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气膜孔加工工艺与孔间距对DD6单晶高温合金氧化行为的影响
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1中国航发北京航空材料研究院,北京 100095;2航空材料检测与评价北京市重点实验室,北京 100095;3中国科学院金属研究所,辽宁 沈阳 110016

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National Science and Technology Major Project(J2019-Vl-0022-0138)and by the Institute fund of AECC Beijing Institute of Aeronautical Materials (KJSZ240769).


Effect of Gas Film Holes Processing Technique and Adjacent Hole Spacing on Oxidation Behavior of DD6 Single-Crystal Superalloy
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Affiliation:

1AECC Beijing Institute of Aeronautical Materials, Beijing 100095;2Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, Beijing 100095;3Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016

Fund Project:

National Science and Technology Major Project (J2019-Vl-0022-0138); Institute Fund of AECC Beijing Institute of Aeronautical Materials (KJSZ240769)

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    摘要:

    采用场发射扫描电子显微镜、能谱仪和ABAQUS有限元分析,研究了不同气膜孔加工工艺和孔间距对DD6单晶高温合金在1000 ℃恒温下氧化行为的影响。结果表明:采用不同打孔工艺和孔间距下,DD6单晶高温合金的氧化增重趋势一致,孔间距排序为0.75 mm>0.95 mm>0.55 mm>0.39 mm,孔间距对单晶高温合金氧化行为的影响比打孔工艺的影响更为显著。两种打孔工艺的高温氧化行为有所不同,电火花打孔产生的再铸层由于微观结构的变化和元素重新分布,导致不同的元素以不同速率发生反应。而飞秒激光打孔后,孔内壁几乎没有再铸层,氧化层直接在单晶高温合金基体上形成。有限元模拟结果表明,孔表面氧化层生长主要受氧化膜脱落应力的影响;随着孔间基体尺寸的增大,应力抵消区域逐渐减小,而氧化膜的脱落应力不断增大,并在孔间距为0.75 mm时达到峰值,此时的氧化膜脱落最为严重,之后又呈逐渐下降的趋势。

    Abstract:

    This study employed a field emission scanning electron microscope, an energy dispersive spectroscope, and ABAQUS finite element analysis to investigate the oxidation behavior of DD6 single-crystal superalloy at a constant temperature of 1000 ℃, focusing on the effects of various processed drilling processes and adjacent hole spacting. The results show that the trend in oxidation mass gain of the DD6 single-crystal superalloy processed by different drilling techniques with different adjacent hole spacting is relatively consistent, following the order: 0.75 mm>0.95 mm>0.55 mm>0.39 mm. Compared with drilling process, adjacent hole spacting emerges as the primary factor affecting oxidation mass gain. The high-temperature oxidation behavior differs between the two drilling processes. The change in microstructure and elemental redistribution in the recast layer produced by electrical discharge machining may cause a variety of elements at different states to react at different rates simultaneously. In contrast, after femtosecond laser processing, there is almost no recast layer on the inner wall of the holes, and the oxide layer forms directly on the single-crystal alloy matrix. Finite element analysis reveals that oxide layer developed on hole surfaces is primarily governed by shedding stress. As adjacent hole spacing increases, the areas of stress cancellation diminish, while shedding stress escalates to a peak under the adjacent hole spacing of 0.75 mm, at which point oxide film shedding is the most pronounced, and then decreases.

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胡春燕,董美静,刘新灵,陈星,刘昌奎.气膜孔加工工艺与孔间距对DD6单晶高温合金氧化行为的影响[J].稀有金属材料与工程,2026,55(8):1907~1916.[Hu Chunyan, Dong Meijing, Liu Xinling, Chen Xing, Liu Changkui. Effect of Gas Film Holes Processing Technique and Adjacent Hole Spacing on Oxidation Behavior of DD6 Single-Crystal Superalloy[J]. Rare Metal Materials and Engineering,2026,55(8):1907~1916.]
DOI:10.12442/j. issn.1002-185X.20250472

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  • 收稿日期:2025-09-16
  • 最后修改日期:2025-12-30
  • 录用日期:2026-01-13
  • 在线发布日期: 2026-06-22
  • 出版日期: 2026-06-05