Thermodynamic Study on Equilibrium Phases in Nickel-Base Single Crystal Superalloys

Article Preview

Abstract:

In order to improve the composition and microstructure of nickel-base single crystal superalloys, equilibrium phases of third generation single crystal superalloys RenéN6 and CMSX-10 have been researched by using thermodynamic calculation software JMatPro. The calculated results indicated that the two superalloys have the same equilibrium phases, such as liquid phase, γ phase, γ’ phase and TCP (topologically close-packed phases), however, there are differences in the quantity and temperature range. RenéN6 alloy has higher content of μ phase. And CMSX-10 alloy has higher γ’ phase precipitation temperature and more γ’ phase precipitates.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

149-154

Citation:

Online since:

January 2019

Authors:

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2019 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] D.A. Ford, R.P. Arthey, Development of single crystal alloys for specific engine applications, Superalloys1984, Seven springs, PA: TMS, 1984: 115-124.

DOI: 10.7449/1984/superalloys_1984_115_124

Google Scholar

[2] T. Khan, P. Caron, Development of a new single crystal superalloy for industrial gas turbine blades, High temperature materials for power engineering, Liege, Belgium, 1990: 1261-1270.

Google Scholar

[3] P. Caron, D. Comu, T. Khan, Development of a hydrogen resistant superalloy for single crystal blade application in rocket engine turbopumps, Superalloys1996, PA: TMS, 1996: 53-60.

DOI: 10.7449/1996/superalloys_1996_53_60

Google Scholar

[4] S. Walston, A. Cetel, R. MacKay, Joint development of a fourth generation single crystal superalloy, Superalloy2004, Seven springs, PA: TMS, 2004: 15-24.

DOI: 10.7449/2004/superalloys_2004_15_24

Google Scholar

[5] W. Schneide, J. Hammer, H. Mughrabi, Creep deformation and rupture behavior to the monocrystalline superalloy, Superalloys1992, Seven springs, PA: TMS, 1992: 589-598.

Google Scholar

[6] F.R.N. Nabarro, The superiority of superalloys, Mater. Sci. Eng. 184 (1994) 167-171.

Google Scholar

[7] W.R. Walston, U.S. Patent 5,270,123. (1993).

Google Scholar

[8] C.M. Auslin, U.S. Patent 5,151,249. (1992).

Google Scholar

[9] J.J. Jackson, M.J. Domachie, R.J. Henrich, The volume percent of fine γ' on creep in Mar-M200+Hf, Metall Trans. 8A (1977) 1615-1618.

Google Scholar

[10] M. Gell, D.N. Duhl, A.F. Giamei, The development of single crystal superalloy turbine blades, Superalloys1980, PA: TMS, 1980: 205-214.

DOI: 10.7449/1980/superalloys_1980_205_214

Google Scholar

[11] M.J. Goulette, The future costsless-high temperature materials form an aeroengineer prospective, Superalloys1996, Seven springs, PA: TMS, 1996: 3-6.

Google Scholar

[12] K. Harris, G.L. Erickson, U.S. Patent 4, 582, 548. (1986).

Google Scholar

[13] E.W. Ross, K.S. O'Hara, RenéN4: a first generation single crystal turbine airfoil alloy with improved oxidation resistance, low angle boundary strength and superior long time rupture strength, Superalloys1996, Seven spring, PA: TMS, 1996: 19-25.

DOI: 10.7449/1996/superalloys_1996_19_25

Google Scholar

[14] T. Khan, Recent developments and potential of single crystal superalloys for advanced turbine blades, High Temepature Alloys for Gas Turbines and Other Applications 1986, D. Reidel Publishing Company, Dordrecht, Holland, 1986: 21-50.

Google Scholar

[15] G.L. Erickson, The development of the CMSX-11 alloy for industrial gas turbine application, Superalloys1996, Seven springs, PA: TMS, 1996: 45-52.

Google Scholar

[16] A.D. Cetel, D.N. Duhl, Second generation nickel-base single crystal superalloy, Superalloys1988, Seven springs, PA: TMS, 1988: 235-244.

DOI: 10.7449/1988/superalloys_1988_235_244

Google Scholar

[17] K. Harris, G.L. Erickson, U.S. Patent 4, 634, 782. (1987).

Google Scholar

[18] C.S. Wukusick, L. Buchakjian, U.K. Patent 2, 235, 697. (1991).

Google Scholar

[19] X. Nguyen-Dinh, U.S. Patent 4,935,072. (1990).

Google Scholar

[20] G.L. Erickson, The development and application of CMSX-10, Superalloys1996, Seven springs, PA: TMS, 1996: 35-44.

Google Scholar

[21] W.S. Walston, K.S. O'Hara, E.W. Ross, RenéN6-third generation single crystal superalloy, Superalloys1996, Seven springs, PA: TMS, 1996: 27-34.

Google Scholar

[22] J.R. Li, D.Z. Tang, R.L. Lao, Effects of rhenium on creep rupture life of a single crystal superalloys, J. Mat. Sci. & Tech. 15 (1999) 53-57.

Google Scholar

[23] N. Saunders, Z. Guo, X. Li, Using JMatPro to model materials properties and behavior, J. Met. 55 (2003) 60-65.

Google Scholar