Rod end with locking device for struts

    公开(公告)号:US11959511B2

    公开(公告)日:2024-04-16

    申请号:US17225353

    申请日:2021-04-08

    CPC classification number: F16B7/042

    Abstract: The present invention concerns a rod end that has a locking mechanism where the locking mechanism has an insert, a fork end, a female torque locking element, and a male torque locking element. Upon activation of the locking mechanism, the female torque locking element engages with the male torque locking element in a form-fitting connection. The locking mechanism of the present invention can easily be activated and is capable of withstanding a torque.

    Method for Producing a Positive-Locking Load Application for Rod-Shaped Fiber Composite Structures, and the Design Thereof

    公开(公告)号:US20210071707A1

    公开(公告)日:2021-03-11

    申请号:US17012547

    申请日:2020-09-04

    Abstract: Disclosed are methods and related compositions for producing a positive-locking load application for rod-shaped fiber composite structures, and the design thereof.
    The present invention concerns a method for producing a positive-locking load application for tension-compression rods from a fiber plastic hollow structure by means of an outer sleeve. In this process, a force pushes the fiber plastic hollow structure at least partially over at least one force application element, which is provided with at least one undercut to create a positive-locking connection. An object of the present invention is attained through local heating of the fiber plastic hollow structure to the point of plasticity of the fiber plastic hollow structure, at least in the region of the undercut(s) of the force application element, and application of at least one outer sleeve to the fiber plastic hollow structure in the region of the force application element.

    Fiber composite strut
    10.
    发明授权

    公开(公告)号:US11703078B2

    公开(公告)日:2023-07-18

    申请号:US16811136

    申请日:2020-03-06

    CPC classification number: F16C7/026 F16D1/072 B29C70/86 F16C2220/28

    Abstract: The invention relates to a strut, such as fiber composite struts used in aircraft or spacecraft, which has a largest possible outer diameter within a cylindrical installation space of the strut. The invention concerns an insert connected to a fiber composite hollow structure, such as a fiber plastic composite hollow structure, where the hollow structure engages an undercut of the insert, wherein the outer region of the fiber composite hollow structure likewise has an undercut and this undercut is filled with a fiber composite jacket, such as a fiber plastic composite jacket, and the inner region of the fiber composite hollow structure has, at least in one subregion, a core connected thereto.

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