Study on Delamination Fatigue Strength of Thermal Barrier Coating at Elevated Temperature
Study on Delamination Fatigue Strength of Thermal Barrier Coating at Elevated Temperature
批准号:
20560087
负责人:
KANEKO Kenji
金额:
$3.08万
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2008
资助国家:
日本
项目状态:
已结题
起止时间:
2008 至 2010
中文摘要
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英文摘要
In this study, it is investigated experimentally and analytically that fracture process and fatigue behavior of Thermal Barrier Coatings (TBCs) used in a high temperature component in a land based gas turbine. The effects of the thermal load on TBCs and delamination strength are investigated by measuring residual stress of top coat, using the finite element method and various cyclic shearing, tensile and torsion tests.It is found that (1)the TGO layer thickness increases with increasing heating time for both cases of 900 and 1000℃, and it saturates gradually after 20 hours for the both cases. (2)A delamination of top coat under thermal load occurs at a peak of undulation in top coat and bond coat interface. This is because that tensile tearing stress which is normal to the interface occurs at the peak area after cooling. So, about failure patterns of TBCs, we can find two patterns, the first one is that a crack initiates at TC surface and propagates in the thickness direction. After th … More e crack arrives near the interface, a delamination occurs at the interface and grows. Another pattern is that a local delamination can be observed without any crack grown from the TC surface. In the both cases, it is observed that delaminations run from a peak to peak of undulation of BC near the interface. (3)It is found that the mechanical property of bond coat changes after thermal aging and the shear fatigue behavior of TBCs is affected by bond coat strength. (4) Delamination energy increases quickly with increasing heating time up to 40 hours and then decreases slightly. So, the delamination strength of TC is thought to decrease apparently after long time heating. This is because that residual stress in TC increases and so elastic strain energy increases with increasing heating time. (5) Softening of BC caused by long heating makes fatigue life of TBCs small.(6)We can find that the shearing using small plating specimens gives reliable data with small scatter bands on delamination strength. (7)Also, the torsion pin-test was found to be a good method which obtains a delamination strength of thermal sprayed coating under combined shearing with tensile stresses. Less
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DOI:
--
发表时间:
2010
期刊:
Journal of Solid Mechanics and Materials Engineering 4
影响因子:
--
作者:
[金子堅司・大森明]
通讯作者:
金子堅司・大森明
Study on Shear Fatigue Fracture and Delamination Mechanism of Thermal Barrier Coatings After Thermal Loadine
热障涂层热负荷后剪切疲劳断裂及分层机理研究
DOI:
--
发表时间:
2010
期刊:
Journal of Solid Mechanics and Materials Engineering 4
影响因子:
--
作者:
[金子堅司・大森明, 金子堅司・高藤聡・榎本和城, 金子堅司・高藤聡・榎本和城, 金子堅司・高藤聡・榎本和城, 金子堅司, 金子堅司・高藤聡・榎本和城]
通讯作者:
金子堅司・高藤聡・榎本和城
遮熱被膜の高温におけるはく離発生および進展挙動に関する研究
高温下热障涂层剥离发生及扩展行为研究
DOI:
--
发表时间:
2010
期刊:
影响因子:
--
作者:
[金子堅司・大森明, 金子堅司・高藤聡・榎本和城, 金子堅司・高藤聡・榎本和城, 金子堅司・高藤聡・榎本和城, 金子堅司, 金子堅司・高藤聡・榎本和城, 金子堅司, 金子堅司・大矢将人, 金子堅司・檜垣圭太朗, 金子堅司・近藤英明]
通讯作者:
金子堅司・近藤英明
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作者:
[]
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ねじりピンテスト法による溶射被膜の付着強度評価に関する研究
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DOI:
--
发表时间:
2011
期刊:
影响因子:
--
作者:
[金子堅司, 檜垣 圭太朗,野澤 利恵]
通讯作者:
檜垣 圭太朗,野澤 利恵
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Three-dimensional visualization of age-hardening process by multi-dimensional electron microscopy
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Influence of Oxidation and Thermal Cycling on Bonding Strength of Thermal Barrier Coating at Elevated Temperature
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Characteristics of Rotating stall in High Specific Speed diagonal Flow Fan and Suppression of Rotating Stall
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依托单位:
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