first lower tab and the second lower tab along at least one straight path.

    ROTOR ASSEMBLY AND METHOD OF ASSEMBLING SAME

    公开(公告)号:US20210387717A1

    公开(公告)日:2021-12-16

    申请号:US17462546

    申请日:2021-08-31

    Abstract: A rotor assembly has a rotor hub having a unitary structure. The rotor assembly further includes a unitary crosshead having a first upper tab and a first lower tab located vertically below the first upper tab. The first upper tab and the first lower tab define a slot therebetween to accept a first pin of the first rotor blade. A second upper tab and a second lower tab located vertically below the second upper tab define a slot therebetween to accept a second pin of the second rotor blade. A first recess is provided between the first lower tab and the second lower tab so that the crosshead comprises no material directly between at least a portion of the first lower tab and the second lower tab along at least one straight path.

    Rotor blade weight system
    5.
    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.

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