Impact deformation of large colony Ti6Al4V

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Authors

Colleges, School and Institutes

External organisations

  • Ecole Nationale Supérieure des Ingénieurs en Arts Chimiques et Technologiques

Abstract

The impact defonnation mechanism of Ti6Al4V is of interest for aerospace and other applications where the material may be subjected to a sudden external force such as bird strike. This research studies the deformation mechanism of Ti6Al4V with a large colony size under different conditions using transmission electron microscopy. The original as-rolled Ti6Al4V alloy was slow cooled from the β phase and subjected to impact test at liquid nitrogen temperature and room temperature, with the impact energy varying from 10J to 300J, Deformation twinning has been observed in all specimens tested. In addition to the TEM observations, the nature of the twinning and its role in the impact deformation will be discussed vis-à-vis literature on the plastic deformation of the alloy system.

Details

Original languageEnglish
Title of host publicationTi 2011 - Proceedings of the 12th World Conference on Titanium
Publication statusPublished - 1 Dec 2012
Event12th World Conference on Titanium, Ti 2011 - Beijing, China
Duration: 19 Jun 201124 Jun 2011

Conference

Conference12th World Conference on Titanium, Ti 2011
CountryChina
CityBeijing
Period19/06/1124/06/11

Keywords

  • Impact deformation, Microstructure, Ti-6Al-4V, Timnning

ASJC Scopus subject areas