A thrust-reversing aircraft (1, 1 ', 1' ') is described, comprising: a fuselage (2) having a first longitudinal axis (A) and in turn comprising a head (12) and a tail (13); a pair of wings (3) respectively arranged on opposite sides of the fuselage (2), carrying respective rotors (5) and generating lift values; and a pair of engines (4) operatively connected to the respective rotors (5); each rotor (5) comprising a main shaft (9) rotatable about a second axis (B) between a helicopter configuration and an aircraft configuration; and each engine (4) is inserted between the fuselage (2) and the corresponding rotor wing (5) along the extension direction of the corresponding wing (3).

    描述了一种推力换向式飞机(1,1’,1”),其包括:机身(2),其具有第一纵向轴线(A)并且又包括头部(12)和尾部(13);分别设置在机身(2)的相对两侧上的一对机翼(3),它们承载相应的旋翼(5)并且产生升力值;以及操作性地连接至相应的旋翼(5)的一对发动机(4);每个旋翼(5)包括能围绕第二轴线(B)在直升机构造与飞机构造之间旋转的主轴(9);每个发动机(4)沿着相关机翼(3)的延伸方向插在机身(2)与相关旋翼(5)之间。


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    Titel :

    Thrust reversing type aircraft


    Weitere Titelangaben:

    推力换向式飞机


    Beteiligte:

    Erscheinungsdatum :

    2022-09-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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