胡霖,高志坤.DD6 单晶合金涡轮转子叶片裂纹与内腔等轴晶成因研究[J].航空发动机,2018,44(6):
DD6 单晶合金涡轮转子叶片裂纹与内腔等轴晶成因研究
Study on the Crack and the Origin of Inner Cavity Equiaxed Crystal in DD6 SingleCrystal Alloy Turbine Rotor Blade
  
DOI:
中文关键词:  DD6 单晶合金  涡轮转子叶片  内腔  等轴晶  高温合金焊料;航空发动机
英文关键词:DD6 single crystal alloy  turbine rotor blade  inner cavity  equiaxed crystal  superalloy solder  aeroengine
基金项目:航空动力基础研究项目资助
作者单位E-mail
胡霖,高志坤 中国航发沈阳发动机研究所沈阳100015 1259691509@qq.com 
摘要点击次数: 1299
全文下载次数: 1465
中文摘要:
      为排除某航空发动机DD6 单晶合金涡轮转子叶片振动试验过程中出现异常裂纹的故障,开展了裂纹外观检查、断口宏 观和微观形貌分析、表面检查、解剖分析、显微组织检查、成分分析及应力分布计算等工作,对故障叶片失效原因及内腔局部区域的 等轴晶成因和机理进行研究。结果表明:DD6 单晶合金涡轮转子叶片裂纹性质为高周疲劳,裂纹过早萌生与叶片内腔存在等轴晶有 直接关系,且附近存在无枝晶的异常组织也促进了疲劳裂纹的萌生及扩展。同时,等轴晶在叶片使用之前已存在,是由于内腔工艺 孔处的高温合金焊料遗留,高温真空焊接时形成易形核质点。建议加强对叶片内腔生产质量的控制,并对叶片内腔工艺孔附近危险 部位进行严格检查,避免此类故障再次发生
英文摘要:
      In order to eliminate the malfunction of abnormal crack in the vibration test of turbine rotor blade of DD6 single crystal alloy in an aeroengine,crack appearance inspection,macroscopic and microscopic morphology analysis of fracture,surface inspection, anatomical analysis,microstructure examination,component analysis and stress distribution calculation were carried out. The reason of blade failure and the origin and mechanism of equiaxial crystal in the local area of the inner cavity were studied. The results show that the crack property of turbine rotor blade of the DD6 single crystal alloy is high cycle fatigue. The premature initiation of crack is directly related to the existence of equiaxed crystal in the inner cavity of the blade,and the abnormal structure without dendrites in the vicinity also promotes the initiation and propagation of fatigue crack. At the same time,the equiaxed crystal already exists before the blade is used,due to the residual superalloy solder at the technological hole in the inner cavity and the free-form nucleation particle equiaxed crystal is formed during the high-temperature vacuum welding. It is suggested that the quality control of blade inner cavity should be strengthened,and the dangerous position near the technological hole of blade inner cavity should be strictly checked to avoid the recurrence of this kind of malfunction.
查看全文  查看/发表评论  下载PDF阅读器