Systems and methods are provided for an aircraft propulsor (108) with a fan cowl with one or more tangential restraints. The tangential restraints may be configured to contact one or more tangential receiving portions of a fixed portion of the aircraft propulsor (108). The fan cowl may receive a load that may include a bending load. The tangential restraints may be configured to convert the bending load to membrane tension and thus decrease deflection of the fan cowl.


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    Title :

    NACELLE FAN COWL TANGENTIAL RESTRAINT


    Additional title:

    TANGENTIALSTÜTZE EINER TRIEBWERKSGONDELFANHAUBE
    SUPPORT TANGENTIEL DE CAPOT DE SOUFFLANTE D'UNE NACELLE


    Contributors:

    Publication date :

    2019-11-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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