Unlock instant, AI-driven research and patent intelligence for your innovation.

End structure of hollow fiber membrane air separator

A technology of air separator and fiber membrane, which is applied in the direction of semipermeable membrane separation, separation method, and separation of dispersed particles, which can solve the problems of increasing use cost, scrapping of cylinder body 1, and coating treatment of hollow fiber monofilament, etc., and achieves convenience The effect of replacement, prolonging the service life and reducing the cost of use

Active Publication Date: 2016-03-30
HEFEI JIANGHANG AIRCRAFT EQUIP CORP LTD
View PDF4 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of this structure is: since the outer diameter of the epoxy resin end 3 is greater than the aperture of the cylinder body 1, and the two ends of the hollow fiber tow 2 have epoxy resin ends 3, so that the hollow fiber tow 2 is at the end The head cannot be removed from the barrel 1 after sealing
However, my country does not yet have the ability to coat hollow fiber monofilaments, and the surface coating treatment of the entire tow can only be carried out after being packaged into a hollow fiber tow.
However, the surface coating treatment method of hollow fiber monofilaments is kept secret in foreign countries, and the terminal structure of the current hollow fiber membrane air separator cannot be loaded into the cylinder 1 after the terminal is sealed first, which is not suitable for hollow fiber filaments in my country. The need for the surface coating treatment process of the beam has become a difficult problem in the development of hollow fiber membrane air separators
In addition, after the activity of the hollow fiber tow 2 disappears, only the hollow fiber membrane air separator can be replaced, causing the cylinder 1 to be scrapped and increasing the use cost

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
  • End structure of hollow fiber membrane air separator
  • End structure of hollow fiber membrane air separator

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0008] The present invention will be described in further detail below. see figure 2 , the end structure of the hollow fiber membrane air separator, including a cylindrical shell 1 and a hollow fiber tow 2 located in the inner hole of the shell 1, at the end of the hollow fiber tow 2, between the hollow fiber Bonded as a whole through epoxy resin; it is characterized in that: there is a tow end assembly, which is composed of epoxy resin end 4, retaining ring 5 and sealing ring 6; epoxy resin end 4 is a ring , its inner ring surface and the end of the hollow fiber tow 2 are bonded as a whole through epoxy resin, the outer diameter of the epoxy resin end 4 is matched with the inner hole clearance of the cylinder body 1, and the end of the epoxy resin end There is an annular retaining ring groove on the outer cylindrical surface of 4, and there is an annular sealing groove inside the retaining ring groove. The epoxy resin end 4 is inserted into the port of the cylinder body 1 n...

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 belongs to the inerting technology of an airplane oil tank, and relates to the improvement of a hollow fiber membrane air separator end structure in an airplane oil tank inerting system. The hollow fiber membrane air separator end structure comprises a cylindrical barrel (1) and a hollow filament bundle (2) which is arranged in an inner hole of the barrel (1). The hollow fiber membrane air separator end structure is characterized by comprising a filament bundle end assembly, wherein the filament bundle end assembly consists of an epoxy resin end (4), a retainer ring (5) and a sealing ring (6). The invention provides an improvement scheme of the hollow fiber membrane air separator end structure, the requirement of the hollow filament bundle coating processing process can be met, and the research difficulty in the hollow fiber membrane air separator in China can be solved.

Description

technical field [0001] The invention belongs to the aircraft fuel tank inertization technology, and relates to the improvement of the end structure of the hollow fiber membrane air separator in the aircraft fuel tank inertization system. Background technique [0002] The function of the hollow fiber membrane air separator is to separate the nitrogen in the air for inerting the fuel tank. The end structure of a current hollow fiber membrane air separator can be found in figure 1 . It consists of a cylindrical body 1 , a hollow fiber bundle 2 located in the inner hole of the body 1 , and an epoxy resin end 3 . At the ends of the hollow fiber bundles 2, the hollow fiber filaments are bonded as a whole by epoxy resin. The inner ring surface of the epoxy resin end 3 and the end of the hollow fiber bundle 2 are bonded as a whole through epoxy resin. The disadvantage of this structure is: since the outer diameter of the epoxy resin end 3 is greater than the aperture of the cyli...

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
Patent Type & Authority Patents(China)
IPC IPC(8): B01D63/02B01D53/22
Inventor 赵宏韬蒋东升李春睦郑玉田黄雪飞
Owner HEFEI JIANGHANG AIRCRAFT EQUIP CORP LTD
Features
  • R&D
  • Intellectual Property
  • Life Sciences
  • Materials
  • Tech Scout
Why Patsnap Eureka
  • Unparalleled Data Quality
  • Higher Quality Content
  • 60% Fewer Hallucinations
Social media
Patsnap Eureka Blog
Learn More