There is provided a component which is configured to be joined to a further component in a preselected relative orientation. The further component has an interface surface and the component is configured to contact the interface surface when joined to the further component. The component comprises a surface facing the interface surface when the components are joined, a plurality of recesses formedin the surface, and a plurality of spacer elements. Each recess has a preselected orientation relative to the component. Each spacer element comprises a contact surface contacting the interface surface when the components are joined. Each spacer element is disposed in one of the recesses such that the orientation of a given contact surface is defined by the orientation of the corresponding recess. Optionally, the surface is curved and convex and the interface surface is flat. Spacers may be cylindrical and recesses may comprise counterbores or sockets. Components may include aircraft wing, interface plate or engine mounting pylon.

    提供了一种部件,该部件被配置成以预选相对取向接合至另一部件。该另一部件具有接口表面,并且该部件被配置成在接合至该另一部件时接触接口表面。该部件包括:设置在该部件的旨在当部件被接合时面向接口表面的一侧上的表面;形成在该表面中的多个凹部;以及多个间隔元件。每个凹部具有相对于该部件的预选取向,该预选取向根据该预选相对取向来选择。每个间隔元件包括接触表面,该接触表面被配置成在部件被接合时接触接口表面。每个间隔元件设置在凹部之一中,使得给定的接触表面的取向由对应的凹部的取向限定。


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    Titel :

    Joining components


    Weitere Titelangaben:

    接合部件


    Beteiligte:
    WILLIAM TULLOCH (Autor:in) / PAT BROOMFIELD (Autor:in)

    Erscheinungsdatum :

    2020-10-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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