Mall unmanned aerial vehicle capable of taking off and landing vertically
A small unmanned aerial vehicle, vertical take-off and landing technology, applied in the field of aircraft, can solve the problem of slow horizontal flight speed of rotor unmanned aerial vehicles, and achieve the effect of simple structure, stable flight and convenient operation
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[0016] Such as figure 1 As shown, a small UAV that can take off and land vertically includes a rotatable wing part I (1), a hinge I (2), a rudder angle I (3), a steering gear I (4), and a wing body I ( 5), Ducted Engine I (6), Ducted Air Inlet I (7), Fuselage Main Body (8), Ducted Air Inlet II (9), Ducted Engine II (10), Wing Main Body II (11), steering gear II (12), rudder angle II (13), hinge II (14), rotatable wing part II (15); the overall bottom surface of the UAV is flat, and the front edge of the body is curved upwards shape, the rear part of the fuselage is in a certain arc-shaped structure, the fuselage main body (8) is a hollow semicircular structure, and the ducted engine I (6) and ducted engine II (10) are installed on both sides of the fuselage main body (8). ), the wings on both sides have a dihedral angle of 2-5 degrees, and the two ends of the wing are the rotatable wing part I (1) and the rotatable wing part II connected by the hinge I (2) and the hinge II (1...
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