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1.
A. J. Slifka B. J. Filla J. M. Phelps G. Bancke C. C. Berndt 《Journal of Thermal Spray Technology》1998,7(1):43-46
The conductivity of a thermal-barrier coating composed of atmospheric plasma sprayed 8 mass percent yttria partially stabilized
zirconia has been measured. This coating was sprayed on a substrate of 410
stainless steel. An absolute, steady-state measurement method was used to measure thermal conductivity
from 400 to 800 K. The thermal conductivity of the coating is 0.62 W/(m×K). This measurement has shown
to be temperature independent. 相似文献
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机械零件在工作温度和环境温度偏离标准设计温度后,其形状会发生改变,但由于温度场分布的不均匀性、构件材料的原子间距、内部缺陷形态等因素的影响,使得构件的热膨胀不能自由发生,导致构件热变形前后在形状上具有非相似性,理论和实验都证明这种非相似性是普遍存在的。 相似文献
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文章针对某电缆厂的拉线机的电动机故障问题,给出一些切实可行的保护措施.对其他电动机的保护也有一定的参考价值. 相似文献
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S. A. Tsipas I. O. Golosnoy T. W. Clyne R. Damani 《Journal of Thermal Spray Technology》2004,13(3):370-376
Superalloy substrates coated with plasma-sprayed CoNiCrAlY bond coats and yttria-stabilized zirconia top coats (TCs) have
been subjected to a high heat flux under a controlled atmosphere. The sintering exhibited by the TC under these conditions
has been studied and compared with the behavior observed during isothermal heating. Sintering has been characterized by (a)
microstructural examinations, (b) dilatometry, in both the in-plane and through-thickness directions, and (c) stiffness measurements,
using both cantilever bending and nanoindentation. A numerical model has been used to explore the stress state under isothermal
and thermal gradient conditions. Dilatometry data indicate significant linear contractions during holding at elevated temperatures,
particularly in the through-thickness direction. This is largely attributed to microstructural changes associated with sintering,
with any volume changes due to phase transformations making relatively small contributions. Sintering proceeds faster at higher
temperatures but is retarded by the presence of tensile stresses (from differential thermal expansion between the coating
and substrate) within the TC. Thus, it occurs preferentially near the free surface of the TC under gradient conditions, not
only due to the higher temperature, but also because the in-plane stress is more compressive in that region. 相似文献
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J.H.Liu ) S.H.Jiang ) M.Yao ) ) Department of mechanical Engineering Engineering college Yangzhou University Yangzhou China ) Department of Material Science Yanshan University Qinhuangdao China 《金属学报(英文版)》1999,12(5):852-855
1.IntroductionFig.1 ThermalfatiguetestmachinewithOutercinstraintThedamagecausedbythermalfatigueisoneofthemainfailureformsofmetalworkingpiecesunderthetemperaturevariationconditions.Alotofthermalfatiguetestsconcerningthefailurewereconductedonthevariou… 相似文献
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Anisotropic thermal conductivities of the plasma-sprayed ceramic coating are explicitly expressed in terms of the microstructural
parameters. The dominant features of the porous space are identified as strongly oblate (cracklike) pores that tend to be
either parallel or normal to the substrate. The scatter in pore orientations is shown to have a pronounced effect on the effective
conductivities. The established quantitative microstructure-property relations, if combined with the knowledge of the processing
parameters-resulting microstructure connections, can be utilized for controlling the conductivities in the desired way. 相似文献
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从实用出发对3168不锈钢管材进行了热循环下的裂纹扩展试验,试验表明该材料在交变热应力下的裂纹扩展速率缓慢,带裂纹的管道在监督下可以继续运行。 相似文献
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An experimental rig based on the use of infrared quartz lamps has been developed to monitor the degradation mechanisms causing
failure of thermal barrier coatings (TBC) under thermal-cycling conditions. An acoustic emission (AE) technique monitored
these degradation mechanisms, and advanced signals processing identified the key parameters that classify the AE signals according
to the long-term behavior of the TBC. The AE technique enabled the localization of degradation sources inside the TBC with
a linear resolution of ∼5 mm by the use of two transducers fixed at both ends of the sample. Furthermore, sample zones of
high AE activity showed typical vertical cracks at the surface and delaminations at the interface between the ceramic and
the bond-coat layer. Vertical cracks were induced preferentially during the heating period of the thermal cycles when the
ceramic coating was in a tensile-stress state, while delaminations were induced during the cooling period when the TBC was
in a compressive-stress state. 相似文献
12.
通过固相反应法合成了Gd2Zr2O7-SrZrO3 (GZSZ,Gd2Zr2O7:SrZrO3=7:3)复合陶瓷粉末,并采用喷雾造粒法和大气等离子喷涂法分别制备了适合等离子喷涂使用的相应喷涂粉末及涂层。使用X射线衍射、扫描电子显微镜对粉末和涂层的相组成、显微结构进行分析。借助激光热导仪、高温热膨胀仪对涂层的热扩散系数和热膨胀系数、烧结系数进行了表征。结果表明,制备的GZSZ复合陶瓷粉末和涂层都由Gd2Zr2O7和SrZrO3两相组成,粉末中的Gd2Zr2O7为烧绿石结构,而涂层中的Gd2Zr2O7为萤石结构,SrZrO3都为钙钛矿结构。制备态GZSZ涂层的孔隙率为~14%。GZSZ涂层1400℃热处理5 h后的热膨胀系数为(9.8~11.2)×10-6 K-1。制备态GZSZ涂层的热导率为~0.8 W·m-1·K-1,与制备态SrZrO3涂层的热导率~1.0 W·m-1·K-1相比降低~20%。1400℃热处理360 h后GZSZ涂层的热导率增加到~1.5 W·m-1.K-1。综上表明,GZSZ涂层是一种很有前景的复合陶瓷热障涂层材料。 相似文献
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提高等离子喷涂热障涂层隔热性能的方法 总被引:1,自引:0,他引:1
为进一步提高等离子喷涂热障涂层的隔热性能,对陶瓷材料的导热理论及热障涂层的热导率进行了研究.提出了包括寻求新型热障涂层陶瓷材料、添加掺杂剂、制备纳米涂层及双陶瓷层热障涂层等能够改善等离子喷涂涂层隔热性能的方法;并指出,采用等离子喷涂技术制备带颜色的稀土锆酸盐纳米双陶瓷层热障涂层,将会进一步改善热障涂层的隔热性能. 相似文献
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The curling up of the edges of splats of molten metal deposited on a cold substrate was investigated both experimentally and
numerically. An analytical model, based on mismatch of thermal expansion between the splat and substrate, was developed to
calculate the deformation of splats after curling up. The curling-up angle was measured from both millimeter-sized splats
of aluminum alloy and bismuth and plasma-sprayed nickel particles. The curling-up angles were predicted using both the analytical
model and a numerical code and were found to agree reasonably well with experimental measurements.
This article was originally published inBuilding on 100 Years of Success, Proceedings of the 2006 International Thermal Spray Conference (Seattle, WA), May 15–18, 2006, B.R. Marple, M.M. Hyland, Y.-Ch. Lau, R.S. Lima, and J.Voyer, Ed., ASM International, Materials
Park, OH, 2006. 相似文献
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制备8批次EB-PVD双层结构热障涂层试样,采用循环加热快速冷却实验装置模拟热障涂层服役环境,开展了热障涂层试样在不同热循环保温时间条件下的热循环性能评价实验,采用指数下降的数学模型对热循环实验数据进行拟合分析,获得了表征热障涂层试样静态氧化性能和热疲劳性能的物理量.结果表明,在本实验工艺条件下制备的不同批次热障涂层试样的静态氧化性能和热疲劳性能具有不同的匹配关系,热障涂层试样静态氧化性能总体估计值为(677±194)h,热疲劳性能总体估计值为(6789±1818)次. 相似文献
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采用电子束物理气相沉积工艺(EB-PVD)制备了针对第二代单晶高温合金的热障涂层,用SEM观察分析了不同成分粘结层的热障涂层热循环试验后的结构和晶体形貌,在N2条件下对比了不同成分粘结层材料与第二代单晶高温合金的热膨胀系数,分析了热循环试验后粘结层与热生长氧化(TGO)层成分、厚度及完整性情况。结果表明:NiCoCrAlYHf与第二代单晶高温合金热膨胀系数更为接近,匹配性更好;采用EB-PVD工艺制备的热障涂层在热循环试验过程中会产生大量垂直裂纹使涂层具有良好的应变容限;粘结层中Al元素含量的提高以及Hf等元素的加入,使得热循环试验后涂层TGO层的Al2O3纯度较高、生长缓慢无块状物生成,并且极大地改善了粘结层和合金基体的内氧化,涂层1 100℃循环氧化寿命达到1 200 h以上。 相似文献
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Ann Bolcavage Albert Feuerstein John Foster Peter Moore 《Journal of Materials Engineering and Performance》2004,13(4):389-397
Various methods of thermal shock testing are used by aircraft and industrial gas turbine engine (IGT) manufacturers to characterize
new thermal barrier coating systems in the development stage as well as for quality control. The cyclic furnace oxidation
test (FCT), widely used in aircraft applications, stresses the ceramic/bondcoat interface, predominantly through thermally
grown oxide (TGO) growth stress. The jet engine thermal shock (JETS) test, derived from a burner rig test, creates a large
thermal gradient across the thermal barrier coating (TBC), as well as thermomechanical stress at the interface. For IGT applications
with long high-temperature exposure times, a combination of isothermal preoxidation and thermal shock testing in a fluidized
bed reactor may better represent the actual engine conditions while both types of stress are present. A comparative evaluation
of FCT, JETS, and a combined isothermal oxidation and fluidized bed thermal shock test has been conducted for selected ceramic/bondcoat
systems. The results and the failure mechanisms as they relate to the TBC system are discussed. A recommendation on the test
method of choice providing best discrimination between the thermal shock resistance of the ceramic layer, the ceramic/bondcoat
interface, and even substrate related effects, is given.
This paper was presented at the 2nd International Surface Engineering Congress sponsored by ASM International, on September
15–17, 2003, in Indianapolis, Indiana, and appeared on pp. 520–29. 相似文献
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采用激光熔覆定向凝固技术修复损伤定向凝固涡轮叶片,研究熔覆层在1000℃高温下的热震性能.自配粉末l和粉末2制备熔覆层进行对比.热震实验结果表明:粉末2熔覆层抗冷热冲击性能优于粉末1熔覆层;366次热震实验后,粉末1熔覆层组织开裂,基本剥离基体,熔覆层失效;404次热震实验后,粉末2熔覆层部分剥离基体,熔覆层内部分布着细小的裂纹,多数裂纹平行于结合带方向,熔覆层失效;熔覆层失效首先是由于熔覆层与基体结合带产生裂纹;熔覆层内部产生裂纹大多产生于层与层之间的过渡区域;为提高涂层抗冷热冲击性能,应减小熔覆层与基体的热膨胀系数差异,采用合适的工艺参数,减小层与层之间的横向应力,保证多层熔覆层之间的良好过渡. 相似文献