Obtainment of Beta Titanium Alloys for Aerospace Applications by Powder Metallurgy

2006-01-2639

11/21/2006

Event
2006 SAE Brasil Congress and Exhibit
Authors Abstract
Content
The titanium is on excellent material for fabrication of aerospace springs in substituting to steels, due to its high corrosion resistance, 60% lower density, and lower elastic modulus. The production of the titanium alloys by powder metallurgy (M/P), starting from the elemental powders is a feasible route considering its lower costs and versatility. In this work, results of the Ti-3Al-8V-6Cr-4Mo-4Zr (β-C) and Ti-35Nb-7Zr-5Ta alloys production are presented. Samples were cold isostatic pressing (350 MPa) with subsequent densification by sintering at 1200, 1400 and 1500 °C, in vacuum. Sintered samples were characterized for phase composition, microstructure and microhardness by X-ray diffraction, scanning electron microscopy and Vickers indentation, respectively. Density was measured by Archimedes method. It was shown that the samples were sintered to high densities and presented homogeneous microstructure.
Meta TagsDetails
DOI
https://doi.org/10.4271/2006-01-2639
Pages
8
Citation
Taddei, E., Henriques, V., Cairo, C., and Silva, C., "Obtainment of Beta Titanium Alloys for Aerospace Applications by Powder Metallurgy," SAE Technical Paper 2006-01-2639, 2006, https://doi.org/10.4271/2006-01-2639.
Additional Details
Publisher
Published
Nov 21, 2006
Product Code
2006-01-2639
Content Type
Technical Paper
Language
English