Hot working of Ti-6Al-4V via equal channel angular extrusion
Creators
- 1. Air Force Research Lab., Wright-Patterson AFB, OH (United States)
Description
The deformation behavior of Ti-6Al-4V during high-temperature equal channel angular extrusion (ECAE) with or without an initial increment of upset deformation was determined for billets with either a lamellar or an equiaxed alpha preform microstructure. For conventional ECAE (i.e., deformation by simple shear alone), flow localization and fracture occurred at temperatures between 900 C and 985 C. In contrast, billets deformed at temperatures between 485 C and 985 C using an initial increment of upset deformation immediately followed by the simple shear deformation of ECAE exhibited uniform flow with no significant cracking or fracture. A simple flow-localization criterion was used to explain the influence of preupsetting on the suppression of localization in billets with the lamellar microstructure. The suppression of flow localization for the equiaxed microstructure and the elimination of edge cracking for both types of microstructures were explained in terms of heat transfer (die chill) and workpiece geometry. Further evidence of the relative importance of microstructural and thermal effects was extracted from the results of two-pass extrusions, the first with upsetting and the second without upsetting
Additional details
Publishing Information
- Journal Title
- Metallurgical and Materials Transactions. A, Physical Metallurgy and Materials Science
- Journal Volume
- 30
- Journal Issue
- 9
- Journal Page Range
- p. 2473-2482
- ISSN
- 1073-5623
- CODEN
- MMTAEB
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 31002243
- Subject category
- S36: MATERIALS SCIENCE;
- Descriptors DEI
- ALUMINIUM ALLOYS; DEFORMATION; EXTRUSION; FLOW STRESS; FRACTURES; MICROSTRUCTURE; TEMPERATURE RANGE 1000-4000 K; TITANIUM ALLOYS; VANADIUM ALLOYS
- Descriptors DEC
- ALLOYS; FABRICATION; FAILURES; MATERIALS WORKING; STRESSES; TEMPERATURE RANGE; TRANSITION ELEMENT ALLOYS