Wingtip fuselage applied to unmanned aerial vehicle

Abstract

The invention discloses a wingtip fuselage applied to an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The wingtip fuselage comprises a first fuselage body,a second fuselage body, a third fuselage body, a first wingtip small wing and a second wingtip small wing. The first fuselage body comprises a windward part, a first body and a first connecting part.The first body is provided with a first forewing and a second forewing. The second fuselage body comprises a second connecting part, a second body and a third connecting part. The second body comprises a first side face, a second side face and a third side face. The first side face is provided with a first rear wing. The second side face is provided with a second rear wing. The third side face isprovided with a vertical wing. The third fuselage body comprises a four connecting part, a third body and a tail. The first wingtip fastening end and the first rear opening end of the first wingtip small wing are fixedly connected. The second wingtip fastening end and the second rear opening end of the second wingtip small wing are fixedly connected. According to the wingtip fuselage applied to the unmanned aerial vehicle, the technical effects that the stability of the unmanned aerial vehicle is improved, and daily maintenance of the unmanned aerial vehicle is convenient are achieved.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, in particular to a wingtip fuselage applied to unmanned aerial vehicles. Background technique [0002] Unmanned UAV, referred to as "UAV", is an unmanned UAV controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device, information collection device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. It can take off like an ordinary UAV under radio remote control or be launched into the air with a booster rocket, or it can be brought into the air by the parent aircraft for flight. [0003] For the unmanned aerial vehicle, the unmanned aerial vehicle fuselage in the prior art is made of a one-piece struct...

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is that when the UAV is in flight, the wingtips will reduce the stability of the UAV; the daily maintenance of the UAV is also difficult.

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