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International Journal of Material Forming
Erschienen in: International Journal of Material Forming 3/2013

01.09.2013 | Original Research

Thermo-mechanical sheet metal forming of aero engine components in Ti-6Al-4V—PART 2: Constitutive modelling and validation

verfasst von: E.-L. Odenberger, M. Schill, M. Oldenburg

Erschienen in: International Journal of Material Forming | Ausgabe 3/2013

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Abstract

In this work constitutive models suitable for thermo-mechanical forming of the titanium alloy Ti-6Al-4V are evaluated. A tool concept for thermo-mechanical forming of a double-curved sheet metal component in Ti-6Al-4V is proposed. The virtual tool design is based on finite element (FE) analyses of thermo-mechanical sheet metal forming in which two different anisotropic yield criteria are evaluated and compared with an isotropic assumption to predict global forming force, draw-in, springback and strain localisation. The shape of the yield surface has been found important and the accuracy of the predicted shape deviation could be slightly improved by including the cooling procedure. The predicted responses show promising agreement with the corresponding experimental observations when the anisotropic properties of the material are considered.
Vorheriger Artikel Thermo-mechanical sheet metal forming of aero engine components in Ti-6Al-4V – PART 1: Material characterisation
Nächster Artikel On the influence of deformation rate and cooling media on the static strain aging of a warm-rolled low carbon steel

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Metadaten
Titel
Thermo-mechanical sheet metal forming of aero engine components in Ti-6Al-4V—PART 2: Constitutive modelling and validation
verfasst von
E.-L. Odenberger
M. Schill
M. Oldenburg
Publikationsdatum
01.09.2013
Verlag
Springer Paris
Erschienen in
International Journal of Material Forming / Ausgabe 3/2013
Print ISSN: 1960-6206
Elektronische ISSN: 1960-6214
DOI
https://doi.org/10.1007/s12289-012-1094-7

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