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等离子喷涂ZrO2涂层的火焰喷烧和水淬热冲击 总被引:5,自引:1,他引:4
研究了等离子喷涂ZrO2涂层在水淬和火焰喷烧两种条件下的热冲击性能,采用ANSYS软件对两种条件下涂层的热冲击性能进行了有限元计算.结果表明:水淬条件下垂直裂纹主要分布在距离涂层中心12mm的范围内,随着热冲击次数的增加垂直裂纹最终进入次表层,靠近中心处裂纹扩展较快;火焰喷烧条件下,垂直裂纹分布在距离涂层中心10mm的范围内,随着热冲击次数的增加裂纹在表面层和次表层界面处发生偏转,中心处裂纹扩展较快;火焰喷烧条件下涂层的抗热震性能优于水淬条件,涂层中的孔隙加速了两种条件下裂纹的扩展. 相似文献
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目的 探究重型燃机喷嘴壳体及遮热板热障涂层剥落机制,为该部件的全寿命管理提供参考。方法 采用等离子喷涂方法,分别制备以06Cr25Ni20不锈钢和Hastelloy X合金为基材的热障涂层试验件,并结合水淬热冲击表征方法与瞬态热力耦合仿真方法,表征热障涂层水淬后的剥落状态,获得热障涂层残余剪应力的分布状态随基材和服役工况的变化行为,揭示热障涂层在多层热失配工况下的剥落机制。结果 在水淬热冲击条件下,2种不同基材的热障涂层试验件表现出类似的剥落行为,但由于基材热膨胀系数的差异,以06Cr25Ni20不锈钢为基材的热障涂层的残余剪应力(70.1 MPa)比Hastelloy X合金基材的热障涂层(52.7 MPa)更大,热冲击寿命更短。在梯度温度载荷下,2种不同基材热障涂层试验件的失效模式不同,前者的最大残余剪应力为39.2 MPa,后者为25.7 MPa。结论 在2种温度载荷下,以Hastelloy X合金为基材的热障涂层具有较低的残余应力和较长的服役寿命。此外,水淬热冲击可以快速表征热障涂层的寿命行为,但其失效模式与实际梯度温度载荷下的失效模式仍有一定区别。 相似文献
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等离子喷涂ZrO2-NiCoCrAlY梯度热障涂层的抗热震性及失效机理 总被引:1,自引:0,他引:1
《材料热处理学报》2001,22(4):21-24
研究了ZrO2-NiCoCrAlY热障涂层的抗热震性和热震失效机理.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.热震裂纹形成与扩展主要在粘结层与基体的界面处.随热循环次数的增加,热震裂纹可在表面陶瓷层内和陶瓷层与过渡层的界面处形成.实验表明热障涂层热震失效的过程主要是裂纹形成、扩展及涂层剥落,粘结层的氧化是导致涂层剥落失效的重要原因. 相似文献
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稀土锆酸盐与8YSZ所组成的双陶瓷层涂层是目前热障涂层领域研究的热点,而陶瓷层厚度对其热冲击性能有着显著影响。采用有限元软件ANSYS研究了表层厚度对Sm2Zr2O7/8YSZ热障涂层淬冲击热应力的影响,并与单一Sm2Zr2O7涂层进行了比较。结果表明,在Sm2Zr2O7/8YSZ涂层的表面处具有最大的径向热冲击应力,最大轴向应力则存在于陶瓷层/金属粘结层界面处,涂层各处剪应力基本相当。涂层表面及两陶瓷层界面处的径向热应力随表层厚度的增加而减小,陶瓷层/粘结层界面处径向应力则随表层厚度增加而增大。每个界面处的轴向应力随表层厚度增加而降低,而剪应力绝对值则随表层厚度增加而增大。与单一Sm2Zr2O7涂层相比,Sm2Zr2O7/8YSZ涂层的热应力明显偏小,说明增加涂层的层数有利益改善涂层的抗热冲击性能。 相似文献
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目的 为了探究玻璃沉积物CMAS(CaO-MgO-Al2O3-SiO2)对新型结构热障涂层在1250 ℃下的热冲击寿命的影响,揭示热障涂层的失效行为。方法 通过火焰喷涂技术将制备的CMAS粉体均匀地沉积到铈酸镧/氧化钇部分稳定二氧化锆双陶瓷层热障涂层(LC/YSZ DCL-TBCs)和梯度热障涂层(LC/YSZ FGM-TBCs)的表面,于1250 ℃热冲击实验中进行涂层样品的抗热冲击性能及失效机理研究。利用扫描电镜(SEM)和能谱仪(EDS)追踪CMAS的位置,观察CMAS与涂层反应层的厚度与形貌。采用X射线衍射仪(XRD)测试反应层产物,并总结其失效方式。结果 高温热冲击结果显示梯度涂层的热冲击寿命(435次)远高于双陶瓷层热障涂层的寿命(229次),约为铈酸镧/氧化锆双陶瓷层热障涂层寿命的1.9倍。铈酸镧层与梯度层都能在一定程度上阻碍CMAS渗入涂层内部,提高其CMAS腐蚀条件下的热冲击寿命。双陶瓷层热障涂层与梯度热障涂层的失效均是以层状剥落为主,剥落层主要是CMAS与LC的反应层以及反应层下的烧结层,反应层是由Ca2(LaxCe1-x)8(SiO4)6O6-4x、萤石相和MgAl2O4等难熔氧化物组成,这层致密氧化物类似于密封层,能阻止CMAS继续渗入。结论 功能梯度结构具有比双陶瓷层结构更优异的抗CMAS热冲击性能和更好的应力耐受性。 相似文献
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在优化热障梯度涂层和过渡层的成分设计及氧乙炔火焰法制备工艺的基础上,获得了组织致密,有良好冶金结合的Al2O3/Fe热障梯度涂层。结果表明,涂层中的Al2O3分布基本均匀,且在整个涂层中,从钢基体到涂层表面的化学成分呈梯度分布,涂层与钢基体及各涂层之间存在明显的冶金结合;所获得的Al2O3热障梯度涂层与普通纯Al2O3热障涂层和带底层(Ni)和过渡层(Cu)的热障涂层相比,与基体间的结合力显著提高,弯曲强度、耐热冲击性能大为增强,涂层热障效果随涂层的数量和Al2O3含量的增加也获得明显提高。 相似文献
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等离子喷涂ZrO2—NiCoCrAlY梯度热障涂层的抗热震性及失效机理 总被引:4,自引:0,他引:4
研究了ZrO2-NiCoCrAlY热障涂层的抗热震性和热震失效机理。实验结果表明,梯度热隙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。热震裂纹形成与扩展主要在粘结层与基体的界面处。随热循环次数的增加,热震裂纹可在表面陶瓷层内和陶瓷层与过渡层的界面处形成。实验表明热障涂层热震失效的过程主要是裂纹形成、扩展及涂层剥落,粘结层的氧化是导致涂层剥落失效的重要原因。 相似文献
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Guo Cean Chen Minghui Liao Yimin Su Bei Xie Dongbai Zhu Shenglong Wang Fuhui 《金属学报》2018,(12):1825-1832
High-temperature-resistant enamel coatings have been reported to be applied in non-critical hot end components of aero-engine and gas turbine recently. Although the enamel with a series of excellent properties can be as high-temperature-resistant coating material under appropriate condition, its lower soft point and inherent brittleness limit their use in broader application under severe service condition. Enamel-based composite coatings (an enamel matrix with the addition of ceramic particles and/or metal platelets) can remarkably increase the properties of the enamel coating and their protection mechanism under dynamic thermal shock needs further investigation. In this work, two kinds of enamel-based composite coatings, 70%enamel+25%Al2O3 and 70%enamel + 20%Al2O3 + 10%NiCrAlY (mass fraction, %) abbreviated to E25A and E20A10M respectively, were designed and fired on K38G superalloy substrate, and their protection mechanism was comparatively studied at 900. under the simulated combusting gas shock. The thermal shock fire was produced by the mixture gas of C3H8+O-2 and its ejecting pressure on the coating surface was 0.4 MPa. After the temperature has been stable at 900 degrees C, samples were hold for 15 s and then cooling down in air for 120 s, constituting a thermal shock cycle. Results indicated that, after 150 cyc of thermal shock, both the coatings bond well with the alloy substrate, thus shows high resistance to spallation along interface. For the E25A coating, its microstructure had no obvious change after thermal shock and the surface is still intact. The addition of secondary phase Al2O3 increases the stability of enamel at high temperature. With regard to the E20A10M coating, holes and cracks form consecutively, and peeling off occurs at surface after thermal shock. Interfacial reaction between the NiCrAlY particles and enamel following Cr-(NiCrAlY) + ZnO(enamel)-> CrO(interface) + Zn up arrow results in the formation of enamel swelling, which then, under the synergistic effect of combusting gas shear stress and interface thermal stress, leads to the peeling off of enamel and metal inclusions at surface. 相似文献
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The adhesion strength of thermal sprayed coatings is relatively low, and they sometimes tend to delaminate from the substrate
during operation. In particular, sprayed ceramic coatings for thermal barriers, such as ZrO2, often delaminate because of thermal shock; therefore, ceramic coatings are often submitted to thermal shock tests. A nondestructive
inspection method using ultrasound to detect the delamination of sprayed coating was proposed. In this study, a coating model
was made with acrylic plates, and an ultrasonic test was applied to investigate the precision of detecting delamination by
the ultrasonic testing method. Results indicate that delamination more than 1mm in diameter can be detected by the ultrasonic
testing method. Moreover, the delaminating process of sprayed coatings under thermal shock tests can be detected by this method. 相似文献
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等离子喷涂La2(Zr0.7Ce0.3)2O7热障涂层的抗热震性能 总被引:2,自引:0,他引:2
采用等离子喷涂制备了La2(Zr0.7Ce0.3)2O7(LZ7C3)热障涂层,并对涂层的微观组织、相结构、成分、相稳定性、涂层热导率以及抗热震性能进行了研究.结果表明,LZ7C3涂层由单相烧绿石结构物质组成,高温稳定性较好;涂层的热导率较块材下降约20%,这是由于涂层具有较高的孔隙率所致:涂层在不同温度范围的热震寿命和失效机制不同,在室温至约1000℃间的热震寿命为116 cyc,涂层失效方式以片状剥落为主:在室温至1100℃间的热震寿命为53 cyc,涂层失效方式为片状剥落和层状撕裂;在室温至1200℃间的热震寿命为3 cyc,涂层失效方式以层状撕裂为主. 相似文献
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采用纳米氧化锆团聚粉末和等离子喷涂技术制备了纳米氧化锆涂层,试验研究了激光重熔工艺参数(激光比能量)对纳米氧化锆涂层抗热冲击性能的影响.结果表明,激光重熔工艺参数对重熔涂层的抗热冲击性能影响显著,采用合适的工艺参数(激光比能量),可以使重熔涂层获得最佳的抗热冲击性能.不同激光重熔工艺参数处理的涂层形成的组织结构不同,使得涂层的抗热冲击性能不同.合适的激光重熔工艺参数下涂层表现出高的抗热冲击性能,主要是因为重熔后的涂层组织结构有利于热应力的释放以及其相结构在高温冲击下具有良好的稳定性. 相似文献
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Al/Ni-ZrO2 gradient thermal barrier coatings are made on aluminum substrate using plasma spraying method and one direction thermal shock properties of the coatings are studied in this paper. The results show that pores in coatings link to form cracks vertical to coating surface. They go through the whole ZrO2 coating once vertical cracks form. When thermal shock cycles increase, horizontal cracks that result in coatings failure forms in the coatings and interface. And vertical cracks delay appearance of horizontal cracks and enhance thermal shock property of coatings. Failure mechanisms of coating thermal shock are discussed using experiments and finite element method. 相似文献