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热喷涂TBCs涂层对高温合金组织结构影响的研究
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作者 何箐 程家龙 +1 位作者 汪瑞军 东岩 《金属加工(热加工)》 2008年第20期53-55,64,共4页
针对热喷涂前后高温合金基体材料金相组织变化,以及喷涂热障涂层(英文缩写:TBCs)后合金基体材料在瞬时高温下的组织结构变化开展研究。结果表明热喷涂TBCs涂层过程中,高温合金基体材料组织没有明显结构变化;在1300K温度下,10min后的高... 针对热喷涂前后高温合金基体材料金相组织变化,以及喷涂热障涂层(英文缩写:TBCs)后合金基体材料在瞬时高温下的组织结构变化开展研究。结果表明热喷涂TBCs涂层过程中,高温合金基体材料组织没有明显结构变化;在1300K温度下,10min后的高温合金组织会形成枝晶状并析出二次γ相,而同等条件下,采用热喷涂TBCs涂层保护后的高温合金基体材料的组织没有发生明显的变化。 展开更多
关键词 高温合金 合金组织 tbcs 热障涂层 热喷涂 结构影响 组织结构变化 基体材料
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Effects of Shot Peening Process on Thermal Cycling Lifetime of TBCs Prepared by EB-PVD 被引量:4
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作者 ZHOU Zhao-hui GONG Sheng-kai +3 位作者 LI He-fei XU Hui-bin ZHANG Chun-gang WANG Lu 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2007年第2期145-147,共3页
Conventional two-layered thermal barrier coatings (TBCs) are prepared by electron beam physical vapor deposition (EB-PVD) with ZrO2-8 wt% Y2O3 (8YSZ) as top coat and CoCrAlY as bond coat on disk-shaped Ni based ... Conventional two-layered thermal barrier coatings (TBCs) are prepared by electron beam physical vapor deposition (EB-PVD) with ZrO2-8 wt% Y2O3 (8YSZ) as top coat and CoCrAlY as bond coat on disk-shaped Ni based super-alloy. In this paper, three kinds of shot peening process with different lengths of operating time were adopted for bond coating. As a result, changes took place in its surface roughness and the surface micro-hardness. A thermal cycling test at 1 273 Kx55 rain and another at room temperature for 5 min were performed to study the effects of shot peening process on the thermal cycling lifetime of TBCs. It is found that a moderate shot peening process will be able to prolong the life time. The oxidation dynamic of the as-processed TBCs basically accords with the parabolic rule, and the oxidation test also attests to the spallation between YSZ and thermal growth oxide (TGO) responsible mainly for the failure of TBCs. 展开更多
关键词 thermal cycling lifetime shot peening thermal barrier coatings tbcs
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THE INFLUENCE OF Mo DIFFUSION ON THE THERMAL BEHAVIOR OF TBCs ON Ni_3Al BASED ALLOY IC-6 被引量:2
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作者 D.B. Zhang S.K. Gong +1 位作者 H.B. Xu Y.F. Han 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 2002年第1期45-48,共4页
Conventional two-layered structure thermal barrier coatings (TBCs) were prepared onto γ'-Ni3Al based alloy IC-6 by electron beam physical vapor deposition (EB-PVD). Isothermal oxidation and thermal cycling tests ... Conventional two-layered structure thermal barrier coatings (TBCs) were prepared onto γ'-Ni3Al based alloy IC-6 by electron beam physical vapor deposition (EB-PVD). Isothermal oxidation and thermal cycling tests were carried out to investigate the effect of Mo content at the interface between bond coat and ceramic top coat caused by diffusion. It has been found that the alloy coated with TBCs presented the lowest oxidation weight gain value for the reason that the ceramic top coat in TBC system can effectively stop Mo oxides evaporating. The life time of TBCs has close relation with Mo content at the interface between the bond coat and top coat. Spaliation of ceramic top coat occurred during thermal cyclic testing when Mo atoms accumulated at the interface up to certain amount to decline the combination between the bond coat and top coat. 展开更多
关键词 EB-PVD thermal barrier coatings (tbcs) thermal cyclic diffusion
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等离子喷涂-物理气相沉积(PS-PVD)制热障涂层(TBCs)抗燃气热腐蚀性能研究
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作者 袁小虎 李定骏 《东方汽轮机》 2019年第1期64-68,共5页
文章分析了等离子喷涂-物理气相沉积(PS-PVD)TBCs的抗燃气热腐蚀性能。结果表明:高温合金(Mar 247)直接暴露在燃气热腐蚀环境下腐蚀最严重,平均失重速率达2.035 9 g/m^2·h;涂覆MCrAlY涂层后, MCrAlY涂层腐蚀平均失重速率为0.157 8 ... 文章分析了等离子喷涂-物理气相沉积(PS-PVD)TBCs的抗燃气热腐蚀性能。结果表明:高温合金(Mar 247)直接暴露在燃气热腐蚀环境下腐蚀最严重,平均失重速率达2.035 9 g/m^2·h;涂覆MCrAlY涂层后, MCrAlY涂层腐蚀平均失重速率为0.157 8 g/m^2·h,基材未被腐蚀得到保护;涂覆TBCs(MCrAlY+8YSZ)后, MCrAlY/YSZ涂层未出现腐蚀剥落现象,抗燃气热腐蚀效果最好。 展开更多
关键词 等离子喷涂-物理气相沉积 tbcs 高温合金 抗燃气热腐蚀
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High Temperature Sintering and Oxidation Behavior in Plasma Sprayed TBCs [Single Splat Studies] Paper 1—Role of Heat Treatment Variations
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作者 Swarnima Deshpande 《Journal of Surface Engineered Materials and Advanced Technology》 2013年第1期106-115,共10页
The TBC system is examined with regards to its response to thermal exposure at high temperature. It has been established before that the thermally grown oxide (TGO) layer that forms upon bond coat oxidation is the key... The TBC system is examined with regards to its response to thermal exposure at high temperature. It has been established before that the thermally grown oxide (TGO) layer that forms upon bond coat oxidation is the key factor determining the performance of the TBC system and/or its failure. However, characteristics of TGO growth, bond coat rumpling, principles governing failure of TBC systems and the various failure mechanisms have been studied extensively in case of just super alloy with bond coat or with thick top coating. In this study super alloy/bond coat system with single splats of YSZ instead of thick topcoat is analyzed in order to scrutinize the effect on the first layer of splats during thermal exposure. The splats with microcracks are the building blocks of the top coat. The most important aspect of this layer is the inherent inter-splat and intra-splat porosity which undergoes sintering during thermal exposure. The interactions between the YSZ splats and the evolving TGO is directly linked to the presence or absence of bond coat oxidation. Therefore the high temperature behavior of this system is analyzed with variations in heat treatment involving, temperature, duration and environment of thermal exposure. 展开更多
关键词 TBC Bond COAT Top COAT Thermal Exposure Vacuum Environment Oxidation TGO Imperfections Sintering
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High Temperature Sintering and Oxidation Behavior in Plasma Sprayed TBCs [Single Splat Studies] Paper 2—Relevance of Variation in Materials Systems of TBC Components
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作者 Swarnima Deshpande 《Journal of Surface Engineered Materials and Advanced Technology》 2013年第1期116-132,共17页
The TBC system’s response to thermal exposure at high temperature is discussed here. The relevance of the microstructural aspects of each component of the TBC system is emphasized. The top coat is a YSZ ceramic coati... The TBC system’s response to thermal exposure at high temperature is discussed here. The relevance of the microstructural aspects of each component of the TBC system is emphasized. The top coat is a YSZ ceramic coating consisting of a collection of splats on top of one another. The most important aspect of this layer is the inherent inter-splat and intra-splat porosity which undergoes sintering during thermal exposure. This study investigates the effect of thermal exposure on the microstructure and sintering behavior in single splats produced using different starting powders since this has been shown to influence the basic microstructure of YSZ topcoat. The bond coat is an MCrAlY metallic coating which serves as an Al reservoir and allows the formation of a protective alumina, Thermally Grown Oxide (TGO) layer between the bond coat (BC) and the top coat (TC) layers. This oxide scale formed upon thermal exposure prevents further oxidation of the underlying component (substrate) and thus provides protection. As such, the content of free Al in the bond coat layer is of significance and makes it crucial to understand the influence of bond coat microstructure evolution and oxidation involved during its formation. The interaction between the bond coat, the TGO and the top coat layers is examined in this study to understand the high temperature behavior of the TBC system with regards to variations in the top coat and bond coat material systems used. 展开更多
关键词 TBC HVOF Bond COAT Top COAT Thermal Exposure Vacuum Environment Oxidation TGO Imperfections Sintering MICROCRACKS
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Thermal insulation performance of 7YSZ TBCs adjusted via Al modification 被引量:1
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作者 Jun-Gui Zhang Xi Tan +5 位作者 Xiu-Juan Fan Jie Mao Chun-Ming Deng Min Liu Ke-Song Zhou Xiao-Feng Zhang 《Rare Metals》 SCIE EI CAS CSCD 2023年第3期994-1004,共11页
ZrO_(2)-7 wt% Y_(2)O_(3)(7YSZ)thermal barrier coatings(TBCs)with three different structures were prepared by atmospheric plasma spraying(APS),electron beam physical vapor deposition(EB-PVD)and plasma spray-physical va... ZrO_(2)-7 wt% Y_(2)O_(3)(7YSZ)thermal barrier coatings(TBCs)with three different structures were prepared by atmospheric plasma spraying(APS),electron beam physical vapor deposition(EB-PVD)and plasma spray-physical vapor deposition(PS-PVD).Al films were deposited onto the top 7YSZ TBCs by magnetron sputtering,and the Al-deposited 7YSZ TBCs were subjected to vacuum heat treatment.The effects of Al modification on the thermal insulation properties of 7YSZ TBCs were investigated.The results showed that Al modification could significantly improve the thermal insulation of 7YSZ TBCs at 1000℃.Moreover,the maximum improvement of thermal insulation for PS-PVD 7YSZ TBCs was approximately 100℃,but the improvement decreased with increasing temperature.This is mainly because with increasing temperature,the rate of radiation heat transfer increases,and the effects of convection heat transfer and thermal conductivity on thermal insulation are weakened.At the same temperature,Al modification of PS-PVD7YSZ TBCs provides better temperature insulation than those of APS 7YSZ TBCs and EB-PVD 7YSZ TBCs because of its wider and deeper inter-columnar gaps.When the temperature was 12000C,Al modification still caused a good insulation effect in PS-PVD 7YSZ TBCs;the improvement was approximately 50℃,but in APS and EB-PVD 7YSZ TBCs,the insulation effect disappeared. 展开更多
关键词 Al modification Thermal barrier coatings(tbcs) Thermal insulation Inter-columnar gap
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Design of Ti_(2)AlC/YSZ TBCs for more efficient in resisting CMAS attack 被引量:1
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作者 Lei Guo Yanyan Li Guang Li 《Journal of Advanced Ceramics》 SCIE EI CAS CSCD 2023年第9期1712-1730,共19页
Ti_(2)AlC has been demonstrated as the promising protective layer material for thermal barrier coatings(TBCs)against calcium-magnesium-alumina-silicate(CMAS)attack.In this study,the reliability of Ti_(2)AlC coatings a... Ti_(2)AlC has been demonstrated as the promising protective layer material for thermal barrier coatings(TBCs)against calcium-magnesium-alumina-silicate(CMAS)attack.In this study,the reliability of Ti_(2)AlC coatings against the CMAS corrosion was explored,and new Ti_(2)AlC/YSZ TBCs more efficiently resistant to CMAS were designed.The fabricated Ti_(2)AlC coatings inevitably contain some impurity phases(TiC and Al2Ti3),the contents of which were minimized by optimizing the spraying distance.Corrosion tests revealed that Ti_(2)AlC/YSZ TBCs yielded higher resistance to the CMAS attack than YSZ TBCs,but with long-term exposure to CMAS,the Ti_(2)AlC protective coating exhibited microstructure degradation due to the presence of the impurity phases,which caused the formation of a layer mixed with Al_(2)O_(3)and TiO_(2)rather than a continuous compact Al_(2)O_(3)layer on the surface.Pre-oxidation schemes were designed in air or with a controlled oxygen partial pressure,which revealed that the pre-oxidation at an oxygen partial pressure of~630 Pa could promote a continuous Al_(2)O_(3)layer formed on the Ti_(2)AlC protective coating surface.Furthermore,a vacuum heat treatment at 867℃for 10 h before pre-oxidation was beneficial for the formation of the compact Al_(2)O_(3)layer.Through the above scheme design,new Ti_(2)AlC/YSZ TBCs were obtained,which had reduced impurity phase contents and a pre-oxide layer with an ideal structure on the surface.New TBCs exhibit higher microstructure stability exposed to CMAS and more efficient CMAS resistance. 展开更多
关键词 thermal barrier coatings(tbcs) calcium-magnesium-alumina-silicate(CMAS) Ti_(2)AlC/YSZ pre-oxidation design corrosion resistance mechanisms
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锆基陶瓷热障涂层的腐蚀研究进展
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作者 韩旭 耿洪滨 +2 位作者 王铀 李仰 张晓东 《航空制造技术》 CSCD 北大核心 2024年第4期89-103,共15页
近年来随着航空与航海工业的迅速发展,具有耐高温、长寿命、耐腐蚀等优势的发动机叶片成为开发新一代航空发动机和涡轮发动机的重要一环。热障涂层(TBCs)作为常用的热防护技术,一方面可为发动机叶片部分金属基底提供隔热保护,使其免受... 近年来随着航空与航海工业的迅速发展,具有耐高温、长寿命、耐腐蚀等优势的发动机叶片成为开发新一代航空发动机和涡轮发动机的重要一环。热障涂层(TBCs)作为常用的热防护技术,一方面可为发动机叶片部分金属基底提供隔热保护,使其免受高温气体的影响;但另一方面,更高的发动机工作温度使得叶片及其表面TBCs遭受严重的环境沉积物腐蚀,造成过早失效,腐蚀类型主要有热腐蚀、CMAS腐蚀、熔盐腐蚀等。腐蚀已成为限制TBCs工作温度和服役寿命的难题,抗腐蚀防护是目前TBCs领域研究的重点。本文首先简述了以氧化钇稳定氧化锆陶瓷(YSZ)为主的热障涂层材料的主要特性,再简述了TBCs的不同腐蚀的反应机理,重点从涂层的微观结构设计、梯度涂层的设计、涂层成分改性及掺杂改性等方面与涂层腐蚀过程之间的影响关系出发,阐述了TBCs改性方法与涂层腐蚀的特点。提出未来涂层改进与防护的几种方法,最后对TBCs的腐蚀防护发展方向进行了展望。 展开更多
关键词 热障涂层(tbcs) 氧化钇稳定氧化锆陶瓷(YSZ) 腐蚀失效 热生长氧化物(TGO) 改性
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牦牛TBC1D7基因克隆、生物信息学及表达分析
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作者 张娟香 欧杰次仁 +6 位作者 喇永富 马晓明 吴晓云 郭宪 褚敏 阎萍 梁春年 《中国草食动物科学》 CAS 北大核心 2024年第2期10-17,共8页
为探究西藏牦牛Tre2-Bub2-CDC16结构域家族成员7(TBC1D7)基因的特征及结构,利用RT-PCR克隆了TBC1D7基因的CDS区序列,并对其进行了生物信息学分析,利用实时荧光定量PCR(qPCR)检测了TBC1D7基因在牦牛心脏、肝脏、脾脏、肺脏、肾脏、肌肉... 为探究西藏牦牛Tre2-Bub2-CDC16结构域家族成员7(TBC1D7)基因的特征及结构,利用RT-PCR克隆了TBC1D7基因的CDS区序列,并对其进行了生物信息学分析,利用实时荧光定量PCR(qPCR)检测了TBC1D7基因在牦牛心脏、肝脏、脾脏、肺脏、肾脏、肌肉及脂肪组织的表达水平。结果表明,牦牛TBC1D7基因的CDS区全长为882 bp,共编码293个氨基酸;系统进化树分析结果表明,西藏牦牛与野牦牛的亲缘关系最近,与兔的最远;生物信息学分析结果表明,牦牛TBC1D7蛋白不存在信号肽和跨膜结构,属于亲水性蛋白,主要存在细胞核中,且该蛋白具有24个潜在的磷酸化位点,蛋白的高级结构由α-螺旋(65.53%)、延伸连(3.75%)、β-转角(3.75%)和无规则卷曲(29.96%)构成。qPCR检测结果显示,TBC1D7基因在西藏牦牛脾脏组织中的表达最高,极显著高于其他组织(P<0.01)。 展开更多
关键词 西藏牦牛 TBC1D7基因 克隆 生物学分析 组织表达
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高温多组分工况下气膜冷却及TBCs传热特性
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作者 李明飞 尹洪 +2 位作者 孙鹏 任静 蒋洪德 《工程热物理学报》 EI CAS CSCD 北大核心 2013年第7期1251-1255,共5页
煤基联合循环电站系统的燃气轮机透平将会工作在高温高湿的环境中。文中基于高温多组分气膜冷却试验台,分析在高温气膜冷却系统中导热/对流/辐射多场耦合作用机理.研究表明,高温环境下辐射作用不可忽略,不同的高温气体组分将对透平传热... 煤基联合循环电站系统的燃气轮机透平将会工作在高温高湿的环境中。文中基于高温多组分气膜冷却试验台,分析在高温气膜冷却系统中导热/对流/辐射多场耦合作用机理.研究表明,高温环境下辐射作用不可忽略,不同的高温气体组分将对透平传热产生影响;随着主流高温燃气中水蒸气和二氧化碳体积分数之和每增加7%,平板上表面中心线总体冷却效率降低约0.02;TBCs在各组分工况下都有明显的温降效果,且燃气的水蒸气含量越高,温降效果越明显。由于辐射在高温高湿工况下的综合作用,在透平的设计中必须综合考虑不同燃气组分在导热/对流/辐射耦合作用下的气膜冷却传热机理。 展开更多
关键词 气体组分 tbcs 辐射 耦合换热
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BDS在资阳大地控制网的运用与精度分析
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作者 吴勇 涂继友 田觉有 《测绘通报》 CSCD 北大核心 2024年第S01期101-105,195,共6页
北斗卫星导航系统(BDS)在全球服务方面的性能持续提升,其在大地测量和地理信息系统(GIS)领域的应用潜力不断被挖掘。本文以资阳市全域大地控制网建设项目为例,通过分析评估GPS和BDS观测数据的主要指标,以及使用常规解算软件加载广播星... 北斗卫星导航系统(BDS)在全球服务方面的性能持续提升,其在大地测量和地理信息系统(GIS)领域的应用潜力不断被挖掘。本文以资阳市全域大地控制网建设项目为例,通过分析评估GPS和BDS观测数据的主要指标,以及使用常规解算软件加载广播星历分别对GPS单系统和BDS单系统观测数据进行基线解算,目的在于采用常规数据处理方式验证北斗系统在大地控制网建立中的实际应用效果及可行性。分析结果表明,BDS在水平方向上的基线解算精度优于GPS,垂直方向上的基线解算精度与GPS相当。结果证实,BDS采用常规数据处理方式能够满足大地控制网建设的需求,为BDS在相关领域的进一步研究与应用奠定了一些实践基础。 展开更多
关键词 大地控制网 BDS TBC 广播星历
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Seismic safety assessment with non-Gaussian random processes for train-bridge coupled systems
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作者 Zhao Han Gao Lei +4 位作者 Wei Biao Tan Jincheng Guo Peidong Jiang Lizhong Xiang Ping 《Earthquake Engineering and Engineering Vibration》 SCIE EI CSCD 2024年第1期241-260,共20页
Extensive high-speed railway(HSR)network resembled the intricate vascular system of the human body,crisscrossing mainlands.Seismic events,known for their unpredictability,pose a significant threat to both trains and b... Extensive high-speed railway(HSR)network resembled the intricate vascular system of the human body,crisscrossing mainlands.Seismic events,known for their unpredictability,pose a significant threat to both trains and bridges,given the HSR’s extended operational duration.Therefore,ensuring the running safety of train-bridge coupled(TBC)system,primarily composed of simply supported beam bridges,is paramount.Traditional methods like the Monte Carlo method fall short in analyzing this intricate system efficiently.Instead,efficient algorithm like the new point estimate method combined with moment expansion approximation(NPEM-MEA)is applied to study random responses of numerical simulation TBC systems.Validation of the NPEM-MEA’s feasibility is conducted using the Monte Carlo method.Comparative analysis confirms the accuracy and efficiency of the method,with a recommended truncation order of four to six for the NPEM-MEA.Additionally,the influences of seismic magnitude and epicentral distance are discussed based on the random dynamic responses in the TBC system.This methodology not only facilitates seismic safety assessments for TBC systems but also contributes to standard-setting for these systems under earthquake conditions. 展开更多
关键词 train-bridge coupled(TBC)system random vibration new point estimate method(NPEM) seismic safety assessment moment expansion approximation(MEA) non-Gaussian distributions
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Al-modification for PS-PVD 7YSZ TBCs to improve particle erosion and thermal cycle performances
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作者 Xiaofeng ZHANG Ming LI +9 位作者 Ao ZHANG Shuangquan GUO Jie MAO Chunming DENG Panpan WANG Changguang DENG Junli FENG Min LIU Kesong ZHOU Cheng LAI 《Journal of Advanced Ceramics》 SCIE EI CAS CSCD 2022年第7期1093-1103,共11页
Plasma spray-physical vapor deposition(PS-PVD)as a novel process was used to prepare feather-like columnar thermal barrier coatings(TBCs).This special microstructure shows good strain tolerance and non-line-of-sight(N... Plasma spray-physical vapor deposition(PS-PVD)as a novel process was used to prepare feather-like columnar thermal barrier coatings(TBCs).This special microstructure shows good strain tolerance and non-line-of-sight(NLOS)deposition,giving great potential application in aero-engine.However,due to serious service environment of aero-engine,particle erosion performance is a weakness for PS-PVD 7YSZ TBCs.As a solution,an Al-modification approach was proposed in this investigation.Through in-situ reaction of Al and ZrO2,anα-Al2O3 overlay can be formed on the surface of 7YSZ columnar coating.The results demonstrate that this approach can improve particle erosion resistance since hardness improvement of Al-modified TBCs.Meanwhile,as another important performance of thermal cycle,it has a better optimization with 350-cycle water-quenching,compared with the as-sprayed TBCs. 展开更多
关键词 plasma spray-physical vapor deposition(PS-PVD) thermal barrier coatings(tbcs) Al-modification particle erosion resistance thermal cycle performance
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高精度GNSS静态平面控制网的解算技术探讨
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作者 黄波 《中文科技期刊数据库(文摘版)工程技术》 2024年第3期0090-0093,共4页
在工程项目建设中布测平面控制网是一项必要的基础工作,它为项目提供平面起算依据、框架基准。基于GNSS系统建立的静态平面控制网是当前最经济、最高效和最高精度的技术手段,该方法快速、准确、累计误差小、控制点无需通视,相比于传统... 在工程项目建设中布测平面控制网是一项必要的基础工作,它为项目提供平面起算依据、框架基准。基于GNSS系统建立的静态平面控制网是当前最经济、最高效和最高精度的技术手段,该方法快速、准确、累计误差小、控制点无需通视,相比于传统的导线、三角网控制网测量,有显著的优势。本文依托项目的实施,归纳梳理了此类项目作业的方法和思路,为同类项目的拓展提供参考。 展开更多
关键词 天宝TBC软件 科傻GPS数据处理系统 三维无约束平差 二维约束平差 网平差 异步环
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热冲击环境下涂层/基底界面的微观形貌及元素扩散规律研究
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作者 杨来侠 高伟 +2 位作者 赵晋超 高扬 徐超 《航空制造技术》 CSCD 北大核心 2023年第19期14-21,共8页
针对热障涂层在高温环境中长期服役的需求,研究热障涂层在热冲击环境下涂层/基底界面形貌演变及元素扩散规律。通过自主搭建的石英灯加热平台对热障涂层进行热冲击试验。利用SEM和EDS对热冲击后涂层/基底界面的微观形貌及元素分布进行分... 针对热障涂层在高温环境中长期服役的需求,研究热障涂层在热冲击环境下涂层/基底界面形貌演变及元素扩散规律。通过自主搭建的石英灯加热平台对热障涂层进行热冲击试验。利用SEM和EDS对热冲击后涂层/基底界面的微观形貌及元素分布进行分析,利用Boltzmann-Matano扩散模型计算了涂层/基底界面Al元素的扩散系数。结果表明,沉积态的热障涂层中黏结层(BC)主要由β和γ相组成,并且在涂层/基底界面已经出现扩散区;随着热冲击试验的进行,Al元素快速消耗致使BC层和基底间Al元素浓度梯度转变,Al元素开始向外扩散,部分拓扑密堆(TCP)相中富集的难熔元素可以重新固溶到基底中,最终各元素在界面区的分布逐渐均匀;Al元素的扩散系数在热冲击试验开始前为正值,到600次热冲击循环后为负值,且扩散系数的最大值均出现在涂层/基底界面处,距离界面越大,扩散系数就越低。 展开更多
关键词 热障涂层(tbcs) 热冲击 元素扩散 扩散系数 拓扑密堆相(TCP)
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氧化钇部分稳定氧化锆陶瓷涂层的高温耐久性辨析
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作者 杜博宇 杨加胜 +7 位作者 陶诗倩 赵华玉 钟兴华 庄寅 盛靖 倪金星 邵芳 陶顺衍 《航空制造技术》 CSCD 北大核心 2023年第17期89-95,共7页
氧化钇部分稳定的氧化锆(YSZ)作为热障涂层材料广泛应用于复杂高温工况,其优异的高温耐久性主要由不可相变介稳四方相(t′)所贡献。然而,目前对t′相可靠服役温度上限的界定较为模糊,主流观点仍停留在1200℃左右。基于此,采用大气等离... 氧化钇部分稳定的氧化锆(YSZ)作为热障涂层材料广泛应用于复杂高温工况,其优异的高温耐久性主要由不可相变介稳四方相(t′)所贡献。然而,目前对t′相可靠服役温度上限的界定较为模糊,主流观点仍停留在1200℃左右。基于此,采用大气等离子体喷涂(APS)工艺制备YSZ陶瓷涂层,经不同时效热处理,针对涂层微结构、相组成、烧结收缩和断裂韧性等变化进行分析研究。结果表明,经24 h@1400℃热处理附加7年室温存放后,陶瓷层未见单斜相;300 h@1400℃和300 h@1600℃热处理涂层中单斜相体积分数分别为3.55%和35.41%,且均未碎裂。300 h@1600℃涂层烧结线性收缩率为0.4%。高温时效热处理同时伴随晶粒生长和孔隙愈合,涂层抗折强度和断裂韧性随之增加,因而认为APS YSZ涂层可在1400℃下长时间(~300 h)服役。 展开更多
关键词 氧化钇部分稳定氧化锆(YSZ) 热障涂层(tbcs) 等离子体喷涂 高温耐久性 相组成 力学性能
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不同钇含量氧化锆基热障涂层材料CMAS腐蚀行为研究
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作者 张晗 王晶 +3 位作者 陆杰 陈小龙 黄轶男 赵晓峰 《航空制造技术》 CSCD 北大核心 2023年第17期46-56,共11页
系统研究了不同YO1.5含量掺杂氧化锆基材料(8YSZ、20YSZ、38YSZ、55YSZ)以及纯氧化钇材料(Y_(2)O_(3))在1300℃下的CaO-MgO-Al_(2)O_(3)-SiO_(2)(CMAS)腐蚀行为。结果表明,不同钇含量氧化锆基材料表现出具有显著差异的CMAS腐蚀行为。对... 系统研究了不同YO1.5含量掺杂氧化锆基材料(8YSZ、20YSZ、38YSZ、55YSZ)以及纯氧化钇材料(Y_(2)O_(3))在1300℃下的CaO-MgO-Al_(2)O_(3)-SiO_(2)(CMAS)腐蚀行为。结果表明,不同钇含量氧化锆基材料表现出具有显著差异的CMAS腐蚀行为。对于YO1.5含量较低的8YSZ与20YSZ而言,腐蚀行为由溶解-再析出及晶界腐蚀所主导,前者析出小球颗粒ZrO_(2),后者的析出物则是直接沉积在原始ZrO_(2)表面形成核壳结构;随着YO1.5含量的增加,腐蚀行为逐渐转变成反应腐蚀,38YSZ以及55YSZ与CMAS熔盐快速反应结晶,形成一层连续致密、含磷灰石相的保护层,能够有效阻挡CMAS熔盐的进一步侵蚀,并且55YSZ所形成的保护层中磷灰石相的体积分数更多,抗CMAS腐蚀能力更佳;纯Y_(2)O_(3)样品也能与CMAS熔盐快速反应,从而形成一层致密的纯磷灰石层,抗CMAS腐蚀能力良好。因此,可以通过调控氧化锆基材料中的钇含量,从而调控热障涂层抗CMAS腐蚀能力。 展开更多
关键词 热障涂层(tbcs) CMAS腐蚀 氧化钇掺杂氧化锆 磷灰石 陶瓷材料
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PS-PVD制备YSZ热障涂层的CMAS腐蚀行为研究
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作者 严刚 刘伟 +4 位作者 罗俊辉 谷凯凯 李聪 杨丽 周益春 《航空制造技术》 CSCD 北大核心 2023年第17期57-63,共7页
热障涂层(TBCs)广泛应用于先进航空发动机热端部件,有效延长了发动机热端部件的服役寿命,成为先进航空发动机必不可少的热防护材料。但在服役过程中一些大气沉积物CMAS加热后变为熔融体吸附在热障涂层表面,并沿着孔隙和裂纹等缺陷渗透... 热障涂层(TBCs)广泛应用于先进航空发动机热端部件,有效延长了发动机热端部件的服役寿命,成为先进航空发动机必不可少的热防护材料。但在服役过程中一些大气沉积物CMAS加热后变为熔融体吸附在热障涂层表面,并沿着孔隙和裂纹等缺陷渗透至涂层内部,诱导涂层过早失效。采用等离子-物理气相沉积技术(PS-PVD)制备YSZ热障涂层,利用XRD、SEM等表征手段,对不同腐蚀时间的涂层物相成分、微观结构进行了表征。研究结果表明,YSZ涂层在1250℃下经过CMAS腐蚀后发生了相变;随着腐蚀时间的增加,CMAS沉积物会沿着热障涂层类柱状晶间隙渗透至内部,导致涂层结构出现疏松,并且在陶瓷层上部区域出现了类柱状晶断裂现象,涂层宏观表现为部分陶瓷层剥落;腐蚀8 h后陶瓷层部分区域出现了类柱状晶从粘结层上整体剥离;CMAS渗透深度随腐蚀时间的增加不断加大,在腐蚀3 h内其渗透速度相对较快,腐蚀3 h以后其渗透速度会相对变得缓慢。 展开更多
关键词 等离子喷涂-物理气相沉积(PS-PVD) 热障涂层(tbcs) CMAS腐蚀 渗透速度 失效行为
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孔隙对热障涂层微压痕响应影响的数值模拟
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作者 赵伟玲 王亮 +2 位作者 刘楠 曹枝军 苏怀宇 《航空制造技术》 CSCD 北大核心 2023年第17期103-109,共7页
微纳米压痕技术是表征陶瓷涂层系统力学性能和弹塑性响应行为的一项重要技术。通过Python二次开发在ABAQUS软件中建立含随机分布的圆形孔隙的热障涂层模型,研究孔隙对大气等离子法(APS)制备的热障涂层的微纳米压痕响应的影响,并在含随... 微纳米压痕技术是表征陶瓷涂层系统力学性能和弹塑性响应行为的一项重要技术。通过Python二次开发在ABAQUS软件中建立含随机分布的圆形孔隙的热障涂层模型,研究孔隙对大气等离子法(APS)制备的热障涂层的微纳米压痕响应的影响,并在含随机圆形孔隙热障涂层模型的基础上,利用扩展有限元法(XFEM)模拟分析微纳米压痕试验过程中陶瓷层内的裂纹扩展,探究微裂纹和孔隙间的相互影响,以及涂层内裂纹萌生扩展的规律。模拟结果表明,孔隙的存在会在加载和卸载过程中释放一定的应力集中,从而改变涂层应力的分布特征;孔隙的存在会导致裂纹向孔隙的方向偏移扩展,并在一定程度上阻止裂纹扩展。将这些工作与微纳米压痕试验的试验数据联系起来,可以对热障涂层体系的力学性能进行有效预测。 展开更多
关键词 孔隙 热障涂层(tbcs) 微压痕 力学行为 有限元
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