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A double-layer bulkhead type inflatable cabin

A technology of bulkheads and cabins, which is applied in the field of aerospace cabins, can solve the problems of low impact protection and heat insulation efficiency of space debris in inflated cabins, heavy space cabins, and difficult launches, so as to reduce the total impact energy and The impact energy per unit area, the emission volume is small, and the effect of improving the heat insulation effect

Active Publication Date: 2016-05-18
HARBIN INST OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides a double-layer bulkhead type inflatable cabin to solve the problem of heavy weight, large volume, high launch cost and difficulty in launch of the existing rigid metal structure space cabin, as well as the impact protection and isolation of space debris in the inflatable cabin. The problem that thermal efficiency is low, for this reason the present invention adopts following technical scheme:

Method used

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  • A double-layer bulkhead type inflatable cabin
  • A double-layer bulkhead type inflatable cabin

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Embodiment Construction

[0011] This article will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. The embodiments described below are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0012] Such as figure 1 and figure 2 As shown, a double-layer bulkhead inflatable cabin body provided in this specific embodiment includes a manned cabin body 1 and an inflatable support frame 2, and the manned cabin body 1 includes an inner bag 11 and an outer protective shell 12. The bag 11 is arranged in the outer protective shell 12, and a debris cloud space 13 is formed between the inner bag 11 and the outer protective shell 12, and the inflatable su...

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Abstract

The invention provides a dual-layer cabin wall type inflation cabin body. A manned cabin body comprises an inner bag and an outer protecting shell, wherein the inner bag is arranged in the outer protecting shell; a fragment cloud ball space is arranged between the inner bag and the outer protecting shell; an inflation supporting frame is arranged in the fragment cloud ball space; the bag wall of the inner bag consists of an airtight layer and a bearing layer, the airtight layer is the innermost layer of the bag wall, and the bearing layer is positioned on the outer side of the airtight layer; the bag wall of the outer protecting shell consists of an airtight layer and a stiffening layer, the airtight layer is the innermost layer of the outer protecting shell, and the stiffening layer is the outermost layer of the outer protecting shell. The cabin body is high in folding efficiency, small in emitting size and light in weight; the inner bag and the outer protecting shell are connected through the inflation supporting frame to form a space with a certain distance, so that transfer and a convection effect between inner heat and outer heat of the inflation cabin body are baffled, the heat isolation effect of the cabin body is effectively improved, a protecting structure similar to a Wyeth shield is formed for the dual-layer inflation cabin body, and the space fragment preventing and protecting efficiency of the inflation cabin body is effectively improved.

Description

technical field [0001] The invention relates to a double-layer bulkhead type inflatable cabin, which belongs to the technical field of aerospace cabins. Background technique [0002] Space cabins (such as living cabins, experimental cabins, instrument cabins, or airlock cabins, etc.) are the main places where humans work and live on space stations or planetary bases. Future space stations, manned moon landings, and lunar bases need to have an inner diameter of several meters. Even large airtight cabins over tens of meters. Existing space cabins are mainly rigid metal cabin structures. Space cabins using rigid metal structures are heavy in weight, large in volume, high in launch cost, difficult in launch, and difficult to meet the needs of space stations, manned moon landings or lunar bases. The demand for large space cabins, in order to improve the environmental protection capability of the cabin space, some auxiliary structures or protective materials need to be added to t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/52B64G1/58
Inventor 苗常青周佳
Owner HARBIN INST OF TECH
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