An aircraft (1), in particular a passenger or cargo aircraft, with a fuselage (2), has a tandem wing arrangement and has at least two aero engines (5, 6) disposed on the upper surface of the rear wing (4). In this way the disadvantages of the known solutions of the prior art are avoided and an improved aircraft configuration with improved aerodynamics, namely clearly reduced induced drag, is provided. Moreover, the invention creates an environmentally friendly aircraft design which conserves resources, increasing the acceptance of such aircraft among the population.


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    Title :

    AIRCRAFT CONFIGURATION


    Contributors:

    Publication date :

    2015-07-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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