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

Method of actively adjusting balanced discharging of parallel connection tanks of satellite two component propelling system

A propulsion system, two-component technology, applied in the direction of the propulsion system of the spacecraft, etc., can solve the problems of unbalanced discharge of parallel tanks, deflection of the satellite's center of mass, and uncontrollable attitude when the orbit-changing engine is ignited. Longevity, simple and easy method, strong and practical effect

Active Publication Date: 2013-07-24
BEIJING INST OF CONTROL ENG
View PDF6 Cites 43 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In addition, if the discharge of parallel storage tanks is unbalanced, the center of mass of the satellite will be deflected, and in severe cases, the attitude of the orbit changing engine will be uncontrollable when it is ignited.

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
  • Method of actively adjusting balanced discharging of parallel connection tanks of satellite two component propelling system
  • Method of actively adjusting balanced discharging of parallel connection tanks of satellite two component propelling system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0032] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0033] like figure 1 Shown is the structural diagram of the propulsion system of the present invention that can actively adjust the balanced discharge of parallel storage tanks. It can be seen from the figure that the propulsion system includes a gas cylinder 1, a pressure sensor 2, a discharge valve 3, a pressure reducer 4, a one-way valve 5, a normally open Electric explosion valve 6, propellant tank 8, orbit control engine 9, attitude control thruster 10, gas bypass 11, first normally open electric explosion valve 12, first normally closed electric explosion valve 14 and second normally open electric explosion valve Explosion valve 15, wherein: connect with gas bypass 11 between gas cylinder 1 and every component propellant tank 8, gas bypass 11 is formed by connecting two self-locking valves 7 and a gas container 13, gas The container 13 is...

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 relates to a method of actively adjusting the balanced discharging of parallel connection tanks of a satellite two component propelling system. A simulation model of a propelling system is firstly established; the current system mixing ratio r0 is calculated according to the current system state data; then the pressure difference dpo1 of oxidant tanks (MON-A and MON-B) and the pressure difference dpf1 of incendiary agent tanks (MMH-A and MMH-B) are calculated through an optimization algorithm according to the target value of the balanced discharging of the parallel connection tanks; the target pressure of each tank is finally calculated through the optimization algorithm by taking the r0 as the target value and the dpo1 and dpf1 as the initial conditions; and the pressure of the tanks can be adjusted to the target pressure point by utilizing gas bypasses when a satellite is in orbit, so that not only is the balanced discharging of the parallel connection tanks adjusted, but also the system mixing ratio is not influenced.

Description

technical field [0001] The invention relates to a method for actively adjusting the balanced discharge of parallel storage tanks of a satellite dual-component propulsion system, which is suitable for the balanced discharge control of parallel storage tanks of the satellite dual-component propulsion system. Background technique [0002] For the satellite bicomponent propulsion system with parallel storage tank structure, an important issue is the propellant balance discharge capability. If the propellant discharge of two parallel storage tanks is unbalanced, when the propellant in one storage tank is emptied, the helium in the storage tank will be discharged if the propellant in one storage tank is emptied, so that the propellant in the propellant pipeline will be entrained. Thrusters and engines fail, and the satellite is at the end of its life. And the remaining propellant in the other storage tank will become heavy and cannot be used. For a satellite carrying 3000kg of p...

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): B64G1/40
Inventor 梁军强李永宋涛马云华李湘宁李泽耿永兵王晓磊樊超林震林星荣林长杰王雪婷张广科
Owner BEIJING INST OF CONTROL 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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com