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阵列拉瓦尔喷嘴干冰微粒喷雾升华传热研究

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为了提高高热流密度半导体激光器在干冰微粒喷射冷却过程中的传热效果,提出了阵列喷嘴喷射冷却,建立了拉瓦尔阵列喷嘴的物理与数学模型,并利用Fluent软件中的欧拉模型模拟了干冰微粒的升华过程,研究了喷嘴喉管直径和干冰微粒流体喷雾高度对传热性能的影响。结果显示,高热流密度半导体激光器干冰微粒喷射冷却的适宜参数为喉管直径4 mm、喷雾高度5~25 mm。此外,研究了不同热流密度激光器工作时的最高工作温度、平均工作温度及传热系数,拉瓦尔阵列喷嘴可以保证热流密度在180 W/cm2以内的激光器正常工作,相应的传热系数为20470。82 W/(m2·K)。本研究为高热流密度半导体激光器干冰微粒喷射冷却系统的深入研究和推广应用提供了依据。
Sublimation Heat Transfer of Dry Ice Particle Spray with Array Laval Nozzle
Objective To meet the market demand,the performance of semiconductor lasers is continuously improving.In the digital era,the increasing integration of various electronic components is leading to a rapid increase in power densities and operating temperatures.During normal operations,approximately 40%-60%of the optical energy is converted into heat energy that is stored within the laser.The performances of semiconductor lasers are closely related to their thermal management.Research has shown that under adequate cooling conditions(the ideal state),significant enhancements can be achieved in terms of the emission efficiency,output power,beam quality,temperature stability,and reliability.The traditional cooling media for semiconductor lasers include R32,water,and liquid nitrogen,which dissipate heat under certain conditions.However,with a continuous increase in the laser heat flux density,traditional cooling media exhibit significant limitations.Carbon dioxide,which is a non-polar molecule with a simple structure,exists as a colorless and odorless gas in liquid and solid forms.When throttled to reduce the pressure to atmospheric levels,liquid carbon dioxide transforms into solid dry ice at extremely low temperatures.This study introduces dry ice as a cooling medium and proposes a novel array nozzle device.Combining jet impingement with dry ice phase-change cooling enables the efficient thermal management of high-heat flux density semiconductor lasers.Methods This study focused on practical stacked high-power semiconductor lasers.Initially,an array nozzle device utilizing dry ice cooling was designed based on the dry ice particle formation mechanism.The device primarily comprises jetting chambers,array nozzles,and simulated laser heat sources.During the modeling,a uniform arrangement with equal spacing and size in a parallel layout between the array nozzles and laser heat sources was adopted.The array nozzle configuration was 3X4 with a Laval nozzle consisting of a converging section,throat,and diverging section.Subsequently,computational fluid dynamics(CFD)software was employed to simulate the heat exchange process.For the sublimation heat transfer of dry ice and the two-phase flow heat transfer process,user-defined functions(UDF)were employed for the numerical simulation,thereby enabling the determination of the optimal nozzle parameters by varying the throat diameter of the Laval array nozzle and adjusting the spray height.These parameters were then applied to investigate the cooling characteristics of lasers with different heat flux densities using a relatively optimal nozzle configuration.Finally,through experimental validation and comparison with numerical simulation results,minor experimental errors were obtained,ensuring the feasibility of using Laval array nozzles for the dry ice cooling of high heat flux density semiconductor lasers.Results and Discussions The physical model of the Laval array nozzle dry ice sublimation heat transfer established in this study was used to analyze the influence of the throat diameter on the temperature uniformity of the laser and its cooling effect in local regions.The throat diameter affects the exit velocity,direction,and mass flow rate of the dry ice particle spray,thereby affecting the heat transfer effectiveness of dry ice particle spray cooling.When the throat diameter is<4 mm,the temperature distribution at the impact position of the Laval array nozzle exhibits a ring shape.The interference between the nozzle outlet velocities decreases,resulting in lower temperatures closer to the center,whereas relatively higher temperatures occur in the edge and gap areas outside the region directly facing the jet impact.When the throat diameter is<4 mm,the temperature of local high-temperature region largely remains within the safe operating range of the laser(Fig.2).At a spray height of 15 mm,there is a significant increase in the proportion of the high-temperature regions of the heat source.For lasers with heat flux densities below 100 W/cm2,it is advisable to maintain the spray height within a range of 10-15 mm(Fig.5).The temperatures at measurement points along the laser length at x=-10 mm,x=0 mm,and x=10 mm show minimal variation at heights of H=15-25 mm(Fig.6).Utilizing the relatively optimal nozzle configuration for cooling different heat flux density lasers,spray heights of H=5 mm,8 mm,and 10 mm can ensure that the temperatures of semiconductor lasers with heat flux densities of 165 W/cm2,156 W/cm2,and 125 W/cm2 do not exceed 40 ℃,with a heat transfer coefficient reaching up to 20113.47 W/(m2·K).This configuration guarantees the normal operation of kilowatt-level high-power semiconductor lasers(Fig.7).Conclusions Based on the Laval array nozzle dry ice particle sublimation cooling model,numerical simulations and experimental studies are conducted on the heat dissipation process of the laser.The research reveals that under the same heat flux density,a smaller throat diameter results in a higher spray outlet velocity,which leads to a lower average temperature and better temperature uniformity of the laser.With the same throat diameter,as the spray height decreases,the proportion of the low-temperature area increases,with a heat transfer coefficient of 19516 W/(m2·K)at 5-10 mm.As the heat flux density increases under the same spray height conditions,the temperature of the laser increases linearly.The array nozzle meets the requirements for the normal operation of lasers within 180 W/m2,with a heat transfer coefficient of 20470.82 W/(m2·K).

spray coolingdry ice sublimationarray nozzlenumerical simulationhigh heat flux density

宁静红、孙璐瑶、张青雨、任子亮、宋志朋、祝森

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天津商业大学天津市制冷技术重点实验室,天津 300134

喷雾冷却 干冰升华 阵列喷嘴 数值模拟 高热流密度

2024

中国激光
中国光学学会 中科院上海光机所

中国激光

CSTPCD北大核心
影响因子:2.204
ISSN:0258-7025
年,卷(期):2024.51(22)