An arrangement may comprise a spring member. A proximal end and a distal end of a compression rod may contact engagement features via the spring member in a core cowl of a gas turbine engine. The compression rod may transmit loads between halves of the core cowl. The spring member may compress and decompress in response to vibrations or other relative movement between halves of the core cowl.


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    Titel :

    THRUST REVERSER COMPRESSION ROD WITH SPRING BIASED ENGAGEMENT


    Beteiligte:
    LU JACQUES (Autor:in)

    Erscheinungsdatum :

    27.07.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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