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基于極性交互模型的MoLa合金鍛造工藝優(yōu)化及熱變形行為研究
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南昌航空大學(xué)航空制造工程學(xué)院,南昌航空大學(xué)航空制造工程學(xué)院

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中圖分類號:

TG146.4+12

基金項目:

國家自然科學(xué)基金項目(面上項目,重點項目,重大項目)


Research on Hot Deformation Behavior and Forging Process Optimization of MoLa Alloy Based on Polar Reciprocity Model
Author:
Affiliation:

school of Aeronautial Manufacturing Engineering, Nanchang Hangkong University,school of Aeronautial Manufacturing Engineering, Nanchang Hangkong University

Fund Project:

The National Natural Science Foundation of China (General Program, Key Program, Major Research Plan)

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    摘要:

    采用Geeble1500型熱模擬試驗,對MoLa合金進行等溫恒應(yīng)變速率壓縮實驗,研究其在變形溫度800~1150℃,應(yīng)變速率0.001~10s-1范圍內(nèi)的熱變形行為。通過對不同變形參數(shù)下的流變曲線分析發(fā)現(xiàn),隨應(yīng)變的增加,流變曲線大多呈現(xiàn)為緩慢上升或保持穩(wěn)定,但在應(yīng)變速率為0.001s-1時,1000~1150℃變形溫度下流變應(yīng)力隨應(yīng)變的增加而下降;采用PSO-BP神經(jīng)網(wǎng)絡(luò)建立MoLa合金本構(gòu)模型,經(jīng)過誤差計算得出,該模型的相關(guān)系數(shù)和平均相對誤差分別為:0.995和1.48%,具有良好的精度;基于極性交互模型繪制MoLa合金本征熱加工性能參數(shù)ξ圖,并通過對失穩(wěn)區(qū)和穩(wěn)定區(qū)組織分析發(fā)現(xiàn),失穩(wěn)區(qū)主要以局部流動為失穩(wěn)形式,穩(wěn)定區(qū)主要以動態(tài)回復(fù)為變形機制;通過ξ圖和組織觀察可知,MoLa合金適宜的變形參數(shù)范圍為:變形溫度1100~1150℃,應(yīng)變速率0.001~0.05s-1。

    Abstract:

    To investigate the flow stress characteristics and deformation?mechanism of MoLa Alloy,The isothermal compression tests were performed over the ranges of temperature 800-1150oC and the strain rate range of 0.001-10 s -1.The results show that the flow stress increases or remain stable with the increase of strain .But the flow stress decrease with the increase of strain in which the deformation temperature is 1000-1150 ℃ and the strain rate is 0.001s-1.A PSO-BP neural network has been established to describe the changing rule of flow stress with the strain rate and deformation temperature .The correlation coefficient and average?relative?error of the network have been calculated to be 0.995 and 1.48% respectively.So it is clear that the PSO-BP model has?good?accuracy .The intrinsic hot workability maps have been constructed based on the polar reciprocity model at strains of 0.3,0.6 and 0.92.?Combing microstructure observation ,it has been found that the buckling form in instability area mainly was local plastic deformation,and deformation mechanism in stability region mainly was dynamic recovery.The suitable processing parameters ranges of MoLa alloy could be inferred to be the deformation temperature range of 1100-1150 ℃ and the strain rates range of 0.001- 0.05 s-1.

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引用本文

汪雨佳,王克魯.基于極性交互模型的MoLa合金鍛造工藝優(yōu)化及熱變形行為研究[J].稀有金屬材料與工程,2018,47(7):2225~2231.[wangyujia, wangkelu. Research on Hot Deformation Behavior and Forging Process Optimization of MoLa Alloy Based on Polar Reciprocity Model[J]. Rare Metal Materials and Engineering,2018,47(7):2225~2231.]
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歷史
  • 收稿日期:2016-09-06
  • 最后修改日期:2017-03-07
  • 錄用日期:2017-03-15
  • 在線發(fā)布日期: 2018-10-10
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