Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

High-temperature-resistant self-sealing gas cylinder

A self-sealing, high-temperature-resistant technology, applied in gas processing applications, fixed-capacity gas storage tanks, gas/liquid distribution and storage, etc., can solve problems such as gas cylinders that cannot withstand high temperature assessments, and aerospace power system operation hazards

Pending Publication Date: 2021-09-10
SHENYANG AEROSPACE XINGUANG GRP
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Today, aerospace power systems are developing towards integration, economy, light weight, and miniaturization. Aerospace power systems use a large number of high-pressure gas cylinders, and with the exploration of deep space, the use environment is gradually becoming harsher. During the operation of the aircraft, its internal temperature will change greatly with the change of the operating time and the external environment, and it will experience high and low temperatures. There are high requirements for the reliability of the aerospace power system and the high and low temperature resistance of the parts. However, at present, most gas cylinders generally cannot withstand high temperature assessment, which brings danger to the operation of aerospace power systems.

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
  • High-temperature-resistant self-sealing gas cylinder
  • High-temperature-resistant self-sealing gas cylinder
  • High-temperature-resistant self-sealing gas cylinder

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0019] Now in conjunction with accompanying drawing, invention is described further, as figure 1 As shown, a high-temperature-resistant self-sealing gas cylinder has a structure comprising: an inner tank 1, a composite material winding layer 2, an elastic layer 3, and a heat-insulating layer 4. The liner 1 is wrapped with a composite winding layer 2, the composite winding layer 2 is wrapped with an elastic layer 3, the elastic layer 3 is wrapped with a heat insulating layer 4, and the heat insulating layer 4 is in contact with the external environment. The function of the liner 1 is to seal the gas in the gas cylinder, the function of the composite winding layer 2 is to withstand the gas pressure in the gas cylinder, and ensure the strength of the gas cylinder, and the function of the elastic layer 3 is to offset the deformation of the gas cylinder when the gas cylinder is inflated and deflated, preventing The composite wrapping layer 2 on the gas cylinder is in hard contact w...

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 discloses a high-temperature-resistant self-sealing gas cylinder comprising an inner container, a composite material winding layer, an elastic layer and a heat insulation layer from inside to outside, the inner container comprises an inflation and deflation connector part at the front end and an inner container body, and the inner container body and a shell of the inflation and deflation connector part at the front end are connected in a welded mode to form the inner container; the inflation and deflation connector part comprises a spring, a valve element, a piston and a rubber ring, one end of the spring is installed in a clamping groove in the inner container body, the other end of the spring is connected with the valve element, the valve element is pressed against the inclined face of the shell of the inflation and deflation connector at the front end of the inner container through elastic force of the spring, and the non-outlet conical face end of the piston makes contact with the valve element. The valve element is pushed to move through the movement of the piston. According to the high-temperature-resistant self-sealing gas cylinder, the gas cylinder can work in a high-temperature environment, and the high-temperature-resistant self-sealing gas cylinder has the characteristics of being simple in structure, good in economical efficiency, small in size, light in weight and the like.

Description

technical field [0001] The invention relates to the technical field of aerospace pressure vessels, in particular to a high-temperature-resistant self-sealing gas cylinder. Background technique [0002] With the development of the aerospace field, higher requirements are put forward for the aerospace power system. Today, aerospace power systems are developing towards integration, economy, light weight, and miniaturization. Aerospace power systems use a large number of high-pressure gas cylinders, and with the exploration of deep space, the use environment is gradually becoming harsher. During the operation of the aircraft, its internal temperature will change greatly with the change of the operating time and the external environment, and it will experience high and low temperatures. There are high requirements for the reliability of the aerospace power system and the high and low temperature resistance of the parts. However, at present, most gas cylinders generally cannot wi...

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): F17C1/12F17C13/04F17C13/06
CPCF17C1/12F17C13/04F17C13/06F17C2270/0186F17C2203/0304
Inventor 王维东刘博廉彬胡森苏雷
Owner SHENYANG AEROSPACE XINGUANG GRP
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products