共查询到19条相似文献,搜索用时 343 毫秒
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选取双进双出流径液冷系统作为研究对象,采用试验的方法,对2并12串的电池模块热特性进行分析,结果表明:室温下,液冷系统的散热性能并不是随进液流量增大而改善的,而是呈现先提高后降低的趋势,进液流量为450L/h时满足最佳散热要求,同时也具有最佳的散热效率;电池模块中部间隙增大4mm时的散热性能同样不是随着进液流量增大而改善的,与原电池模块相比,最高温升和内部最大温差均有所降低,散热性能得到改善;35℃环境温度下,相同进液流量时的电池模块内部温差较室温时变大,
可见冷却液温度过多地低于环境温度并不一定会改善电动汽车液冷系统的散热性能,
而45℃环境温度下液冷系统的散热性能更差。所得结论为液冷系统散热性能分析提供了参考依据。
相似文献
可见冷却液温度过多地低于环境温度并不一定会改善电动汽车液冷系统的散热性能,
而45℃环境温度下液冷系统的散热性能更差。所得结论为液冷系统散热性能分析提供了参考依据。
相似文献
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随着大功率器件的普及,单点热耗高且热流密度大的问题越发突出。以往的解决方法都采用液冷散热,但液冷散热相较于风冷散热存在设备量大、成本高等缺点。文中探讨采用风冷散热解决单点热耗高且热流密度大的问题,使风冷散热方式在高热耗、高热流密度工程上得到应用。通过仿真分析,采用蒸汽腔(Vapor Chamber, VC)均温板并进行风冷冷板结构参数优化,达到减小传热路径上各热阻的目的,从而设计出了满足散热要求的风冷冷板。装机后对实物进行测试,验证了风冷散热在高热耗、高热流密度散热问题上的可行性。 相似文献
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排尘孔涡轮冷却叶片叶顶流动与传热研究 总被引:2,自引:0,他引:2
涡轮叶片叶顶排尘孔用于清除冷气中掺杂的尘粒,以保证气膜孔和冲击孔的可靠工作,但排尘孔射流引起叶顶流动和传热问题。采用参数化方法建立有、无排尘孔涡轮冷却叶片几何模型,基于包含叶片主体、主燃气通道和三腔回流式内冷却通道的全局模型,采用流热耦合数值分析,开展排尘孔对涡轮冷却叶片叶顶流动与传热问题的初步研究。研究结果表明,对比有、无排尘孔叶片,排尘孔射流可降低叶顶平均温度约25 K;冷却通道对流换热作用和叶顶排尘孔射流可使叶顶平面降温400~600 K,冷却效果与冷却通道冷气流量和尘孔结构在叶顶位置相关;排尘孔叶顶射流对叶顶间隙高温燃气泄漏具有阻碍作用,可以提高叶片总压恢复系数约0.5%~1.5%,随着冷气流量的增大,这种作用增强;尘孔结构设计应兼顾射流对叶顶流动与传热的共同影响。 相似文献
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Yoon Jo Kim Yogendra K. Joshi Andrei G. Fedorov 《Journal of Mechanical Science and Technology》2008,22(2):338-349
Theoretical analysis and simulation of performance of an air-cooled microchannel absorber is reported in this study. It is
shown that the air-cooled microchannel absorber can be integrated into an absorption-based miniature electronics cooling system
by which the chip junction temperature can be maintained near room temperature, while removing 100 W of heat load. Water/LiBr
pair is used as the working fluid and refrigerant vapor is intended to counter-currently flow against aqueous LiBr solution
flow. Parametric study is carried out to determine the effects of several operating parameters, including inlet temperature
and mass flow rate of the coolant, and inlet temperature of LiBr solution. To facilitate the air-cooling of microchannel absorber,
an offset-strip-fin array is adopted, by which enhanced air-side heat transfer coefficient and large heat transfer area are
obtained. The performance of the air-cooled absorber is compared to liquid-cooled absorber. 相似文献
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为了解决某八通道收发模块的冷却问题,文中设计了一套基于高效热虹吸回路的两相冷却系统样机,分别对冷却系统的启动特性以及工作倾角、冷凝能力对系统冷却性能的影响进行了实验研究。研究结果表明:该冷却系统的启动性能和工作性能良好,可在-30°~75°倾角范围内保证收发模块正常工作;冷凝风速增大将有效提升系统的冷却性能,冷凝风机功耗也随之增大;在倾角为20°、冷凝风速约为6.5 m/s 时,冷却系统综合性能最优,具备对热耗475 W、局部热流密度60 W/cm2的收发模块进行冷却的能力。 相似文献
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现代电子设备中大量采用冷板类构件,而冷板的冷却流道排布密集,结构复杂,内部洁净度一旦失控,液冷系统堵塞、泄漏等故障就将发生,严重影响电子设备的正常工作运行。为提高液冷系统密封性及运行可靠性,针对液冷冷板制造加工过程的污染高风险工序环节,开展机加工过程防护技术、高效清洗技术和流道洁净度检测技术相结合的全过程污染控制技术研究。试验验证和电子设备研制实践表明,采用该控制方法可有效控制加工过程的切屑、油污、切削液等各类污染物残留,有效提升冷却系统的整体洁净度。 相似文献
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W. Ghopa Wan Aizon Ken-ichi Funazaki Takemitsu Miura 《Journal of Mechanical Science and Technology》2013,27(6):1611-1617
The endwall and blade film cooling systems are the typical solution adopted within gas turbines to allow further increase of turbine inlet temperature, avoiding critical material thermal damages. Due to the complex secondary flow field in the blade passage, endwall is more difficult to be cooled than blade surfaces. In the matter of fact, in endwall film cooling studies, it is necessary to investigate the interaction between coolant air and the secondary flow. In present study, the flow field of high-pressure turbine in linear cascade has been investigated by 5-holes pitot tube to reveal the secondary flows behaviour under the influenced of purge flows through a slot which is located 0.63 Cax upstream of blade leading edge. Both measurement and numerical simulation presented almost similar trend of aerodynamics performance thus enable the authors to excute the flow visualizations accurately. The presence of newly generated vortical structures was considered to be responsible to the additional loss at higher MFR cases. 相似文献
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文中详细介绍了采用贴附型漏斗进气口作为引气道的环控系统设计。通过数值计算和仿真,分析了环控系统在全飞行包线范围内的制冷性能,并进行了试验验证,取得了以下主要结论:环控系统在全飞行包线的制冷能力呈单峰特性,在高度为3~7 km、马赫数为0.75 ~ 0.9时,其制冷能力达到峰值;在相同飞行高度条件下,随着马赫数的增加,环控系统的制冷量先增加后减小;在相同飞行速度条件下,随着高度的增加,环控系统的制冷量先增加后减小;在低空低速、高空低速等飞行工况下,因冲压空气进气压力低、空气质量流量小,环控系统的制冷量较小,对电子吊舱长时间全功率工作时间有限制。文中阐述的设计思路及计算方法,对类似进气口环控系统设计具有较高的参考价值。 相似文献
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Gas/steam combined cycle is synergetic combination of Brayton cycle based topping cycle and Rankine cycle based bottoming cycle, which have capability of operating independently too. Combined cycle performance depends on the constituent cycles and it can be reasonably improved by enhancing gas cycle performance using gas turbine blade cooling. Amongst different cooling techniques the transpiration cooling offers effective utilization of coolant as compared to film cooling because of better shrouding of blade surface as the coolant is discharged from entire blade surface. The present work deals with evaluation of performance enhancement of combined cycle by using steam transpiration cooling of gas turbine blades. The combined cycle performance parameters e.g. overall efficiency and specific power output etc. have been compared for air transpiration cooling and steam transpiration cooling. The results revealed that for the specified conditions the steam is superior coolant in comparison to air and the combined cycle performance can be enhanced by applying transpiration cooling in gas turbine blades with steam as coolant. With a turbine inlet temperature of 1800 K and compressor pressure ratio of 23, the combined cycle efficiency with steam transpiration cooling of gas turbine blades is higher by 1.94 percent approximately as compared to the efficiency of combined cycle with air transpiration cooling of gas turbine blades. 相似文献