A vertical take-off and landing fixed-wing aircraft
A vertical lift, fixed-wing technology, applied in the field of aircraft, can solve the problems of increased resistance, large take-off and landing space, small lift, etc., to achieve the effects of improving stability, reducing resistance, and increasing power
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Embodiment 1
[0040] Embodiment 1 of the present invention discloses a fixed-wing aircraft that can be lifted vertically, including a fuselage 1, wings 2, a retractable empennage 3, a rear rotor mechanism 4 and a front rotor mechanism 5; the wings 2 are symmetrically arranged on the fuselage 1 on both sides; the telescopic empennage 3 is arranged on the tail of the fuselage 1; the rear rotor mechanism 4 is arranged on the rear side of the wing 2, and the rear rotor mechanism 4 includes a retractable telescopic mechanism 15; the front rotor mechanism 5 advances along the The direction is set on the front side of the wing 2, and the front rotor mechanism 5 can be tilted upwards by 0-90°.
[0041] The beneficial effects of the above preferred technical solutions are: a vertical liftable fixed-wing aircraft disclosed by the present invention, wherein the telescopic empennage 3 can be stretched back and forth according to the requirements of use, and the empennage 7 and the aircraft can be increa...
Embodiment 2
[0059] A fixed-wing aircraft capable of vertical lift, comprising a fuselage 1, wings 2, a retractable empennage 3, a rear rotor mechanism 4 and a front rotor mechanism 5;
[0060] The wing 2 comprises a first group of wings 2a and a second group of wings 2b, the first group of wings 2a and the second group of wings 2b are located on different horizontal planes, and are located on different vertical planes, the first group of wings 2a and the second group of wings 2b The second group of wings 2b are all symmetrically arranged on both sides of the fuselage, the front sides of the first group of wings 2a and the second group of wings 2b are all provided with a front rotor mechanism 4, the first group of wings 2a and the second group of wings The rear side of the wing 2b is provided with a rear rotor mechanism 5;
[0061] The retractable empennage 3 is arranged on the afterbody of the fuselage 1; the rear rotor mechanism 4 is arranged on the rear side of the wing 2, and the rear ...
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