METALS AND METAL MATRIX COMPOSITES |
|
|
|
|
|
Effect of TBCs on Gas Thermal Corrosion Resistance and Mechanical Properties of DD6 Single Crystal |
WANG Yufeng1,2,*, FU Qiangang1,*, YANG Jun3, ZHANG Hua2, YANG Yan2
|
1 National Elite Institute of Engineering, Northwestern Polytechnical University, Xi’an 710072, China 2 AECC Aviation Power Co., Ltd., Xi’an 710021, China 3 The Military Representative Office of the Air Force Equipment Department in Xi’an, Xi’an 710021, China |
|
|
Abstract DD6 single crystal high-temperature alloy material has a very broad application prospect in the field of multi type aviation engine manufacturing in China due to its excellent high-temperature service performance. With the continuous development of aviation engine technology in China, the service temperature of the combustion chamber turbine is constantly increasing. DD6 single crystal superalloy cannot fully meet the service environment of high temperature, high pressure, and high speed, and there is an urgent need to research DD6 single crystal surface thermal barrier coating technology. In view of this, this article uses multi arc ion plating technology to prepare NiCoCrAlY metal bonding layer on DD6 single crystal high-temperature alloy, and then uses electron beam physical vapor deposition technology to prepare Y2O3·ZrO2 ceramic surface layer, to study the effect of thermal barrier coating on the gas thermal corrosion resistance and mechanical properties of DD6 single crystal. The results indicate that, after 100 hours of gas hot corrosion performance testing at 900 ℃, a thickness of approximately 100 μm corrosion porosity, pores, and transverse cracks was formed on the surface of DD6. There were no corrosive elements such as Na, K, Ca, Cl, S present inside the BC coating or YSZ coating. A uniform and continuous Al2O3 layer was formed on the surface of the BC coating, and the Na2SO4 adhered to its surface did not undergo high-temperature decomposition. The corrosive medium did not corrode the BC coating. The YSZ coating columnar crystals have good strain tolerance. At high temperatures, the expansion of columnar crystals leads to a reduction in the gap between columnar crystals, and external corrosion media cannot effectively penetrate into the interior of YSZ coating, thus avoiding corrosion damage to the coating or substrate caused by corrosion media. Tensile strength of thermal barrier coating on DD6 single crystal alloy at 980 ℃, there is no adverse effects onσb,σ0.2,δ and ψ, and the fracture mode of the sample is basically consistent. High temperature endurance time and elongation of DD6 single crystal sample coated with thermal barrier coating at 980 ℃,250 MPa, there is no significant difference, and the fracture has a typical dimple fracture morphology, with the fracture mechanism being a ductile fracture mechanism of plastic deformation and creep deformation. Based on the research results of this work, the technical support for the technical development and engineering application of DD6 single crystal super alloy TBCs is established.
|
Published:
Online: 2024-10-12
|
|
Fund:This work was financially supported by the Science and Technology Major Project (2017-Ⅶ-0007-0100). |
|
|
1 Padture N P, Gell M, Jordan Eric H. Science, 2002, 296, 280. 2 Darolia R. International Materials Reviews, 2013, 58, 315. 3 He L M. High temperature protective coating, National Defense Industry Press, China, 2012, pp.21(in Chinese). 何利民. 高温防护涂层技术, 国防工业出版社, 2012, pp.21. 4 Li M H, Sun X F, Zhang C Y, et al. Rare Metal Materials and Engineering, 2004, 33(1), 55(in Chinese). 李美姮, 孙晓峰, 张重远, 等. 稀有金属材料与工程, 2004, 33(1), 55. 5 Li L, Duan L, Qin Gehua. Journal of Functional Materials, 2017, 48(2), 2084(in Chinese). 李磊, 段力, 秦格华. 功能材料, 2017, 48(2), 2084. 6 Dmitry N, Vladimir S, Lorenz S, et al. Journal of Materials Science, 2009, 44, 1687. 7 Shayan A, Eric H J. Surface & Coatings Technology, 2014, 244, 109. 8 Nath S, Manna I, Dutta M, et al. Corrosion Science, 2014, 88, 10. 9 Shi Z X, Liu S Z, Wang X G, et al. Journal of Iron and Steel Research, 2015, 27(5), 61(in Chinese). 史振学, 刘世忠, 王效光, 等. 钢铁研究学报, 2015, 27(5), 61. 10 Obrtlik K, Pospisilova S, Julis M, et al. Procedia Engineering, 2011, 10, 1360. 11 Itoh Y, Saitoh M, Takaki K, et al. Fatigue & Fracture of Engineering Materials & Structures, 2001, 24, 843. 12 Li J R, Zhong Z G, Tang D Z, et al. In:Superalloys. Seven Springs, 2000, pp.777. |
[1] |
ZHAO Yunsong, ZHANG Mai, DAI Jianwei, GUO Huiming, SUN Zhijun, GUO Yuanyuan, ZHANG Jian, HUA Yinqun, HUO Kun, DAI Fengze. Research Progress of Thermal Barrier Coatings for Aeroengine Turbine Blades[J]. Materials Reports, 2023, 37(6): 21040168-7. |
|
|
|
|