The invention discloses an embedded micro fluid control module for a satellite, the embedded micro fluid control module for the satellite comprises a pipeline, an overflowing space is formed in the pipeline, and the pipeline is provided with a first inlet, a second inlet and an outlet which are communicated with the overflowing space; the flow regulating part is rotatably mounted in the overflowing space and divides the overflowing space into a first overflowing space and a second overflowing space, the first overflowing space is communicated between the first inlet and the outlet, and the second overflowing space is communicated between the second inlet and the outlet; and in the direction from the first inlet and/or the second inlet to the outlet, the sectional area of the cross section of the flow adjusting part is gradually increased. Compared with the prior art, the embedded micro fluid control module for the satellite is smaller in size, miniaturization design of the embedded micro fluid control module is facilitated, meanwhile, the structure is simpler, flow loss is small, and self-adaptive adjustment can be achieved.

    本申请公开了一种用于卫星的嵌入式微型流体控制模块,所述用于卫星的嵌入式微型流体控制模块包括管路,管路内形成有过流空间,且管路设有与过流空间连通的第一进口、第二进口和出口;流量调节件,流量调节件可转动地安装于过流空间内且将过流空间间隔为第一过流空间和第二过流空间,第一过流空间连通于第一进口和出口之间,第二过流空间连通于第二进口和出口之间;其中,在第一进口和/或第二进口到出口的方向上,流量调节件的横截面的截面积逐渐增大。本申请的用于卫星的嵌入式微型流体控制模块的体积更小,利于实现其小型化设计,同时,结构更加简单,流动损失小,且能够实现自适应调节。


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    Titel :

    Embedded microfluid control module for satellites


    Weitere Titelangaben:

    用于卫星的嵌入式微型流体控制模块


    Beteiligte:
    ZHANG BING (Autor:in) / HUI HUANHUAN (Autor:in)

    Erscheinungsdatum :

    08.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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