热端

脉冲管制冷机热端小孔调相机构的实验研究

Experimental Research on Phase Adjusting Orifice at the Hot End of Pulse Tube Refrigerator

航空发动机热端部件测控技术的发展

Development in Testing Technology for Aeroengine Hot Components

P型与n型半导体内的温度分布及传热机理是不同的，热电制冷器冷、热端温度场是不均匀的。

Temperature distributing inside p type and n type and diathermanous mechanism are different . temperature field of the cold surface and heat surface is asymmetric .

半导体冷藏箱热端风冷散热器CFD辅助设计和实验研究

Utilizing CFD software package to design the radiator on the hot side of thermoelectric refrigerator and experiment research

PROFIBUS-DP现场总线在浮法线热端控制中的应用

Application of Profibus-DP Field bus to float glass line

对使用200h热端SiC晶粒表面形貌进行了观察，发现在气孔较大处有晶须长出，晶须的主要成分为SiO2。

The surface morphology of hot side of SiC was observed after using 200 hours . The results show there are dehiscences of grain and crystal whiskers in bigger pores .

制备技术的发展，从早期的等离子喷涂法到近期的电子束物理汽相沉积法，使TBCs质量得到了明显的提高，在改善航空发动机热端部件性能方面发挥了积极作用；

The quality of TBC and the performance of hot side part of aeroengine have been improved significantly with the changing of technology from air plasma spraying to electron beam physical vapor deposition .

结果表明，国产铬酸镧电热元件由尺寸均匀的等轴晶组成，元件的热端在使用2000h后晶粒长大十分明显，并存在调幅分解。

There was spinodal decomposition and remarkable increase of grain size in the internal electrothermic element composed of uniform equiaxial grains after heating for 2000h .

10000m3／h制氧机板式换热器损坏修复后，热端跑冷严重，氧气取出量不足，制氧机工况恶化，通过分析找出了原因是因某单元氧通道堵塞，并采取了处理措施。

The plate heat exchangers of 10000m3 / h oxygen making machine was damaged . After maintenance of it cold air releasing in the heat-end was serious and oxygen amount made decreased . The working state of the oxygen making machine deteriorated .

研究表明，当冷、热端工作温差为80K时，其输出功率和发电效率均比单段式结构的热电模块提高80%左右。

When the difference of temperature between cold end and hot one is 80k , both its output power and generation efficiency are 1 . 8 times more than single-section one ' s.

Y2O3稳定的ZrO2（YSZ）涂层具有高温隔热性能好、高温下相稳定、耐冲刷等特点，并已在燃气轮机热端部件、涡轮叶片等高温工况部件中获得广泛应用。

Yttria stabilized zirconia ( YSZ ) coating has excellent thermal barrier properties , good stability and abrasion resistance at high temperature ; therefore it has been widely used in the gas turbine and some components operating in high-temperature condition .

某航空发动机热端件寿命消耗计算模型及寿命监视

A computational model for life consumption and life monitoring of Aeroengine

直接在热端顶部淋水。

Sprays water at the top of hot end , respectively .

热端长度对脉冲管制冷机的性能影响研究

Effect of hot end length on performance of pulse tube refrigerator

航空发动机热端部件隔热陶瓷涂层应用研究

A survey on Application of TBC for Aeroengine hot sections

这盘肉应当趁热端上。

This dish of meat must be served up hot .

一种用于热端部件高温蠕变分析的统一型粘塑性本构模型&模型分析之一

A new unified viscoplastic constitutive model for creep analysis ── part ⅰ

研究了水冷式半导体冷藏箱冷端和热端传热对冷藏箱性能的影响。

A thermoelectric refrigerator with a water-cooled hot side was designed and constructed .

高推重比发动机热端部件发展的技术途径与战略对策

Technology Ways and Strategic Countermeasures for Developing Heated Ends of High Thrust-to-Weight Ratio Engine

高频脉冲管热端调相机构阻力特性的实验研究

Experimental Analysis of the Flow Characteristics of the Phase Adjuster in a Pulse Tube

半导体冷藏柜用热端散热器的实验研究

Experiment Research on Radiator Used at Semiconductor Refrigerator

排风经过填料式直接蒸发冷却器降温后进入热端；

Exhaust air is handled by wet film , then passes through hot end ;

板式换热器热端跑冷问题的分析及处理

Analysis and Treatment of Cold Air Releasing in the Heat-end of a Plate Heat Exchanger

热端管长度对涡流管性能影响的实验研究

Experimental Study on the Length of Vortex Hot Tube Effect on the Performance of Vortex Tube

小流量涡流管热端加湿制冷系统实验研究

Experimental study on cooling system of small flow vortex tube with humidifier at the hot end

分析了瓶罐生产线热端喷涂增强处理后的结果。

The result after hot and spray treatment in production line of container glass was analysed .

适用于发动机热端部件非线性结构分析。

The coded subroutine can be applied to the nonlinear structure analysis of aeroengine hot sections .

热端温度对高频微型同轴脉冲管制冷机性能的影响及其在空间技术中的应用研究

Effect of the hot end temperature on the performance of the high frequency CO-AXIAL PULSE TUBE REFRIGERATOR

在航空发动机热端件寿命消耗模型中考虑了离心负荷、热负荷及蠕变的影响。

A mathematical model is set up for life consumption of the high temperture parts in aero-engine .

冷、热端温度对半导体热电堆发电性能影响的初步研究

A primary research on generation performance of the semiconductor thermoelectric module under variable cold-side and hot-side temperature