a multi-propeller aircraft
A technology of aircraft and wings, applied in the field of aircraft, can solve problems such as low safety and stability, difficulty in taking off and landing in a short distance, and low efficiency
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[0011] Now in conjunction with accompanying drawing the present invention is described in detail: a kind of multi-rotor aircraft comprises fuselage 1, left compound wing 2, right compound wing 3, empennage 4 and landing gear 5. The fuselage 1 is equipped with a control system and airborne equipment. The left compound wing 2 and the right compound wing 3 have the same structure, and they are symmetrically installed on the left and right sides of the fuselage 1. Empennage 4 is positioned at the tail of fuselage 1, and empennage 4 comprises horizontal empennage and vertical empennage. The horizontal stabilizer acts as a horizontal stabilizer and elevator, and the vertical stabilizer acts as a vertical stabilizer and rudder. Landing gear 5 adopts wheel structure. The structure of the left compound wing 2 is: the left compound wing 2 comprises front wing 21, rear wing 22, wing shaft 23, outer rotor 24, inner rotor 25, outer engine 26, inner engine 27 and support 28. The rear end...
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Abstract
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