A supporting structure arrangement for fastening an aircraft gas turbine engine to an aircraft, including: a supporting structural element of the aircraft engine and a supporting structure with at least one support and at least one bearing, by means of which the support can be connected or is connected to the aircraft, wherein the support can be connected or is connected rigidly to the supporting structural element of the aircraft engine by means of a connecting device.


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    Title :

    INTEGRIERTE TRAGSTRUKTUR FÜR EIN FLUGZEUGTRIEBWERK UND DESSEN ZUBEHÖRKOMPONENTEN


    Additional title:

    INTEGRATED SUPPORT STRUCTURE FOR AN AIRCRAFT ENGINE AND COMPONENT PARTS THEREOF
    STRUCTURE PORTANTE INTÉGRÉE POUR UN MOTEUR D'AVION ET SES COMPOSANTS ACCESSOIRES


    Contributors:

    Publication date :

    2021-05-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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