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    SYSTEMS AND METHODS FOR RESTRAINING CARGO ON AIRCRAFT LOADING SYSTEMS USING INDEXING MECHANISMS
    1.
    发明申请
    SYSTEMS AND METHODS FOR RESTRAINING CARGO ON AIRCRAFT LOADING SYSTEMS USING INDEXING MECHANISMS 有权

    公开(公告)号：US20220324573A1

    公开(公告)日：2022-10-13

    申请号：US17226962

    申请日：2021-04-09

    申请人： Goodrich Corporation

    发明人： Brandon David Lee ,  Wallace Harold Larson ,  Alexander Mitchell Heyd ,  Lynne M Almvig ,  Zachary Meyer

    IPC分类号： B64D9/00 ,  B64C1/20

    摘要： A cargo restraint system includes a driving shaft, a first restraint, and a second restraint. The first restraint is operatively coupled to the driving shaft via a first indexing mechanism arrangement. The second restraint is operatively coupled to the driving shaft via a second indexing mechanism arrangement. The first and second indexing mechanism arrangements are arranged such that rotation of the driving shaft in a first rotational direction causes the first restraint to rotate between a lowered position and a raised position, and further rotation of the driving shaft in the same rotational direction causes the second restraint to rotate between the lowered position and the raised position. The first restraint may be axially offset from the second restraint to allow sequential loading and unloading of cargo.

    Restraint System Utilizing Co-Axial Actuation
    2.
    发明公开
    Restraint System Utilizing Co-Axial Actuation 审中-公开

    公开(公告)号：US20230150670A1

    公开(公告)日：2023-05-18

    申请号：US17528065

    申请日：2021-11-16

    申请人： GOODRICH CORPORATION

    发明人： Zachary Meyer ,  Brandon David Lee ,  Wallace Harold Larson ,  Alexander Mitchell Heyd

    IPC分类号： B64D9/00

    CPC分类号： B64D9/003

    摘要： A cargo restraint system may comprise an inner shaft and a first outer tube coaxially configured to rotate about an axis and a first restraint located about the first outer tube and configured to rotate about the axis. A second outer tube coupled to the inner shaft configured to rotate about the axis and a second restraint located about the second outer tube and configured to rotate about the axis. The first restraint and the second restraint may include a head configured to rotate about the axis and a plunger configured to translate between an engaged state and a disengaged state.

    Systems and methods for misalignment adjustment utilizing double eccentric bushings
    3.
    发明授权
    Systems and methods for misalignment adjustment utilizing double eccentric bushings 有权

    公开(公告)号：US11905985B2

    公开(公告)日：2024-02-20

    申请号：US17674404

    申请日：2022-02-17

    申请人： GOODRICH CORPORATION

    发明人： Brandon Lee ,  Wallace Harold Larson ,  Zachary Meyer ,  Michael A. Schulz

    IPC分类号： F16B21/18 ,  F16B5/02 ,  F16B19/02

    CPC分类号： F16B21/186 ,  F16B5/025 ,  F16B5/0225 ,  F16B19/02

    摘要： A double eccentric bushing arrangement comprises a first eccentric bushing comprising a first eccentric aperture, a second eccentric bushing comprising a second eccentric aperture, a fastener, a washer configured to be received around a portion of the second eccentric bushing, and a snap ring configured to be received around a portion of the second eccentric bushing to secure the washer in an installed position. The first eccentric bushing is configured to receive the second eccentric bushing in the first eccentric aperture. The second eccentric bushing is configured to receive the fastener in the second eccentric aperture. The first eccentric bushing is rotatable with respect to the second eccentric bushing to adjust a position of the fastener with respect to an adjacent component to which the fastener is being attached.