The invention provides a spacecraft efficient temperature equalization-heat diffusion-heat storage integrated plate and an additive manufacturing method thereof. The spacecraft efficient temperature equalization-heat diffusion-heat storage integrated plate comprises a gas-liquid phase change chamber and a solid-liquid phase change chamber, and the gas-liquid phase change chamber and the solid-liquid phase change chamber are arranged in an up-down adjacent mode; a cone frustum configuration capillary suction structure is arranged on the inner wall of the gas-liquid phase change chamber, and a uniparted hyperboloid configuration bearing column is further arranged in the gas-liquid phase change chamber; a heat conduction enhancing framework is arranged in the solid-liquid phase change cavity and comprises a three-dimensional lattice network structure. Compared with the prior art, larger capillary driving force and smaller flow resistance can be provided, the gas-liquid phase change heat transfer efficiency is improved, three-dimensional heat expansion and temperature equalization of a high-heat-flow device are achieved, and the problems that an original thermal control system formed by gluing a heat expansion block of a high-power device mounting plate, a heat pipe and other assemblies is large in weight and low in efficiency, and a channel heat pipe can only conduct heat in a one-dimensional mode in the axial direction are solved. And the requirements of high-efficiency temperature equalization and heat expansion of a new-generation spacecraft high-heat-flux area array distributed device are met.

    本发明提供了一种航天器高效均温‑扩热‑储热一体化板及其增材制造方法,包括气液相变腔室和固液相变腔室,气液相变腔室和固液相变腔室二者呈上下相邻设置;气液相变腔室的内壁上设置有圆锥台构型毛细抽吸结构,气液相变腔室内还设置有单叶双曲面构型承力柱;固液相变腔室内设置有导热增强骨架,导热增强骨架包括三维晶格网络构型。能够提供更大的毛细驱动力和更小的流动阻力,提高气液相变传热效率,实现对高热流器件的三维扩热、均温,解决原有高功率器件安装板扩热块与热管等多组件胶接的热控系统重量大且效能低、槽道热管仅能够沿着轴向一维传热的问题,满足新一代航天器高热流密度面阵列分布式器件的高效均温、扩热需求。


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    Title :

    Spacecraft efficient temperature equalization-heat diffusion-heat storage integrated plate and additive manufacturing method thereof


    Additional title:

    航天器高效均温-扩热-储热一体化板及其增材制造方法


    Contributors:
    YANG BIQI (author) / ZHANG LIXIN (author) / LIU GANG (author) / CHEN HAORAN (author) / SONG BINGKE (author) / XU JUN (author)

    Publication date :

    2023-06-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64G Raumfahrt , COSMONAUTICS / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS




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