The present invention relates to an apparatus capable of adjusting aircraft lift force in the structure. According to the apparatus, the stretching sub-wings are adopted and are applied during takeoff and landing so as to increase/decrease the flying speed, achieve the same lift force, increase adaptation energies of the aircraft at different speeds, improve safety performance, and provide the high speed and low speed compatibility, and the development direction of the new generation of the aircraft is provided. The apparatus of the present invention comprises the auxiliary wings, a rotation regulation device, and fixed concave grooves, wherein the auxiliary wings are provided with the concave grooves for adjusting the wind direction, and each side wall of the aircraft body is provided with the one fixed concave groove.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Apparatus capable of adjusting aircraft lift force in structure


    Beteiligte:
    SU XI AN (Autor:in) / CAO YING (Autor:in)

    Erscheinungsdatum :

    17.06.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    LIFT APPARATUS FOR CAR MAINTENANCE CAPABLE OF ADJUSTING GUIDE

    Europäisches Patentamt | 2019

    Freier Zugriff

    LIFT APPARATUS FOR CAR MAINTENANCE CAPABLE OF ADJUSTING GUIDE

    BEAK JIN MOON | Europäisches Patentamt | 2019

    Freier Zugriff

    Roof-wing aircraft capable of flying by utilizing vortex lift force

    YANG WEIHUA | Europäisches Patentamt | 2023

    Freier Zugriff

    No-flapping-hinge helicopter rotor wing capable of automatically adjusting rotor wing lift force

    WANG YUN / TANG JIANXIANG | Europäisches Patentamt | 2022

    Freier Zugriff