Launch vehicle, pyrotechnic cutting cable protection cover and its components

A technology of pyrotechnic cutting and protective cover, which is applied in the aerospace field, can solve the problem of weak axial adjustment ability of pyrotechnic cutting cable protective cover, and achieve the effect of reducing requirements

Active Publication Date: 2021-08-17
广州中科宇航探索技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in order to prevent the blasting airflow and cabin fragments of the pyrotechnic cutting cable 120 from leaking from the gap, the gap d is generally small, so the ability of the pyrotechnic cutting cable protective cover 110 to be adjustable around the axial direction is also weak.

Method used

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  • Launch vehicle, pyrotechnic cutting cable protection cover and its components
  • Launch vehicle, pyrotechnic cutting cable protection cover and its components
  • Launch vehicle, pyrotechnic cutting cable protection cover and its components

Examples

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Embodiment Construction

[0030] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0031] see figure 2 , figure 2 It is a structural schematic diagram of the pyrotechnic cutting cable protection cover provided by the embodiment of the present application.

[0032] The present application provides a protective cover 210 for pyrotechnic cutting cables, including: four cover sections, namely a cover section 211 , a cover section 212 , a cover section 213 and a cover section 214 .

[0033] Wherein, the extension direction of the end face of each cover section (cover section 211, cover section 212, cover section 213 and...

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Abstract

This application relates to the field of aerospace technology, and in particular to a launch vehicle, a pyrotechnic cutting cable protective cover and its components, wherein the pyrotechnic cutting cable protective cover includes: four cover segments, and the extension direction of the end surface of each cover segment is The extension direction is the same as one diameter A-A of the pyrotechnic cutting cable protective cover; wherein, the two cover sections are arranged symmetrically with the other diameter B-B of the pyrotechnic cutting cable protective cover, and the diameter B-B is the same as the diameter A-A is vertical; the other two cover segments are respectively inserted into the gap between the two cover segments symmetrically arranged with the diameter B-B as the axis of symmetry; a gap with a certain distance is formed between the end faces of two adjacent cover segments , and there is a certain overlap between the inner surface of one cover segment and the outer surface of the other adjacent cover segment. The protective cover for pyrotechnic cutting cables provided by the present application can reduce the requirement for cabin space for installing the protective cover for pyrotechnic cutting cables.

Description

technical field [0001] The present application relates to the field of aerospace technology, in particular to a launch vehicle, a pyrotechnic cutting cable protection cover and components thereof. Background technique [0002] When the multi-stage booster vehicle is separated, the cabin section will be cut off with a pyrotechnic cutting cable to realize the unlocking and separation of the cabin section. In the prior art, such as figure 1 As shown, the pyrotechnic cutting cord 120 is arranged circumferentially along the inner wall of the cabin section 130 , and there are two initiators 140 on the pyrotechnic cutting cord 120 at a relative 180°, so as to ignite the pyrotechnic cutting cord 120 through the detonator 140 . During the cutting process of the pyrotechnic cutting cable 120, the impact force generated will impact the pyrotechnic cutting cable 120 fixed on the inner wall of the cabin section 130; . [0003] Based on this, in the prior art, in order to fix the pyrot...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/64
CPCB64G1/645
Inventor 明爱珍杨毅强杨浩亮张东博孙良杰姜沂魏凯乐雪辉
Owner 广州中科宇航探索技术有限公司
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