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A small aerial array docking and separation mechanism and method satisfying electrical connection

A docking mechanism and electrical connection technology, which is applied to aircraft parts, transportation and packaging, etc., can solve the problems of discontinuous electrical connection action and structural connection action, mutual interference of connection actions, and it is difficult to meet the requirements of air docking, so as to maintain reliability , Simple and reliable structure, stable connection effect

Active Publication Date: 2022-04-29
XIDIAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since this mechanism does not have a guiding action, it is difficult to meet the needs of aerial docking, and the electrical connection action and the structural connection action are discontinuous, which is likely to cause mutual interference between the connection actions
[0006] In addition, most of the aerial UAV docking systems designed based on the above-mentioned mechanism scheme occupy a large space, the rigidity of the mechanism connection is poor, and the gap between the mechanisms is large, resulting in loosening and collision between the UAVs due to the relative speed.
Does not have the ability to work in small spaces, high rigidity, and reliable electrical connections

Method used

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  • A small aerial array docking and separation mechanism and method satisfying electrical connection
  • A small aerial array docking and separation mechanism and method satisfying electrical connection
  • A small aerial array docking and separation mechanism and method satisfying electrical connection

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Embodiment Construction

[0031] The present invention will be described in detail below in conjunction with specific examples. The following description helps those skilled in the art to further understand the present invention, but does not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0032] Such as Figure 1A , Figure 1B , Figure 2A , Figure 2B As shown, a small aerial array docking and separation mechanism that meets electrical connections includes a passive docking mechanism 1 and an active docking mechanism 2, the passive docking mechanism 1 and the active docking mechanism 2 are movably connected, and the passive docking mechanism includes at least: an electrical female head 101 , female screw 102, passive docking lead screw slider 103, passive docking cushion 104, pass...

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Abstract

The invention belongs to the technical field of space docking, and in particular relates to a small air array docking and separating mechanism and method satisfying electrical connection, which includes a passive docking mechanism and an active docking mechanism, and the passive docking mechanism and the active docking mechanism are movably connected. The utility model provides a mechanism and method for docking and separating a small aerial array satisfying electrical connection, which is focused on electrical connection, occupies less space, has a reliable guide surface, and has a small movable gap.

Description

technical field [0001] The invention belongs to the technical field of space docking, and in particular relates to a small air array docking and separating mechanism and method that satisfy electrical connection. Background technique [0002] The development and application of aerial docking of drones has attracted great attention from all countries. People put forward higher requirements for the airborne time of drones, the information transmission between drones, the load of drones, and the modular design of operating units. Require. A docking / separation mechanism that can ensure the electrical connection and structural connection of two UAVs at the same time, can ensure the reliability of information transmission between UAVs and the structural stability of the aerial array assembly flight; The functional object design of the UAV system is modularized, which reduces the cost and storage space of the UAV system. It greatly enriches the suitability and application possibi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D39/00B64D47/00
CPCB64D39/00B64D47/00
Inventor 张树新姜伟涛王耀华段宝岩张硕代季鹏
Owner XIDIAN UNIV
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