Future use of gamma titanium aluminides by Rolls-Royce

Aircraft Engineering and Aerospace Technology

Volumn 71, Issue 4, 1999, Pages 337-340

  Voice, Wayne ^a  

^a ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINE MANUFACTURE; AIRCRAFT ENGINES; COMBUSTORS; COMPOSITION; CREEP; MACHINING; METAL CASTINGS; METALLOGRAPHIC MICROSTRUCTURE; OPTIMIZATION; STRENGTH OF MATERIALS; TURBINES;

AEROENGINE COMPONENTS; DESIGN CRITERIA; GAMMA TITANIUM ALUMINIDES;

TITANIUM ALLOYS;

EID: 0032682559     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022669910371031     Document Type: Article

References (7)

1. Cheng, T.T. (in press), "The effects of thermal exposure on the microstructure and properties of a γ-TiAI based alloy containing 44AI-4Nb-4Zr-0.2Si-0.3B", Intermetaltics.
2. Cheng, T.T. and Jones, I. (undated), "TiAI alloys", European Patent Publication Number 0889143A1.
3. Cheng, T.T. and Willis, M.R. (1998), "Effects of ageing on the microstructure and creep properties of γ-TiAI containing heavy alloying", Scripta Materialia, Vol. 39 No. 9, pp. 1255-65.
4. Cheng, T.T., Willis, M.R. and Jones, I.P. (1999), "Effects of major alloying additions on the microstructure and mechanical properties of γ-TiAI", Intermetallics, Vol. 7, pp. 89-99.
5. Crofts, P.D. (1997), "The creep behaviour of lamellar based TiAI alloys", PhD thesis, The University of Birmingham, p. 132.
6. Jeon, J.-H. et al. (1998), "Recrystallisation in cast Ti-45-2-2-XD titanium aluminide during hot isostatic pressing", to be published.
7. Perrin, I.J. (1997), "Design approaches for gamma-titanium aluminides", Proceedings of the 4th International Charles Parsons Turbine Conference, The Institute of Materials, pp. 148-58.