宇航材料工艺2024，Vol.54Issue(5)：62-69,8.DOI:10.12044/j.issn.1007-2330.2024.05.008
复合材料T型桁条的VARTM成型工艺研究
Study on VARTM Forming Process of Composite T-shaped Stringer
摘要
Abstract
Vacuum assisted resin transfer molding(VARTM)was a cost-effective method for fabricating wing T-shaped stringer,but the cross-section characteristics of the stringer were not conducive to the balanced resin flow during the molding process.Aiming at the problem of resin enrichment in triangle area of T-shaped stringer but insufficient wetting in edge area,the fiber filling method of corner triangle area of mold was adopted in this paper to optimize VARTM process parameters and improve the mechanical properties of T-shaped stringer.The influence of process scheme on the thickness uniformity of each part of stringer was studied.Optical microscope was used to observe the microstructure of the stringer.Moreover,the void content and fiber volume fractions were quantitatively analyzed by burning method.Besides,the mechanical properties of the stringer were tested by universal material testing machine.The results show that the T-shaped stringer formed by VARTM process has good thickness uniformity,high fiber volume fractions,low void content and good mechanical properties,the bending resistance of the stringer is increased by 15.72％and the void content is less than 1％(0.9％).关键词
VARTM/T型桁条/复合材料/玻璃纤维/孔隙率/纤维体积分数Key words
VARTM/T-shaped stringer/Composite/Glass fiber/Void content/Fiber volume fractions分类
通用工业技术引用本文复制引用
申儒林,刘和华,邹湘伏,龚艳玲..复合材料T型桁条的VARTM成型工艺研究[J].宇航材料工艺,2024,54(5):62-69,8.基金项目
湖南省科技创新重大项目"通航用国产复合材料工艺与验证技术研究(2021GK1024) （2021GK1024）
