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Multi-rotor gear reversing mechanism and unmanned aerial vehicle

A reversing mechanism and multi-rotor technology, applied in the field of drones, can solve the problems of complex reversing mechanism and heavy structural weight

Pending Publication Date: 2018-06-29
天津凤凰智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a multi-rotor gear reversing mechanism and an unmanned aerial vehicle, so as to solve the problems of the existing multi-rotor unmanned aerial vehicle gear reversing mechanism complex and heavy structural weight

Method used

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  • Multi-rotor gear reversing mechanism and unmanned aerial vehicle
  • Multi-rotor gear reversing mechanism and unmanned aerial vehicle
  • Multi-rotor gear reversing mechanism and unmanned aerial vehicle

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Embodiment Construction

[0027] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and through specific implementation methods.

[0028] The present invention provides a multi-rotor gear reversing mechanism, including an intermediate commutator 1, an intermediate transmission shaft and a rotor reversing device 2, wherein:

[0029] Can refer to figure 1 , the above-mentioned intermediate commutator 1 includes a first case 11, a large bevel gear 12 and a small bevel gear 13, wherein the first case 11 is in a closed structure, and the above-mentioned large bevel gear 12 is rotatably arranged in the first case 11, and the above-mentioned There are two large bevel gears 12, and the two large bevel gears 12 are symmetrically arranged on figure 1 The two large bevel gears 12 are respectively connected with connecting shafts 14 at the upper and lower ends of the first box body 11 shown, and the two connecting shafts 14 are arranged o...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles and discloses a multi-rotor gear reversing mechanism and an unmanned aerial vehicle. The multi-rotor gear reversing mechanism comprises: an intermediate reverser including a first box, a large bevel gear rotationally disposed in the first box and at least three small bevel gears engaged with the large bevel gear, wherein thesmall bevel gears are not engaged with one another, and at least one small bevel gear is a power input source; rotor reversers in one-to-one correspondence with the small bevel gears, wherein each rotor reverser includes a second box, a rotor bevel gear rotationally disposed in the second box, an input bevel gear engaged with the rotor bevel gear, and the input bevel gear is driven to rotate by the corresponding small bevel gear. With the intermediate reverser and the rotor reverser for two-stage reversing, the multi-rotor gear reversing mechanism has the advantages that the traditional reversing structure is simplified, the structural weight is reduced, and transmission efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a multi-rotor gear reversing mechanism and an unmanned aerial vehicle. Background technique [0002] With the development of UAV technology, it has played an indispensable role in aerial photography, detection, stability maintenance, investigation, rescue, plant protection, etc., and has occupied an extremely important position in both civilian and military fields. In recent years, multi-rotor UAVs have gradually become the mainstream in the field of UAVs, and multi-rotor UAVs of various styles and functions have appeared in the market. [0003] Most of the existing multi-rotor UAVs are powered by electric motors, but the energy density of batteries is far lower than that of fuel, so most of the existing multi-rotor UAVs have the disadvantages of small load capacity and short battery life. Seriously restrict the development of multi-rotor UAV. The oil-powered m...

Claims

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Application Information

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IPC IPC(8): B64D35/00B64C27/08F16H1/22F16H57/021F16H57/023F16H57/038
CPCF16H1/222F16H57/021F16H57/023F16H57/038B64C27/08B64D35/00F16H2057/02039B64U10/10
Inventor 赵曙光
Owner 天津凤凰智能科技有限公司