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Multi-rotor unmanned aerial vehicle detachable tail thrust structure

A multi-rotor unmanned aerial vehicle, a detachable technology, is applied in the field of unmanned aerial vehicles and can solve the problems of carrying and inconvenient transportation of hybrid-wing unmanned aerial vehicles.

Pending Publication Date: 2019-12-20
无锡圣恢弘科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The problem to be solved by the present invention is to provide a detachable tail thruster structure for multi-rotor UAVs, which can solve the problem of inconvenient carrying and transportation of mixed-wing UAVs, and at the same time can choose the speed and range use, the scope of application is wider

Method used

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  • Multi-rotor unmanned aerial vehicle detachable tail thrust structure
  • Multi-rotor unmanned aerial vehicle detachable tail thrust structure
  • Multi-rotor unmanned aerial vehicle detachable tail thrust structure

Examples

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Embodiment Construction

[0017] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0018] Such as figure 1 and figure 2 As shown, the detachable tail thruster structure of the multi-rotor drone of the present invention includes a female connecting seat 1 and a sub-connecting seat 6, the female connecting seat 1 and the sub-connecting seat 6 are plug-in electrically connected, and the female connecting seat 1 is used for Attached to the multi-rotor UAV rack. The sub-connecting base 6 is provided with a tail thrust mechanism.

[0019] Wherein, the lower surface of the rear end of the female connector 1 has an inverted ridge-shaped chute 3, and the inner end of the chute 3 has a conductive slot 2, and the conductive slot 2 is used for the power control system of the multi-rotor drone. connected. An inverted ridge-shaped slider 5 is provided on the upper part of the sub-connecting seat 6 , and the sliding block 5 is adapted to the chute 3 ...

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Abstract

The invention relates to the field of unmanned aerial vehicles, in particular to a multi-rotor unmanned aerial vehicle detachable tail thrust structure. The structure is characterized by comprising amain connecting seat and a sub connecting seat, wherein the main connecting seat is electrically connected with the sub connecting seat in a plug-in mode, the main connecting seat is used for being connected with a multi-rotor unmanned aerial vehicle frame, and a tail thrust power mechanism is arranged on the sub connecting seat. According to the structure, the problem of inconvenient carrying andinconvenient transportation of a hybrid wing unmanned aerial vehicle can be solved, meanwhile, the high or low navigation speed and the long or short voyage can be selected for use, and the application range is wider.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a detachable tail thruster structure of a multi-rotor unmanned aerial vehicle. Background technique [0002] At present, the UAVs on the market mainly include multi-rotor UAVs, fixed-wing UAVs, unmanned helicopters, and hybrid-wing UAVs. Among these types of UAVs, except for fixed-wing UAVs, the rest can both hover in the air and fly on the route. Under the same energy consumption, the multi-rotor drone has the slowest speed and the shortest range. Since its multi-rotor propellers are arranged horizontally relative to the frame and rotate horizontally, it is almost impossible to increase its speed to a higher level. And to increase its voyage, it will inevitably lead to the improvement of energy consumption, which is not worth the candle. It is in this context that hybrid wing UAVs were created. [0003] The so-called mixed-wing UAV is the combination of multi-rotor UA...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C39/02
CPCB64C27/08B64C39/02B64U10/10B64U50/19
Inventor 王君浩张硕顾维春许必成
Owner 无锡圣恢弘科技有限公司
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