HAN Xiaoyong, SU Jiazhi, XU Shaochen, CHEN Jiping, ZHENG Yizhu. Research on the Springback of Composites C-Shape Ribs. Aeronautical Manufacturing Technology, 2016, 59(20): 63-67.
HAN Xiaoyong, SU Jiazhi, XU Shaochen, CHEN Jiping, ZHENG Yizhu. Research on the Springback of Composites C-Shape Ribs. Aeronautical Manufacturing Technology, 2016, 59(20): 63-67. DOI: 10.16080/j.issn1671-833x.2016.20.063.
采用碳纤维织物预浸料在阳模上按既定固化工艺制备C 型肋零件,利用三坐标测量机测量了模具型面,零件在三端封边、大端切口及大端切口且缘条切边3 种状态下的零件内型面,以及大端切口且缘条切边状态下的零件外型面,对零件的回弹进行了分析、验证。结果表明:对于铺层为[(±45°)/( - +45°)]n(3 ≤ n ≤ 6)的三端封边肋零件模具两侧缘条回弹补偿1.35°,大端缘条回弹补偿0.32°;大端切口与未切口状态对比缘条回弹变化很大;大端切口后,缘条切边与未切边状态对比缘条回弹稍有变化;大端切口肋零件模具两侧缘条回弹补偿1.69°,大端缘条回弹补偿1.62°。
Abstract
Composites C-shape ribs are made of carbon fiber fabric prepreg on the male moulds under certain curing process. A coordinate measuring machine is used to measure the surface of the moulds
the inner surface of the ribs under three conditions (three flanges closed
large end cut and three flanges trimmed after large end cut)
and the outer surface of the ribs when the large end is cut and the three flanges are trimmed. The springback of the ribs are measured and analyzed. The results shows that the springback compensation of the two side flanges of the ribs is 1.35°
and the springback compensation of the large end flange is 0.32° when the three flanges are closed. The springback results varied a lot before and after the large end is cut
but varied little before and after the flanges are trimmed. The springback compensation is 1.69° for the two side flanges
and 1.62° for the big end flange when the ribs are cut at the large end.