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铝合金基体上含化学镀过渡层的二氧化锆热障涂层失效机制

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为了缓解涂层和基体之间的热失配应力,采用化学镀方法在2A70铝合金表面上制备Ni-P和Ni-Cu-P过渡层;然后在镀层表面依次制备CoNiCrAlY粘结层和ZrO2-8%Y2O3(8YSZ)陶瓷层(质量分数),获得复合热障涂层;并采用热循环方法评定该涂层体系的抗热震性能。结果表明,采用Ni-P镀层和Ni-Cu-P镀层作为过渡层的试样的热震寿命分别约为1000次和500次;Ni和Al元素的互扩散使过渡层与基体界面区域形成了扩散层和岛状颗粒,一些颗粒与扩散层连通后提高了涂层与基体的结合强度,但孤立的颗粒由于变形能力差,对涂层的寿命有不利影响;在交变应力下颗粒与基体界面处会形成裂纹,并最终导致涂层剥离。
Failure mechanism of ZrO2-8%Y2O3 thermal barrier coatings on aluminum alloy with electroless plating interlayer
To relieve the thermal mismatch stress between coatings and substrate, Ni-P and Ni-Cu-P electroless platings were fabricated onto 2A70 aluminum as interlayers. Subsequently, the specimen with plating was covered by CoNiCrAlY bond coat and ZrO2-8%Y2O3(8YSZ) top coat (mass fraction), then a novel thermal barrier coating (TBC) was produced. The thermal shock resistance of TBCs was evaluated by heat cycle test. The results indicate that the lifetimes of TBC with Ni-P interlayer and Ni-Cu-P interlayer are about 1000 cycles and 500 cycles, respectively. The interdiffusion of Ni and Al results in the formation of diffusion layers and island particles at the interface between interlayers and substrate. The connection between particles and diffusion layers improves the adhesion of coatings with substrate, while isolate particles are harmful to the lifetime of coatings due to their poor deformation ability under alternative stress. Crack initiation happens at the interfaces between particles and substrate, which leads to coatings spallation.

thermal barrier coatingair plasma sprayelectroless platingfailure mechanism

陆冠雄、郝利军、刘彻、叶福兴

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天津大学 材料科学与工程学院,天津 300072

天津大学 天津市现代连接技术重点实验室,天津 300072

热障涂层 大气等离子喷涂 化学镀 失效机制

天津市自然科学基金资助项目

12JCYBJC12300

2014

中国有色金属学报
中国有色金属学会

中国有色金属学报

CSTPCDCSCD北大核心EI
影响因子:1.108
ISSN:1004-0609
年,卷(期):2014.(5)
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