文章摘要
TC11钛合金压气机盘闭模锻造过程中的缺陷预测
Prediction of Defects During Closed Die Forging of TC11 Alloy Compressor Disks
Received:April 20, 2009  Revised:July 10, 2009
DOI:
中文关键词: 钛合金  压气机盘  损伤模型  缺陷  数值分析
英文关键词: titanium alloy  compressor disk  damage model  defect  numerical analysis
基金项目:
Author NameAffiliation
ZHANG Hai-yan Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 
ZHANG Shi-hong Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 
CHENG Ming Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 
LI Zhen-xi Beijing Institute of Aeronautica1 Materials, Beijing 100095, China 
CAO Chun-xiao Beijing Institute of Aeronautica1 Materials, Beijing 100095, China 
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中文摘要:
      TC11钛合金压气机盘在实际生产中存在各种缺陷,降低了压气机盘的使用性能。将基于试验数据建立的TC11钛合金高温塑性变形时的延性损伤演化模型以及本构模型与有限元相结合,对某TC11钛合金压气机盘等温闭模锻造过程中的温度、等效应变和损伤变量的分布进行了数值分析,同时预测了塑性失稳区的位置。为优化其成形工艺提供了一种有效的方法。
英文摘要:
      There are some defects in the actual forging of TC11 alloy compressor disks, which decreases the performance of the compressor disks. In this paper, a ductile damage evolution model and a constitutive model for TC11 alloy during high temperature deformation developed based on the data from experiments were coupled with a FE simulator. Furthermore, the distributions of temperature, equivalent strain and damage value of TC11 alloy compressor disk during closed die forging were simulated and analyzed, and the plastic instability areas were predicted. It has provided an effective method to optimize the forging process of TC11 alloy compressor disks.
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