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Material and component investigations on a Ti-6-4 fittingelement

Published online by Cambridge University Press:  04 November 2011

Wen Tan ,
Michael Stoschka ,
Martin Riedler ,
Wilfried Eichlseder ,
Fernando Romagnoli  and
Vinícius Rondon
Wen Tan*
Affiliation:
Christian Doppler Laboratory for Fatigue Analysis, Franz-Josef-Str. 18, 8700 Leoben, Austria
Michael Stoschka*
Affiliation:
Chair of Mechanical Engineering, Montanuniversität Leoben, Franz-Josef-Str. 18, 8700 Leoben, Austria
Martin Riedler
Affiliation:
Böhler Schmiedetechnik GmbH & Co KG, Mariazeller Strasse 25, 8605 Kapfenberg, Austria
Wilfried Eichlseder
Affiliation:
Christian Doppler Laboratory for Fatigue Analysis, Franz-Josef-Str. 18, 8700 Leoben, Austria Chair of Mechanical Engineering, Montanuniversität Leoben, Franz-Josef-Str. 18, 8700 Leoben, Austria
Fernando Romagnoli
Affiliation:
EMBRAER Brasileira de Aeronautica S.A, Av. Brigadeiro Faria Lima 2170, São José dos Campos, Brasil
Vinícius Rondon
Affiliation:
EMBRAER Brasileira de Aeronautica S.A, Av. Brigadeiro Faria Lima 2170, São José dos Campos, Brasil
*
aCorresponding author:[email protected]
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Abstract

An improvement in the life time calculation is aspired by the characterisation of thelife time behaviour of a typically lightweight aircraft titanium alloy by describing themicrostructure. Therefore, extensive research on a Ti-6-4 fitting element has been carriedout. In addition to static tensile tests, rotating bending tests and fracture mechanicaltests, component tests with constant and variable load were performed. Simultaneously, themicrostructures of the specimens and tested components are extensively analysed at severalpoints including the lug area, as well as, the specimen’s microstructure taken out of thelower link fitting. A common consideration of life time results as well as results of themicrostructure in the life time calculation shows the possibilities for more precise lifetime estimation.

Keywords

High cycle fatiguefracture mechanicslife predictiontitanium alloysmicrostructures
Type
Research Article
Information
Mechanics & Industry , Volume 12 , Issue 5 , 2011 , pp. 361 - 378
Copyright
© AFM, EDP Sciences 2011

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References

G. Lütjering, J.C. Williams, Titanium: Engineering materials and processes, Berlin, Springer, 2003
M. Peters, C. Leyens, Titan und titanlegierungen, Weinheim, Wiley, 2002
M. Riedler, M. Stockinger, M. Stoschka, B. Oberwinkler, W. Tan, Linking microstructure and fatigue of forged Ti-6Al-4V aerospace parts LCF6, Berlin, 2008, pp. 129–134
M. Stoschka, M. Stockinger, H. Leitner, M. Riedler, Assessment of lifetime calculation of forged IN718 aerospace components based on a multi-parametric microstructural evaluation superalloys, Champion, 2008, pp. 573–582
B. Oberwinkler, M. Riedler, W. Eichlseder, Importance of residual stresses and surface roughness regarding fatigue of titanium forgings, J. ASTM Int. 7 (2009)
W. Eichlseder, B. Unger, Trends in der Betriebsfestigkeitssimulation, DVM-Conference, 2005
G. Fleischer, 40 Jahre Bewertung von Reibung und Verschleiß mit Hilfe der Energiedichte, Tribologie und Schmierungstechnik, 2004, pp. 5–11