Fuselage conductive structure of unmanned aerial vehicle and manufacturing method of fuselage frames

Abstract

The invention discloses a fuselage conductive structure of an unmanned aerial vehicle and a manufacturing method of fuselage frames, the fuselage conductive structure comprises a battery pack, a fuselage assembly and blade motor power supply wires; the battery pack includes a lithium battery pack body and a power supply circuit board, the fuselage assembly includes two fuselage frames and two fuselage cross beams, the fuselage frames and the fuselage cross beams are respectively prepared from a thickening-type double-sided copper clad plate which is double-sided printed with conductive layers, the fuselage frames are respectively arranged at trisection cross sections in a fuselage cabin, PI shaped supporting structures are formed on the fuselage frames, two ends of the fuselage cross beams are respectively fixed on the PI shaped supporting structures of the two fuselage frames, the two fuselage frames are also provided with banana jacks, and a plurality of groups of blade motor power supply wires are in plug connection with the power supply banana jacks of the fuselage frames. The fuselage conductive structure has the advantages of simple structure, light weight and compact structure, and solves the problems of a complex fuselage mechanical structure and many electrical circuits of a traditional multi-rotor unmanned aerial vehicle, the weight of the fuselage structure is reduced, meanwhile a stable large current output is realized, and time of endurance is improved.

Description

technical field [0001] The invention relates to a fuselage conductive structure of an unmanned aerial vehicle and a manufacturing method thereof. Background technique [0002] Unmanned aircraft, referred to as "drone" for short, and "UAV" for English abbreviation, is an unmanned aircraft controlled by radio remote control equipment and its own program control device. From a technical point of view, it can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parawing aircraft, etc. [0003] The existing common electric multi-rotor UAVs are all powered by lithium batteries. When the power supply system supplies power to the power motor on the outermost edge of the machine arm, it needs to connect long and thick power wires. It is difficult to avoid the problem of self-heaviness in the traditional fuselage structure. In the case of the same task load weight...

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Problems solved by technology

[0005] The object of the present invention is to provide a fuselage conductive structure and a manufacturing method of the fuselage frame of the UAV. To solve the problem of many lines and heavy weight, the structural components of the f

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