Aero-engine titanium from alloys to composites

Materials Science Forum

Volumn 618 619, Issue , 2009, Pages 127-134

  Doorbar, Phill ^a   Dixon, Mark ^a   Chatterjee, Amit ^b  

^a ROLLS ROYCE PLC   (United Kingdom)

^b ROLLS ROYCE CORPORATION   (United States)

Author keywords

Aero engine; Composites; Titanium

Indexed keywords

AIRCRAFT ENGINES; ALUMINUM ALLOYS; BINARY ALLOYS; BONDING; CERAMIC MATERIALS; COMPOSITE MATERIALS; CREEP; CREEP RESISTANCE; ENGINES; HIGH STRENGTH ALLOYS; INDUSTRIAL RESEARCH; INTERMETALLICS; LIGHT METALS; METALLIC MATRIX COMPOSITES; NIOBIUM ALLOYS; REINFORCEMENT; TERNARY ALLOYS; TITANIUM; TITANIUM CASTINGS; URANIUM ALLOYS;

AERO-ENGINE; APPLICATION DEVELOPMENT; COMPOSITIONAL CONTROL; INTERMEDIATE TEMPERATURES; INTERMETALLIC MATERIALS; INTERMETALLIC SYSTEMS; MODERATE TEMPERATURE; TEMPERATURE CAPABILITY;

TITANIUM ALLOYS;

EID: 70349496398     PISSN: 02555476     EISSN: 16629752     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/MSF.618-619.127     Document Type: Conference Paper

References (4)

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2. Voice, W. (1997) 'The future use of gamma titanium aluminides', Aircraft Engineering and Aerospace Technology, 1997, Vol. 71, Issue 4, 337-340.
3. Hu, D. et al. (2007) 'Designing TiAl alloys to transform massively during slow cooling', 2007, Proceedings of 11th World Titanium Conference, Ti-2007, 1317-1320.
4. Chatterjee, A., Brown, L.E., Roessler, J.R, Heitman P.W. and Richardson, G.E. (1997), Proceedings of the Second International Symposium of Structural Intermetallics, M. V. Nathal et al eds. Sept 1997, 903-912