Effect of cooling rate on microstructure of Ti-6AI-4V forging

被引:16
作者
Senkov, ON
Valencia, JJ
Senkova, SV
Cavusoglu, M
Froes, FH
机构
[1] Universal Energy Syst Inc, Dayton, OH 45432 USA
[2] Concurrent Technol Corp, Johnstown, PA 15904 USA
[3] Univ Idaho, IMAP, Moscow, ID 83844 USA
关键词
D O I
10.1179/026708302225007808
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The objectives of this work were to study the microstructural changes and tensile properties that resulted from controlled cooling of a Ti-6Al-4V alloy that had been pancake forged. The alloy was forged at 954degreesC and specimens cut from the forging were annealed at 975degreesC for 30 min and cooled down to room temperature at different cooling rates ranging from 20 K min(-1) to 490 K min-1. The specimens had a duplex microstructure consisting of elongated primary alpha particles and secondary finer a lamellae with some residual beta phase layers between them. The average length and width of primary alpha particles decreased and the aspect ratio and volume fraction of particles increased when the cooling rate was increased. The average lamellar spacing decreased from about 1 mum to 0.3 mum when the cooling rate increased from 25 K min(-1) to 490 K min(-1). Lamellar alpha contained 3.0-5.2 wt-%Al and 1.4-2.1 wt-%V, while the beta layers contained 1.4-2.8 wt-%Al, 12-18 wt-%V and 1.5-2.4 wt-%Fe. In the alpha lamellae, the concentration of aluminium increased and the concentration of vanadium went through a minimum with an increase in cooling rate. In the beta layers, the concentration of aluminium increased, while the concentration of vanadium decreased with increasing cooling rate. The volume fraction of the beta phase decreased from 10-12% to 4-5% as the cooling rate increased from 25 to 490 K min(-1). The tensile strength increased by approximately 7% when increasing the cooling rate from 25 to 370 K min(-1), while the reduction in area achieved a 29% peak increase when the cooling rate was increased from 25 to approximately 325 K min(-1). A discussion of the effects of cooling rate on microstructure and properties is also given.
引用
收藏
页码:1471 / 1478
页数:8
相关论文
共 13 条
[1]  
Boyer R., 1994, Materials Properties Handbook, V1st
[2]  
BOYER RR, 1993, TITANIUM 92 SCI TECH, V1, P77
[3]  
COLLINGS EW, 1984, PHYSICAL METALLURGY
[4]  
Murakami Y, 1980, TITANIUM 80 SCI TECH, V1, P153
[5]   CRYOGENIC TEMPERATURE MECHANICAL-PROPERTIES OF BETA-ANNEALED TI-6AL-4V ALLOYS [J].
NAGAI, K ;
HIRAGA, K ;
OGATA, T ;
ISHIKAWA, K .
TRANSACTIONS OF THE JAPAN INSTITUTE OF METALS, 1985, 26 (06) :405-413
[6]  
NAGAI K, 1987, P C CRYOG ENG, V30, P375
[7]  
PETERS M, 1980, TITANIUM 80 SCI TECH, V2, P925
[8]  
PHILIPPE MJ, 1996, TITANIUM 95 SCI TECH, V2, P956
[9]   Microstructural modeling and process control during hot working of commercial Ti-6Al-4V: Response of lamellar and equiaxed starting microstructures [J].
Prasad, YVRK ;
Seshacharyulu, T ;
Medeiros, SC ;
Frazier, WG .
MATERIALS AND MANUFACTURING PROCESSES, 2000, 15 (04) :581-604
[10]  
SEAGLE SR, 1982, SOURCE BOOK TITANIUM, P23