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引用次数: 2

摘要

电子元件集成密度的增加加剧了电子系统开发人员面临的热管理挑战。新兴设备的高功率、热流和体积产热正在推动从依赖传导和扩散的远程冷却向嵌入式冷却的转变,嵌入式冷却有助于产热设备和冷却剂流之间的直接接触。微间隙冷却器采用在器件之间的加热通道中经历相变的介电流体的强制流动。虽然两相微冷却器通常用于地面系统,但由于缺乏可接受的微重力操作模型和相关性,限制了它们在航天器热管理中的应用。先前的研究表明,重力加速度的作用随着通道直径的减小而减小,但在提出的重力不敏感通道尺寸和对矩形管道的最小研究之间存在相当大的差异。实现重力不敏感流动沸腾性能的可靠标准将使航天系统能够利用这种强大的热管理技术,并通过依赖地面测试减少开发时间和成本。在高218 pm、宽13.0 mm的微间隙冷却器中,研究了蒸发器方向对HFE7100流动沸腾性能的影响。在5个蒸发器方向上获得了相似的传热系数和临界热流密度,表明重力的影响可以忽略不计。
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Gravity effects in microgap flow boiling
Increasing integration density of electronic components has exacerbated the thermal management challenges facing electronic system developers. The high power, heat flux, and volumetric heat generation of emerging devices are driving the transition from remote cooling, which relies on conduction and spreading, to embedded cooling, which facilitates direct contact between the heat-generating device and coolant flow. Microgap coolers employ the forced flow of dielectric fluids undergoing phase change in a heated channel between devices. While two-phase microcoolers are used routinely in ground-based systems, the lack of acceptable models and correlations for microgravity operation has limited their use for spacecraft thermal management. Previous research has revealed that gravitational acceleration plays a diminishing role as the channel diameter shrinks, but there is considerable variation among the proposed gravity-insensitive channel dimensions and minimal research on rectangular ducts. Reliable criteria for achieving gravity-insensitive flow boiling performance would enable spaceflight systems to exploit this powerful thermal management technique and reduce development time and costs through reliance on ground-based testing. In the present effort, the authors have studied the effect of evaporator orientation on flow boiling performance of HFE7100 in a 218 pm tall by 13.0 mm wide microgap cooler. Similar heat transfer coefficients and critical heat flux were achieved across five evaporator orientations, indicating that the effect of gravity was negligible.
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