Described is a thrust-reversing aircraft (1, 1 ', 1' ') comprising: a fuselage (2) having a first longitudinal axis (A) and a head (12) and a tail (13); the wings (3) are respectively arranged on two opposite sides of the fuselage (2) and are used for carrying corresponding rotors (5); a pair of engines (4) operatively connected to respective rotors (5); at least one first lift surface (19, 16) provided on the tail (13); and a pair of canards (14) disposed on the head (12) of the fuselage (2) and defining a respective second lift surface adapted to produce a third lift/negative lift value; each rotor (5) comprising a main shaft (9) rotatable relative to the fuselage (2) about a second axis (B) and about an associated third axis (E) transverse to the second axis (B), so as to place the thrust-reversing aircraft (1, 1 ', 1' ') between the helicopter configuration and the aircraft configuration; in use, each second axis (B) is transverse to the first axis (A) of the thrust-reversing aircraft (1, 1 ', 1' ') in the helicopter configuration and parallel to the first axis (A) in the aircraft configuration.
描述了一种推力换向式飞机(1,1’,1”),其包括:具有第一纵向轴线(A)以及头部(12)和尾部(13)的机身(2);分别设置在机身(2)的相对两侧上的承载相应的旋翼(5)的一对机翼(3);操作性地连接至相应的旋翼(5)的一对发动机(4);设置在尾部(13)上的至少一个第一升力表面(19,16);以及设置在机身(2)的头部(12)上并限定了适于产生第三升力/负升力值的相应的第二升力表面的一对鸭翼(14);每个旋翼(5)包括能围绕第二轴线(B)和围绕横切于第二轴线(B)的相关第三轴线(E)相对于机身(2)旋转的主轴(9),以将推力换向式飞机(1,1’,1”)设置在直升机构造与飞机构造之间;在使用中每条第二轴线(B)在直升机构造中横切于推力换向式飞机(1,1’,1”)的第一轴线(A)并在飞机构造中平行于第一轴线(A)。
Thrust reversing type aircraft
推力换向式飞机
2022-09-30
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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