Tilt-rotor fixed wing aircraft with vertical take-off and landing function
A tilt-rotor, vertical take-off and landing technology, applied in vertical take-off and landing aircraft, rotorcraft, aircraft control and other directions, can solve problems such as the wasted weight of aircraft structure, too many auxiliary supporting facilities, and shortened aircraft cruising radius, etc. Achieve the effect of performing tasks quickly, taking off and landing anytime, anywhere, and saving the weight of the structure
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[0034] As a specific embodiment, the front end of the fuselage is provided with a pitot tube 4;
[0035] As a specific embodiment, a direction light 9 is provided at the end of the wing.
[0036] As a specific embodiment, the wing is provided with a quick-release structure. The quick-release mechanism uses the fuselage front beam 2012 and the fuselage rear beam 2013 to fix through concave and convex positions, and then uses the taper pin 20 to perform pre-tightening connection.
[0037] As a specific embodiment, the fuselage is provided with an external cooling fin 6 at the place where the motor of the pitching and tilting power device is installed.
[0038] See Figure 4 , as a specific embodiment, the anti-torsion balance power device 16 includes a propeller 1601, a power motor 1602, a motor mounting base 1603, a rotating assembly 1604, a rear end surface 1605 of the fuselage, an electric regulator 1606, a drive transmission mechanism 1607, a reinforced end surface 1608, S...
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