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    ATTACHMENT DEVICE FOR A NON-STRUCTURAL COMPONENT OF A BUILDING
    7.
    发明公开
    ATTACHMENT DEVICE FOR A NON-STRUCTURAL COMPONENT OF A BUILDING 审中-实审

    公开(公告)号：EP4357655A2

    公开(公告)日：2024-04-24

    申请号：EP24161545.9

    申请日：2020-08-13

    申请人： Eaton Intelligent Power Limited

    发明人： WITHERBEE, Martin Lee ,  THORAT, Hemraj K. ,  KHALKAR, Amol

    IPC分类号： F16L3/133

    CPC分类号： F16B11/006 ,  F16B2/22 ,  F16B7/04 ,  F16L3/133

    摘要： An attachment device for securing a non-structural component of a building to a structural component of the building includes a non-structural component holder defining a receiving space configured to receive the non-structural component to couple the non-structural component to the attachment device. The non-structural component holder applies generally no compressive force against the non-structural component when the non-structural component is disposed in the receiving space so that the non-structural component is free to move relative to the non-structural component holder. A stop is configured to be secured to the non-structural component. The stop is configured to engage the non-structural component holder to inhibit movement of the non-structural component relative to the non-structural component holder when the stop and non-structural component holder are secured to the non-structural component.

    AIRCRAFT JOINT
    8.
    发明授权
    AIRCRAFT JOINT 审中-公开

    公开(公告)号：EP3243742B1

    公开(公告)日：2018-12-26

    申请号：EP17169317.9

    申请日：2017-05-03

    申请人： Airbus Operations Limited

    发明人： SALISBURY, Ross

    IPC分类号： B64C3/26 ,  B64C3/28 ,  F16B5/00

    CPC分类号： B64F5/10 ,  B64C3/187 ,  B64C3/26 ,  B64C3/28 ,  F16B11/006

    摘要： An aircraft joint includes a first component having an outer aerodynamic surface and an inner surface, a second component having an outer aerodynamic surface and an inner surface, and a strap assembly bridging between the inner surfaces of the first and second components. The strap assembly has a first strap part attached to the inner surface of the first component, a second strap part attached to the inner surface of the second component, and a third strap part received in the first and second strap parts in a sliding manner. The third strap part when received in the first and second strap parts constrains movement of the first component relative to the second component in a direction normal to the outer aerodynamic surfaces of the first and second components in the vicinity of the strap assembly. Also a method of forming the joint, and a method of replacing a panel on an aircraft wing.