本文为您带来热障的英文翻译，包括热障用英语怎么说，热障用英语怎么说，热障的英语造句，热障的英文原声例

本文为您带来热障的英文翻译，包括热障用英语怎么说，热障用英语怎么说，热障的英语造句，热障的英文原声例句，热障的相关英语短语等内容。

热障的英文翻译，热障的英语怎么说？

热障的英语网络释义

热障中文名称：热障英文名称：thermal barrier定义：飞机作高速飞行时，因气动加热而引起的结构和材料上的困难。所属学科：航空科技（一级学科）；飞行原理（二级学科）热障的单位 定义 热障与宇宙

... heat-balance equation 热平衡方程 heat barrier 热障 heat booster 加热器，预热器 ...

... thermodynamic model 热力学模型 thermodynamic barrier 热力学障 ; 热障 thermodynamic constant 热力学常数 ...

Thermal Curtain(热障), 此释义来源于网络辞典。

热障的汉英大词典

热障[rè zhàng]

• heat barrier; {航空} thermal barrier; thermal curtain

热障的英语短语

热障的英文例句

梯度热障涂层是一种新型耐热材料，可充分缓和热应力。

Gradient thermal barrier coatings, a new type heat resisting material, can sufficiently release heat stresses.

对于热障涂层而言，等轴组织对提高涂层隔热能力有利。

The equal-axis structure is profitable to thermal insulate ability of zirconia coatings.

综述了目前国内外抗高温氧化涂层和热障涂层的研究现状。

The study of oxidation resistance coatings and thermal resistance coatings was overviewed.

模拟结果表明，热障涂层中的残余应力是界面形貌尺寸的函数。

The result shows that the residual stress in thermal barrier coatings is a function of interface topography parameters.

简述了梯度热障涂层的国内外研究进展、设计及主要制备方法。

The paper introduces its domestic and abroad research progresses, design and main preparation methods.

外衣应作为热障以及风块，由于通过冷空气循环，增加风寒因素。

The outer garment should serve as thermal barrier as well as a wind block, since cycling through cold air increases the wind chill factor.

粉末流动性好、振实密度高，可以用来热喷涂制备纳米结构热障涂层。

Such powders with good flow ability and high tap density are suitable for thermal spray used in the deposition of nanostructured thermal barrier coatings.

探索热障涂层在热震中裂纹的形成规律，揭示涂层热震危险截面位置。

Explores the rule of formation of thermal shock cracks in thermal coatings and studies position of dangerous coating sections in thermal shocks.

复合热障涂层是有用的燃气轮机部件，如密封环段，叶片部分罩，转换和燃烧室。

The composite thermal barrier coating is useful on combustion turbine components such as ring seal segments, vane segment shrouds, transitions and combustors.

综述了等离子喷涂结构涂层的研究进展，包括耐磨涂层、热障涂层、耐蚀涂层；

Progress of research on the plasma sprayed structural coatings, including WBCs TBCs and CRCs, was summarized.

复合热障涂层系统包括蜂窝金属结构具有高的热膨胀磷酸盐保税基陶瓷空心球填补。

A composite thermal barrier coating system includes a honeycomb metallic structure filled with high thermal expansion ceramic hollow spheres in a phosphate bonded matrix.

独特的热障结构设计阻止水分渗透到保温系统中，防止热能从暴露的金属手柄上流失。

Its unique thermal barrier design keeps moisture from infiltrating your insulated system while preventing thermal energy loss through exposed metal handles.

复合热障涂层系统的制造，可在目前的热障涂层厚度超过系统，从而提高热保护传授。

The composite thermal barrier coating system may be manufactured to thicknesses in excess of current thermal barrier coating systems, thereby imparting greater thermal protection.

采用理化分析方法对电站燃气轮机高温部件热障涂层的喷涂修复质量进行了检测和评定。

The methods of physical testing and chemical analysis are introduced for quality inspection on thermal barrier coats of the high temperature parts used in gas turbine power station.

实验结果表明，梯度热障涂层能明显延缓热震裂纹的形成和扩展，具有较高的抗热震性。

The test results show that retardation of thermal shock crack initiation and propagation and higher thermal shock resistance property were displayed in graded thermal barrier coating.

前言：随着燃气涡轮发动机进口工作温度的提高，热障涂层技术受到了广泛的关注。

With the elevation of inlet working temperature of gas turbine engine, thermal barrier coatings (TBCs)are receiving a great deal of attention.

梯度功能热障涂层是FGM的重要应用之一，它与传统的热障涂层相比可明显提高耐久性。

One of the important applications of FGMs is the functionally graded thermal barrier coating(TBC), which may markedly improve the durability compared with those conventional ones.

热障涂层是一类高温防护涂层，由于其应用的广泛性，已成为近年来涂层研究领域的热点之一。

Thermal barrier coating(TBC) is a kind of high temperature protection coating. Because of its wide application, it has attracted more and more interests in recent years.

其独特的热障结构避免潮气的形成和渗透到保温系统中，避免通过暴露的金属手柄损失的热量。

Its unique thermal barrier design keeps moisture from forming and infiltrating your insulated system while preventing thermal energy loss through exposed metal handles.

介绍了作为热障涂层活塞的功能梯度材料的应用机理、材料特性组合方案、依据及优化设计方法。

The application mechanism, characteristic combination scheme basic and optimization design method of FGMs as piston is discussed.

结果表明：K417G合金无涂层和涂覆热障涂层状态下的低周疲劳均属于应力疲劳，以弹性损伤为主；

The results indicate that the LCF of K417G alloy and K417G alloy with TBCs are stress fatigue, and the primary damage of LCF processing is elastic damage.

结果表明：等离子喷涂（APS）热障涂层在高温氧化过程中，黏结层被氧化生成热生长氧化物（TGO）。

The results show that thermally grown oxide(TGO)was formed for the oxidation of bond coat during high temperature oxidization of APS TBC.

广泛应用于高温部件的热障涂层，在热载荷作用下各层间所集聚的残余应力是导致其层裂和失效的重要原因。

Thermal barrier coating (TBC) has been used widely in heat components, the residual stress concentrated by thermal load can lead to spalling or failure for the entire coating system.

测试结果表明，热障涂层系统的显微硬度存在压痕尺寸效应，即表观显微硬度随施压载荷的增加而显著降低。

Through centrifugal model tests, the influence of plate size on the results of plate loading tests was studied.

证明了在风口上喷涂金属-陶瓷梯度热障涂层的可行性以及利用HVOF打底层制备金属-陶瓷热障层的优势。

The feasibility of metal-ceramic gradient coating on the work surface of BF tuyere was proved, and the superiority of HVOF tie coating on the work surface of BF tuyere was confirmed.

为确定热障涂层的残余应力、结合力、断裂韧性、疲劳裂纹扩展速率等性能和特性，需要知道其杨氏模量和泊松比。

To analyze the characteristics of TBCs such as residual stress, bond strength, fracture toughness, and crack propagation ratio, the Young's modulus and Poisson's ratio are important parameters.

这些结论为提高涂层界面结合强度的热障涂层界面造形提供了理论支持，也为热障涂层界面的优化提供了指导意见。

This conclusion provides theoretical supports for the interface sculpting to enhance the interfacial bonding strength, and advices for optimization of interface topography of...

文中对热障涂层的力学性能、抗氧化和抗热腐蚀、抗磨蚀和热学特性等性能的评价及性能判断与分析进行了综合回顾。

The performance valuation and analysis was reviewed to the mechanics property, oxidation resistance, hot corrosion resistance, erosion resistance, and thermal property of thermal barrier coatings.

文中对热障涂层的力学性能、抗氧化和抗热腐蚀、抗磨蚀和热学特性等性能的评价及性能判断与分析进行了综合回顾。

The performance valuation and analysis was reviewed to the mechanics property, oxidation resistance, hot corrosion resistance, erosion resistance, and thermal property of thermal barrier coatings.

热障的原声例句

热障的网络释义

热障 当飞行器在稠密大气中作超音速飞行时，受激波与机体间高温压缩气体的加热和机体表面与空气强烈摩擦的影响，飞行器蒙皮的温度会随M数（即飞行速度与周围大气的音速之比，M数也成为马赫数）的提高而急剧上升。飞行 M数为 2.0时，机头处的温度略超过100℃。而当 M数等于3.0时，飞行器表面的温度则升至350℃左右，已超过了铝合金的极限温度，使其强度大大削弱。航空界把飞行器作高速飞行时所遭遇到的这种高温情况称之为“热障”。简单来说，热障是指飞机的飞行速度超过一定界限时因高速气流引起机体表面温度急剧升高而遇到的障碍。

以上关于热障的英语翻译来自英汉大词典，希望对您学习热障的英语有帮助。