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新型超高強(qiáng)韌鈦合金熱變形行為研究
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北京航空材料研究院,北京航空材料研究院,北京航空材料研究院,北京航空材料研究院,北京航空材料研究院,北京航空材料研究院,北京航空材料研究院,北京航空材料研究院

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裝備預(yù)先研究項(xiàng)目(項(xiàng)目號(hào)51312JQ01)


Study on hot deformation behavior of new high strength and toughness titanium alloy
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Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials,Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials,Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials,Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials,Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials,Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials,Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials,Titanium Alloys Laboratory,Beijing Institute of Aeronautical Materials

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    摘要:

    本文采用Gleeble3800熱壓縮模擬試驗(yàn)機(jī)研究了新型超高強(qiáng)韌TB17鈦合金775℃~905℃溫度范圍內(nèi)、應(yīng)變速率0.001s-1~10s-1條件下的熱變形行為。分析了該合金在熱變形過程中流變應(yīng)力軟化特點(diǎn)及顯微組織演變規(guī)律,建立了該合金Arrhenius型本構(gòu)方程。試驗(yàn)結(jié)果表明:采用不同變形溫度,TB17鈦合金峰值應(yīng)力對(duì)應(yīng)變速率敏感程度不同,在相變溫度以下變形時(shí),峰值應(yīng)力對(duì)低應(yīng)變速率敏感,而在相變溫度以上變形,峰值應(yīng)力對(duì)高應(yīng)變速率敏感。應(yīng)變速率對(duì)TB17鈦合金顯微組織具有重要影響,合金應(yīng)變速率大于0.1s-1時(shí),以發(fā)生動(dòng)態(tài)回復(fù)為主,而應(yīng)變速率為0.001 s-1~0.1s-1時(shí)以發(fā)生動(dòng)態(tài)再結(jié)晶為主;降低應(yīng)變速率有利于動(dòng)態(tài)再結(jié)晶發(fā)生,合金在應(yīng)變速率0.001s-1時(shí)可獲得約25μmβ的晶粒。變形溫度對(duì)動(dòng)態(tài)再結(jié)晶具有重要影響,在相變溫度以下變形僅發(fā)生初生α相再結(jié)晶,而相變溫度以上變形則發(fā)生β相動(dòng)態(tài)再結(jié)晶。TB17鈦合金相變點(diǎn)溫度以下的熱變形激活能為538.4KJ/mol,相變點(diǎn)溫度以上的熱變形激活能為397.4KJ/mol,該合金在775℃~905℃熱變形軟化機(jī)制為晶界滑移機(jī)制。

    Abstract:

    The hot deformation behaviors of a new type high strength and toughness TB17 titanium alloy was investigated on the thermo mechanical simulator (Gleeble3800). The experiment conducted at temperatures ranging from 775 °C to 905 °C and strain rates various from 0.001 s?1 to 1 s?1. The softening mechanism of flow stress and microstructure were investigated during hot deformation process and the Arrhenius type constitutive equation were established as well. The stress of TB17 titanium alloy varies with sensitivity of the strain rate at defferent deformation temperatures. Duing deforming at α+β field,the peak stress was sensitive to low strain rates,while at β field deforming,the peak stress was sensitive to high strain rates. The strain rate has a major impact on the microstructure of TB17 titanium alloy. The dynamic recovery mechanisms plays an dominant role as the strain rate exceeds 0.1s-1. Dynamic recrystallization plays an significant role while the strain rate is in the range of 0.001 s-1~0.1s-1. Recrystallization processing can be promoted with the decreasing of strain rate. The microstructure of equiaxed grains with a size of 25μm was obtained with a strain rate of 0.001 s-1. The temperature also has great influence on the dynamic recrystallization. During deformed at α+β field lead to primary α phase recrystallization, while at β field lead to the β grain recrystallization. The activation energy for hot deformation below and above the temperature of phase transformation point is 538.4KJ/mol and 397.4KJ/mol, respectively. The softening mechanism of hot deformation temperature ranged from 775 to 905℃ transformation point is grain boundary glide.

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王哲,王新南,商國(guó)強(qiáng),祝力偉,李靜,費(fèi)躍,田帥,朱知壽.新型超高強(qiáng)韌鈦合金熱變形行為研究[J].稀有金屬材料與工程,2018,47(3):810~815.[Wang Zhe, Wang Xinnan, Shang Guoqiang, Zhu Liwei, Li Jing, Fei Yue, Tian Shuai, Zhu Zhishou. Study on hot deformation behavior of new high strength and toughness titanium alloy[J]. Rare Metal Materials and Engineering,2018,47(3):810~815.]
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  • 收稿日期:2016-01-19
  • 最后修改日期:2016-05-26
  • 錄用日期:2016-06-12
  • 在線發(fā)布日期: 2018-04-11
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