Aerodynamic layout of flapping-wing matrix aircraft
An aerodynamic layout and aircraft technology, applied in the field of aircraft, can solve the problems of inability to achieve high load, long-term or long-distance flight, and limited load of flapping aircraft, achieve high flight efficiency and energy utilization, improve flight efficiency and Energy utilization, the effect of improving utilization
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[0030] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.
[0031] Such as Figure 1 to Figure 3 As shown, the aerodynamic layout of the flapping wing matrix aircraft of the present invention has a linear cylindrical fuselage as a whole, identical groups of bird-like flapping wings, a large aspect ratio straight wing frame, and a flapping wing and a wing frame. composed of flapping wing matrix.
[0032] The overall shape of the fuselage is straight, the head and tail are streamlined, and the middle section is cylindrical. The flapping wing matrix is installed in the middle section of the fuselage and symmetrically distributed on both sides of the fuselage. The control system, power system, navigation system, camera, cargo warehouse, flapping wing matrix connectors are installed inside the fuselage, and the sled landing gear and load hook are instal...
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