Published August 1994 | Version v1
Journal article

Temperature and microstructural dependence of the deformation of a high Nb Ti-Al alloy

  • 1. Naval Air Warfare Center, Warminster, PA (United States). Aircraft Division

Description

Compression testing of a Ti-44-Al-11Nb alloy was carried out at various temperatures and for different microstructures. Annealing was done at temperatures from 1,000 C to 1,500 C to produce the unrecrystallized, duplex (gamma grains plus lamellar colonies) and the fully lamellar microstructures. Sample of each of these microstructures were then tested in air at room temperature and at various temperatures from 1,000 C to 1,300 C. Results indicate that successively higher temperature anneals produce increasing grain or colony sizes from 138 μm in the unrecrystallized microstructure to 1,017 μm in the fully lamellar microstructure. A sequentially lower yield stress was produced on samples tested at increasingly higher temperatures for a given microstructure. In addition, a minimum yield stress on each yield stress vs temperature curve was recorded for the duplex microstructure with a colony size of 154 μm. One promising result was a sample of this microstructure tested at room temperature, where a yield stress of better than 800 MPa and a compressive strain at the cessation of testing of better than 14 pct were obtained

Additional details

Publishing Information

Journal Title
Metallurgical Transactions. A, Physical Metallurgy and Materials Science
Journal Volume
25
Journal Issue
8
Journal Page Range
p. 1667-1692.
ISSN
0360-2133
CODEN
MTTABN

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
26009710
Subject category
S36: MATERIALS SCIENCE;
Descriptors DEI
ALUMINIUM ALLOYS; DEFORMATION; MECHANICAL TESTS; MICROSTRUCTURE; NIOBIUM ALLOYS; TEMPERATURE DEPENDENCE; TITANIUM ALLOYS
Descriptors DEC
ALLOYS; CRYSTAL STRUCTURE; MATERIALS TESTING; TESTING