宇航材料工艺2012，Vol.42Issue(6)：39-42,51,5.
F-12纤维/氰酸酯树脂基复合材料力学性能研究
Study on Mechanical Properties of F-12 Fiber/Cyanate Resin Matrixed Composites
惠雪梅 1尤丽虹 1廖英强1
作者信息
- 1. 西安航天复合材料研究所,西安710025
- 折叠
摘要
Abstract
The NOL rings, laminates and 0150mm standard pressure vessels of F-12 aramid fiber/cyanate resin matrix composites were manufactured by pre-impregnated wind process. The mechanical properties and fracture morphology of F-12 aramid fiber/cyanate composites were also studied. The results show that the interlaminar shear strength(ILSS) was less than 35 MPa,and vessel performance factor (PV/Wc) of 0150 mm standard pressure vessels were 34. 22 km. The strength transfer rate of F-12 fiber in 0150 mm pressure vessels was 70. 22% . The form of fracture surface mainly reveals tearing and fibrillation of F-12 fiber.关键词
F-12纤维/氰酸酯树脂/层间剪切强度(ILSS)/容器特性系数/纤维强度转化率Key words
F-12 aramid fiber/ Cyanate resin/ Interlaminar shear strength(ILSS) / Vessel performance factor/ Fiber strength transfer rate引用本文复制引用
惠雪梅,尤丽虹,廖英强..F-12纤维/氰酸酯树脂基复合材料力学性能研究[J].宇航材料工艺,2012,42(6):39-42,51,5.
