The effect of microstructure and strain rate on the 25 °C and 700 °C compression deformation behavior of powder metallurgy processed Ti-45Al-2Nb-2Mn (at.%)-0.8 TiB2 (vol%) alloy
Creators
- 1. Department of Chemical Engineering and Materials Science, Michigan State University, 428 South Shaw Lane, 2100 Engineering Building, East Lansing, MI 48824 (United States)
- 2. Department of Materials Science and Engineering and Chemical Engineering, University of Carlos III of Madrid, Avda. Universidad 30, 28911 Leganés (Spain)
- 3. IMDEA Materials Institute, C/Eric Kandel 2, 28906 Getafe (Spain)
Description
Highlights: • The near fully-lamellar microstructures exhibited higher strengths than the duplex microstructure. • For all the strain rates and temperatures examined, the near fully-lamellar microstructures exhibited higher strengths than the duplex microstructure. • The activation volume, which ranged between 0-100b3 (b is the Burger's vector), was found to be inversely proportional to the flow stress at 700 °C. This dependence was shown to be qualitatively consistent with the assumption that dislocation glide is controlled by the thermally activated overcoming of forest junctions. • The RT deformation was considered to be controlled by dislocation glide, while at elevated temperature, the likely thermally activated process controlling dislocation glide was associated with the forest junctions acting as pinning points. The effect of microstructure and strain rate on the room-temperature (RT) and 700 °C compression deformation behavior of a powder metallurgy processed γ-TiAl intermetallic alloy, Ti-45Al-2Nb-2Mn (at.%)-0.8 (vol%) TiB2, was investigated. Samples were heat-treated to obtain a duplex two-phase α2+γ microstructure and two nearly fully-lamellar α2+γ microstructures with different lamellar spacings and γ-phase volume fractions. Compression experiments were performed to a minimum deformation of 10% true strain under strain rates of 10−2, 10−3, 10−4, and 10−5 s−1. The compression strength, strain rate sensitivity, colony size, interlamellar spacing, and microhardness were dependent on microstructure. The nearly fully-lamellar microstructures exhibited higher compression strengths than the duplex microstructure for all the testing conditions. The strain rate sensitivity index (m), tended to increase with increasing temperature, and for the 700 °C deformation, m increased with increasing true strain. The apparent activation volumes, decreased with increasing true strain at 700 °C. Scanning electron microscopy observations showed that cracking preferentially occurred within the γ phase and the extent of cracking increased with increased temperature, strain, and strain rate. Overall, the RT deformation was considered to be controlled by dislocation glide, while at elevated temperature, the likely thermally activated process controlling dislocation glide was associated with the forest junctions acting as pinning points.
Availability note (English)
Available from http://dx.doi.org/10.1016/j.matchar.2020.110856Additional details
Identifiers
- DOI
- 10.1016/j.matchar.2020.110856;
- PII
- S1044580320323275;
Publishing Information
- Journal Title
- Materials Characterization
- Journal Volume
- 172
- Journal Page Range
- vp.
- ISSN
- 1044-5803
- CODEN
- MACHEX
INIS
- Country of Publication
- United States
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 54039256
- Subject category
- S36: MATERIALS SCIENCE; S46: INSTRUMENTATION RELATED TO NUCLEAR SCIENCE AND TECHNOLOGY;
- Descriptors DEI
- COMPRESSION STRENGTH; DISLOCATIONS; FLOW STRESS; HEAT TREATMENTS; INTERMETALLIC COMPOUNDS; MICROHARDNESS; MICROSTRUCTURE; POWDER METALLURGY; SCANNING ELECTRON MICROSCOPY; STRAIN RATE; TESTING; TITANIUM BORIDES; VECTORS
- Descriptors DEC
- ALLOYS; BORIDES; BORON COMPOUNDS; CRYSTAL DEFECTS; CRYSTAL STRUCTURE; ELECTRON MICROSCOPY; HARDNESS; LINE DEFECTS; MECHANICAL PROPERTIES; METALLURGY; MICROSCOPY; STRESSES; TENSORS; TITANIUM COMPOUNDS; TRANSITION ELEMENT COMPOUNDS
Optional Information
- Copyright
- Copyright (c) 2020 Elsevier Inc. All rights reserved.