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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    Title :

    THRUST REVERSER COMPRESSION ROD WITH SPRING BIASED ENGAGEMENT


    Contributors:
    LU JACQUES (author)

    Publication date :

    2017-07-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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