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熱處理對激光沉積DZ125合金組織與摩擦磨損性能的影響
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1.沈陽航空航天大學(xué)航空制造工藝數(shù)字化國防重點學(xué)科實驗室;2.沈陽工業(yè)大學(xué)機械工程學(xué)院;3.中國航發(fā)沈陽黎明航空發(fā)動機有限責(zé)任公司焊接技術(shù)室

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遼寧省自然科學(xué)基金(20170540690)國家重點研發(fā)計劃資助(2017YFB1104002)


Effect of Heat Treatment on Microstructure and Friction and Wear Properties of Laser Deposition DZ125 Alloy
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1.KeySLaboratorySofSFundamentalSScienceSforSNationalSDefenceSofSAeronauticalSDigitalSManufacturingSProcess,ShenyangSAerospaceSUniversity;2.School of Mechanical Engineering,Shenyang University of Technology

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    摘要:

    研究了不同熱處理制度對激光沉積DZ125高溫合金顯微組織、硬度及摩擦磨損性能的影響規(guī)律。結(jié)果表明:沉積區(qū)枝晶形貌為外沿生長的柱狀枝晶,平均一次枝晶間距約為10.8μm,經(jīng)單級時效(870 ℃/20h,AC)和雙級時效(1100 ℃/4h,AC to 870 ℃/20h,AC)熱處理后,試樣的枝晶形貌與沉積態(tài)差別不大,γ"相均發(fā)生粗化現(xiàn)象,且雙級時效熱處理后的γ"相粗化程度更高、尺寸分布更為均勻;雙級時效熱處理制度下,不同低溫時效溫度γ"相的平均尺寸和含量不同,其中 1100 ℃/4h,AC to 870 ℃/20h,AC制度下,γ"相的平均尺寸和含量最大;經(jīng)單級時效和雙級時效熱處理后,碳化物中Ti元素含量均呈下降趨勢;雙級時效熱處理后,析出兩種形貌不規(guī)則的MC碳化物,分別為富含Cr、Co元素的M23C6型碳化物和富含W、Mo元素的M6C型碳化物;單級時效和雙級時效熱處理試樣的磨損機理均為磨粒磨損,雙級時效熱處理試樣的顯微硬度及耐磨性能均優(yōu)于單級時效。

    Abstract:

    The effects of different heat treatment regimes on the microstructure, hardness and friction and wear properties of laser deposited DZ125 superalloys were investigated. The results show that the dendritic morphology of the depositional area is columnar dendrite growing on the outer edge, and the average primary dendrite spacing is about 7.8μm. After single-stage aging (870 °C/20h, AC) and two-stage aging (1100 °C/4h, AC to 870 °C/20h, AC), the dendritic morphology and sedimentary state of the sample are not much different, γ" The coarsening phenomenon occurs in each phase, and the γ" phase coarsening degree and the size distribution are more uniform after the two-stage aging heat treatment; Under the two-stage aging heat treatment system, the average size and content of different aging temperature γ" phases are different, including 1100 °C/4h, AC to 870 °C/20h, and the average size and content of γ" phase are the largest under AC system; After single-stage aging and two-stage aging heat treatment, the content of Ti in the carbides showed a downward trend; After two-stage aging heat treatment, two kinds of irregularly shaped MC carbides are precipitated, which are M23C6 type carbides rich in Cr and Co elements and M6C type carbides rich in W and Mo elements; The wear mechanism of the unipolar aging and the two-stage aging heat treatment specimens is abrasive wear. The microhardness and wear resistance of the two-stage aging heat treatment samples are better than the single-stage aging.

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卞宏友,邸騰達,王世杰,曲伸,王偉,楊光.熱處理對激光沉積DZ125合金組織與摩擦磨損性能的影響[J].稀有金屬材料與工程,2020,49(8):2839~2844.[Bian Hongyou, Di Tengda, Wang Shijie, Qu Shen, Wang Wei, Yang Guang. Effect of Heat Treatment on Microstructure and Friction and Wear Properties of Laser Deposition DZ125 Alloy[J]. Rare Metal Materials and Engineering,2020,49(8):2839~2844.]
DOI:10.12442/j. issn.1002-185X.20190643

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  • 收稿日期:2019-08-05
  • 最后修改日期:2019-08-13
  • 錄用日期:2019-08-21
  • 在線發(fā)布日期: 2020-09-27
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