首页 | 本学科首页   官方微博 | 高级检索  
     检索      

TC4 钛合金框类零件热挤压数值模拟及工艺优化
引用本文:林 尧,陈 伟,陈明和,李 枫.TC4 钛合金框类零件热挤压数值模拟及工艺优化[J].宇航材料工艺,2010,40(3).
作者姓名:林 尧  陈 伟  陈明和  李 枫
作者单位:1. 南京航空航天大学机电学院,南京,210016
2. 苏州有色金属研究院,苏州,215026
摘    要:为了获得TC4某框类零件热挤压成形工艺方案及其合适的工艺参数,利用有限元软件Msc/su-perforge对零件整体热挤压成形和分段热挤压成形两工艺方案进行数值模拟,得出:整体热挤压成形工艺所需挤压力过高,成形困难,不适合该零件;分段热挤压成形工艺所需挤压力低、成形状况良好适合该零件,并以初始挤压温度920℃、挤压速率3 mm/s为成形的合适条件。

关 键 词:热挤压  TC4钛合金  数值模拟

Numerical Simulation and Process Optimization ofTC4 Titanium Alloy Frame Part on Hot Extrusion
Lin Yao,Chen Wei,Chen Minghe,Li Feng.Numerical Simulation and Process Optimization ofTC4 Titanium Alloy Frame Part on Hot Extrusion[J].Aerospace Materials & Technology,2010,40(3).
Authors:Lin Yao  Chen Wei  Chen Minghe  Li Feng
Institution:College of Mechanical and Electrical Engineering,Nanjing University of
Abstract:In order to obtain forming process scheme and suitable parameters for TC4 titanium alloy frame part,
Msc/ Superforge software was used in simulating overall hot extrusion and segment parts hot extrusion. The simulation results show that high extrusion force and difficulty in forming in overall extrusion process made it not suitable for this product,but low extrusion force in segment parts hot extrusion resulted in good shaping. This process is suitable for this product and the initial extrusion temperature 920, extrusion speed 3mm/ s is better condition for it.
Keywords:Msc/Superforge
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《宇航材料工艺》浏览原始摘要信息
点击此处可从《宇航材料工艺》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号