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    LATCH SOLENOID ACTUATED FULLY AUTOMATIC AUXILIARY GUIDE ASSEMBLY
    1.
    发明公开
    LATCH SOLENOID ACTUATED FULLY AUTOMATIC AUXILIARY GUIDE ASSEMBLY 审中-公开

    公开(公告)号：US20240317401A1

    公开(公告)日：2024-09-26

    申请号：US18319992

    申请日：2023-05-18

    申请人： GOODRICH CORPORATION

    发明人： ELVIS JACK PEREIRA ,  Sayooj Adavalath Puthiyaveettil

    IPC分类号： B64D9/00

    CPC分类号： B64D9/003 ,  B64D2009/006

    摘要： An auxiliary guide assembly is disclosed. The auxiliary guide assembly including a head including a guiding surface and an overriding surface, a pinion, a hub configured to receive the pinion, a union unit configured to secure the pinion to the hub, the union unit rotationally coupled to the pinion and the head, a solenoid coupled to the hub, the solenoid configured to receive a first electric polarity, a reciprocating rod disposed through the solenoid, the reciprocating rod having a first rod end including a rack operatively coupled to the pinion, and an armature adjacent the solenoid and configured to engage the reciprocating rod, the armature moves in a first direction in response to the solenoid receiving the first electric polarity, the armature moving the reciprocating rod in the first direction, and the head rotates in a second direction in response to the reciprocating rod moving in the first direction.

    TIE DOWN FOR CARGO HANDLING SYSTEMS
    4.
    发明公开
    TIE DOWN FOR CARGO HANDLING SYSTEMS 审中-公开

    公开(公告)号：US20230322387A1

    公开(公告)日：2023-10-12

    申请号：US17704731

    申请日：2022-03-25

    申请人： GOODRICH CORPORATION

    发明人： RYAN E. PFAU ,  BRIAN J. VAN BERKOM

    IPC分类号： B64D9/00

    CPC分类号： B64D9/003 ,  B64D2009/006

    摘要： A tie down for a cargo handling system may comprise a carriage. the carriage may include a first sidewall surface, a second sidewall surface opposite the first sidewall surface, a first surface extending from the first sidewall surface to the second sidewall surface, and a second surface opposite the first surface. A first rail interface pin may be configured to extend from the first sidewall surface. A second rail interface pin may be configured to extend from the second sidewall surface. A seat fitting channel may be formed in the carriage and may extend between the first sidewall surface and the second sidewall surface.

    SYSTEM AND METHOD FOR RESTRAINING CARGO
    5.
    发明申请
    SYSTEM AND METHOD FOR RESTRAINING CARGO 审中-公开

    公开(公告)号：US20190061945A1

    公开(公告)日：2019-02-28

    申请号：US15692009

    申请日：2017-08-31

    申请人： The Boeing Company

    发明人： Gabriel A. Quixano Mendez ,  Paul M. Wilde ,  Ananthram Kota Shashidhar ,  Haisan K. Trinh

    IPC分类号： B64D9/00

    CPC分类号： B64D9/003

    摘要： An aircraft cargo restraint system includes an attenuator member fixed at two first attachment locations within a cargo storage compartment of a fuselage of an aircraft. The cargo restraint system also includes a cargo restraint configured to be coupled to the attenuator member at a second attachment location of the attenuator member, located between the two first attachment locations. The cargo restraint is configured to restrain cargo loaded on a cargo deck of the cargo storage compartment. The attenuator member is configured to deflect in response to a load applied to the attenuator member by the cargo restraint.

    LOCK ASSEMBLY WITH ROTATING INNER PAWL
    6.
    发明申请
    LOCK ASSEMBLY WITH ROTATING INNER PAWL 审中-公开

    公开(公告)号：US20180222586A1

    公开(公告)日：2018-08-09

    申请号：US15584272

    申请日：2017-05-02

    申请人： GOODRICH CORPORATION

    发明人： Vinodkumar Shivalinga ,  Narain Jayaprakash

    IPC分类号： B64D9/00 ,  B60P7/13

    CPC分类号： B64D9/003 ,  B60P7/0892 ,  B60P7/10 ,  B60P7/13 ,  B64D9/00

    摘要： A lock assembly includes a pawl body having first restraint surface and a second restraint surface, wherein the pawl body rotates between an extended position and a retracted position, an inner pawl rotatably coupled to the pawl body, wherein the inner pawl is rotated away from the second restraint surface in the retracted position of the pawl body, and a biasing member associated with the inner pawl, wherein the biasing member urges the inner pawl to be aligned with the second restraint surface in the extended position of the pawl body.

    Cargo restraint for aircraft
    9.
    发明授权
    Cargo restraint for aircraft 有权

    公开(公告)号：US10017251B2

    公开(公告)日：2018-07-10

    申请号：US15174442

    申请日：2016-06-06

    申请人： Ancra International, LLC

    发明人： John F. Rowles ,  Edward H. Moradians ,  Victor Bassly

    IPC分类号： B60P7/08 ,  B64D9/00 ,  B64D11/06

    CPC分类号： B64D9/003 ,  B60P7/08 ,  B64C1/20 ,  B64D11/0696

    摘要： Systems for restraining palleted cargo within an aircraft are provided. A first system operates to provide vertical and outboard lateral support to cargo at a location where the opposite ends of the system are connected to surfaces that are aligned at different orientations, for example, one end connected to a horizontal floor and the second end connected to a sidewall of the fuselage of the aircraft. A second system operates to provide aft, vertical, and outboard lateral support to cargo upon a pallet proximate to its corner, and at a location where a portion of cargo extends above a stay out zone of the aircraft.