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噴丸強度對TA15鈦合金型材表面完整性影響的數(shù)值和實驗研究
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作者單位:

1.南京航空航天大學(xué) 機電學(xué)院,江蘇 南京 210016;2.中航西安飛機工業(yè)集團股份有限公司,陜西 西安 710089

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基金項目:

航材院鈦合金型材應(yīng)用研究項目(KZ82171509)


Numerical and Experimental Investigations on the Effect of Shot Peening Intensity on the Surface Integrity of TA15 Titanium Alloy Profiles
Author:
Affiliation:

1.College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2.AVIC Xi 'an Aircraft Industry Group Company Ltd, Xi 'an 710089, China

Fund Project:

Titanium Alloy Profile Application Research Project of AECC Beijing Institute of Aeronautical Materials (KZ82171509)

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    摘要:

    利用有限元模擬和噴丸實驗研究了噴丸強度對TA15鈦合金熱擠壓型材表面完整性的影響規(guī)律。對比了由數(shù)值模擬和噴丸實驗得到的表面粗糙度和殘余應(yīng)力分布結(jié)果,驗證了所建立的噴丸有限元模型的可靠性;研究了噴丸強度對材料表層顯微硬度和微觀組織的影響。實驗結(jié)果表明,噴丸處理在TA15鈦合金型材表層產(chǎn)生了最大數(shù)值為558~764 MPa且深度為115~151 μm的殘余壓應(yīng)力層,材料表層發(fā)生塑性變形,位錯密度增大,晶粒細化,表層硬度提高,形成了深度為100~150 μm的硬化層,同時表面粗糙度增大。最大殘余壓應(yīng)力、壓應(yīng)力層深度和表層硬度隨噴丸強度的增大而增大,但強度超過0.188 mmA后增加不明顯,材料表面出現(xiàn)裂紋,且在0.222 mmA強度下,材料表面因折疊缺陷而發(fā)生殘余應(yīng)力松弛,降低了材料表面完整性。

    Abstract:

    The effect of the shot peening intensity on the surface integrity of TA15 titanium alloy hot extruded profile was numerically and experimentally studied. The surface roughness and residual stress distribution obtained by the numerical simulation were compared with the shot peening experimental results, and the reliability of the established finite element model was verified. The effects of shot peening intensity on the microhardness and microstructure of the material surface were investigated. The experimental results show that the compressive residual stress layer with a maximum value of 558~764 MPa and a depth of 115~151 μm was introduced into the surface of TA15 titanium alloy profile after shot peening. The plastic deformation occurs on the material surface, the grain is refined, the dislocation density and the hardness of the material surface increase. The hardened layer with a depth of 100~150 μm forms, and the surface roughness increases. The increase of the shot peening intensity increases the maximum compressive residual stress, the depth of the compressive residual stress layer and the surface hardness. However, the increase is not obvious when the intensity exceeds 0.188 mmA, and the cracks might appear on the material surface. Moreover, at the intensity of 0.222 mmA, the residual stress relaxation occurs on the material surface due to the folding defect, which reduces the surface integrity of the material.

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萬銀根,羅峰,謝蘭生,陳明和,夏明莉.噴丸強度對TA15鈦合金型材表面完整性影響的數(shù)值和實驗研究[J].稀有金屬材料與工程,2022,51(6):1979~1985.[Wan Yingen, Luo Feng, Xie Lansheng, Chen Minghe, Xia Mingli. Numerical and Experimental Investigations on the Effect of Shot Peening Intensity on the Surface Integrity of TA15 Titanium Alloy Profiles[J]. Rare Metal Materials and Engineering,2022,51(6):1979~1985.]
DOI:10.12442/j. issn.1002-185X. E20210007

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  • 收稿日期:2021-04-02
  • 最后修改日期:2021-06-01
  • 錄用日期:2021-06-21
  • 在線發(fā)布日期: 2022-06-29
  • 出版日期: 2022-06-29