channel cooler meaning in Chinese
槽式冷却器
Examples
- Based on the different requirements on the operating mode , the back surface cooling package style by impinge cooler and the module package style by micro - channels coolers were studied respectively
根据对二极管激光器不同工作模式要求，分别研究了采用冲击式冷却器的背冷式二维阵列封装和微通道冷却的模块化封装。 - The blade inner channel cooling is a complex convection - conduction coupling problem . this thesis build a three - dimension . compressible turbulence model , and give a general solve method . with the geometrical model of the glossily rectangle straight channel , the rectangle straight channel with in - line arrays disturb plates , the rectangle straight channel with staggered arrays disturb plates , the rectangle straight channel with slant disturb plates , this thesis compute the flow and heat transfer condition when the cold air path though these channels , and gain the temperature field , pressure field , velocity filed , in addition . this thesis also analyze the influence of the different channel height , the different channel materials , the different channels , and gain the function relation between he nusselt number , friction factor and reynolds number . this thesis is emphasis on the new heat transfer enhancement structure , that is , disturb plates , with the comparison with the glossily channel and channel with pin fins , the heat transfer enhancement effect of the former is better , and the conclusion can be used in the design of aircraft blade
叶片内部通道冷却是一个复杂的对流?导热耦合传热问题，本文在分析叶片内部通道冷却的流动与传热情况的基础上，建立了三维、可压缩紊流的物理模型，得到了通用的求解办法；利用不带扰流片的矩形直通道、带顺排扰流片矩形直通道、带叉排扰流片、带倾斜扰流片的矩形直通道的几何模型，计算了冷却空气通过这几种通道时的流动与换热情况，得到了各种不同情况下计算区域的温度场、压力场、速度场；在此基础上分析了不同的通道高度、不同的叶片通道材质对叶片内部通道冷却的影响，并整理得到了各种通道形式下，努谢尔数和阻力因子与雷诺数的函数关系；本文重点研究了新型的叶片内部通道冷却强化传热措施?带扰流片的内部冷却通道的强化传热效果，通过与光滑矩形直通道、带针肋通道的冷却效果的比较，表明了这种新型鲒构的优势，对于叶片内部通道冷却结构的设计可以起到指导的作用。 - The blade inner channel cooling is very important in the design of turbine blade , with the ever - increasing inlet temperature , the new heat transfer enhancement structures of higher performance are demanded . because of the complexity of the flow and heat transfer of the blade inner channel cooling , the numerical modulation is superior to the experiment . this thesis studied the blade inner channel cooling with the method of numerical modulation
叶片内部通道冷却在航空发动机叶片的设计中占有重要的位置，航空发动机进口温度的增高对其提出了更高的要求。由于叶片内部通道冷却的流动与传热的复杂性，数值模拟较实验的研究方法有其优越性，本文利用数值模拟的方法对叶片内部通道冷却进行了研究。