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真空 ›› 2024, Vol. 61 ›› Issue (5): 21-29.doi: 10.13385/j.cnki.vacuum.2024.05.03

• 薄膜 • 上一篇    下一篇

Yb2O3改性Gd2Zr2O7热障涂层的显微组织和热循环性能研究*

李婷玥, 王鑫, 甄真, 李娜, 许振华   

  1. 中国航发北京航空材料研究院,航空材料先进腐蚀与防护航空科技重点实验室,北京 100095
  • 收稿日期:2024-03-31 出版日期:2024-09-25 发布日期:2024-10-10
  • 通讯作者: 许振华,研究员。
  • 作者简介:李婷玥(2000-),女,北京人,硕士研究生。
  • 基金资助:
    *国家科技重大专项(J2019-VII-0010-0150)

Microstructure and Thermal Cycling Properties of Yb2O3 Modified Gd2Zr2O7 Thermal Barrier Coatings

LI Ting-yue, WANG Xin, ZHEN Zhen, LI Na, XU Zhen-hua   

  1. Aviation Key Laboratory of Science and Technology on Advanced Corrosion and Protection for Aviation Material, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China
  • Received:2024-03-31 Online:2024-09-25 Published:2024-10-10

摘要: (Yb0.1Gd0.92Zr2O7(YbGdZrO)稀土复合氧化物是适用于更高温度的新型热障涂层(TBCs)候选材料之一。采用电子束物理气相沉积(EB-PVD)工艺在单晶合金(Ni,Pt)Al粘结层表面分别制备了单陶瓷层YbGdZrO和双陶瓷层YbGdZrO/YSZ两种热障涂层,并对涂层的相结构、化学组成、显微形貌和热循环行为进行了表征分析。结果表明:沉积态YbGdZrO陶瓷涂层的主相结构为单一的缺陷型萤石相,并有少量Yb2O3共存;与单陶瓷层涂层相比,双陶瓷层涂层的柱状晶簇较为纤细,且可观察到明显的柱状晶间隙;双陶瓷层涂层1100 ℃热循环寿命约为单陶瓷层涂层的1.5倍;经长期冷热交替循环后,单陶瓷层涂层内横向裂纹滋长,并扩展到YbGdZrO/TGO层界面上方几微米处,导致界面退化分离,且陶瓷层中的Yb元素内扩散进入TGO层;双陶瓷层涂层内出现纵向裂纹,而YbGdZrO/YSZ和YSZ/TGO层间界面基本完好;热循环失效后,单陶瓷层和双陶瓷层试样TGO层内均出现横向和纵向裂纹,甚至进一步诱发了层内断裂分离现象。

关键词: 电子束物理气相沉积, 热障涂层, 改性锆酸钆, 热循环, 界面分离

Abstract: The rare earth composite oxide of (Yb0.1Gd0.92Zr2O7 (YbGdZrO) is a candidate material for novel thermal barrier coatings (TBCs), which can be potentially applied in higher temperatures. Both of single-ceramic-layer YbGdZrO and double-ceramic-layer YbGdZrO/YSZ TBCs were directly fabricated on top of (Ni,Pt)Al bond coat surface via electron beam physical vapor deposition (EB-PVD). The phase structure, chemical constituent, morphology and thermal cycling behavior of those TBCs were systematically investigated. The results show that the primary phase structure of the as-deposited YbGdZrO ceramic coating is single defective fluorite phase with co-existing of a small amount of Yb2O3. Compared with the single-ceramic-layer coating, each beam of columnar crystal clusters in the sample with double-ceramic-layer TBC is relatively slender, and obvious columnar gain gaps can be observed. The 1100 ℃ thermal cycling lifetime of double-ceramic-layer TBC is about 1.5 folds as that of single-ceramic-layer YbGdZrO coating. After long-term alternating thermal cycling, the transverse microcracks grow in the single-ceramic-layer YbGdZrO coating and extend to several microns above the interface of YbGdZrO/TGO layer, causing interfacial degradation and separation. Moreover, the Yb element contained in single-ceramic-layer has inwardly diffused into the TGO layer. Longitudinal cracks appear within the double-ceramic-layer coating, while both of YbGdZrO/YSZ and YSZ/TGO interfaces remain basically intact. After thermal cycling failure, transverse and vertical microcracks are formed in the TGO layer of the single-ceramic-layer and double-ceramic-layer specimens, and even further induce the phenomenon of intra-layer fracture separation.

Key words: electron beam physical vapor deposition, thermal barrier coating, modified Gd2Zr2O7, thermal cycling, interfacial separation

中图分类号:  T32

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