Vertical take-off and landing aircraft
A vertical take-off and landing aircraft and airframe technology, applied in the field of aircraft, can solve problems such as low reliability, impact on flight safety, complex airframe, etc., and achieve the effects of reducing the number of engines, improving safety performance, and good flightworthiness
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[0017] Hereinafter, the present invention will be further described in detail with reference to specific embodiments in conjunction with the drawings.
[0018] In Figure 1: 1 is the body, 2 is the main wing, 3 is the engine, 4 is the propeller, 5 is the vertical tail, and 6 is the horizontal tail. The torque produced by the engine 3 installed on the body 1 or the main wing 2 is transmitted to the input shaft 10 of the clutch 9 installed in the body 1 through the transmission gear 8 (or transmission belt, chain, etc.). The clutch 9 engages the central transmission (or deceleration). The transmission (or reducer) 11 transmits the torque after the torque conversion to the end bevel gear 13 of the transmission shaft 12 (or transmission belt, transmission chain, hydraulic transmission mechanism, etc.) to the center of gravity of the aircraft or before and after the main wing 2. The shaft ends of the drive shaft 14 of at least two pairs of the propeller 4 are input to the bevel gear 15....
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