2016
DOI: 10.1007/s11666-016-0497-2
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Failure Behavior of Plasma-Sprayed Yttria-Stabilized Zirconia Thermal Barrier Coatings Under Three-Point Bending Test via Acoustic Emission Technique

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Cited by 16 publications
(7 citation statements)
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“…In order to generate cracks in the coatings, the three-point flexural test, one of the methods most collected in the literature for this purpose, was performed [12,14,15], with a configuration like the one presented in Figure 1a,b.…”
Section: Mechanical Testsmentioning
confidence: 99%
See 2 more Smart Citations
“…In order to generate cracks in the coatings, the three-point flexural test, one of the methods most collected in the literature for this purpose, was performed [12,14,15], with a configuration like the one presented in Figure 1a,b.…”
Section: Mechanical Testsmentioning
confidence: 99%
“…In order to generate cracks in the coatings, the three-point flexural test, one of the methods most collected in the literature for this purpose, was performed [12,14,15], with a configuration like the one presented in Figure 1a To know the stress state of the ceramic coating at a given moment, Equation ( 1) is used [16], which allows the calculation of the maximum stress on the thermal barrier as a function of the load applied during the three-point flexural test.…”
Section: Mechanical Testsmentioning
confidence: 99%
See 1 more Smart Citation
“…A host of research results have showed that the cracks exist in the top-coat layer or near the TC (top-coat)/TGO interfaces in APS-TBCs. During the thermal shock, these cracks can propagate along the stratiform interface or through lamella under complex stress states [44][45][46]. The spallation of coating frequently take place owing to the crack initiation along the layer interface, which is accountable for the failure of APS-TBCs.…”
Section: Apsmentioning
confidence: 99%
“…铌合金具有优异的高温力学性能而用作航空航 天领域的结构材料 [1][2][3] ,但是较差的高温抗氧化性能 又制约了铌合金的应用 [4][5][6] 。因此,通常采用涂层包 覆的方法来提高合金的高温抗氧化性能 [7][8][9] 。常见的 高温防护涂层,如 Si-Cr-Ti 体系涂层已经成功应用 多年 [2,[10][11] 。研究表明,涂层在高温服役过程中结 构与组分的演变是涂层失效的主要原因,其中微裂 纹的影响最为显著 [12] 。随着航天技术的进一步发展, 对高温抗氧化涂层提出了更高的使用要求。为了针 对性地提高涂层性能,对其破坏过程中裂纹演化过 程的研究十分重要。 对于高温抗氧化涂层失效过程的研究,通常采 用分时采样的方法,即对不同服役时间的样品进行 机械加工,利用扫描电子显微镜观察氧化前后涂层 的形貌与组分的变化情况 [12][13][14][15][16] 。但这种方法在制样 过程中会对涂层造成二次伤害, 干扰分析失效机理。 声发射技术(AE) [17][18][19][20][21] 、数字图像相关法(DIC) [22][23][24][25] 、光致发光光谱法(PLPS) [26][27][28][29][30] 、红外光谱法 [31][32] 和热成像法 [33] 等无损检测技术常被用来确定 损伤部位以及评价损伤程度。高温抗氧化涂层在高 温服役条件下的失效过程是一个与温度场变化、材 料成分变化以及微结构演变等联系在一起的动态变 化过程,静态研究方式势必会掩盖涂层裂纹结构的 真实信息。因此,在这些方法中,声发射技术兼具 实时、无损和连续监测的优点,十分适合进行破坏 过程机理的研究。目前对于声发射技术在失效过程 研究的应用主要集中于岩土材料、复合材料以及热 障涂层 [17][18][19][20][21] ,而对于 Si-Cr-Ti 高温抗氧化涂层失效 机理的研究未见报道。尽管同为涂层,由于声发射 信号对材料成分以及结构的敏感性,仍然有必要进 行 Si-Cr-Ti 高温抗氧化涂层失效机理中声发射信号 的研究。 由于声发射信号的特点与裂纹的破坏模式紧密 相关,而与引起裂纹的外载荷属性无关 [20] [40] :…”
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