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UAV (unmanned aerial vehicle) protection hood and rotor UAV

A technology of unmanned rotor and protective cover, which is applied to the combustion of aircraft parts, aircraft indicating devices, and air intakes of power devices, can solve the problems of reducing power system power, high noise, affecting power output, etc., to improve output power. , the effect of reducing noise and reducing heat

Pending Publication Date: 2020-11-24
中科灵动航空科技成都有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The invention with the patent number ZL 201820403697 .0 discloses a protective cover for a rotor drone. Although the protective cover for the drone can provide good protection for the drone, since the power system of the drone is all located in the protective cover In the interior, especially the air intake of the engine is also located in the protective cover, which will reduce the power of the power system and affect the power output, and the noise is loud during flight, which needs further improvement

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  • UAV (unmanned aerial vehicle) protection hood and rotor UAV
  • UAV (unmanned aerial vehicle) protection hood and rotor UAV
  • UAV (unmanned aerial vehicle) protection hood and rotor UAV

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Embodiment Construction

[0029] The present invention will be further described below in conjunction with the accompanying drawings and specific preferred embodiments, but the protection scope of the present invention is not limited thereby.

[0030] The drone protective cover of this embodiment, such as figure 1 and figure 2 As shown, it includes a cover body, and also includes a first airway cover and a second airway cover respectively installed on both sides of the cover body; the first airway cover and the cover body together form the first airway; the second airway cover and the cover body The cover forms the second airway together; the first through hole is opened on the shell covered by the first airway cover; the second through hole is opened on the cover covered by the second airway cover . The part of the cover body covered by the first airway cover is sunken inward; the part of the cover body covered by the second airway cover is sunken inward. In this embodiment, the UAV adopts gasolin...

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Abstract

The invention discloses a UAV (unmanned aerial vehicle) protection hood and rotor UAV. The UVA protection hood comprises a hood body and further comprises a first air channel cover and a second air channel cover which are mounted on two sides of the hood body respectively; the first air channel cover and the hood body jointly form a first air channel; the second air channel cover and the hood bodyjointly form a second air channel; a first through hole is formed in a shell, covered with the first air channel cover, of the hood body; and a second through hole is formed in the shell, covered with the second air channel cover, of the hood body. The UAV protection hood and the rotor UAV have the advantages that not only can good protection be provided for the UAV, but also good engine air intake in a power system can be guaranteed, so that output power of an engine is improved, and the heat dissipation effect is better.

Description

technical field [0001] The invention relates to the field of rotor drones, in particular to a drone protective cover and a rotor drone. Background technique [0002] Due to the advantages of large load capacity and long battery life, the oil-electric hybrid rotor UAV has gradually become an important development direction of industrial-grade rotor UAVs. However, the oil-electric hybrid rotor UAV uses an internal combustion engine to drive a generator to generate electricity for the rotor UAV. The entire power generation device is inevitably larger and heavier than the power supply system of a pure electric rotor UAV. , high heat generation, large vibration and so on. Therefore, the protective cover of the battery-powered rotary-wing drone in the prior art is not suitable for the oil-electric hybrid rotary-wing drone. The invention with the patent number ZL 201820403697 .0 discloses a protective cover for a rotor drone. Although the protective cover for the drone can provid...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/00B64D33/02B64D33/08
CPCB64D33/02B64D33/08B64D45/00
Inventor 张代智叶祖峰杨超梁虎王帅州
Owner 中科灵动航空科技成都有限公司