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Unmanned aerial vehicle capable of taking off and landing vertically

A technology of unmanned aerial vehicles and synchronous wheels, applied in the field of aerial photography, can solve the problems of fast power consumption, heavy weight of unmanned aerial vehicles, and unclear aerial photography, etc., and achieve the effect of low cost, light weight, and consistent rotor synchronization

Inactive Publication Date: 2014-05-14
张家港锐泰智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0009] The purpose of the present invention is to provide an unmanned aerial vehicle, which solves the problems in the prior art that the unmanned aerial vehicle is heavy, the aerial photography is not clear, the power consumption is fast, and the synchronization of the rotor is difficult to control.

Method used

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  • Unmanned aerial vehicle capable of taking off and landing vertically
  • Unmanned aerial vehicle capable of taking off and landing vertically
  • Unmanned aerial vehicle capable of taking off and landing vertically

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Embodiment Construction

[0028] The technical solutions in the embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0029] ginseng Figure 1 to Figure 3 As shown, in the embodiment of the present invention, the unmanned aerial vehicle includes a bracket and a drive system installed on the bracket.

[0030] The bracket is a supporting platform, under which a landing gear, aerial photography platform, etc. can be fixed, and above which can carry components such as a power supply and a circuit board.

[0031] The bracket includes a first side rod 11 and a second side rod 12 ar...

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Abstract

The invention discloses an unmanned aerial vehicle. The unmanned aerial vehicle comprises a support and a driving system arranged on the support, wherein the driving system comprises a motor and a plurality of rotor wings, a synchronous driving mechanism is arranged between each rotor wing and the motor, and the motor drives the plurality of rotor wings to rotate at the same speed by the synchronous driving mechanisms respectively. According to the unmanned aerial vehicle, one motor is arranged and is used for driving all the rotor wings to rotate synchronously, and as only one motor is arranged, the cost is low, and the weight is light; compared with a plurality of motors, one motor can greatly weaken the influence of high-frequency vibration on aerial photo definition; besides, one motor can drive all the rotor rings to rotate simultaneously, so that the synchronicity can be controlled easily.

Description

technical field [0001] This application belongs to the field of aerial photography, and in particular relates to an unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicles have the characteristics of small size, light weight, low cost, flexible operation and high safety, and can be widely used in aerial photography, monitoring, search and rescue, resource exploration and other fields. [0003] In the prior art, an unmanned aerial vehicle generally includes a plurality of rotors, and each rotor is driven by a motor respectively, and its disadvantages are: [0004] 1. Due to the installation of multiple motors, the overall weight of the unmanned aerial vehicle is relatively heavy; [0005] 2. Multiple motors work together, and the high-frequency vibration generated by them can easily affect the clarity of aerial photography; [0006] 3. The synchronization of multiple rotors is difficult to control; [0007] 4. The existing multi-axis aircraft uses m...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/12
Inventor 杨华东许剑吴奇才赵江
Owner 张家港锐泰智能科技有限公司
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