Micro fixed-wing aircraft capable of hovering

Abstract

The invention discloses a micro fixed-wing aircraft capable of hovering. The micro fixed-wing aircraft comprises an aircraft body as well as two horizontal rudder surfaces, two vertical tails, even sets of motors and propellers which are symmetrically arranged on the axle wire of the aircraft body; the motors are connected with the propellers and then are arranged at the head of the aircraft body; the two horizontal rudder surfaces are hinged to the tail of the aircraft body through hinges; the two vertical tails are vertically arranged on two sides of the tail of the aircraft body and are protruded relative to the upper surface and the lower surface of the aircraft body; a flight control system is arranged inside the aircraft body. The direction of the aircraft disclosed by the invention is controllable in a three-dimensional space at a vertical take-off, a landing and a hovering stage; under the control of assisted augmentation of the flight control system, flight motion of the aircraft in the three-dimensional space can be realized. With a wing-body integrated structure and a thin-wall aircraft body, substantial reduction of the size of the aircraft body can be realized; the aircraft disclosed by the invention has the advantages of convenience in carrying and use, small structure and conservation of manufacturing materials.

Description

technical field [0001] The invention relates to the field of aviation aircraft, in particular to a miniature hoverable fixed-wing aircraft applied to unmanned aircraft technology. Background technique [0002] In recent years, with the rapid development of electronic technology, drones have played an increasingly important role in communication relay, environmental monitoring, forest fire prevention, geological exploration, aerial photography, power line inspection, remote sensors and other fields. Existing unmanned aerial vehicles can be roughly divided into two classes, namely two kinds of multi-rotor aircrafts and fixed-wing aircrafts. Because multi-rotor aircraft needs multiple motors to work at the same time to provide enough power for the aircraft to achieve maneuvers such as hovering and level flight, it has the disadvantages of high energy consumption, short flight time, and slow flight speed; while fixed-wing aircraft has good aerodynamic Features, long flight time...

AI Technical Summary

Problems solved by technology

[0004] Aiming at the disadvantages of the aircraft in the above-mentioned prior art, such as difficulty in take-off and landing, inability to realize three-dimensional movement, and inconvenient portability, the applicant provides a miniature hovering fixed-wing aircraft with integrated wing and body, which can take off and land vertically, is easy to use, and is easy to fly. Fast speed, able to hover and fly peacefully, realize three-dimensional free movement

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