A loc structure

Abstract

The embodiment of the invention discloses A lock structure,relating to the field of aerospace technology, which mainly aims at solving the problem that the connection between an artificial satellite and a space flight vehicle is loose, and weak loosening will cause the internal vibration of the artificial satellite, thereby destroying the internal structure and function, and directly causing the error of the data detected by the artificial satellite. The invention relates to an aerospace technology field, which mainly aims at solving the problem that the connection between the artificial satellite and the space flight vehicle is loosened, and weak loosening will cause the internal vibration of the artificial satellite, thereby destroying the internal structure and function, and directly causing the error of the data detected by the artificial satellite. The technical proposal of the embodiment of the invention comprises the following steps: a locking fork comprises a first rotating shaft, wherein the first rotating shaft is used for connecting one end of the locking fork and a leaf spring; The brake is provided with a second rotating shaft connected with the locking fork through the second rotating shaft, and is used for controlling the locking of the locking fork according to the energized state. A leaf spring, one end of which is connected with the first rotating shaft and the other end of which is connected with a leaf spring fixing bracket, wherein the leaf spring has elasticity; A leaf spring fixing bracket for connecting and fixing the leaf spring.

Description

technical field [0001] The embodiments of the present invention relate to the field of aerospace technology, in particular to a locking structure suitable for aerospace vehicles. Background technique [0002] Artificial earth satellites, also known as artificial satellites, are unmanned spacecraft that orbit the earth and orbit more than one circle in space. At present, artificial satellites are the fastest-growing and most versatile spacecraft. It is mainly used in various fields such as weather forecasting, land use, communication, tracking, and navigation. [0003] The prerequisite for an artificial satellite to realize its designated function is to successfully launch it into a designated closed orbit for periodic operation. Generally, it will be launched into space by a space flight vehicle such as a rocket or a space shuttle. The inventor found during the process of launching the artificial satellite that the artificial satellite is attached to the space flight vehic...

AI Technical Summary

Problems solved by technology

[0004] In view of this, the embodiment of the present invention provides a locking structure, the main purpose of which is to solve the loosening of the connection between the artificial satellite and the space flight vehicle. The slight loosening will cause vibration inside the artificial satellite, and damage the internal structure and function. This directly leads to the problem of errors in the data detected by artificial satellites

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