碳纤维湿法缠绕基体配方及成型研究  

Study on the Matrix Formulation and Forming for Carbon Fiber Composites in Wet Winding Process

作　　者：王晓洁[1] 张炜[1] 刘炳禹[1] 

机构地区：[1]中国航天科技集团公司四院四十三所,西安710025

出　　处：《固体火箭技术》2001年第1期60-63,共4页Journal of Solid Rocket Technology

摘　　要：研究了碳纤维增强复合材料用湿法成型工艺、基体配方的性能和使用期。研究的 HT1 1 A、HT1 1 B两种配方浇注体拉伸强度达到 1 0 0 MPa以上 ,模量为 3.9GPa,力学性能优良。配方具有较高的耐热性 ,使用期大于 9h,完全适用于湿法缠绕成型。缠绕的 Φ1 50 mm碳纤维增强复合材料容器特性系数 ( PV/W)均大于 34 km,纤维强度转化率 ( K)达到 82The wet-winding process for carbon fiber reinforced composites, the properties and service life of the resin matrix are studied. The mechanical properties of the casts for two resin formula, i.e. HT11A and HT11B, are excellent. The results show that tensile strength and modulus reach over 100MPa and 3.9GPa respectively. The formulae have a good heat-resistance performance and the service life exceed 9h, meeting the demand for wet-winding processes. Their PV/W values of Φ150mm pressure vessels wound with the carbon fiber reinforced composite are all over 34km and their translation ratio (K) of carbon fiber strength is up to 82%.

关 键 词：湿法缠绕 成型 配方 基体 转化率 碳纤维增强复合材料 耐热性 浇注 力学性能 拉伸强度 

分 类 号：V258[一般工业技术—材料科学与工程] TQ433.437[航空宇航科学与技术—航空宇航制造工程]