Finite Element Analysis of TA15 Titanium Alloy Beam Hammer Forging Forming at Different Temperatures

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Abstract:

The hammer forging forming process of TA15 titanium alloy girder is taken as an example on this study. When girder were formed at different original temperature as 850 °C、900 °Cand 950 °C, the needed hammering times and each hammer’s stroke and varieties of damage factor were researched respectively based on software Deform. By simulation analysis, the needed hammering times is 7 times, 5 times and 4 times in order, and the damage factor which dangerous place located at the right top fillet of girder reached the highest point at about 86mm stroke ,and the original temperature 950 °C gave the best answer. The results are significant theoretical foundation for the practical production and study of TA15 titanium alloy.

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180-183

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September 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] Xingwu Li, Aixue Sha, etc. TA15 Titanium Alloy and Its Applying Prospects on Airframe[J]. Titanium Industry Progress, 2003, 20 (progress 4-5) : 90-94. (In Chinese)

Google Scholar

[2] Yongchao Gao, Lin Hua, etc. 3D FEM Simulation and Optimization of Precision Alternator Pole Forging Process [J]. CHINA MECHANICAL ENGINEERING, 2005, 16 (12) : 1110-1113. (In Chinese)

Google Scholar

[3] Yamin Hu. Forging technology and mould design [M]. Beijing: China's forestry press, 2006. (In Chinese)

Google Scholar

[4] Xuewen Chen, Jin Wang etc. The Technological Parameter Optimization of Gear Billet Hot Forging Process with Damage Minimization [J]. JOURNAL OF SHANGHAI JIAOTONG UNIVERSITY, July 2005 (7) : 1070-1072. (In Chinese)

Google Scholar

[5] Ceretti E, Lucchi M, t. Altan FEM simulation of the orthogonal cutting: serrated chip formation. [J]. Sums of Technology: may, 1999, 95, (1-3) : 17-26

DOI: 10.1016/s0924-0136(99)00261-7

Google Scholar