The invention belongs to the field of aircrafts, and provides a vertical take-off and landing amphibious ground-effect aircraft. The vertical take-off and landing amphibious ground-effect aircraft comprises a fuselage, wings, an empennage, propeller blades, take-off and landing propellers, outer wings, propeller cover plates, buoys, a nose landing gear, a main landing gear, an engine and an oil tank. Four rotors are additionally arranged in the middle of the wing to achieve the vertical take-off and landing function, the two tiltable rotors are arranged at the empennage, lift force is providedduring take-off and landing, advancing power is provided during level flight, wing cover plates are closed during level flight, and the high lift-drag ratio is kept. A front three-point retractable undercarriage is arranged at the lower part of the fuselage. The vertical take-off and landing amphibious ground-effect aircraft has the functional characteristics of a rotor wing helicopter and a fixed wing aircraft, does not need any runway during take-off and landing, and can complete take-off and landing on land and in open places on the sea surface.

    本发明属于飞行器领域,提供一种垂直起降水陆两栖地效飞行器,包括:机身,机翼,尾翼,推进桨,起降螺旋桨,外翼,螺旋桨盖板,浮筒,前起落架,主起落架,发动机,油箱。在机翼中部增加四处旋翼,实现垂直起降功能,尾翼处布置两台可倾转旋翼,起降时提供升力,平飞时提供前进动力,在平飞时机翼盖板封闭,保持了较高的升阻比。机身下部布置有前三点式可收放起落架。本发明所述垂直起降水陆两栖地效飞行器具备旋翼直升机及固定翼飞行器的功能特点,其起飞降落不需任何跑道,在陆地及海面空旷的地方就能完成起降。


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    Titel :

    Vertical take-off and landing amphibious ground-effect aircraft


    Weitere Titelangaben:

    一种垂直起降水陆两栖地效飞行器


    Beteiligte:
    CHEN SHUAI (Autor:in) / LUO BEN (Autor:in) / WU MENGJUN (Autor:in) / WANG KUNLUN (Autor:in) / WANG BINBIN (Autor:in)

    Erscheinungsdatum :

    2020-04-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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