The present invention relates to a static discharger, an aircraft, and an installation process for the static discharger. According to an aspect of the present invention, a static discharger (10) is provided which includes: a basement (12) adapted to be installed to a supporting and conductive structure (24) of a moving body (AC); and a discharger body (DB) adapted to be installed to the basement. An installation orientation adjusting mechanism (OA) is provided between the basement and the discharger body, and the installation orientation adjusting mechanism allows the discharger body to be rotationally orientated, with respect to the basement, to a predetermined installation orientation during an on-site-installation of the static discharger. The static discharger further includes a first fixing mechanism (PM1) adapted to fix the discharger body, which has been oriented to the predetermined installation orientation, to the basement. According to the present invention, for example, installation adaptation and universality of the static discharger and adjustment and determination of installation orientation of the static discharger can be improved.


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    Titel :

    STATIC DISCHARGER, AIRCRAFT AND INSTALLATION PROCESS FOR THE STATIC DISCHARGER


    Weitere Titelangaben:

    STATISCHER ABLEITER, FLUGZEUG UND INSTALLATIONSVERFAHREN FÜR DEN STATISCHEN ABLEITER
    DÉPERDITEUR STATIQUE, AÉRONEF ET PROCÉDÉ D'INSTALLATION DU DÉPERDITEUR STATIQUE


    Beteiligte:
    WANG LONG (Autor:in) / HAN ZENGLI (Autor:in)

    Erscheinungsdatum :

    2019-01-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05F STATIC ELECTRICITY , Statische Elektrizität



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