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Six-rotor-wing unmanned aerial vehicle

An unmanned aerial vehicle and six-rotor technology, which is applied to propellers, aircraft parts, fuselage frames, etc., can solve the problems of low flying height, small flight radius, and high operating environment requirements, and optimize the aircraft structure and endurance. Long, quick and easy disassembly and assembly

Pending Publication Date: 2017-05-31
西安三翼航空科技有限公司
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  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

However, this technical solution is limited in practical application, mainly in two aspects: one is that the flight radius of the UAV is restricted by the length of the ground cable, the flight radius is small, and the flight height is low; High requirements, requiring no obstacles on the ground within the flight range

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Embodiment Construction

[0044] In order to overcome the shortcomings of multi-rotor UAVs such as small load and short battery life, as well as the current situation that the cable power transmission method has high requirements for the flight site and the flight radius is small. The present invention proposes a six-rotor large-load unmanned aerial vehicle from the practical point of view of the application of the unmanned aerial vehicle industry.

[0045] The present invention comprises a fuselage cover plate 1, an edge baffle plate 2, a central support frame 3, an undercarriage 8, a battery box 9, a battery 10, a plurality of machine arm connectors 4, a plurality of machine arm connecting rods 5, and a plurality of motors 6 and multiple sets of propellers 7. Wherein, the fuselage cover plate 1 is a regular hexagonal box structure, consisting of a fuselage upper plate, a fuselage lower plate, and an edge baffle 2 connecting the fuselage upper plate and the fuselage lower plate Composition: The centr...

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Abstract

The invention provides a six-rotor-wing unmanned aerial vehicle. A fuselage cover plate is of a polygonal box type structure; a plurality of jib arm connecting parts are fixed in the fuselage cover plate and are located at all corners of the fuselage cover plate respectively. One end of each jib arm connecting rod is fixedly connected with the corresponding jib arm connecting part and a motor is mounted at the other end of each jib arm connecting rod. Batteries are arranged on a fuselage upper plate and a fuselage lower plate. According to the six-rotor-wing unmanned aerial vehicle, the effective load can reach 20kg or more every time; the six-rotor-wing unmanned aerial vehicle has the characteristics of long cruising duration, rapidness and convenience for dismounting and mounting a fuselage and a jib arm again, flexibility and convenience and wide environment adaptability.

Description

technical field [0001] The invention relates to the field of aircraft mechanical structure design, in particular to a six-rotor heavy-duty unmanned aerial vehicle with a load capacity of up to 20 kg. Background technique [0002] UAVs are widely used and have been involved in many fields, including film and television aerial photography, map surveying and mapping, geological survey, meteorological detection, environmental detection, agriculture, forestry and plant protection, etc. As a flying platform, drones can not only realize aerial photography for entertainment purposes, but more importantly, can carry different equipment to complete specific industrial tasks. UAVs will be more and more closely integrated with the industry, including the effective combination of surveying and mapping, agriculture, electric power and other fields, and gradually become a tool in the solution to exert greater value. [0003] In industrial applications, we need the aircraft to carry a larg...

Claims

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Application Information

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IPC IPC(8): B64C1/06B64C11/20
CPCB64C1/06B64C11/20
Inventor 李占科陈伟薛鲲岳魏辰黄拓常欣宋笔锋
Owner 西安三翼航空科技有限公司
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