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

Gas cylinder inflation and deflation subsystem suitable for unattended operation

A sub-system, filling and deflation technology, applied in the pipeline system, container filling method, fixed capacity gas storage tank, etc., can solve the problems of excessive leakage rate of the filling and unloading switch, delay of launch mission, gas leakage, etc., and achieve closure The effect of sealing redundancy, improving safety, and improving sealing reliability

Active Publication Date: 2022-01-11
BEIJING INST OF ASTRONAUTICAL SYST ENG
View PDF3 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the inflatable unloading switch is not closed or the leakage rate is out of tolerance, a large amount of gas in the gas cylinder will leak, resulting in delay or failure of the launch mission
There have been many out-of-tolerance faults in the leakage rate of the inflatable unloading switch in history

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
  • Gas cylinder inflation and deflation subsystem suitable for unattended operation
  • Gas cylinder inflation and deflation subsystem suitable for unattended operation

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0039] The present invention will be further elaborated below in conjunction with the accompanying drawings.

[0040] Such as figure 2 As shown, the present invention is an unattended gas cylinder filling and deflation subsystem, which includes a power measurement and control subsystem, a ground gas supply and distribution subsystem, and an arrow-mounted gas cylinder filling and deflation subsystem. The power measurement and control subsystem includes measurement and control workstation 18, main control network switch 19, PLC measurement and control combination 20, signal conditioning combination 22, and relay execution combination 21; the ground gas supply and distribution subsystem includes ground high-pressure gas source 11, ground solenoid valve 12, electric Pressure reducer 13, post-valve pressure sensor 14, first deflation solenoid valve 15, ground control air source 16, and deflation flow limiting element 17; Upper solenoid valve 2, second arrow upper solenoid valve 3...

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 gas cylinder inflation and deflation subsystem suitable for unattended operation. The system comprises a power measurement and control subsystem, a ground gas supply and distribution subsystem and an on-rocket gas cylinder inflation and deflation subsystem. The power measurement and control subsystem sends out a control instruction, remote closed-loop control over an electric control pressure reducer and an electromagnetic valve of the ground gas supply and distribution subsystem and an on-rocket electromagnetic valve is achieved through a PLC measurement and control combination and a relay execution combination, opening and closing of the electromagnetic valve and the outlet pressure of the electric control pressure reducer are controlled, and the controllable and adjustable gas cylinder inflation rate and the automatic gas cylinder inflation and deflation function are achieved; the unattended operation of gas cylinder inflation and deflation is achieved, and the safety of rocket launching staff is improved; and a filter and two step-by-step direct-acting electromagnetic valves are arranged on a common pipeline of the on-rocket gas cylinder inflation and deflation subsystem, and meanwhile, a step-by-step direct-acting electromagnetic valve is arranged on a gas cylinder branch with higher pressure in the rocket flight process, so that one set of gas supply system can inflate and deflate two gas cylinders at the same time, the single-point fault that the system cannot be shut down is eliminated, and the sealing reliability is greatly improved.

Description

technical field [0001] The invention relates to an unattended gas cylinder filling and deflation subsystem, which is used for filling and deflation of liquid rocket pressurized gas cylinders, launch control blow-off gas cylinders and the like. Background technique [0002] Liquid rockets usually use high-pressure gas cylinders to supply gas to realize functions such as tank boosting, engine control, and blow-off. The gas cylinder charging and discharging subsystem is generally composed of a ground gas supply and distribution system and an arrow cylinder system. The ground gas supply and distribution system is mainly composed of a gas distribution platform and a ground inflation pipeline. The gas cylinder system on the arrow is composed of a gas cylinder, a manual switch, an inflation and unloading switch, and an inflation and discharge pipeline. Gas, supplementary gas and other requirements, see the schematic diagram figure 1 . figure 1 Among them, 1' and 2' are gas cylin...

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 Applications(China)
IPC IPC(8): F17D1/04F17D3/01F17D5/00F17C7/00F17C5/06
CPCF17D1/04F17D3/01F17D5/005F17C7/00F17C5/06F17C2270/0197Y02E60/32
Inventor 丁蕾孙善秀刘文川吴俊峰赵涛吴姮马方超曹荣
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
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