an unmanned transport aircraft

Abstract

The invention relates to the field of unmanned aerial vehicles, in particular to an unmanned transport aircraft vehicle which comprises an air flow central guide plate, eight ailerons, a folding undercart and a lifter, wherein the eight ailerons are symmetrically arranged on the air flow central guide plate; the folding undercart and the lifter are arranged on the lower side of the air flow central guide plate; the air flow central guide plate comprises an upper structure and a lower structure; an air flow guide-out plate and an air flow guide-in plate in a certain distance are arranged between the upper structure and the lower structure; the air flow guide-out plate and the air flow guide-in plate are sealed around to form a cavity structure; the air flow guide-in plate is of a planar structure; the air flow guide-out plate is of a concave surface structure; a plurality of guide-in holes are formed in the air flow guide-in plate; a plurality of guide-out holes are formed in the air flow guide-out plate; the guide-out holes do not correspond to the guide-in holes; the guide-out holes are formed in the air flow guide-out plate between every two adjacent ailerons; the guide-out holes are of inclined structures; the lower edges of the side, close to the center of the air flow guide-out plate, of the guide-out holes have gradients facing to inside of the cavity. When the unmanned transport aircraft vehicle is used, the working efficiency of a motor can be improved, and flying stability of the unmanned transport aircraft vehicle can be improved.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, specifically an unmanned transport aircraft. Background technique [0002] Current status of existing UAVs: With the existing eight-rotor, during the descent of the aircraft, the updraft will affect the stability of the aircraft, causing a large amount of power loss. The flight of the aircraft is unstable, which is very likely to cause a crash. In mountainous areas, the effect of instability is most obvious when the wind shears. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide an unmanned transport aircraft, which solves the problem of poor stability of the aircraft due to the influence of airflow during flight. [0004] The present invention is achieved like this, [0005] An unmanned transport aircraft, comprising: an airflow central guide plate, eight ailerons arranged symmetrically on the airflow central guide plate, a fol...

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is to provide an unmanned transport aircraft to solve the problem of poor stability caused by the influence of airflow during the flight of the aircraft

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