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Lower clamp

A clamp and part of the technology, applied in the aerospace field, can solve the problems of alignment, heavy rocket mass, affecting the launch ability of the rocket body, etc., and achieve the effect of simple structure

Active Publication Date: 2020-06-16
北京中科宇航技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the existing stopping mechanism cannot align the position of the rocket body, and the rocket is heavy, so an additional fixing structure needs to be designed to fix the position of the rocket, which will increase the unnecessary structural weight of the rocket body and affect the launch of the rocket body ability

Method used

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Embodiment Construction

[0022] The technical solutions in the embodiments of the present invention are clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without making creative efforts belong to the protection scope of the present invention.

[0023] Such as figure 1 , 2 , 3, the application provides a lower clamp 0, including a base 1 and a clamp mechanism 2; the base 1 is provided with a connecting hole 11; the clamp mechanism 2 includes a connecting shaft 21 and a power unit 22; the connecting shaft One end of 21 is connected to the power unit 22, and the other end is used to connect with the support ring 3 at the tail of the rocket, so as to fix the rocket and push the rocket to generate displacemen...

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Abstract

The invention discloses a lower clamp. The lower clamp comprises a base and a clamp mechanism; a connecting hole is formed in the base; the clamp mechanism comprises a connecting shaft and a power device; one end of the connecting shaft is connected with the power device, and the other end is connected with a support ring at the tail of a rocket; and one part of the power device and one part of the connecting shaft are arranged in the connecting hole and are connected with the base in a shaft penetrating mode. The lower clamp has the technical effects of being simple in structure and capable of fixing and adjusting the position of the rocket.

Description

technical field [0001] The present application relates to the field of aerospace technology, in particular to a lower clamp. Background technique [0002] A stop mechanism is usually arranged between the existing rocket body and the rocket launcher. One end of the stop mechanism is fixed on the rocket launcher by welding or bolts, and the other end leans against the rocket body to fix the rocket body. However, the existing stopping mechanism cannot align the position of the rocket body, and the rocket is heavy, so an additional fixing structure needs to be designed to fix the position of the rocket, which will increase the unnecessary structural weight of the rocket body and affect the launch of the rocket body ability. Contents of the invention [0003] The purpose of this application is to provide a lower clamp, which has a simple structure, can fix and adjust the position of the rocket, and does not need to design an additional structure to bear the locking force at th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/052
CPCF41F3/052
Inventor 胡小伟滕瑶兰公英杨毅强刘仁昌王永刚刘金程高鹏胡月梅
Owner 北京中科宇航技术有限公司
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