Aircraft with vertical takeoff and landing capability and casing bodies The invention relates to an aircraft (1) with vertical takeoff and landing capability, comprising a fuselage (2) with a longitudinal axis (L) and with multiple casing bodies (30) arranged on the fuselage (2), wherein at least one of the casing bodies (30) is mounted so as to be rotatable about a transverse axis (Q) arranged at an angle with respect to the longitudinal axis (L), and wherein the aircraft (1) comprises at least one propulsion device (10) with a rotatable turbomachine (20) and one of the casing bodies (30), wherein the rotatable turbomachine (20) has an axis of rotation (R) which is rotatable by means of the transverse axis (Q), and the casing body (30) has a substantially cylindrical section (31) extending along the axis of rotation (R), wherein the cylindrical section (31) coaxially surrounds the turbomachine (20). It is provided that the casing body (30) is designed to generate lift, in particular during horizontal flight of the aircraft (1), whereby the casing body is thus in the form of an annular wing.

    本发明涉及一种可竖直起飞和降落的飞行物(1),包括具有纵向轴线(L)的机身(2)以及多个布置在机身(2)处的罩体(30),其中,罩体(30)中的至少一个罩体围绕与纵向轴线(L)成角度地布置的横向轴线(Q)可转动地支承,并且其中,飞行物(1)包括至少一个驱动装置(10),所述驱动装置具有可旋转的涡轮机(20)和罩体(30)中的一个罩体,其中,可旋转的涡轮机(20)具有可通过横向轴线(Q)旋转的旋转轴线(R),并且罩体(30)具有沿着旋转轴线(R)延伸的、基本上柱状的区段(31),其中,柱状的区段(31)同轴地包围涡轮机(20)。设置成,罩体(30)构造成用于,尤其是在飞行物(1)的水平飞行中产生升力,其中,由此罩体构造为环形翼。


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    Titel :

    AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING CAPABILITY


    Weitere Titelangaben:

    可竖直起飞和降落的飞行物


    Beteiligte:
    SAUER SEBASTIAN (Autor:in) / KURZ CARLO (Autor:in) / ZLATKOV BRANISLAV (Autor:in) / FRICKE MARTIN (Autor:in) / TAPPE OLIVER (Autor:in) / SANCHA GARCIA LUIS ANTONIO (Autor:in) / LUDERS RALF (Autor:in)

    Erscheinungsdatum :

    2022-02-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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