Combined type unmanned aerial vehicle

An unmanned aerial vehicle, a combined technology, applied in the field of unmanned aerial vehicles, can solve the problems of difficulty in replacement, the angle of the camera cannot be adjusted, and the casing of the unmanned aerial vehicle cannot be disassembled, etc., and achieves the effect of various forms and convenient shooting.

Inactive Publication Date: 2016-11-09
成都蜀尚星科技有限公司
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  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the rapid development of the drone industry, drones will enter the daily life, work, and entertainment of ordinary consumers like cameras. The shells of existing drones are generally integrated or connected by screws and other connectors. The one-piece drone c

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  • Combined type unmanned aerial vehicle
  • Combined type unmanned aerial vehicle

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[0015] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0016] See Figure 1-4 , The present invention provides a technical solution: a combined unmanned aerial vehicle, comprising an unmanned aerial vehicle main body 1, the inner cavity of the unmanned aerial vehicle main body 1 is provided with a second screw hole 12, A connecting rod 2 is provided on the outer wall. A second screw 10 is fixedly installed on the inner side of the connecting rod 2. The second screw 10 is threadedly connected...

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Abstract

The invention discloses a combined type unmanned aerial vehicle which comprises an unmanned aerial vehicle body. Second screws are fixedly installed on the inner sides of connecting rods and are in threaded connection with second screw holes. First screws are arranged on the outer sides of the second screws. Rotating devices are arranged on the outer walls of the second screws. Rotary shafts are arranged at the top ends of the rotating devices. Propellers are arranged on the outer walls of the rotary shafts. First screw holes are formed in inner cavities of the rotating devices and are in threaded connection with the first screws. By the adoption of the combined type unmanned aerial vehicle, the second screws are in threaded connection with the second screw holes so that the connecting rods can be detached from the unmanned aerial vehicle body; the first screws are in threaded connection with the first screw holes so that the connecting rods can be detached from the rotating devices; third screws are in threaded connection with third screw holes so that an auxiliary unmanned aerial vehicle body can be detached from the unmanned aerial vehicle body; and the unmanned aerial vehicle can be conveniently detached and installed.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a combined unmanned aerial vehicle. Background technique [0002] With the rapid development of the drone industry, drones will enter the daily life, work, and entertainment of ordinary consumers like cameras. The shells of existing drones are generally integrated or connected by screws and other connectors. The one-piece UAV casing cannot be disassembled, and it is relatively difficult to replace. For example, the patent No. 201620146664.3 includes an upper casing and a lower casing. There is a male buckle, although the structure is simple and easy to use, but the angle of the camera cannot be adjusted. Contents of the invention [0003] The purpose of the present invention is to provide a combined unmanned aerial vehicle to solve the problems raised in the above-mentioned background technology. [0004] In order to achieve the above object, the present inve...

Claims

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Application Information

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IPC IPC(8): B64C39/00B64D47/08
CPCB64C39/00B64D47/08B64U2101/30B64U10/10
Inventor 杨淑娟
Owner 成都蜀尚星科技有限公司
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