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鎂合金管材大曲率無芯彎曲損傷及壁厚變化研究
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太原科技大學(xué) 重型機(jī)械教育部工程研究中心,太原科技大學(xué) 重型機(jī)械教育部工程研究中心,太原科技大學(xué) 重型機(jī)械教育部工程研究中心,太原科技大學(xué) 重型機(jī)械教育部工程研究中心,太原科技大學(xué) 重型機(jī)械教育部工程研究中心,太原科技大學(xué) 重型機(jī)械教育部工程研究中心,太原科技大學(xué) 重型機(jī)械教育部工程研究中心,太原科技大學(xué) 重型機(jī)械教育部工程研究中心

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太原科技大學(xué)博士啟動(dòng)基金(項(xiàng)目號(hào):20162034);山西省重點(diǎn)研發(fā)計(jì)劃重點(diǎn)項(xiàng)目(項(xiàng)目號(hào):201603D111005);山西省重點(diǎn)學(xué)科建設(shè)經(jīng)費(fèi)資助; 國家自然科學(xué)(51375325)


Study on Damage and Wall Thickness Variation with Large Curvature and No-Mandrel Bending Process of Magnesium Alloy Tube
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Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology,Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology,Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology,Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology,Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology,Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology,Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology,Heavy Machinery Engineering Research Center of the Ministry of Education,Taiyuan University of Scienceand Technology

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    摘要:

    基于管材彎曲成形機(jī)理及Johnson-Cook損傷理論,利用Deform-3D有限元方法分析了AZ31B鎂合金管材大曲率無芯彎曲初始彎曲溫度、助推速度及助推形式對損傷及管材壁厚變化影響。結(jié)果表明:當(dāng)助推模和壓力模對管材施加的作用一定時(shí),初始彎曲溫度過低或過高均不利于鎂合金管材彎曲成形,最佳初始彎曲溫度為350℃; 在最佳初始彎曲溫度條件下,當(dāng)助推模與壓力模同步運(yùn)動(dòng)時(shí),僅能改善一側(cè)壁厚變化程度,無法同時(shí)改善彎管整體壁厚變化,內(nèi)外側(cè)壁厚不均勻度較大;當(dāng)助推模與壓力模不同步時(shí),通過合理匹配助推模與壓力模二者之間的軸向速度來改變鎂合金管材在進(jìn)給階段軸向拉伸或壓縮變形程度,使得內(nèi)外側(cè)壁厚均勻度達(dá)到較理想效果;當(dāng)外助推模和壓力模同步,內(nèi)助推模和以上二者等速反向運(yùn)動(dòng)時(shí),內(nèi)外側(cè)壁厚均勻度最佳,獲得綜合性能良好的鎂合金管材彎曲成形質(zhì)量。

    Abstract:

    Based on the tube bending forming mechanism and Johnson-Cook damage theory, the influence of initial bending temperature、aid-push speed and aid-push mode of magnesium alloy tube bending process , with large curvature and no-mandrel , on the damage and wall thickness variation was analyzed by the Deform-3D finite element method. The results showed that: when the aid-push die and pressure die exerted a certain effect on the tube, the initial bending temperature was too high or too low, which was detrimental to the bending of the magnesium alloy tube, and the optimum initial bending temperature was 350℃. Under the optimum initial bending temperature , when the aid-push die moved synchronously with the pressure die, the unilateral wall thickness variations degree can only be improved, and the overall wall thickness variations can not be improved simultaneously, so the wall thickness non-uniformity of the tube was remarkable. When the aid-push die and pressure die were not synchronized, the axial tension or compression deformation degree of the tube-bending can be changed with reasonably matching the axial velocity between the aid-push die and the pressure die in the feed stage, thus the wall thickness uniformity can be achieved a rather good effect. When the external aid-push die moved synchronously with the pressure die, and the internal aid-push die moved at a velocity of the same magnitude but in opposite direction with the above two dies, the wall thickness uniformity was optimal, thus the bending quality of magnesium alloy tube with good comprehensive properties was obtained.

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茍毓俊,雙遠(yuǎn)華,周研,蔡偉,代佳,毛飛龍,丁小鳳,趙春江.鎂合金管材大曲率無芯彎曲損傷及壁厚變化研究[J].稀有金屬材料與工程,2018,47(8):2422~2428.[Gou Yujun, Shuang Yuanhua, Zhou Yan, Cai Wei, Dai Jia, Mao Feilong, Ding Xiaofeng, Zhao Chunjiang. Study on Damage and Wall Thickness Variation with Large Curvature and No-Mandrel Bending Process of Magnesium Alloy Tube[J]. Rare Metal Materials and Engineering,2018,47(8):2422~2428.]
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  • 收稿日期:2017-08-30
  • 最后修改日期:2017-11-15
  • 錄用日期:2017-12-13
  • 在線發(fā)布日期: 2018-10-17
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