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高铌TiAl合金的高温断裂韧性

余龙 宋西平 张敏 焦泽辉 于慧臣

工程科学学报2016,Vol.38Issue(3):379-384,6.
工程科学学报2016,Vol.38Issue(3):379-384,6.DOI:10.13374/j.issn2095-9389.2016.03.012

高铌TiAl合金的高温断裂韧性

High-temperature fracture toughness of high Nb-containing TiAl alloys

余龙 1宋西平 2张敏 1焦泽辉 1于慧臣3

作者信息

  • 1. 北京科技大学新金属材料国家重点实验室,北京100083
  • 2. 中国航空工业集团公司北京航空材料研究院,北京100095
  • 3. 中国航空工业集团公司北京航空材料研究院,北京100095
  • 折叠

摘要

Abstract

The fracture toughness of a nearly lamellar Ti-45Al-8Nb-0. 2W-0. 2B-0. 1Y alloy and a fully lamellar Ti-45Al-7Nb-0. 2W-0. 2Hf-0. 3B-0. 15C alloy at 750℃ was investigated by prefabricating a fatigue crack in the compact tension (CT) speci-men, and the corresponding fracture morphologies were observed by optical microscopy and scanning electron microscopy. It is found that the fracture toughness of the nearly lamellar high Nb-containing TiAl alloy is 19. 54 MPa·m1/2 at 750℃, obviously lower than the value of 31. 58 MPa·m1/2 for the fully lamellar alloy. The maximum cyclic load at which the fatigue crack initiates in the nearly lamellar alloy is noticeably less than that in the fully lamellar alloy. Fracture images show that for the nearly lamellar alloy, cracks initiate mainly in equiaxedγgrains and propagate in different ways, intergranularly or transgranularly inγgrains or lamellar colonies. But for the fully lamellar alloy, cracks initiate mainly at lamellar interfaces perpendicular to the load direction and propagate in both interla-mellar and translamellar ways, in accompanying with secondary crack initiation.

关键词

钛铝合金/断裂韧性/高温性能/疲劳裂纹/裂纹萌生/裂纹扩展

Key words

titanium aluminum alloys/fracture toughness/high temperature properties/fatigue cracks/crack initiation/crack propagation

分类

矿业与冶金

引用本文复制引用

余龙,宋西平,张敏,焦泽辉,于慧臣..高铌TiAl合金的高温断裂韧性[J].工程科学学报,2016,38(3):379-384,6.

基金项目

国家重点基础研究发展计划资助项目(2011CB605506) (2011CB605506)

工程科学学报

OA北大核心CSCDCSTPCD

2095-9389

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