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