一种用于小型板式贮PMD管理装置
By using a plug-in structure of large blade assembly, small blade assembly and liquid collector assembly, combined with microgravity surface tension drive, the problem of gas-liquid separation and gas-free discharge of propellant tanks under microgravity is solved, achieving lightweight and stable liquid management.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- HARBIN INST OF TECH
- Filing Date
- 2024-12-16
- Publication Date
- 2026-07-17
AI Technical Summary
Existing technologies struggle to achieve gas-liquid separation and gas-free discharge from propellant tanks under microgravity conditions, especially at low speeds or low flow rates, leading to liquid entrainment during on-orbit refueling.
It employs large and small blade assemblies, combined with blade positioning shafts and liquid collector assemblies, and drives the liquid through a plug-in structure and surface tension under microgravity. It utilizes plate-type liquid management technology to achieve gas-liquid separation. The blades are designed with a hollow structure in the middle to reduce weight and suppress liquid sloshing.
It achieves effective gas-liquid separation and gas-free discharge under microgravity conditions, optimizes structural weight and reliability, and ensures the stability of on-orbit refueling of propellant tanks and the effect of liquid-free venting.
Smart Images
Figure CN119771098B_ABST