thermal sink

Equivalent absorption characteristics of thermal radiation of heat sink in space environment simulator

空间环境模拟器热沉热辐射当量吸收特性研究

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The cooling technology using the physical and chemical heat sink of hydrocarbon fuel provides the best means for the thermal management of engine system and the body of advanced aircraft.

利用碳氢燃料的物理和化学热沉对高超音速飞行器的发动机等高温部件进行冷却是目前最可行的方法。

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The thermal controlling principle of the temperature gradient heat sink is discussed.

本文探讨了利用温度控制波长的原理，提出了温度梯度热沉的初步设想，及耦合光学系统的设计。

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Finite element analysis on steady-state thermal resistance of heat sink of power semiconductors for locomotive

机车大功率半导体散热器稳态热阻的有限元分析

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Utilizing heat sink is effective to reduce the thermometer heat load due to the thermal conductor of the leads, and to increase the accuracy of the temperature measurement.

运用热沉能够有效地减小由引线导热引起的温度计的热负荷，提高温度测量的精确度。

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The thermal oxidation stability, heat sink and mixed-fuel of model hydrocarbon fuels were studied in the present work.

本文主要围绕不同碳氢燃料模型化合物的热氧化安定性、吸热能力及燃料混配等问题进行研究，为吸热型碳氢燃料的配伍及其应用提供重要的实验和理论基础。

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A heat sink of phase of change thermal storage/ radiation for extravehicular activity

一种用于出舱活动的相变储热/辐射器式热沉

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For constant fin width, the heat sink with the highest fins has the best thermal performance.

在固定散热片宽度的条件下, 高度最高的散热片有最佳的散热效果.

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The relation between thermal resistances and sink structure is numerically analyzed on this basis.

在此基础上，定量分析了结构因素对散热器热阻的影响。

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It is unavoidable to thermal sink in all solid-state lasers.

在全固体激光器中，由于热沉积，因而产生热透镜效应。

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At first, an active cooling thermal module is designed for mobile phones embedded optical engine. The thermal module includes heat sink and thermal slices.

论文首先为手机嵌入式光引擎设计了主动散热模组，该模组由散热器与导热片组成。

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At the same time, accumulated thermal deformations thus surface sink and rupture due to higher bonding temperature can be reduced.

同时，又可以抑制过高焊接温度所带来的升温热变形积累，从而减小表面塌陷变形或断裂。

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It is difficult to use the system in large environmental simulator for its thermal lag and unevenness between different heat sink branches.

大型空间环境模拟器中由于热沉的热惯性较大以及各支路温度存在均匀性等问题，大型空间模拟器设备要应用喷射式气氮调温系统存在一定难度。

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Thermal Design of Heat Sink for T/ R Module

T/R组件的散热设计

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Dust acting as a thermal insulator and impeding airflow, thereby reducing heat sink and fan performance.

除尘作为热绝缘层,阻碍气流, 从而减少了散热片和风扇的性能.

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For vehicle which is characterized by short flight time and quick change of velocity and altitude, a concept of thermal management system which uses liquid-hydrogen as major heat sink and PCM material as supplementary heat sink was presented.

对飞行时间短，飞行速度和高度变化快的飞行器，提出了以液氢燃料为主要热沉、相变蓄热材料为辅助热沉的热管理方案；

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