Interface failure analysis of thermal barrier coatings under CMAS penetration

被引:0
|
作者
Zhang Z. [1 ]
Han Y. [2 ]
Wang W. [1 ]
Cai Z. [1 ]
机构
[1] School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai
[2] Shanghai Branch China Petroleum Pipeline Engineering Corporation, Shanghai
来源
关键词
Calcium; magnesium; aluminum; silicon and other oxides; Coating modification; Interface strength; Thermal barrier coating; Thermally growth oxide;
D O I
10.13224/j.cnki.jasp.20200374
中图分类号
学科分类号
摘要
Influences of different calcium, magnesium, aluminum, silicon and other oxides (CMAS) penetration depths under the influences of temperature gradients and the influences of the interface roughness on the interface temperature distribution under CMAS penetration were considered based on the influences of penetration on the properties of the ceramic layer of the thermal barrier coating (TC).The influences of thermally growth oxide (TGO) thickness and interfacial stress behavior were also studied.The results showed that the penetration of CMAS increased the thermal conductivity of the ceramic layer, which further increased the interface temperature, the thickness of TGO, and also made the stress state of the interface more serious.The increase of the interface roughness led to an increase in the temperature difference between the peaks and valleys of the interface, the uneven growth of the interface TGO, and finally caused the change of the stress distribution of the interface. © 2021, Editorial Department of Journal of Aerospace Power. All right reserved.
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页码:1702 / 1711
页数:9
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共 27 条
  • [1] PADTURE N P, GELL M, JORDAN E H., Thermal barrier coatings for gas-turbine engine applications[J], Science, 296, 5566, pp. 280-284, (2002)
  • [2] CLARKE D R, OECHSNER M, PADTURE N P., Thermal-barrier coatings for more efficient gas-turbine engines, MRS (Materials Research Society) Bulletin, 37, 10, pp. 891-898, (2012)
  • [3] SCHLICHTING K W, PADTURE N P, JORDAN E H, Et al., Failure modes in plasma-sprayed thermal barrier coatings, Materials Science and Engineering:A, 342, 1, pp. 120-130, (2003)
  • [4] CHEN W R, ZHAO L R., Review-volcanic ash and its influence on aircraft engine components, Procedia Engineering, 99, pp. 795-803, (2015)
  • [5] DREXLER J M, GLEDHILL A D, SHINODA K, Et al., Jet engine coatings for resisting volcanic ash damage, Advanced Materials, 23, 21, pp. 2419-2424, (2011)
  • [6] KAKUDA T R, LEVI C G, BENNETT T D., The thermal behavior of CMAS-infiltrated thermal barrier coatings, Surface and Coatings Technology, 272, pp. 350-356, (2015)
  • [7] KRAMER S, YANG J, LEVI C G., infiltration-inhibiting reaction of gadolinium zirconate thermal barrier coatings with CMAS melts[J], Journal of the American Ceramic Society, 91, 2, pp. 576-583, (2008)
  • [8] WIESNER V L, BANSAL N P., Mechanical and thermal properties of calcium-magnesium aluminosilicate (CMAS) glass[J], Journal of the European Ceramic Society, 35, 10, pp. 2907-2914, (2015)
  • [9] WU Yiyou, LUO Hua, CAI Canying, Et al., Comparison of CMAS corrosion and sintering induced microstructural characteristics of APS thermal barrier coatings, Journal of Materials Science and Technology, 35, 3, pp. 440-447, (2019)
  • [10] KRAMER S, FAULHABER S, CHAMBERS M, Et al., Mechanisms of cracking and delamination within thick thermal barrier systems in aero-engines subject to calcium-magnesium-alumino-silicate (CMAS) penetration[J], Materials Science and Engineering:A, 490, 1, pp. 26-35, (2008)