The present invention relates to an apparatus capable of adjusting aircraft lift force in the structure. According to the apparatus, the stretching sub-wings are adopted and are applied during takeoff and landing so as to increase/decrease the flying speed, achieve the same lift force, increase adaptation energies of the aircraft at different speeds, improve safety performance, and provide the high speed and low speed compatibility, and the development direction of the new generation of the aircraft is provided. The apparatus of the present invention comprises the auxiliary wings, a rotation regulation device, and fixed concave grooves, wherein the auxiliary wings are provided with the concave grooves for adjusting the wind direction, and each side wall of the aircraft body is provided with the one fixed concave groove.
Apparatus capable of adjusting aircraft lift force in structure
2015-06-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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