Novel hybrid vertical/short take-off and landing (V/STOL) unmanned aerial vehicle

Abstract

The invention discloses a novel hybrid vertical / short take-off and landing (V / STOL) unmanned aerial vehicle, aiming at solving the problems of complicated structure, high cost and the like of the existing aerial vehicles. The unmanned aerial vehicle comprises a body, a main wing, take-off and landing auxiliary wings arranged on the main wing, canards arranged at the front part of the body, a vertical tail arranged at the rear part of the body, a landing gear, an accumulator battery, a control system, a power supply management system and the like, wherein the landing gear, the accumulator battery, the control system, the power supply management system and the like are arranged below the body. The unmanned aerial vehicle adopts a ducted fan to provide a lift and assist balance during vertical take off and landing, and adopts an engine to provide the main push force and to automatically generate electricity so as to effectively utilize oil-electricity complement, simultaneously the reasonable hybrid use of fuel oil and electric energy is achieved through the structure and aerodynamic configuration design of the aerial vehicle, thereby achieving vertical and short take-off and landing, reducing the control difficulty of the aerial vehicle and solving the problem of inconsistence between difficult control and short voyage of the existing V / STOL unmanned aerial vehicles; the novel hybrid vertical / short take-off and landing (V / STOL) unmanned aerial vehicle disclosed by the invention can achieve vertical / short take-off and landing, and has the advantages of flexible and steady flight, wide application range and the like.

Description

technical field [0001] The invention relates to the field of aerospace, in particular to a novel hybrid vertical short-range take-off and landing unmanned aerial vehicle. Background technique [0002] Due to its low cost, good safety and wide range of uses, UAVs have great application potential in both military and civilian fields. In military terms, UAVs can be used for low-altitude reconnaissance, communication, electronic jamming and ground attack; in civilian terms, UAVs can be used for communication relay, environmental research, monitoring and rescue of natural disasters, etc. Therefore, in recent years, unmanned aerial vehicles have attracted people's attention and the attention of the military of various countries. [0003] For early UAVs, their endurance time is short, the flight altitude is low, the reconnaissance and surveillance area is small, and information cannot be obtained continuously, which often leads to intelligence "blind spots". With the deepening of...

AI Technical Summary

Problems solved by technology

The invention adopts the ducted fan to provide lift and assist balance during vertical take-off and landing, and at the same time uses the engine as the main thrust and generates electricity independently, effectively utilizing oil and electricity complementation, and at the same time, realizes the mixed use of fuel and electric energy through the design of the aircraft structure and aerodynamic layout Reasonable configuration, realize vertical and short-distance take-off and landing, reduce the control difficulty of the aircraft, and effectively solve the contradiction between the control difficulty and short range of the existing vertical take-off and landing unmanned aerial vehicle

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