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Fast-assembling mechanism for wings of unmanned aerial vehicle

A technology of unmanned aerial vehicles and wings, applied in the directions of wings, fuselage, aircraft parts, etc., can solve the problems such as the need for other tools for disassembly and assembly, and the time-consuming disassembly and assembly, so as to facilitate field operations, and facilitate assembly and disassembly. The effect of repair and replacement

Inactive Publication Date: 2018-02-02
西安冰果智能航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

This patented technology allows drones with wings that can be easily installed quickly while still being able to perform their tasks effectively. It also simplifies maintenance procedures compared to traditional methods like screwing bolts or welds into place.

Problems solved by technology

This patented describes how conventional methods used in fixing fuel pipelines have been developed overall but they still require some technical problem addressed during their development process.

Method used

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  • Fast-assembling mechanism for wings of unmanned aerial vehicle
  • Fast-assembling mechanism for wings of unmanned aerial vehicle
  • Fast-assembling mechanism for wings of unmanned aerial vehicle

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Embodiment 1

[0025] Such as Figure 1-5 As shown, the present invention provides a quick-installation mechanism for UAV wings, including a frame 1, a button 2, a button shell 3, a button spring 4, a button base 5, a button thimble 6, a fixed block 7, a thick carbon tube 8, a spring Pin seat 9, spring pin 10, pin spring 11, spring pin housing 12, thin carbon tube 13, inner section wing 14 and outer section wing 15, one side of inner section wing 14 is provided with outer section wing 15, The middle part of the inner wing 14 is provided with a frame 1, the middle part of the frame 1 is provided with a button 2, one side of the frame 1 is provided with a thick carbon tube 8, the other side of the frame 1 is provided with a thin carbon tube 13, and the thick carbon tube 8 The top of the fixed block 7 is provided with a fixed block 7, the top of the fixed block 7 is provided with a button thimble 6, the top of the button thimble 6 is provided with a button shell 3, the inside of the button shel...

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PUM

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Abstract

The invention discloses a fast-assembling mechanism for wings of an unmanned aerial vehicle. The fast-assembling mechanism comprises a frame, a button, a button shell, a button spring, a button base,a button center, a fixing block, a thick carbon tube, a spring pin seat, a spring pin, a pin spring, a spring pin shell, a thin carbon tube, the inner segment wing and the outer segment wing. The outer segment wing is arranged on one side of the inner segment wing, the frame is arranged in the middle of the inner segment wing, and the button is arranged in the middle of the frame. The thick carbontube is arranged on one side of the frame, and the thin carbon tube is arranged on the other side of the frame. The fixing block is arranged at the top end of the thick carbon tube, and the button center is arranged at the top end of the fixing block. The button shell is arranged at the top end of the button center and internally provided with the button spring, and the button base is arranged atthe bottom end of the button shell. The wings are mounted through the spring pin, and when the outer segment wing is inserted and pulled, a pin or a screw does not need to be assembled; the fast-assembling mechanism adopts modular design, so that the mechanism is easier to repair and replace; and assembly and disassembly of the wings are convenient, no tool is needed, and out-field operation is facilitated.

Description

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Claims

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Application Information

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Owner 西安冰果智能航空科技有限公司
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