An airplane (10) including an airframe (12) and a turboprop propulsion system (14) is disclosed. The turboprop propulsion system (14) includes a propeller (20) mounted for rotation about a propeller axis (30) and a gas turbine engine (22) coupled to the propeller (20) to drive rotation of the propeller (30). The gas turbine engine (22) rotates about an axis (32) which is offset from the propeller axis (30).


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    Title :

    AIRPLANE WITH ANGLE-MOUNTED TURBOPROP ENGINE


    Additional title:

    FLUGZEUG MIT WINKELMONTIERTEM TURBOPROPTRIEBWERK
    AVION COMPORTANT UN TURBOPROPULSEUR À MONTAGE INCLINÉ


    Contributors:

    Publication date :

    2020-02-19


    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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