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短碳纤维增强聚醚醚酮注塑成型进气道的性能

Properties of Short Carbon Fiber Reinforced Injection-moulded PEEK Air Inlet
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摘要 以含20%的短碳纤维增强聚醚醚酮树脂为主要原料,采用注塑成型的方法制备了进气道及试片。通过对材料力学性能、微观形貌、进气道CT无损检测、内型面三坐标进行分析,结果表明:按照给定的工艺参数注塑成型,复合材料的抗拉强度达208 MPa、拉伸模量16.7 GPa、冲压式剪切强度100 MPa,碳纤维在树脂基体中分布均匀,进气道本体材料内部缺陷较少,进气道内外型面光滑、尺寸精度较高。 With 20%short carbon fiber reinforced PEEK as the main raw materials,the air inlet and samples were prepared by the iniection-moulding method.The mechanical properties and microscopic morphology of samples,X-CT nondestructive testing and three coordinates testing of the air inlet were analyzed.Experimental results show that the tensile strength of PEEK composites reaches 208 MPa,tensile modulus reaches 16.7 GPa,punch-type shear strength reaches 100 MPa,the distribution of irregular fiber is even,the inner defects of inlet are low,both inner and outer contour of inlet are smooth,size precision is higher。
作者 刘妍 杜潮 侯树涛 LIU Yan;DU Chao;HOU Shutao(The Institute of China Aerospace Science&Industry Corp.,Beijing 100074)
出处 《宇航材料工艺》 CAS CSCD 北大核心 2022年第4期58-61,共4页 Aerospace Materials & Technology
关键词 短碳纤维 聚醚醚酮 进气道 Short carbon fiber PEEK Air inlet
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  • 1谭慧俊,郭荣伟.一种背负式无附面层隔道进气道的数值模拟研究与实验验证[J].航空学报,2004,25(6):540-545. 被引量:17
  • 2翁培奋.[D].南京航空航天大学,1986.
  • 3任三星.[D].南京航空航天大学,1999.
  • 4Seddon J,Goldsmith E L. Intake Aerodynamcs[M].London:Blackwell Science, 1999.
  • 5Taskinoglu E S,Knight D.Numerical analysis of submer-ged inlets[R].AIAA 2002-3147,2002.
  • 6Taskinoglu E S,Knight D.Design optimization for subm-erged inlets-Part I[R].AIAA2003-1247,2003.
  • 7Taskinoglu E S,Knight D. Design optimization for subm-erged inlets-Part Ⅱ[R]. AIAA 2003-3926,2003.
  • 8余安远.[D].南京:南京航空航天大学,2003.
  • 9Lee C C,Boekicker C.Subsonic diffuser design and perfor-mance for advanced fighter aircraft[R].AIAA-85-3073,1985.
  • 10杨爱玲,夏阳,郭荣伟,梁德旺.埋入式进气道的设计及其气动性能研究[J].空气动力学学报,1998,16(2):154-161. 被引量:21

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