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