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an unmanned transport aircraft

A technology of transport aircraft and airflow, applied in the field of drones, can solve problems such as poor stability, achieve the effects of improving stability, offsetting turbulence, and improving flight stability

Active Publication Date: 2017-06-06
LIAOYANG POWER SUPPLY COMPANY OF STATE GRID LIAONING ELECTRIC POWER SUPPLY +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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  • an unmanned transport aircraft
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Embodiment Construction

[0018] In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the examples. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0019] see figure 1 , the unmanned transport aircraft provided includes: airflow center guide plate, eight ailerons 16 symmetrically arranged on the airflow center guide plate, and folding landing gear 14 and lifter 15 arranged on the lower side of the airflow center guide plate,

[0020] Wherein, the central guide plate of the air flow includes an upper and lower layer structure, an air flow lead-out plate 11 and an air flow introduction plate 13 with a certain distance in the middle, and the four sides of the air flow lead-out plate 11 and the air flow introduction plate 13 are sealed to form a cavity structure, and the a...

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Abstract

The present invention relates to the field of unmanned aerial vehicles, specifically an unmanned transport aircraft. The airflow center guide plate, eight ailerons symmetrically arranged on the airflow center guide plate, and the folding landing gear and elevator provided on the lower side of the airflow center guide plate, where the airflow center guide plate includes upper and lower structures, with a certain distance of airflow in the middle The air flow introduction plate and the air flow introduction plate are sealed around each other to form a cavity structure. The air flow introduction plate is a planar structure, and the air flow introduction plate is a concave structure. There are multiple holes on the air flow introduction plate. A plurality of lead-out holes are provided on the airflow lead-out plate. The lead-out holes do not correspond to the positions of the lead-out holes. The lead-out holes are arranged on the airflow lead-out plate between two adjacent ailerons. The lead-out holes It is an italic structure, and the lower edge of the edge of the outlet hole close to the center of the airflow outlet plate is provided with a slope facing into the cavity. During the flight, the working efficiency of the motor can be improved and the flight stability of the transport aircraft 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...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/08B64C21/02B64D27/26B64C27/52B64D27/40
CPCB64C21/02B64C27/08B64C27/52B64D27/40
Inventor 刘东兴刘文娟丛培贤王楠丁雷王春宇马识程薛丽敏寿增闵杰
Owner LIAOYANG POWER SUPPLY COMPANY OF STATE GRID LIAONING ELECTRIC POWER SUPPLY
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