宇航材料工艺2017，Vol.47Issue(2)：29-33,5.DOI:10.12044/j.issn.1007-2330.2017.02.007
钛合金板铆接修理复合材料机身蒙皮分析
Research on Composite Fuselage Skin Repair With Titanium Plates Riveting
摘要
Abstract
Fuselage skin is all-composite in Boeing 787.Repair programs for composite fuselage skin are given in Boeing 787 structural repair manual,including composite fuselage skin repair with titanium plates riveting.However,the maintenance theory of these repair programs and repair procedures,strength,stiffness and other mechanical properties of these repair programs are not described.Based on this,two dimensional finite element models of composite fuselage skin repair with titanium plates riveting are established in this paper.Stress size and distribution of matrix,patch and fill flat are analyzed on these two repair programs.Studies have shown that repairing large composite fuselage skin penetration crack with titanium plates riveting can meet the static strength requirements.Destroy sources of titanium patches of these two repair programs will occur at different locations.关键词
复合材料/机身蒙皮/损伤/修理Key words
Composite/Fuselage skin/Damage/Repair分类
航空航天引用本文复制引用
刘礼平,戚春亮,王瑞峰,徐建新,周志强..钛合金板铆接修理复合材料机身蒙皮分析[J].宇航材料工艺,2017,47(2):29-33,5.基金项目
国家自然科学基金(基金号51405491) （基金号51405491）
国家自然科学基金(基金号51605331) （基金号51605331）
中央高校基本科研业务费(3122017028) （3122017028）
