There is described an aircraft (1) comprising a fuselage (2, 2 ', 2' ') having a nose (4) and a tail (5) arranged on mutually opposite portions along a first longitudinal axis (Y); a pair of half wings (3) arranged on respective mutually opposite sides of the fuselage (2, 2 ', 2' '); first and second rotors (22a, 22b) carried by the respective half-wings (3), rotatable about second and third axes (F, G), respectively, tiltable relative to the fuselage (2, 2 ', 2' '), and operable independently of one another; the aircraft (1) being switchable between a first hover flight or takeoff/landing configuration in which the fourth and fifth axes (F, G) are arranged orthogonally to said first axis (Y) and a second forward flight configuration in which the fourth and fifth axes (F, G) are arranged parallel or inclined with respect to said first axis (Y); the aircraft (1) further comprises a tail portion (6) comprising a first aerodynamic surface (8) and third and fourth rotors (21a, 21b) rotatable about fixed fourth and fifth axes (F, G); and support means (31a, 31b) connected to the third and fourth rotors (21a, 21b) of the corresponding said half wings (3) and the corresponding said fins (52).
描述了一种飞行器(1),其包括具有沿着第一纵向轴线(Y)布置在彼此相对的部分上的机头(4)和机尾(5)的机身(2、2’、2”);布置在机身(2、2’、2”)的相应的相互相对的两侧上的一对半机翼(3);由相应的半机翼(3)承载的第一和第二旋翼(22a、22b),该第一和第二旋翼能够分别围绕相对于所述机身(2、2’、2”)可倾斜的第二和第三轴线(F、G)旋转,并且能够彼此独立地操作;飞行器(1)能在第四和第五轴线(F、G)正交于所述第一轴线(Y)布置的第一悬停飞行或起飞/着陆形态与第四和第五轴线(F、G)相对于所述第一轴线(Y)平行或倾斜布置的第二向前飞行形态之间切换;飞行器(1)还包括机尾部分(6),该机尾部分包括第一空气动力学表面(8)以及能够围绕固定的第四和第五轴线(F、G)旋转的第三和第四旋翼(21a、21b);以及连接到对应的所述半机翼(3)和对应的所述鳍板(52)的第三和第四旋翼(21a、21b)的支撑装置(31a、31b)。
Convertible aircraft capable of hovering
能够悬停的可转换飞行器
2024-12-27
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |