The contribution of advanced high-temperature materials to future aero-engines

Proceedings of the Institution of Mechanical Engineers Part L: Journal of Materials: Design and Applications

Volumn 215, Issue 2, 2001, Pages 63-73

  Winstone, M R ^a   Partridge, A ^b   Brooks, J W ^b  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

^b QINETIQ   (United Kingdom)

Author keywords

Advanced high temperature materials; Future aero engines; Performance

Indexed keywords

EID: 0010251878     PISSN: 14644207     EISSN: None     Source Type: Journal    
DOI: 10.1177/146442070121500201     Document Type: Article

References (32)

1. Husniaux, A. Life cycle cost - an introduction. In Design for Low Cost Operation and Support, RTO-MP-37, 2000 (NATO Research and Technical Organisation, Paris).
2. Goulette, M. J. The future costs less - high temperature materials from an aero-engine perspective. In Superalloys 1996, 1996, pp. 3-6 (Metallurgical Society of AIME, Warrendale, Pennsylvania).
3. Ford, D. A. Impact of second generation single crystal superalloys on foundry technology. Proc. Instn Mech. Engrs, Part G, Journal of Aerospace Engineering, 1996, 210(G2), 147-155.
4. Caron, P. and Khan, T. Third generation superalloys for single crystal blades. In Materials for Advanced Power Engineering, Part II, 1998, p. 897 (Kluwer Academic, Dordrecht, The Netherlands).
5. Proceedings of the Thermal Barrier Coating Workshop, NASA Conference Publication 3312, 1995.
6. Morrell, P. and Rickerby, D. S. Advantages/disadvantages of various TBC systems as perceived by the engine manufacturer. In Thermal Barrier Coatings, NATO AGARD Report 823, 1998, Paper 20.
7. Nicholls, J. R., Lawson, K. J., Rickerby, D. S. and Morrell, P. Advanced processing of TBC's for reduced thermal conductivity. In Thermal Barrier Coatings, NATO AGARD Report 823, 1998, Paper 6.
8. Dalby, S., Tong, J. and Byrne, J. Effects of loading waveform on fatigue crack growth at elevated temperature in nickel-base superalloys. In COMPASS 1999, Swansea, 1999, p. 371.
9. Austin, C. M., Kelly, T. J., McAllister, K. G. and Chestnut, J. C. Aircraft engine applications for gamma titanium aluminide. In Proceedings of the International Symposium on Structural Intermetallic, 1997, p. 413 (Metallurgical Society of AIME, Warrendale, Pennsylvania).
10. Partridge, A. and Winstone, M. R. Gamma titanium aluminide alloys: current status and future potential. In Advances in Turbine Materials, Design and Manufacturing, Proceedings of the Fourth International Charles Parsons Turbine Conference, 1997, p. 358.
11. Larsen, J. M., Worth, B. D., Balsone, S. J. and Rosenberger, A. H. Reliability issues affecting the implementation of gamma titanium aluminides. In Titanium '95: Science and Technology, 1995, pp. 113-120.
12. Perrin, I. J. Design approaches for gamma titanium aluminide alloys. In Advances in Turbine Materials. Design and Manufacturing, Proceedings of the Fourth International Charles Parsons Turbine Conference, 1997, p. 148.
13. Dolley, E. J., Ashbaugh, N. E. and Worth, B. D. Isothermal high cycle fatigue of a Ti-46.5AI-3.0Nb-2.1Cr-0.2W gamma titanium aluminide. In Proceedings of the Sixth International Fatigue Congress, Berlin, Germany, 1996, p. 1755 (Pergamon, Oxford).
14. Kumpfert, J. and Leyens, C. Microstructure evolution, phase transformations and oxidation of an orthorhombic titanium aluminide alloy. In Proceedings of the International Symposium on Structural Intermetallics, 1997, pp. 895-904 (Metallurgical Society of AIME, Warrendale, Pennsylvania).
15. Ward-Close, C. M., Godfrey, S. P. and Robertson, J. G. Titanium MMC's - design and manufacturing. In Proceedings of the European Materials Conference (EUROMAT), 1999 (in press).
16. Botton, G. A., Guo, G. Y., Temmerman, W. M. and Humphreys, C. J. Phys. Rev. B, 1996, 54, 1682-1691.
17. Saunders, N. Phil. Trans. R. Soc. Lond. A, 1995, 351, 543-561.
18. Fox, S. P. and Neal, D. F. The role of computer modelling in the development of large scale primary forgings of titanium alloys. In Titanium 95 - Science and Technology, 1996, pp. 628-635 (Institute of Materials, London).
19. Dandre, C. A., Roberts, S. M., Evans, R. W. and Reed, R. C. Microstructural evolution of INCONEL 718 during ingot breakdown; process modelling and evaluation. Mater. Sci. Technol., 2000, 16, 14-25.
20. Brooks, J. W. Thermomechanical processing in theory, modelling and practice. Swed. Soc. Mater. Technol., 1997, 52, 52-77.
21. Brooks, J. W., Dean, T. A., Hu, Z. M. and Wey, E. Three dimensional finite element modelling of a titanium aluminide aerofoil forging. J. Mater. Processing Technol., 1998, 20, 149-155.
22. Blackwell, P. L., Brooks, J. W. and Bate, P. S. J. Mater. Sci. Technol., 1998, 14, 1181-1188.
23. Flower, H. M. Mater. Sci. Technol., 1990, 6, 1082.
24. Sabin, T. J., Bailer-Jones, C. A. L., Roberts, S. M. and Withers, P. J. In Proceedings of the International Conference ICFT 1998, 1998, p. 411 (Professional Engineering Publishing Limited, London).
25. Homewood, T., Ward, T. J., Henderson, M. B. and Harrison, G. F. The DERA slip system creep law for the modelling of face centred cubic single crystal material behaviour. In Proceedings of the Conference on The Modelling of Microstructural Evolution in Creep Resistant Materials, Imperial College, London, 1998, pp. 273-292.
26. McElhone, M. The hollow wide chord fan blade (WCFB): a stiffened metallic structure. In Proceedings of the Symposium on Designing High Performance Stiffened Structures, 1999 (Professional Engineering Publishing Limited, London).
27. Dean, A. J., Corman, G. S., Bagepalli, B., Luthra, K. L., DiMascio, P. S. and Orenstein, R. M. Design and testing of CFCC shroud and combusted components. In Proceedings of the International Gas Turbine and Aero-Engine Congress, Indianapolis, Indiana, 1999, p. 235 (American Society of Mechanical Engineers, New York).
28. Lee, K. N. Key durability issues with mullite-based environmental barrier coatings for Si-based ceramics. In Proceedings of the International Gas Turbine and Aeroengine Congress, Indianapolis, Indiana, 1999, p. 443 (American Society of Mechanical Engineers, New York).
29. Berczik, D. M. US Pat. 5,176,762, 5 January 1993.
30. Li, Y. G., Zhang, X. D., Blenkinsop, P. A., Saunders, N., Walker, N. A., Spilling, P. D. and Small, C. The development and evaluation of β titanium alloys for aerospace applications. In Titanium '95: Science and Technology, 1995, pp. 2317-2324 (Institute of Materials, London).
31. Li, Y. G., Blenkinsop, P. A., Loretto, M. H., Rugg, D. and Voice, W. Effect of carbon and oxygen on the mechanical properties of Tl-25V-15Cr-2Al alloys. Acta Mater., 1999, 47, 2889-2905.
32. Harrison, G. F. and Weaver, M. J. Life assessment of fracture critical aeroengine parts. In Engineering Against Fatigue (Eds J. H. Beynon, M. W. Brown, R. A. Smith, T. C. Lindley and B. Tomkins), 1999 (A. A. Balkema, Rotterdam).