CHEN Rongzhang WANG Luobao WANG Yuping ** Institute of Aeronautical Materials
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Beijing
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100095
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China+ To whom correspondence should be addressed
材料科学技术（英文）
Alloy DZ22 possesses rather high intermediate and elevated temperature mechanical properties comparable with the advanced commercial DS al- loy PWA1422.The alloy composition is based on PWA1422 alloy,only the content ranges of Hf,C and Zr are changed for systematic study.The pres- ent melting technology for master alloy ingot and DS process parameters for components are suitable for this alloy.The alloy revert which has been specially processed can be reused.The mould with- drawal rate during directional solidification affects the crystal orientation,alloy structure and the me- chanical properties of DS castings.The increment of solution-treatment temperature increases obvi- ously the longitudinal stress-rupture life at high temperature but decreases transversal one at inter- mediate temperature.The production practice in batches has demonstrated that alloy DZ22 has not only high mechanical properties but also excellent processing performance,including castability, weldability and machinability.It is indeed a favorable material for advanced aero and land gas turbine engine blades with complex inner cooling passage.
关键词:
directional solidification
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null
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李友林
,
袁超
,
郭建亭
金属学报
利用开有V形缺口的平板试样，研究了一种新型铸造高温合金K445在最高温度分别为800、850、900℃，最低温度为室温的热循环下的热疲劳行为. 通过光学显微镜和扫描电镜观察合金的组织和热疲劳裂纹形貌，研究热疲劳损伤机制. 结果表明，热疲劳主裂纹主要从V形缺口处萌生，沿晶界扩展，而二次裂纹则穿晶扩展. 当最高循环温度为800℃时，碳化物的组成和分布起主要作用，(Ti, Ta)C的开裂处以及碳化物与基体分离的界面处是裂纹优先形成区域. 当最高循环温度为900℃时，高温氧化的作用占主导地位. 应力辅助作用下的晶界氧脆是此时的主要损伤机制.
关键词:
铸造高温合金
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thermal fatigue
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carbide
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oxidation
