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Effect of Rhenium Addition on Isothermal Oxidation Behavior of Tribaloy T-800 Alloy 被引量:3

铼对Tribaloy T-800合金等温氧化行为的影响(英文)
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摘要 The effects of 4 wt% rhenium (Re) addition on isothermal oxidation behavior of Tribaloy T-800 alloy have been studied at 800 °C and 1 000 °C in air. At 800 °C,T-800 shows nonuniform oxidation between dendritic and eutectic areas. Re addition clearly promotes the nonuniform oxidation,leading to considerably higher mass gains than that of T-800 at this temperature. At 1 000 °C exposure,the thickness of scale on T-800 increases significantly,accompanied by severe scale spallation during cooling to room temperature. On the contrary,T-800Re shows a marked decrease of oxide growth rate compared to the linear one of T-800 at 1 000 °C. The scale adhesion is also improved with Re addition at this higher temperature. Therefore,the role of Re depends on the exposure temperature. Re addition gives high oxidation rate at 800 °C,however,the excellent oxidation resistance is obtained by the addition of Re at a higher temperature of 1 000 °C. The effects of 4 wt% rhenium (Re) addition on isothermal oxidation behavior of Tribaloy T-800 alloy have been studied at 800 °C and 1 000 °C in air. At 800 °C,T-800 shows nonuniform oxidation between dendritic and eutectic areas. Re addition clearly promotes the nonuniform oxidation,leading to considerably higher mass gains than that of T-800 at this temperature. At 1 000 °C exposure,the thickness of scale on T-800 increases significantly,accompanied by severe scale spallation during cooling to room temperature. On the contrary,T-800Re shows a marked decrease of oxide growth rate compared to the linear one of T-800 at 1 000 °C. The scale adhesion is also improved with Re addition at this higher temperature. Therefore,the role of Re depends on the exposure temperature. Re addition gives high oxidation rate at 800 °C,however,the excellent oxidation resistance is obtained by the addition of Re at a higher temperature of 1 000 °C.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2010年第3期370-376,共7页 中国航空学报(英文版)
关键词 RHENIUM co-based alloy Tribaloy T-800 high temperature OXIDATION rhenium co-based alloy Tribaloy T-800 high temperature oxidation
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  • 1Halstead A, Rawlings R D. Structure and hardness of Co-Mo-Cr-Si wear resistant alloys (Tribaloys). Metal Science 1984; 18(10): 491-500.
  • 2Bolelli G, Cannillo V, Lusvarghi L, et al. Microstructural and tribological comparision of HVOF-sprayed and post-treated M-Mo-Cr-Si (M=Co, Ni) alloy coatings. Wear 2007; 263(7-12): 1397-1416.
  • 3Navas C, Cadenas M, Cuetos J M, et al. Microstructure and properties of Tribaloy T-800 coatings deposited by laser cladding. Boletin De La Sociedad Espanola De Ceramica Y Vidrio 2004; 43(2): 319-322.
  • 4Navas C, Cadenas M, Cuetos J M, et al. Microstructure and sliding wear behavior of Tribaloy T-800 coatings deposited by laser cladding. Wear 2006; 260(7-8): 838-846.
  • 5Tobar M J, Amado J M, Alvarez C, et al. Characteristics of Tribaloy T-800 and T-900 coatings on steel substrates by laser cladding. Surface and Coatings Technology 2008; 202(11): 2297-2301.
  • 6Xie Y J, Wang M C, Zhang G, et al. Analysis of superalloy turbine blade tip cracking during service. Engineering Failure Analysis 2006; 13(8): 1429-1436.
  • 7Gurrappa I, Rao A S. Thermal barrier coatings for enhanced efficiency of gas turbine engines. Surface and Coatings Technology 2006; 201(6): 3016-3029.
  • 8Pomeroy M J. Coatings for gas turbine materials and long term stability issues. Materials and Design 2005; 26(3): 223-231.
  • 9Wright I G, Gibbons T B. Recent developments in gas turbine materials and technology and their implications for syngas firing. International Journal of Hydrogen Energy 2007; 32(16): 3610-3621.
  • 10Czech N, Schmitz F, Stamm W. Improvement of MCrAlY coatings by addition of rhenium. Surface and Coatings Technology 1994; 68-69: 17-21.

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  • 5Haynes J A, Lance M J, Pint B A, Wright I G. Char- acterization of commercial EB-PVD TBC systems with CVD (Ni,Pt)AI bond coatings [J]. Surf. Coat. Techn- ol. , 2001 , 146-147 : 140.
  • 6Sadowski T, Golewski P. Multidisciplinary analysis of the operational temperature increase of turbine blades in combustion engines by application of the ceramic thermal barrier coatings (TBC) [ J ]. Comp. Mater. Sci. , 2011, 50(4) : 1326.
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  • 10Sohn Y H, Kim J H, Jordan E H, Gell M. Thermal cycling of EB-PVD/MCrA1Y thermal barrier coatings: I Microstructural development and spallation mechanisms [J]. Surf. Coat. Technol. , 2001, 146-147: 70.

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