一种微流量贮存供给系统及方法
By designing a micro-flow storage and supply system with pure mechanical gas pressure regulation and control, the problem of unstable flow supply in micro-nano satellite propulsion systems was solved, achieving stable output and precise control of liquid propellant, and improving the control accuracy and reliability of the spacecraft.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING INST OF CONTROL ENG
- Filing Date
- 2023-10-20
- Publication Date
- 2026-07-17
AI Technical Summary
Existing micro-flow control systems occupy a large volume and have flow rates far exceeding the requirements of propulsion systems for micro and nano satellites and other micro-space vehicles. They cannot achieve stable flow supply and precise control, which affects the control accuracy, lifespan and reliability of the spacecraft.
A micro-flow storage and supply system is designed using a purely mechanical gas pressure regulation and control scheme. The system includes a gas storage and control module, a propellant storage and supply module, and a micro-flow control module. Constant output and precise flow control of liquid propellant are achieved through a mechanical pressure reducer and a microfluidic chip.
This invention achieves stable output and precise flow control of liquid propellant in the propulsion system of small spacecraft. The system has a simple structure and high reliability, and is suitable for the storage and supply of propellant under microgravity conditions in space and the ultra-low flow output of liquid working fluid on the ground.
Smart Images
Figure CN117429626B_ABST