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Inhabiting device, multi-rotor bionic inhabiting unmanned aerial vehicle and attachment movement method

A multi-rotor unmanned aerial vehicle and threaded flange technology are applied in the field of habitation devices and multi-rotor bionic habitat unmanned aerial vehicles and attachment motion fields to achieve the effects of uniform pre-pressure, easy desorption and simple structure.

Active Publication Date: 2021-06-11
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] At present, there is no report on the research of multi-rotor UAVs to achieve all-weather work through habitat devices

Method used

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  • Inhabiting device, multi-rotor bionic inhabiting unmanned aerial vehicle and attachment movement method
  • Inhabiting device, multi-rotor bionic inhabiting unmanned aerial vehicle and attachment movement method

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Embodiment Construction

[0045] Below in conjunction with accompanying drawing and specific implementation case the present invention is described in further detail:

[0046] combine Figure 1-26 , the purpose of the present invention is to provide a multi-rotor UAV bionic habitat device, characterized in that it includes curled soles 10, adhesive materials 9, guide rollers 8, claw push rods 11, threaded push rod motors 2, and motor supports 7. Threaded flange 3, threaded flange support 4, push rod guide rail 6 and sole support 5, wherein four curly soles 10 are symmetrically installed on sole support 5;

[0047] One end of the curled sole 10 is connected with the sole support 5 by bolts, the adhesive material 9 is attached to the upper surface of the curled sole 10, and the guide roller 8 is tangent to the lower surface of the curled sole 10 all the time, and the guide roller 8 provides required uniform preliminary for the sole adhesion. The pressure and the guiding curl sole 10 unfold, and one end ...

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Abstract

The invention relates to an inhabiting device, a multi-rotor bionic inhabiting unmanned aerial vehicle and an attachment movement method, and belongs to the technical field of robot application. The inhabiting device (B) is fixed right above the multi-rotor unmanned aerial vehicle (A) through a connecting plate (1) and comprises N symmetrically mounted toe mechanisms (C-F) and a power system (G); a threaded push rod motor (2) rotates forwards or reversely to drive the inhabiting device (B) to contract or expand; each toe mechanism (C-F) comprises a curled sole (10), an adhesive material (9), a guide roller (8) and a claw push rod (11); and the first end of the claw push rod (11) is hinged to a threaded flange support (4), and the guide roller (8) is installed at the second end of the claw push rod (11) and is always tangent to the lower surface of the second end of the curled sole (10). The inhabiting device can be charged in the air and is suitable for a horizontal top surface, a horizontal cylindrical surface and a horizontal round hole top surface, and the all-weather multi-inhabiting function of the multi-rotor unmanned aerial vehicle is achieved.

Description

technical field [0001] The invention belongs to the technical field of robot application, and specifically relates to a perching device, a multi-rotor bionic perching UAV and an attachment movement method, mainly through the perching device to make the propeller of the multi-rotor UAV in a stop state during multi-habitation operations to prolong the working time and Over-the-air charging via roost for 24 / 7 operation. [0002] technical background [0003] In recent years, the application of multi-rotor drones in various fields has achieved unprecedented development. In terms of civilian use, it mainly focuses on aerial photography, supervision, surveying and mapping, plant protection and fire protection; in terms of military use, it focuses on individual combat and reconnaissance. Multi-rotor drones have developed from four-axis to six-axis, eight-axis, etc. This process is accompanied by an increase in their own power and weight, and the endurance time has not changed signif...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/12B64C25/24B64C25/32B64C27/08
CPCB64C25/32B64C25/12B64C25/24B64C27/08B64U10/10
Inventor 俞志伟姬宇李凯吉爱红郭策
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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