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Fastener structure

A technology of clips and clips, applied in the field of unmanned aerial vehicles, can solve the problems of complicated loading and unloading operations of support rods, inconvenient use, etc.

Inactive Publication Date: 2015-04-08
湖南基石信息技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Based on this, it is necessary to provide a clamp structure with simple structure and convenient loading and unloading for the problems of complicated loading and unloading operations and inconvenient use of the adjacent support rods of the UAV load platform.

Method used

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Embodiment Construction

[0022] In order to facilitate the understanding of the present invention, the present invention will be described more fully below with reference to the associated drawings. Preferred embodiments of the invention are shown in the accompanying drawings. However, the present invention can be embodied in many different forms and is not limited to the embodiments described herein. On the contrary, these embodiments are provided to make the understanding of the disclosure of the present invention more thorough and comprehensive.

[0023] It should be noted that when an element is referred to as being “fixed” to another element, it can be directly on the other element or there can also be an intervening element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and similar expressions are used herein for purposes ...

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Abstract

The invention discloses a fastener structure comprising a main fastener body and a first clamping lug. A first clamping groove is formed in the inner wall of the main fastener body, the first clamping lug is arranged on the outer wall of the main fastener body, and a second clamping groove is formed in one side, back to the main fastener body, of the first clamping lug. During use of the fastener structure, a support rod is clamped by each the first clamping groove and the second clamping groove, so that the purpose of connecting the adjacent support rods is achieved; compared with bolted connection, the fastener structure is simple to assemble and disassemble without a professional assembling and disassembling tool, and is easy to use.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a clip structure. Background technique [0002] In recent years, with the frequent occurrence of natural disasters such as earthquakes and floods, and the demand for aerial photography, the research on small multi-rotor drones has gradually become a hot spot in the research of unmanned aerial vehicles. Small multi-rotor drones have the advantages of low cost, high cost-effectiveness, no risk of casualties, and can work in harsh environments. They have a wide range of applications in various fields, such as low-altitude reconnaissance, weather surveys, and aerial photography. [0003] At present, the adjacent support rods of the UAV load platform are mainly connected by bolts, which require professional tools for disassembly and assembly by ordinary users, and the loading and unloading operations are complicated and inconvenient to use. Contents of the invention...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00
Inventor 张长隆李潇
Owner 湖南基石信息技术有限公司
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