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钛合金高温FLD试验系统
英文标题:Hot FLD test system for titanium alloy
作者:马博林 刘俊雄 王文平 吴向东 万敏 李新军 
单位:北京航空航天大学 
关键词:钛合金板材 高温成形 感应加热 成形极限图 试验平台 
分类号:
出版年,卷(期):页码:2015,40(10):76-81
摘要:

在考虑了高温成形极限试验中高温模具的传热理论分析之后,设计了高温成形极限模具和板料的加热冷却控温系统,并建立了钛合金板材热成形环境下的高温成形极限试验平台。基于该高温成形极限试验系统和高温成形极限试验流程,获得并分析了TC钛合金板料在650,700和750 ℃ 这3种试验条件下的板料温度变化趋势,同时完成了700 ℃下的TC钛合金高温成形极限试验。温度验证结果表明,钛合金板料在3种温度的试验条件下,温度变化幅度均小于±10 ℃,验证了系统的可靠性。在通过验证该高温试验系统的可靠性之后,获得700 ℃高温环境下钛合金板材的成形极限试验数据。

 By considering the theoretical analysis on heat transfer process of hot tools in hot FLD test, the heating-cooling temperature reflecting-controlling system for hot forming dies and sheet were designed, and a hot FLD test platform for TC alloy sheet in high temperature environment was established. Based on this hot FLD test system and the hot FLD test process, the temperature variations of TC alloy sheet were obtained and analyzed at the test temperature of 650, 700 and 750 ℃. Furthermore, the hot FLD test of TC alloy sheet at  700℃ was performed. The temperature verification results show that the temperature variation is less than ±10 ℃, and the system reliability is confirmed. Based on the above results, the FLD experimental data of TC alloy sheet at 700 ℃ condition was obtained.

基金项目:
国家自然科学基金资助项目(51275026)
作者简介:
马博林(1986-),男,博士研究生
参考文献:

[1[丁少行,李晓星.钛合金蒙皮拉形数值模拟与试验[J].锻压技术,2014,39(7):24-29.

Ding S X, Li X X. Numerical simulation and experiment of stretch forming for titanium alloy skin[J]. Forging & Stamping Technology, 2014,39 (7):24-29.

[2]朱宁愿,夏琴香.难变形金属热强旋成形技术及研究现状[J]. 锻压技术,2014, 39 (9):42-46.

Zhu N Y, Xia Q X. Hot power spinning technology and research status of difficult-to-deforming metal[J]. Forging & Stamping Technology,2014, 39 (9):42-46.

[3]Odenberger E L, Schill M, Oldenburg M. Thermo-mechanical sheet forming of aero engine components in Ti-6Al-4V-PART2: Constitutive modeling and validation[J]. International Journal of Material Forming,2012,6(3):403-416.

[4]Filice L, Gagliardi F, Lazzaro S,et al.FE simulation and experiments consideration on TI alloy superplastic forming for aerospace applications[J]. International Journal of Material Forming,2010,(3):41-46.

[5]鞠小波. AZ3镁合金自阻加热超塑成形工艺[D].哈尔滨:哈尔滨工业大学,2010.

Ju X B. Processing of Superplastic Forming by Direct Resistance Heating for AZ31 Magnesium Alloy[D]. Harbin:Harbin Institute of Technology, 2010.

[6]范国强.TC4板料局部自阻电加热数控渐进成形的研究[D].南京:南京航空航天大学,2010.

Fan G Q. Research on Electric Hot Incremental Forming of Ti-6Al-4V Titanium Sheet[D].Nanjing: Nanjing University of Aeronautics and Astronautics,2010.

[7]Semenova I P, Raab G I. Service properties of ultrafine-grained Ti-6AI-4V alloy at elevated temperature[J].J. Mater. Sci.,2013,48:4806-4812.

[8]Rayudu R K, Bhattacharya S S.Experimental studies on the superplastic forming of square shaped components from sheets of Ti-6Al-4V alloy[J].Transactions of The Indian of Metals,2011,64(1):21-25.

[9]Keeler S P, Backofen W A. Plastic instability and fracture in sheets stretched over rigid punches[J].ASM Trans. Quart.,1963,56(1):25-48.

[10]马博林.高强钢热冲压成形极限试验研究及数值模拟[D].北京:北京航空航天大学,2010.

Ma B L. Experimental Study and Numerical Simulation of Hot Stamping Forming Limit for the HSS[D]. Beijing:Beihang University,2010.

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