Transactions of Nonferrous Metals Society of China The Chinese Journal of Nonferrous Metals

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中国有色金属学报

ZHONGGUO YOUSEJINSHU XUEBAO

第20卷    第2期    总第131期    2010年2月

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文章编号:1004-0609(2010)02-0250-07
热连轧Ti-6Al-4V合金的蠕变行为及影响因素
田素贵1,包宪宇1,陈礼清2,刘  洋1,赵忠刚1,刘相华2

(1. 沈阳工业大学 材料科学与工程学院,沈阳 110178;
2. 东北大学 轧制技术及连轧自动化国家重点实验室,沈阳 110004
)

摘 要: 采用热处理、蠕变性能测试及位错组态的衍衬分析,研究热连轧Ti-6Al-4V合金的蠕变行为及影响因素。结果表明:经低于β相变点的固溶处理,合金的组织结构由高固溶度的等轴α相和网篮组织组成;随着固溶温度提高,网篮组织数量增多;经1 000 ℃固溶处理后合金可获得完全网篮组织;与940 ℃固溶时效合金相比,经     1 000 ℃固溶时效合金在420 ℃、575 MPa条件下具有较低的应变速率和较长的蠕变寿命;在试验的温度和应力范围内,计算出该合金的蠕变激活能为249.8 kJ/mol;在蠕变期间,热连轧合金的变形机制是位错在具HCP结构的α相中发生双取向滑移,940 ℃固溶处理合金的蠕变机制是波浪状áa+cñ位错在α相中发生锥面滑移,而经1 000 ℃固溶处理合金的变形机制是(1/2)á111ñ位错在具BCC结构的β相中发生多系滑移;经1 000 ℃固溶处理合金中所含的高含量富V的β相可提高合金蠕变抗力,这是合金具有较低应变速率和较长蠕变寿命的主要原因。

 

关键字: Ti-6Al-4V合金;热连轧;固溶处理;蠕变;变形机制

Creep behaviors and effect factors of
hot continuous rolled Ti-6Al-4V alloy
TIAN Su-gui1, BAO Xian-yu1, CHEN Li-qing2, LIU Yang1, ZHAO Zhong-gang1, LIU Xiang-hua2

1. School of Materials Science and Engineering, Shenyang University of Technology, Shenyang 110178, China;
2. State Key Laboratory of Rolling and Automation, Northeastern University, Shenyang 110004, China

Abstract:By heat treatment, measurement of creep properties and contract analysis of dislocations configuration, the creep behaviors and the effect factors of hot continuous rolled (HCR) Ti-6Al-4V alloy were investigated. The results show that, after the alloy solution treated at temperatures lower than β phase transformation point, the microstructures of the alloy consist of the supersaturation equiaxial α phase and network basket structure. The quantities of the network basket structure increase as the solution temperature increases, and the full network basket structure may be obtained after solution-treated at 1 000 ℃. Compared with the alloy solution treated at 940 ℃, the alloy solution treated at 1 000 ℃ displays a lower strain rate and a longer creep lifetime under the conditions of the applied stress of 575 MPa at 420 ℃. In the range of the applied temperatures and stresses, the creep activation energy of the alloy is calculated to be 249.8 kJ/mol. The deformed mechanism of HCR alloy during creep is double orientation slipping of dislocations activated within α phase with HCP structure, while the deformed feature of the alloy solution treated at 940 ℃ is the wave-like áa+cñ dislocations activated on the pyramidal planes in α phase. After solution treated at 1 000 ℃, the deformed mechanism of the alloy is the multiple slipping of (1/2) á111ñ dislocations activated within β phase with BCC structure. In this alloy, the high volume fraction V-riched β phase may enhance the creep resistance of the alloy. This is the main reason why this alloy possesses relatively low strain rate and long creep lifetime.

 

Key words: Ti-6Al-4V alloy; hot continuous rolling; solution treatment; creep; deformation mechanism

ISSN 1004-0609
CN 43-1238/TG
CODEN: ZYJXFK

ISSN 1003-6326
CN 43-1239/TG
CODEN: TNMCEW

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