Metal diaphragm storage box made of carbon-fiber composite materials and manufacturing method thereof

A technology of metal diaphragms and composite materials, which is applied in the direction of jet propulsion devices, mechanical equipment, rocket engine devices, etc., can solve the problem of not giving a spherical pressure vessel implementation plan, failing to solve the lightweight design of products, and the adaptability of mechanical environments To solve problems such as limited capacity, achieve the effects of ensuring process feasibility, facilitating deformation matching, and strong adaptability to the mechanical environment

Active Publication Date: 2013-12-11
SHANGHAI INST OF SPACE PROPULSION
View PDF6 Cites 22 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The invention patent of European Publication No. EP0941925A2 discloses a propellant tank, but this invention only provides the basic configuration of the metal diaphragm tank, and fails to solve the problem of lightweight design of the product
[0007] The invention patent of Chinese Patent Publication No. CN102275067 discloses a method for processing and preparing a hemispherical metal tank for spacecraft fuel. The method provides a method for manufacturing a titanium material metal diaphragm, which is easy to control the quality. As a preparation ma

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Metal diaphragm storage box made of carbon-fiber composite materials and manufacturing method thereof
  • Metal diaphragm storage box made of carbon-fiber composite materials and manufacturing method thereof

Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0052] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be pointed out that for those of ordinary skill in the art, a number of modifications and improvements can be made without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0053] See figure 1 , A carbon fiber composite material metal diaphragm storage tank, including an inner lining 1 and a metal diaphragm 2, and also includes an insulating layer 3 and a carbon fiber composite material layer 4.

[0054] The lining 1 includes an upper flange 11, an upper hemisphere 12, a connecting ring 13, a lower hemisphere 14 and a lower flange 15. The upper hemisphere 12 and the lower hemisphere 14 are connected by a connecting ring 13, and the upper flange ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention provides a metal diaphragm storage box made of carbon-fiber composite materials and a manufacturing method thereof. The metal diaphragm storage box comprises a liner 1 and a metal diaphragm 2 and also comprises an insulating layer 3 and a carbon-fiber composite material layer 4, wherein the liner 1 comprises an upper flange 11, an upper hemisphere 12, a connecting ring 13, a lower hemisphere 14 and a lower flange 15; the upper hemisphere 12 and the lower hemisphere 14 are connected by the connecting ring 13; the upper flange 11 is connected with the upper hemisphere 12; the lower flange 15 is connected with the lower hemisphere 14; the metal diaphragm 2 is butted with the connecting ring 13; the outer surface of the liner 1 is coated with the insulating layer 3; the outer surface of the insulating layer 3 is wound with the carbon-fiber composite material layer 4, and is connected with the carbon-fiber composite material layer 4 in a bonding manner. The metal diaphragm storage box provided by the invention has the advantages that the problems of large weight and low structure efficiency of the metal diaphragm storage box are solved, the light-weight design of the metal diaphragm storage box is realized, the cost is reduced and the performance of a product is improved.

Description

Technical field [0001] The invention relates to a pressure vessel, in particular to a carbon fiber composite material metal diaphragm storage box and a manufacturing method thereof. Background technique [0002] The propellant tank is a medium and low pressure pressure vessel with a liquid management device, designed for the liquid attitude control power system. The key issue of this product is: on the one hand, it must have the ability to effectively manage liquids under space microgravity conditions (gas-liquid isolation); on the other hand, it must be able to withstand the mechanical environment assessment during launch (mechanical overload). Wait). [0003] Commonly used propellant storage tank management devices include surface tension, metal diaphragms and non-metallic capsules. The main feature of the metal diaphragm storage tank is: the use of the metal diaphragm to actively manage the propellant: On the one hand, under the action of the squeezing gas, the diaphragm close...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): F02K9/60F02K9/44C08L63/00C08K7/06C08K3/04
Inventor 张璟邱卫东沈俊何才启施华韩洪武乔艳伟孔方圆魏彦祥曹伟陈剑李和军林森刘锋赵和明金广明
Owner SHANGHAI INST OF SPACE PROPULSION
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products