Development of Life Predictive Method For Thermal Barrier Coating Systems
Development of Life Predictive Method For Thermal Barrier Coating Systems
批准号:
09555027
负责人:
HASHIDA Toshiyuki
金额:
$5.89万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
1997
资助国家:
日本
项目状态:
已结题
起止时间:
1997 至 1998
中文摘要
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英文摘要
The objective of this research is to develop evaluation methods of charcterizing thermal barrier coating (TBC) systems and predictive methodology of their life with special reference to a leading edge of advanced gas turbine blades, The research results are summarized for the following individual task.Task (1) Preparation of TBC specimens : TBC specimens with a top coat of ZrO and a bond coat of NiCrAlY were prepared by air plasma splay and electron beam-physical vapor deposition techniques. The specimen geometry was a cylindrical tube for simulating the curvature of leading edges and the substrate was a Ni-based superal loy.Task (2) Evaluation of interface properties(2-1) Thermal shock/fatigue tests were conducted on the cylindrical specimens with the TBCs using a laser heating method. A air-forced cooling cycle was employed to simulate the thermal transient history during trips. An acoustic emission method was used to examine the fracture process in the laser heating experiment. It w … More as shown from the AE monitoring that the buckling of the top coating layer induced the final spallation of the TBC system. Furthermore, the effect of high-temperature oxidation on the spallation was evaluated in terms of the thermal gradient within the TBC and the number of cycles to failure.(2-2) Thermal stress analyses using a FEM method were performed with reference to the cylindrical specimen geometry. The interface crack was accounted for in the thermal stress analyses. The stress intensity factor was determined as a function of interfacial crack length which formed a foundation for the analysis of the spallation behavior of the TBCs.Task (3) The experimental data of interface crack growth obtained from the laser heating thermal shock/fatigue tests were used to produce the fracture mechanics based relationship of fatigue crack growth rate through the interfacial crack stress intensity factor as determined by the FEM, The relationship was then used to reproduce the fracture process in the laser heating experiment. It was demonstrated that the predicted critical interfacial crack length was close to that observed in the laser heating experiment, indicating the validity of the fracture mechanics based life predictive method. Less
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河 済昌,橋田俊之,庄子哲雄,河合久孝,佐藤 実,橋本英雄: "遮熱セラミックスコーティングの界面破壊特性に及ぼす高温酸化の影響に関する研究" 日本機械学会 第75期通常総会講演会講演論文集(II). No.98-1. 652-653 (1998)
Sashimasa Kawa、Toshiyuki Hashida、Tetsuo Shoko、Hisataka Kawai、Minoru Sato、Hideo Hashimoto:“高温氧化对热障陶瓷涂层界面断裂性能的影响研究”日本学会第75届常会会议记录机械工程师(II)第 98-1 号(1998 年)。
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作者:
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通讯作者:
T.Hashida, S.Jian, H.Takahashi, K.Fujii, M.Kanazawa, H.Yamamoto: Life Predictive Method Based on Interfacial Fracture Mechanics for Gas Turbine Thermal Barrier Coating Systems. Yosya, (in press), (1999)
T.Hashida、S.Jian、H.Takahashi、K.Fujii、M.Kanazawa、H.Yamamoto:基于界面断裂力学的燃气轮机热障涂层系统寿命预测方法。
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通讯作者:
河 済昌, 橋田俊之, 庄子哲雄, 河合久孝, 佐藤 実, 橋本英雄: "遮熱セラミックスコーティングの界面破壊特性に及ぼす高温酸化の影響に関する研究" 日本機械学会 第75期通常総会講演会. (発表予定). (1998)
Sashimasa Kawa、Toshiyuki Hashida、Tetsuo Shoko、Hisataka Kawai、Minoru Sato、Hideo Hashimoto:“高温氧化对热障陶瓷涂层界面断裂性能的影响研究”在日本学会第75届常务大会上的演讲机械工程师。(演示)(1998)
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橋田俊之,簡 春雲,高橋秀明,藤井弘二,金沢 基,山本 弘: "界面破壊力学に基づくガスタービン翼用遮熱セラミックコーティングの耐久性能に関する研究" 溶射. 印刷中. (1999)
Toshiyuki Hashida、Haruun Kan、Hideaki Takahashi、Koji Fujii、Hajime Kanazawa、Hiroshi Yamamoto:“基于界面断裂力学的燃气轮机叶片热障陶瓷涂层的耐久性能研究”热喷涂(1999)。
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通讯作者:
J.Ha, T.Hashida, T.Shoji, H.Kawai, M.Sato, H.Hashimoto: "Influence of High Temperature Oxidation on Interfacial Fracture in Thermal Barrier Coatings" Proceedings of The 75th JSME Spring Annual Meeting (II). [No.98-1]. 652-653 (1998)
J.Ha、T.Hashida、T.Shoji、H.Kawai、M.Sato、H.Hashimoto:“高温氧化对热障涂层界面断裂的影响”第75届JSME春季年会论文集(二)。
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共 8 条
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负责人:HASHIDA Toshiyuki
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海外基金