Electric unmanned aerial vehicle

An electric unmanned aerial vehicle and fuselage technology, applied in the field of unmanned aerial vehicles, can solve the problems of inability to launch weapons obliquely upwards, only to carry out operations downwards, load layout restrictions, etc., and achieve easy expansion of load layout and low cost. The effect of transportation and optimized structural design

Pending Publication Date: 2018-02-09
沈阳旋飞航空技术有限公司
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AI Technical Summary

Problems solved by technology

[0004] The above-mentioned eight rotors of the electric UAV in the prior art are arranged around the body at equal angular intervals, so that the applied load carried on the body can only be set directly below the body, and since all directions are blocked by the rotors, the carried load can only be placed directly below the body. It can carry out operations downwards, and cannot launch weapons or observe obliquely upwards. As introduced in this prior art, the UAV can only be suitable for operations such as spraying below the UAV as described in its manual.
[0005] In addition, because the existing technology adopts a fully symmetrical layout, the center of gravity is concentrated at one point, and the load layout is greatly restricted.
Moreover, the folding arm of the UAV in the prior art is too long after being folded, and the folded motor and propeller part exceeds the landing gear, which is easily damaged during transportation

Method used

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Embodiment Construction

[0025] In order to have a clearer understanding of the technical features, purposes and effects of the present invention, the specific implementation manners of the present invention will now be described with reference to the accompanying drawings. Wherein, the same parts adopt the same reference numerals.

[0026] As mentioned above, most of the existing multi-axis drones adopt a fully symmetrical layout, resulting in the center of gravity being concentrated at one point, and the load layout is greatly restricted, and because the fully symmetrical rotors block all directions of the drone, resulting in The carried load cannot launch weapons or observe obliquely upwards, which limits the application range of existing drones.

[0027] In order to solve the above defects, the application provides an electric drone, such as Figure 1-4 As shown, among them, figure 1 Shown is a schematic diagram of the three-dimensional structure of an electric drone according to a specific embo...

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Abstract

The invention discloses an electric unmanned aerial vehicle. The electric unmanned aerial vehicle comprises a fuselage, two undercarriages and eight motors supported by eight cantilevers connected tothe fuselage, a longitudinal load channel is formed below the fuselage, and the two sides of the longitudinal load channel are symmetrically provided with a first group of four cantilevers and a second group of four cantilevers correspondingly; a first included angle alpha formed between every two adjacent cantilevers of the first group of four cantilevers is same; a second included angle beta formed between every two adjacent cantilevers of the second group of four cantilevers is same; a third included angle theta and a fourth included angle epsilon are correspondingly formed between two adjacent cantilevers between the first group of four cantilevers and the second group of four cantilevers; wherein, alpha is equal to beta, theta is equal to epsilon, and the theta is greater than or equal to 1. 5 times of alpha and less than or equal to 2. 5 times of alpha. According to the electric unmanned aerial vehicle, the longitudinal load channel is formed below the fuselage without shield, loads such as a photoelectric pod propeller and a weapon launcher can be conveniently arranged, the situation that use and operational effectiveness are affected due to interference of the loads and cantilevers as well as a propeller during observation and weapon launching is avoided, and the application range of the unmanned aerial vehicle is improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a multi-rotor electric unmanned aerial vehicle, in particular to an electric unmanned aerial vehicle with eight rotors. Background technique [0002] With the development of digital navigation and control technology, the UAV field has led a new wave of technology development and is considered to be the commanding height of next-generation technology development. The development of UAV technology in China is particularly eye-catching. With the development of the global general aviation industry, the development of various rotorcraft is also increasing day by day, especially the rotor electric unmanned aircraft, which are widely used in agricultural plant protection, forest fire monitoring, aerial photography, land survey, post-disaster loss assessment tasks. However, the existing rotor UAVs generally have low load levels and unreasonable structural layouts, makin...

Claims

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Application Information

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Patent Type & AuthorityApplications(China)
IPC IPC(8): B64C27/08B64C27/32B64C1/00B64C1/30
CPCB64C1/00B64C1/30B64C27/08B64C27/32
Inventor张建飞宗宁孙卫华刘新民庞振岳鲁明
Owner沈阳旋飞航空技术有限公司