刘明坤,李艳明,刘 宇,刘 欢,佟文伟,乔 志.不同温度下DSM11镍基高温合金热腐蚀试验[J].航空发动机,2023,49(2):168-174
不同温度下DSM11镍基高温合金热腐蚀试验
Hot Corrosion Behaviors Test of DSM11 Ni-base Superalloy under Different Temperature
  
DOI:
中文关键词:  DSM11镍基高温合金  热腐蚀  内氧化  内硫化  Al 2 O 3 保护层  航空发动机
英文关键词:DSM11 Ni-base superalloy  thermal corrosion  internal oxidation  internal sulfuration  Al 2 O 3 protective layer  aeroengine
基金项目:航空动力基础研究项目资助
作者单位
刘明坤,李艳明,刘 宇,刘 欢,佟文伟,乔 志 中国航发沈阳发动机研究所沈阳 110015 
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中文摘要:
      为了研究DSM11镍基高温合金的抗热腐蚀性能,对该合金在650、750、850℃条件下涂覆5%NaCl+95%Na 2 SO 4 混合盐膜 进行腐蚀试验。利用金相显微镜(OM)、扫描电子显微镜(SEM)、能谱仪(EDS)和X射线衍射仪(XRD)等手段,对合金被腐蚀200 h 后的表面形貌、物相组成、元素和腐蚀层的分布情况以及腐蚀机理进行分析。结果表明:随着试验温度的升高,合金表面腐蚀程度 逐渐加重、腐蚀产物组成逐渐复杂、失重加大、腐蚀产物层厚度增大;合金的腐蚀产物层均可分为3层,最外层和中间层主要为氧 化物,内层由颗粒状氧化物和硫化物组成,O和S的侵入现象表明合金发生了较明显的内氧化与内硫化现象;在3种温度下,合金 表面生成连续稳定的Al 2 O 3 保护层,抑制了热腐蚀反应的进行,对基体存在有效的保护作用,表明合金具有一定的抗热腐蚀性能。
英文摘要:
      In order to study the thermal corrosion behaviors of DSM11 Ni-base superalloy, corrosion tests were conducted on the alloy coated with 5%NaCl+95%Na 2 SO 4 mixed salt films at 650, 750, and 850 ℃. The surface morphology, phase composition, distribution of ele? ments and corrosion layer, and corrosion mechanism of the alloy after 200 hours corrosion were analyzed using metallographic microscopy (OM), scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), and X-ray diffraction (XRD). The results show that with the increase of temperature, corrosion status on the surface of the superalloy gradually becomes serious, corrosion products become compli? cated, the loss of mass gradually increases and the thickness of the corrosion layer gradually increases. The corrosion layer of the superalloy can be divided into three layers, the outer and middle layers are multilayer oxides, and the inner layer is composed of granular oxides and sulfides, the intrusions of O and S indicate that the superalloy has obvious internal oxidation and internal sulfuration. At three temperatures, a continuous and stable Al 2 O 3 protective layer is formed on the alloy surface, which inhibits the thermal corrosion reaction and effectively protects the matrix, indicating that the alloy has a certain thermal corrosion resistance.
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