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DD6单晶合金涡轮转子叶片裂纹与内腔等轴晶成因研究 被引量:2
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作者 胡霖 高志坤 《航空发动机》 北大核心 2018年第6期91-96,共6页
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... 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。 展开更多
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
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Microstructure and shear strength ofγ-TiAl/GH536 joints brazed with Ti-Zr-Cu-Ni-Fe-Co-Mo filler alloy 被引量:10
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作者 Li LI Wei ZHAO +2 位作者 Zhi-xue FENG Jia SUN Xiao-qiang LI 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2020年第8期2143-2155,共13页
The influence of brazing temperature and brazing time on the microstructure and shear strength ofγ-TiAl/GH536 joints brazed with Ti-Zr-Cu-Ni-Fe-Co-Mo filler was investigated using SEM,EDS,XRD and universal testing ma... The influence of brazing temperature and brazing time on the microstructure and shear strength ofγ-TiAl/GH536 joints brazed with Ti-Zr-Cu-Ni-Fe-Co-Mo filler was investigated using SEM,EDS,XRD and universal testing machine.Results show that all the brazed joints mainly consist of four reaction layers regardless of the brazing temperature and brazing time.The thickness of the brazed seam and the average shear strength of the joint increase firstly and then decrease with brazing temperature in the range of 1090-1170℃and brazing time varying from 0 to 20 min.The maximum shear strength of 262 MPa is obtained at 1150℃for 10 min.The brittle Al3NiTi2 and TiNi3 intermetallics are the main controlling factors for the crack generation and deterioration of joint strength.The fracture surface is characterized as typical cleavage fracture and it mainly consists of massive brittle Al3NiTi2 intermetallics. 展开更多
关键词 γ-TiAl alloy Ni-based superalloy vacuum brazing amorphous filler MICROSTRUCTURE shear strength
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Interfacial microstructure and mechanical properties of GH99 superalloy and Nb brazed joint using Cu75Pt25 filler 被引量:2
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作者 Wen-qiang LI Sheng-peng HU +3 位作者 Yu-zhen LEI Yu LEI Xiao-guo SONG Ji-cai FENG 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2020年第10期2724-2736,共13页
Cu75Pt25 brazing filler was applied to brazing GH99 superalloy to Nb,and the sound joints were obtained by adjusting brazing parameters.The typical interfacial microstructure of the brazed joint was Nb/Nb7Ni6+NbNi3/Ni... Cu75Pt25 brazing filler was applied to brazing GH99 superalloy to Nb,and the sound joints were obtained by adjusting brazing parameters.The typical interfacial microstructure of the brazed joint was Nb/Nb7Ni6+NbNi3/Ni(s,s)+Cr-rich NbNi3+(NbCr2+NbNi3)/GH99.The effects of brazing temperature and holding time on the interfacial microstructure of GH99/Cu75Pt25/Nb joints were studied.The results showed that the solution and diffusion of Ni atoms from GH99 substrate into brazing seam played a critical role in the interfacial microstructure evolution.As the brazing temperature rose,the Nb−Ni reaction layer was formed instead of the initial Nb3Pt layer,and the thickness increased firstly and then remained constant.The highest shear strength of the joint reached 152 MPa when brazed at 1150℃ for 15 min.All of the joints presented a brittle fracture mode during shear test,and the fracture location changed from Nb3Pt layer to Nb−Ni compounds layer. 展开更多
关键词 nickel-based superalloy NB Cu75Pt25 filler BRAZING microstructure mechanical properties
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