The invention relates to a microgravity fluid management device in the field of satellite space navigation. The microgravity fluid management device comprises a base, a net type surface tension management assembly and a gas-liquid phase management cavity; the gas-liquid phase management cavity comprises a gas-liquid two-phase storage cavity, an outer management cavity and an inner management cavity, and the outer management cavity communicates with the base and discharges liquid and adding gas-liquid phase fluid through the base; the net type surface tension management assembly comprises a gas window net piece, a middle-layer net piece and an outer-layer net piece; a bubble breaking point of the gas window net piece is smaller than that of the middle-layer net piece and that of the outer-layer net piece; the gas-liquid two-phase storage cavity communicates with the outer management cavity through the gas window net piece; the outer management cavity communicates with the inner management cavity through the middle-layer net piece; the inner management cavity communicates with the gas-liquid two-phase storage cavity through the outer-layer net piece. The microgravity fluid management device effectively solves the problem that an existing microgravity fluid management device cannot achieve pure liquid phase supply and gas-liquid phase filling functions at the same time through a single connector.
本发明涉及卫星宇航领域内的一种微重力流体管理装置,包括底座、网式表面张力管理组件和气液相管理腔;所述气液相管理腔包括气液两相贮存腔、外管理腔和内管理腔,所述外管理腔与所述底座连通并通过所述底座排液和加注气液相流体,所述网式表面张力管理组件包括气窗网片、中间层网片以及外层网片,所述气窗网片的泡破点小于所述中间层网片和所述外层网片的泡破点;所述气液两相贮存腔与所述外管理腔通过所述气窗网片连通,所述外管理腔与所述内管理腔通过所述中间层网片连通,所述内管理腔与所述气液两相贮存腔通过所述外层网片连通。本发明有效解决了目前微重力流体管理装置无法通过单接口同时实现纯液相供给和气液相加注功能的问题。
Microgravity fluid management device
微重力流体管理装置
2021-10-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |