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Recrystallization behavior and thermal shock resistance of the W-1.0 wt% TaC alloy
- Source :
- Journal of Nuclear Materials. 501:282-292
- Publication Year :
- 2018
- Publisher :
- Elsevier BV, 2018.
-
Abstract
- The high-temperature stability and good mechanical strength of tungsten (W) alloys are highly desirable for a wide range of fusion applications, which can be achieved by dispersion strengthening. In this paper, TaC dispersion effects on the thermal stabilities, tensile properties and thermal shock resistances have been investigated. A hot-rolled W-1.0 wt% TaC plate has been fabricated which contains the high tensile strength and elongation. Nanosized particles in the W matrix improve the recrystallization temperature to about 1400 °C and the ultimate tensile strength to 571 MPa at 500 °C through hindering grain boundary migration, pinning dislocations and refining grains. The effects of edge-localized mode like transient heat events on the rolled and recrystallized W-1.0 wt% TaC alloys were investigated systematically. The cracking threshold (100 shots) at room temperature is in the range of 0.33–0.44 GW/m2 for the rolled W-1.0 wt% TaC. Recrystallization degrades mechanical strength and makes the material more prone to thermal shock damages. Coarse Ta2O5 and Ta-Cx-Oy particles are easy to fracture and introduce a preferential crack initiation in W matrix during cyclic heat loads.
- Subjects :
- Nuclear and High Energy Physics
Thermal shock
Materials science
Alloy
Recrystallization (metallurgy)
chemistry.chemical_element
Fracture mechanics
02 engineering and technology
engineering.material
Tungsten
021001 nanoscience & nanotechnology
Microstructure
01 natural sciences
010305 fluids & plasmas
Nuclear Energy and Engineering
chemistry
0103 physical sciences
Ultimate tensile strength
engineering
General Materials Science
Grain boundary
Composite material
0210 nano-technology
Subjects
Details
- ISSN :
- 00223115
- Volume :
- 501
- Database :
- OpenAIRE
- Journal :
- Journal of Nuclear Materials
- Accession number :
- edsair.doi...........733aac7dfd358d31a294abbfefda81ca