柔性混编预浸料制造热塑性复合材料加筋结构

安学锋;张明;唐邦铭;益小苏

航空材料学报 ›› 2006, Vol. 26 ›› Issue (3) : 217-221.

PDF(577 KB)
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航空材料学报 ›› 2006, Vol. 26 ›› Issue (3) : 217-221.
论文

柔性混编预浸料制造热塑性复合材料加筋结构

  • 安学锋;张明;唐邦铭;益小苏
作者信息 +

Manufacture of Thermoplastic Matrix Composite Stiffened Panel Using Flexible Co-woven Prepreg

  • AN Xue-feng;ZHANG Ming;TANG Bang-ming;YI Xiao-su
Author information +
文章历史 +

摘要

PEEK树脂基复合材料具有突出的韧性和高损伤容限,但因成型工艺条件较为苛刻,且铺覆性能差,影响了曲面成型能力。利用柔性混编预浸料技术则可解决这一难题,高质量、高效率地实现复杂曲面结构件的制备。分别带有“L”型加强筋和帽型材的加筋口盖的制造,对此进行了充分的验证。

Abstract

PEEK matrix composites exhibit great toughness and damage resistance.But the severe processing conditions and poor drapability result in in-efficiency in curved surface forming.This difficulty can be solved by flexible co-woven prepreg technology,facilitating the manufacture of complex curved surface structure with high quality and efficiency.The advantage of this flexible prepreg was demonstrated through the manufacture of stiffened panels with L stiffers and U stiffers,respectively.

关键词

热塑性复合材料 / 柔性预浸料 / 曲面成型 / 共固结

Key words

thermoplastic matrix / flexible prepreg / curved surface formi / co-consolidation

引用本文

导出引用
安学锋;张明;唐邦铭;益小苏. 柔性混编预浸料制造热塑性复合材料加筋结构[J]. 航空材料学报, 2006, 26(3): 217-221
AN Xue-feng;ZHANG Ming;TANG Bang-ming;YI Xiao-su. Manufacture of Thermoplastic Matrix Composite Stiffened Panel Using Flexible Co-woven Prepreg[J]. Journal of Aeronautical Materials, 2006, 26(3): 217-221

参考文献

张凤翻,李元珍,娄葵阳,等.PEEK基体热塑性树脂基复合材料的研究[J].材料工程,1996,6:40-44.
赵巍,杨德安,梁崇,等.PEEK及其复合材料的研究与应用[J].材料导报,2003,17(9):68-70.
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王克俭,益小苏,唐邦铭,等.用共固结和热变形成型技术制造热塑性复合材料加筋结构[J].航空材料学报,2005,25(3):16-20.
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