Multi-wing aircraft and its flight control method
A flapping-wing aircraft and wing technology, applied in the field of aircraft, can solve the problems of complex flapping-wing mechanism, small lift, difficulty in increasing the wing swing frequency, etc., and achieve the effects of low manufacturing cost, large torque, and low magnetic flux leakage.
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[0032] The present invention will be further described below in conjunction with accompanying drawing.
[0033]Overall structure of the present invention is as figure 1 As shown, the long dashed line is the first hinge axis of the left front flapping wing mechanism, and the short dashed line is the shortest line segment between the first hinge axis of the left front flapping wing mechanism and the vertical axis of the flapping wing aircraft. The specific structure includes frame 1 (such as Figure 8 As shown), there is a landing gear below the frame 1, and when the flapping-wing aircraft is parked on a horizontal plane, the bottom surface of the frame 1 is parallel to the horizontal plane. figure 2 It is a plan view that the left front and right rear wings of the present invention swing clockwise to the maximum angle around the second hinge and the left rear and right front wings swing counterclockwise to the maximum angle around the second hinge. image 3 It is a plan view ...
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