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Unmanned aerial vehicle structure

A drone and airframe technology, applied in the field of drones, can solve the problems of difficult center of gravity configuration and heavy weight of the whole machine

Pending Publication Date: 2021-06-18
广州优飞信息科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The technical problem to be solved by the present invention is to provide an unmanned aerial vehicle structure for the problem that the weight of the whole machine is more and more difficult to configure the center of gravity of the whole machine because the specific gravity of its battery is getting larger and larger than that of the whole machine.

Method used

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Embodiment Construction

[0036] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0037] Please also refer to Figure 1 to Figure 16An unmanned aerial vehicle structure provided by an embodiment of the present invention includes a fuselage 1, opposite sides of the fuselage 1 are respectively provided with open slots 11 arranged symmetrically along the vertical direction, and inside the open slots 11 A modular battery 2 is detachably snapped and inserted, and a flight tube box 3 for loading a micro on-board computer is provided at the bottom of the fuselage 1, and a cloud platform 4 is provided at the bottom of the flight tube box 3. The cloud platfor...

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Abstract

The invention provides an unmanned aerial vehicle structure. Opening grooves which are symmetrical in the vertical direction are formed in the two opposite sides of a fuselage of the unmanned aerial vehicle structure correspondingly, module batteries are inserted into the opening grooves correspondingly, a flying pipe box is arranged at the bottom of the fuselage, a holder is arranged at the bottom of the flying pipe box, and each module battery comprises a battery shell and a battery pack arranged in the battery shell. Pressing buckles capable of elastically stretching and retracting towards the interior of the battery shell are arranged at the tops of the two side walls, corresponding to the two opposite sides of the battery shell and the opening groove respectively, of the battery shell, each pressing buckle comprises a pressing part, a buckling part and a connecting part for connecting the pressing part and the buckling part, and buckling grooves matched with the buckling parts are formed in the tops of the two opposite sides of the opening groove respectively. The two module batteries with the same battery capacity are adopted, what is guaranteed is that the total battery capacity is not changed, the single module battery is more convenient to disassemble and assemble, and the two module batteries are symmetrically installed on the two sides of the fuselage, so that hardware such as a miniature airborne computer with the strict gravity center requirement can be placed in the center of the bottom of the fuselage; and the rationality of the overall structure layout is improved.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to an unmanned aerial vehicle structure. Background technique [0002] According to the application field, UAV can be divided into military and civilian. In terms of military use, UAVs are divided into reconnaissance aircraft and target aircraft. In terms of civilian use, it is currently used in aerial photography, agriculture, plant protection, miniature selfies, express transportation, disaster relief, observing wild animals, monitoring infectious diseases, surveying and mapping, news reports, power inspections, disaster relief, film and television shooting, creating romance, etc. Greatly expanded the use of the drone itself. [0003] With the development of drones, the requirements for battery life are getting higher and higher, and the battery capacity, volume and quality are also getting bigger and bigger. Since most traditional drones use a singl...

Claims

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Application Information

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IPC IPC(8): B64D47/08B64D43/00B64D27/26B64C27/08
CPCB64D47/08B64D43/00B64C27/08B64U50/19B64U2101/30B64U10/10B64D27/40
Inventor 熊勇良罗志勇叶涛吴强
Owner 广州优飞信息科技有限公司
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