冷却空气的英文

• air coolant
• cooling air
• cooling-air
• refrigerated air

• "冷却"英文翻译    cool off
• "空气"英文翻译    air; atmosphere
• "冷却空气管" 英文翻译 :    cooling air tube
• "冷却空气孔" 英文翻译 :    cooling air hole
• "冷却空气套" 英文翻译 :    cooling air jacket
• "二次冷却空气" 英文翻译 :    secondary cooling air
• "冷却空气出口" 英文翻译 :    cooling air outlet
• "冷却空气挡板" 英文翻译 :    cooling air baffle
• "冷却空气导管" 英文翻译 :    cooling-air duct
• "冷却空气风扇" 英文翻译 :    cooling air blower
• "冷却空气管路" 英文翻译 :    cooling-air line
• "冷却空气进口" 英文翻译 :    cooling-air intake
• "冷却空气排出" 英文翻译 :    cooling-air exhaust
• "冷却空气温度" 英文翻译 :    cooling air temperature
• "冷却空气叶轮" 英文翻译 :    cooling air impeller
• "冷却空气装置" 英文翻译 :    cold air unit
• "冷却空气出气管" 英文翻译 :    cooling air outlet duct
• "冷却空气导流板" 英文翻译 :    cooling air baffle
• "冷却空气进入口" 英文翻译 :    cooling air intake
• "冷却空气收集器" 英文翻译 :    cooling air collector
• "冷却空气吸入门" 英文翻译 :    cooling suck-in door
• "冷却空气鱼鳞板" 英文翻译 :    cooling air gill
• "空气冷却空气冷却的" 英文翻译 :    air-cooling
• "净化冷却空气用过滤器" 英文翻译 :    filters for cleaning cooling air
• "空调系统冷却空气出口" 英文翻译 :    air conditioning system cooling outlet

• When ejectors are used for pumping this air, attention must be given to minimizing thrust losses .
  当采用引射器来抽引冷却空气时，必须注意减少推力损失。
• Yes , they are used for cooling air , water , lubricating oil etc
  是的，它们用于冷却空气，水和润滑油等。
• Cooling air baffle
  冷却空气挡板
• Clogging up of the cooling air slits in the turbine blades is primarily caused by ultrafine particles with a high specific surface area
  涡轮叶片之间冷却空气缝隙的堵塞主要是因为存在高比表面积的超细粒子。
• Based on practical equipment , the cooling principle and operation mode of the cooling air system for m701f type gas turbine manufactured by mitsubishi coperation in japan have been presented
  根据实际设备，介绍了日本三菱公司m701f型燃气轮机冷却空气系统的冷却原理和运行方式。
• The aerodynamic losses and the coolant consumption due to endwall film - cooling are quantified , thus providing data on both the aerodynamic costs and the cooling benefits of endwall film - cooling
  这种气动力损失和冷却空气损耗的定量化，可为端壁气膜冷却技术的气动力成本和冷却效益提供数据。
• This allows a parallel flow heating in one shaft , i . e . the parallel flow of limestone and combustion gases , and a regenerative preheating of the limestone in the second shaft by the mixture of combustion gases and cooling air
  这就允许在一个窑筒里有并流燃烧，即石灰石和助燃空气的并行流动，而在另一个窑筒里是助燃空气和冷却空气的混合气体对石灰石的再生预热。
• The ejected coolant interacts with the external flow near the endwall and generates aerodynamic and thermodynamic losses in the process . this reduces turbine stage efficiency and together with the consumption of cooling air is detrimental to the overall cycle efficiency
  但这种方法中喷射的冷空气与端壁附近的外流场相互作用产生气动力和热动力损失，并且消耗冷却空气，从而损害涡轮的整体循环效率。
• Measured hole mass flows and a constant static pressure mixing analysis , together with the measured losses , allowed the decomposition of the losses into three distinct entropy generation mechanisms : loss generation within the hole , loss generation due to the mixing of the coolant with the mainstream , and change in secondary loss generation in the " blade passage
  论文还进行了叶片冷却孔质量流的测量与常静压气流混合分析，结合前述气动力损失和冷却空气损耗的测量结果表明，端壁气膜冷却的综合损失明显地由三个部分组成：叶片冷却孔内产生的损失；由于冷却空气与主流热空气的混合产生的损失；二次流的变化产生的损失。
• 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。

• 冷却空气的日语：れいきゃくふう れいきゃくくうき くうきれいきゃくざい