Hot Single Point Incremental Forming of Ti-6Al-4V Alloy

Mikel Ortiz, Mariluz Penalva, Mildred J. Puerto, Petr Homola, Václav Kafka

Producción científica: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

9 Citas (Scopus)

Resumen

The lightweight metal alloy Ti-6Al-4V is widely used in the aeronautical industry due to its excellent mechanical properties. However, it is known the difficulty to deform Ti-6Al-4V sheets at room temperature because of its microstructure conditions. The present work focuses on the evaluation of formability of Ti-6Al-4V sheets using hot single point incremental forming (SPIF) process which it seems appropriate to produce small batches of parts due to its flexibility as it allows a significant reduction of costs and lead times. In order to characterize the SPIF of Ti-6Al-4V under hot forming conditions, a set of forming trials evaluation tests was carried out. The obtained results have allowed identifying the key process features and have demonstrated the potential of the proposed approach to hot form of small amounts of Ti-6Al-4V parts.
Idioma originalInglés
Título de la publicación alojadaunknown
EditorialTrans Tech Publications Ltd
Páginas1079-1087
Número de páginas9
Volumen611-612
ISBN (versión impresa)978-303835106-1, 9783038351061
DOI
EstadoPublicada - 2014
Evento17th Conference of the European Scientific Association on Material Forming, ESAFORM 2014 - Espoo, Finlandia
Duración: 7 may 20149 may 2014

Serie de la publicación

Nombre1013-9826

Conferencia

Conferencia17th Conference of the European Scientific Association on Material Forming, ESAFORM 2014
País/TerritorioFinlandia
CiudadEspoo
Período7/05/149/05/14

Palabras clave

  • Formability
  • Global Heating
  • Incremental Forming
  • Ti6Al4V

Project and Funding Information

  • Project ID
  • info:eu-repo/grantAgreement/EC/FP7/266208/EU/Innovative Manufacturing of complex Ti sheet components/INMA
  • Funding Info
  • Research leading to these results was done within the project INMA – Innovative manufacturing_x000D_ of complex titanium sheet components. This project has received funding from the European_x000D_ Union’s Seventh Framework Programme for research, technological development and_x000D_ demonstration under grant agreement No. 266208._x000D_ Authors would also like to thank Joachim Zettler from Airbus Group Innovations and Alain_x000D_ Dupuy from Airbus for their support to define the scope of the tests and their analysis.

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