Blade rotatable horizontal type four-wheel type movable wing aircraft combined with fixed wing
The invention discloses a blade rotatable horizontal type four-wheel type movable wing aircraft combined with a fixed wing. The aircraft is characterized by comprising wheel type movable wings, transmission mechanisms, cams, rotary shafts, speed reducers, motors, a machine body frame and the fixed w...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention discloses a blade rotatable horizontal type four-wheel type movable wing aircraft combined with a fixed wing. The aircraft is characterized by comprising wheel type movable wings, transmission mechanisms, cams, rotary shafts, speed reducers, motors, a machine body frame and the fixed wing; the four cams are symmetrically mounted and fixed on the two sides of the machine body frame, the four rotary shafts are symmetrically arranged on the two sides of the machine body frame, the axis directions of the four rotary shafts are vertical to the longitudinal symmetry plane of the aircraft, the four rotary shafts are arranged in a front row and a rear row, the four motors arranged on the machine body frame are decelerated by the four speed reducers arranged on the machine body frame separately and then drive the four rotary shafts to continuously rotate, the four wheel type movable wings are fixedly connected to the four rotary shafts separately, and the four sets of transmission mechanisms are connecte |
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