中国有色金属学报(英文版)
Transactions of Nonferrous Metals Society of China
Vol. 13 No. 6 December 2003 |
(National Defense Key Laboratory of Advanced High Temperature Structural Materials,Beijing Institute of Aeronautical Materials, Beijing 100095, China)
Abstract:The true stress—strain curves and processing window of Ti-47Al-2Cr-1Nb were set up through thermal physical simulation. A method for refinement of the as-cast+HIPped structure was submitted, which included two-step deformation with a short intermediate heat-treatment between double deformations. The break-down operation of the canned ingot was performed by the isothermal forging processing mentioned above. The refining mechanism is characterized as breaking and bending of the as-cast+HIPped lamellae, dynamic recrystallization, and static globularization. Thus, a uniform and refined billet microstructure is obtained for the final component by forging operation. The deformation of a model disc is accomplished by the subsequent single-step isothermal forging at 1100-1150℃ using a closed compression die.
Key words: TiAl alloy; isothermal forging; microstructure