Unmanned aerial vehicle capable of patrolling with long endurance, wide speed range and high mobility

An unmanned aerial vehicle and long-endurance technology, applied in the field of aircraft, can solve the problems of not being able to simultaneously meet high and low speed performance requirements, and being unable to adjust

Pending Publication Date: 2020-02-28
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Conventional roving unmanned aerial vehicles often can only meet one of the above performances, but cannot take into account both high and low speed performance requirements
Its flight missions usually have certain limitations, and it is difficult to adjust a reasonable attitude with the complex and changeable external environment, and it is difficult to maximize its advantages

Method used

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  • Unmanned aerial vehicle capable of patrolling with long endurance, wide speed range and high mobility
  • Unmanned aerial vehicle capable of patrolling with long endurance, wide speed range and high mobility
  • Unmanned aerial vehicle capable of patrolling with long endurance, wide speed range and high mobility

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Embodiment Construction

[0021] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. It should be understood that the specific embodiments described here are only used to explain the present invention, and are not intended to limit the protection content of the present invention.

[0022] The unmanned aerial vehicle that the present embodiment can provide for long endurance, wide speed and high maneuverability cruise mainly includes: fuselage 1, foldable wing inner wing section 2, stretchable outer wing section 3 along the span direction, outer wing section A pair of ailerons 4, a pair of one-piece flaperon 5 in the inner wing section, an upper V-shaped tail 6, a power unit 7, an upper V-shaped tail aerodynamic control surface 8, and 9 ventral fi...

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Abstract

The invention provides an unmanned aerial vehicle capable of patrolling with long endurance, wide speed range and high mobility. The unmanned aerial vehicle mainly comprises a fuselage, a pair of foldable inner wing sections arranged on the two sides of the fuselage, outer wing sections which are telescopic in the spanwise direction, a pair of foldable upper V-shaped empennages arranged at the tail of the fuselage, and a pair of foldable ventral fins, and a power unit at the tail of the fuselage. The two changeable foldable wings on the two sides of the fuselage can rotate in the planes of thewings according to the use requirements, so as to realize the functions of folding and changing backswept wings; the outer wing sections which are telescopic in the spanwise direction assists in increasing the aspect ratio of the wing; the pair of foldable upper V-shaped empennages at the tail of the fuselage and the pair of foldable ventral fins are used to improve the maneuverability and have low resistance characteristics compared with conventional empennages; and the power unit is mounted at the rear section of the fuselage, and a turbojet power, piston power and turbojet / piston dual power unit can be optionally mounted to enable the unmanned aerial vehicle to fly efficiently and stably. The change of the position of the foldable wings at different speeds, the outer wing sections which are telescopic in the spanwise direction, the foldable upper V-shaped empennages, the foldable ventral fins and the tail power unit of the fuselage jointly improve the adaptability of the unmanned aerial vehicle at different speeds.

Description

technical field [0001] Embodiments of the present invention relate to aircraft technology, and in particular to an unmanned aerial vehicle capable of long-endurance, wide-speed range, and high-mobility cruising. Background technique [0002] The roving unmanned aerial vehicle is a new concept aircraft that can perform patrol flights in the target area and perform various tasks such as reconnaissance, strike, communication, and relay. At present, in order to meet its comprehensive mission performance and consider the variability of the external environment, the cruising UAV should have the characteristics of high maneuverability, rapid arrival and strike, and long endurance. Conventional roving unmanned aerial vehicles often can only meet one of the above-mentioned performances, but cannot take into account both high-speed and low-speed performance requirements. Its flight missions usually have certain limitations, and it is impossible to adjust a reasonable attitude with th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C3/40B64C3/54B64C5/14B64C5/18
CPCB64C39/02B64C3/40B64C3/546B64C5/14B64C5/18B64U10/25
Inventor 甘文彪向锦武张毅王红波彭博
Owner BEIHANG UNIV
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