STRESS-CORROSION CRACKING AND FATIGUE CRACK GROWTH BEHAVIOR OF TI-6AL-4V PLATES CONSOLIDATED FROM LOW COST POWDERS

被引:0
作者
Imam, M. Ashraf [1 ]
Pao, Peter S. [1 ]
Bayles, Robert A. [1 ]
机构
[1] Naval Res Lab, Mat Sci & Component Technol Directorate, Washington, DC 20375 USA
来源
FATIGUE OF MATERIALS II: ADVANCES AND EMERGENCES IN UNDERSTANDING | 2013年
关键词
Titanium alloy; Armstrong-process; hydride-process; stress-corrosion cracking; fatigue crack growth;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Titanium is highly desirable for a wide range of applications because of its combination of high strength, low density and outstanding corrosion characteristics. However, the cost of titanium, produced by conventional technology, is high compared to steel and aluminum, which is a result of high extraction and processing costs. New approaches are being investigated maintaining required quality while lowering the cost of finished products. Ti alloy powder, Ti-6Al-4V, manufactured by a low cost hydride-process and consolidated into flat products (sheet, plate), were studied. The results of the study were compared with the properties obtained from plates of Armstrong Titanium consolidated powder. To remove the prior history of consolidation, the plates are beta annealed and the test results are compared with "as received" condition. The mechanism of the fatigue crack growth rate difference, fracture toughness, and stress-corrosion cracking resistance in terms of the respective Ti-6Al-4V microstructure differences will be discussed.
引用
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页码:105 / 1116
页数:1012
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