-1在優(yōu)化后的參數(shù)條件下進行數(shù)值模擬和工藝實驗以驗證優(yōu)化結(jié)果的可靠性,結(jié)果表明所優(yōu)化的工藝參數(shù)可以同時細化渦輪盤的平均晶粒尺寸并提高其組織均勻性。本研究可以為高性能航空發(fā)動機渦輪盤生產(chǎn)過程中的工藝制定提供借鑒和參考。"/>

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基于響應(yīng)面法的FGH4113A高溫合金渦輪盤鍛造工藝參數(shù)優(yōu)化
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作者單位:

1.華中科技大學材料科學與工程學院;2.深圳市萬澤中南研究院有限公司

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基金項目:

國家自然科學基金(52175319);中央高校基本科研業(yè)務(wù)費專項資金(YCJJ202202003)


Optimization of the Forging Process Parameters of the FGH4113A P/M superalloy turbine disk based on response surface method
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School of Materials Science and Engineering,State Key Laboratory of Materials Processing and Die Mould Technology,Huazhong University of Science and Technology

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    摘要:

    本研究通過對有限元模擬軟件進行二次開發(fā)并嵌入所建立的微觀組織演變模型,實現(xiàn)了FGH4113A鎳基粉末高溫合金渦輪盤鍛造過程的宏微觀耦合數(shù)值模擬。通過單因素實驗方法,分析了坯料溫度、模具溫度、坯料高徑比和應(yīng)變速率對渦輪盤鍛后平均晶粒尺寸及其分布的影響?;陧憫?yīng)面法,建立了工藝參數(shù)與微觀組織之間的映射關(guān)系模型。以盤件鍛后平均晶粒尺寸和標準偏差為微觀組織優(yōu)化目標,進行渦輪盤工藝參數(shù)的多目標優(yōu)化,得到最優(yōu)工藝參數(shù)為:坯料溫度為1097℃左右、模具溫度為976℃左右、坯料高徑比為2.4、應(yīng)變速率為0.021s-1。在優(yōu)化后的參數(shù)條件下進行數(shù)值模擬和工藝實驗以驗證優(yōu)化結(jié)果的可靠性,結(jié)果表明所優(yōu)化的工藝參數(shù)可以同時細化渦輪盤的平均晶粒尺寸并提高其組織均勻性。本研究可以為高性能航空發(fā)動機渦輪盤生產(chǎn)過程中的工藝制定提供借鑒和參考。

    Abstract:

    In this work, the macro-micro coupled finite element simulation of the FGH4113A P/M superalloy during the forging process was carried out and systematically studied. The effects of workpiece temperature, die temperature, height-diameter-ratio of the workpiece, and strain rate on the microscopic average grain size (dave) and its distribution uniformity of the forged turbine disks were analyzed by single factor simulation. Based on the orthogonal experimental design and response surface method, the mapping relationship between processing parameters and microstructure state variables was established. The dave and the standard deviation of grain size distribution were taken as the optimization targets of processing parameters to achieve microstructural control. Then the optimal processing parameters can be obtained by multi-objective optimization of the established response surface model, listed as: the workpiece temperature of 1097℃, the die temperature of 976℃, height-diameter-ratio of 2.4, and strain rate of 0.021s-1. The validated finite simulation under this deformation condition was carried out to verify the reliability of the optimization results. The results show that the forged turbine disk depicts the characteristics of the finer dave and uniform grain size distribution. This study can provide the guidelines and reference for process formulation in the production process of high-performance superalloy turbine disks.

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溫紅寧,金俊松,章一丁,龔攀,王新云,陳俊志,馬向東,郭建政.基于響應(yīng)面法的FGH4113A高溫合金渦輪盤鍛造工藝參數(shù)優(yōu)化[J].稀有金屬材料與工程,2024,53(9):2633~2641.[Wen Hongning, Jin Junsong, Zhang Yiding, Gong Pan, Wang Xinyun, Chen Junzhi, Ma Xiangdong, Guo Jianzheng. Optimization of the Forging Process Parameters of the FGH4113A P/M superalloy turbine disk based on response surface method[J]. Rare Metal Materials and Engineering,2024,53(9):2633~2641.]
DOI:10.12442/j. issn.1002-185X.20230479

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  • 收稿日期:2023-08-02
  • 最后修改日期:2023-08-31
  • 錄用日期:2023-09-14
  • 在線發(fā)布日期: 2024-09-13
  • 出版日期: 2024-09-04