The invention relates to air transport and can be used in aircraft of various designs. The aircraft wing comprises the lifting surface and turbojet engine. The lifting surface is the combination of conventional aerodynamic wing and carrying plate rigidly connected to it. The engine is rigidly attached to the carrying plate so that the stream of hot gas from it flows around its upper surface. The carrying plate profile is the same as the profile of the Laval nozzle of the turbojet engine. The proposed design of the wing is destined to increase the range, carrying capacity and safety of use of aircrafts for various purposes.


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    Title :

    COMBINATION AIRCRAFT WING


    Additional title:

    FLUGZEUGKOMBINATIONSFLÜGEL
    AILE COMBINÉE D'UN AERONEF


    Contributors:

    Publication date :

    2016-10-26


    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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