Quick connection releasing mechanism

A release mechanism, fast technology, used in offensive equipment, rocket launchers, weapon types, etc., can solve problems such as lack of quick reset protection

Active Publication Date: 2021-01-05
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, there is a lack of technical solutions suitable for harsh environments, anti-overturning of various types of carriers in a vertical state, and quick reset protection after ignition failure.

Method used

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Embodiment Construction

[0030] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0031] Embodiments of the present invention provide a quick release mechanism for anti-overturning and quick reset protection after ignition failure in harsh environments or vertical states for various types of carriers.

[0032] Such as figure 1 , figure 2 As shown, in this embodiment, it includes: two sets of support frames 1, which are ...

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PUM

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Abstract

The invention relates to a quick connection releasing mechanism. The quick connection releasing mechanism comprises two sets of supporting frames arranged on a launching pad in a spaced mode; each setof supporting frames is provided with a connection releasing assembly, and the two connection releasing assemblies are used for jointly clamping a carrier; each connection releasing assembly comprises a driving mechanism and an enclasping mechanism directly or indirectly arranged on the driving mechanism, and the driving mechanism is used for driving the enclasping mechanism to move; locking mechanisms are used for locking positions of the enclasping mechanisms; elastic retraction devices are directly or indirectly connected with the enclasping mechanisms in a tensioning state; and the locking mechanisms are configured to be unlocked when the carrier is launched so as to release the enclasping mechanisms. By adopting the quick connection releasing mechanism, The carrier can be held tightly to be prevented from toppling in a vertical state and can be rapidly separated before being launched, and it is guaranteed that the carrier can be normally blast off.

Description

technical field [0001] The invention relates to the technical field of carrier launch, in particular to a quick pull release mechanism. Background technique [0002] At present, the commercial satellite launch site is single, and it needs to rely on a fixed launch site to meet a certain field slope. There are restrictions on the launch orbit and the landing area, and it is difficult to meet the high-density launch of commercial aerospace. In order to further release the carrying capacity and improve the level of commercial space service, the launch site needs to be expanded. In seas where the environmental conditions are relatively harsh, especially in my country's low-latitude seas, the launch point and launch azimuth can be flexibly selected to fully release the carrying capacity of the carrier, reduce launch costs, and reduce the number of wreckage falling into the population. The risk in the dense area, the safety of the landing area is good. [0003] However, there is ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/052F41F3/04
CPCF41F3/052F41F3/04
Inventor 洪建军李秀珍李明兵郭绍波
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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