AeroMat Home      ASM Homepage
Back to "Session 4: Titanium Modeling" Search
  Back to "Titanium Alloy Technology" Search  Back to Main Search

Wednesday, June 27, 2007 - 5:00 PM
TAL4.7

Predictability Of Fracture Toughness In Ti-6al-4v Alloy Rings For Aerospace Application : A Practical Experience

U. V. Gururaja, M. N. Rao, Mishra Dhatu Nigam Limited (MIDHANI), Hyderabad, India

The present ever increasing designer product performance demands shall be the driving force for continuous improvements in the product manufacturing techniques.  In spite of over four decades of research on workhorse alloy 6-4, it is often quite difficult to fully understand the role of microstructure and alloy chemistry on mechanical properties of Ti-64.

 

            In the current study, a number of production heats were analysed for variation in Fracture toughness values, keeping constant processing parameters.  The paper brings out the Fracture toughness prediction band in the form of NAF (Net Alpha Formers) and NBF (Net Beta Formers) for a given chemistry and process route.  The observed effect of primary alpha with respect to NAF and NBF on Fracture toughness values will also be presented.


Summary: The present ever increasing designer product performance demands shall be the driving force for continuous improvements in the product manufacturing techniques. In spite of over four decades of research on workhorse alloy 6-4, it is often quite difficult to fully understand the role of microstructure and alloy chemistry on mechanical properties of Ti-64. In the current study, a number of production heats were analysed for variation in Fracture toughness values, keeping constant processing parameters. The paper brings out the Fracture toughness prediction band in the form of NAF (Net Alpha Formers) and NBF (Net Beta Formers) for a given chemistry and process route. The observed effect of primary alpha with respect to NAF and NBF on Fracture toughness values will also be presented.