Variable power wing vertical short-range taking off and landing aircraft

Variable power wing vertical short-range taking off and landing aircraft

  • CN 102,991,672 A
  • Filed: 05/18/2012
  • Published: 03/27/2013
  • Est. Priority Date: 05/18/2012
  • Status: Active Application
First Claim
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1. this patent is:

  • power is on wing, wing links with vertical pressure fluted disc by the horizontal beam axle with body, wing can with the body vertical rotary, the aircraft of change of flight direction can be made the unprecedented aircraft aircraft such as various aircrafts, airship, dirigible, hovercar, unmanned aerial vehicle, model airplane machine, flying trapeze'"'"'s device, rocket and hydroairplane.Can hold autogyro and fixed wing aircraft advantage, fly surely, load carrying ability is large, speed is fast, the multiple exceedingly difficult movements such as landing, hovering, inverted flight, upset of can taking off vertically.On the variable power wing wing various power engines can be installed, can fill single-shot, two and multiple-motor unit.Vertical tail can horizontally rotate driving engine be contained on the vertical fin can after the landing of overturning.But aircraft is Horizontal Take-off and Landing also, and distance is very short in airfield runway.The fuel-efficient usable runway landing of heavy duty.Can fill the support feeler lever on the wing and improve the landing functional stabilization that takes off.The independent use of the various functions of above claim also can multinomially be used in combination.

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