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A modular unmanned aerial vehicle

An unmanned aerial vehicle, modular technology, applied in the field of aircraft, can solve the problems of difficulty in production and assembly, inability to maintain, and fall, and achieve the effects of reducing maintenance costs and time, improving quality, and reducing costs

Inactive Publication Date: 2018-01-05
SHENZHEN RAPOO TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The small unmanned aerial vehicles sold on the market generally adopt the upper and lower cover design. The motors, flight indicators, flight control systems, GPS systems, geomagnetic systems, etc. required by the aircraft are all placed in the upper and lower covers of the aircraft. Production and assembly are very difficult. easy maintenance
When the aircraft is flying at high speed, it is easy for the operator to operate improperly. The aircraft hits a building or a big tree at a high altitude, or even falls directly from a high altitude, causing the aircraft to be damaged and cannot be repaired.
Operators can only buy new products, but aircraft are currently relatively expensive, which is a big loss for consumers

Method used

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  • A modular unmanned aerial vehicle
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  • A modular unmanned aerial vehicle

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Embodiment Construction

[0030] In order to fully understand the technical content of the present invention, the technical solutions of the present invention will be further introduced and illustrated below in conjunction with specific embodiments.

[0031] The concrete structure of the embodiment of the present invention is as Figure 1 to Figure 12 shown.

[0032] The modular unmanned aerial vehicle of this embodiment includes a fuselage device, a control box 20 , a photographing device 30 for photographing and transmitting the photographed data to external equipment, and a power supply device 40 for powering the unmanned aerial vehicle.

[0033] The fuselage device includes an outer shell 10 of the UAV, a propeller 14 arranged on the outer shell 10 and a motor 13 for driving the propeller 14 to rotate. The control box 20 is embedded in the middle of the casing 10 . The main control circuit board 24 , the GPS circuit board 22 , the RF module and the geomagnetic circuit board 27 of the UAV are fixe...

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Abstract

The invention relates to a modular unmanned aerial vehicle. The unmanned aerial vehicle includes a fuselage unit, the fuselage unit includes a shell of the unmanned aerial vehicle, a propeller and a motor, the aircraft also includes a control box, a photographing device for photographing and transmitting the photographed data to an external device, and a photographing device for the unmanned aerial vehicle The power supply device for power supply, the photographing device and the power supply device are fixed below the control box, and the main control circuit board of the unmanned aerial vehicle is arranged in the control box, and the power supply device is electrically connected with the photographing device, the main control circuit board and the motor respectively. The invention divides the components of the unmanned aerial vehicle into several independent devices. When assembling, each device can be assembled and tested separately, and then assembled into an unmanned aerial vehicle. The cost is reduced and the quality of the aerial vehicle is also improved; When the manned aircraft is damaged by impact, the damaged device can be repaired or replaced, and other undamaged devices can be kept, and the maintenance cost and time are reduced.

Description

technical field [0001] The invention relates to aircraft, in particular to a modular unmanned aircraft. Background technique [0002] At present, small unmanned aerial vehicles are widely used in aerial photography, agriculture, fire, natural disaster early warning and other fields. With the maturity of technology and the reduction of cost, it will be used in more and more fields. [0003] Small unmanned aerial vehicles on the market generally adopt the design of upper and lower covers. The motors, flight indicators, flight control systems, GPS systems, geomagnetic systems, etc. required by the aircraft are all placed in the upper and lower covers of the aircraft. Production and assembly are very difficult. Easy maintenance. When the aircraft is flying at high speed, it is easy for the operator to operate improperly. The aircraft hits a building or a big tree at a high altitude, or even falls directly from a high altitude, causing the aircraft to be damaged and cannot be re...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/08B64C27/14B64D47/08
Inventor 郑贤成
Owner SHENZHEN RAPOO TECH