Variant tiltrotor aircraft and working method thereof
A tilt-rotor and variant technology, applied in the field of aviation aircraft, can solve the problems of low power utilization rate, poor flight performance, poor maneuverability, etc., to improve safety and reliability, improve coordination and maneuverability, and improve controllability Effect
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[0023] In order to facilitate the understanding of those skilled in the art, the present invention will be further described below in conjunction with the embodiments and accompanying drawings, and the contents mentioned in the embodiments are not intended to limit the present invention.
[0024] refer to figure 1 , figure 2 As shown, a variant tiltrotor of the present invention comprises: blade 1, fairing 2, wing 3, transition fuselage 4, high T-shaped tail 5, horizontal tail 6, vertical tail 7, engine short Cabin 8, landing gear 9, and fuselage 10; wherein, propeller blade 1 is fixedly connected on fairing 2, and fairing 2 is fixedly connected on the engine nacelle 8, and engine nacelle 8 is connected with fuselage 10 interior through transmission shaft respectively. The transmission system is connected, and the wing 3 is fixed on the top of the fuselage 10. The tiltrotor adopts a high T-shaped empennage 5 layout, which is fixed on the tail of the fuselage 10. The empennag...
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