航空工程进展
航空工程進展
항공공정진전
ADVANCES IN AERONAUTICAL SCIENCE AND ENGINEERING
2012年
1期
64-70
,共7页
叶军%陈普会%崔卫军%李庆飞
葉軍%陳普會%崔衛軍%李慶飛
협군%진보회%최위군%리경비
复合材料加筋板%内聚单元%渐进损伤分析%损伤扩展%损伤抑制带
複閤材料加觔闆%內聚單元%漸進損傷分析%損傷擴展%損傷抑製帶
복합재료가근판%내취단원%점진손상분석%손상확전%손상억제대
composite stiffened panel%cohesive element%progress damage analysis%damage propagation%tear strap
研究损伤抑制带对损伤扩展的抑制机理以及损伤止裂效果对于提高结构强度和效率具有重要意义。采用渐进损伤分析方法和有限元模型分析了抑制带对蒙皮/筋条的损伤扩展的抑制情况和发生机理;讨论了损伤抑制带数量和其沿蒙皮厚度的分布等设计变量对结构剩余强度的影响。结果表明:0°损伤抑制带将蒙皮损伤抑制在缘条附近并维持一段加载历程,从而提高了复合材料加筋板的承载能力;蒙皮的失效应力随着0°损伤抑制带层数的增加而增加;对于相同数量的0°损伤抑制带,其沿着蒙皮厚度的不同分布对结构承载能力的影响很小。
研究損傷抑製帶對損傷擴展的抑製機理以及損傷止裂效果對于提高結構彊度和效率具有重要意義。採用漸進損傷分析方法和有限元模型分析瞭抑製帶對矇皮/觔條的損傷擴展的抑製情況和髮生機理;討論瞭損傷抑製帶數量和其沿矇皮厚度的分佈等設計變量對結構剩餘彊度的影響。結果錶明:0°損傷抑製帶將矇皮損傷抑製在緣條附近併維持一段加載歷程,從而提高瞭複閤材料加觔闆的承載能力;矇皮的失效應力隨著0°損傷抑製帶層數的增加而增加;對于相同數量的0°損傷抑製帶,其沿著矇皮厚度的不同分佈對結構承載能力的影響很小。
연구손상억제대대손상확전적억제궤리이급손상지렬효과대우제고결구강도화효솔구유중요의의。채용점진손상분석방법화유한원모형분석료억제대대몽피/근조적손상확전적억제정황화발생궤리;토론료손상억제대수량화기연몽피후도적분포등설계변량대결구잉여강도적영향。결과표명:0°손상억제대장몽피손상억제재연조부근병유지일단가재역정,종이제고료복합재료가근판적승재능력;몽피적실효응력수착0°손상억제대층수적증가이증가;대우상동수량적0°손상억제대,기연착몽피후도적불동분포대결구승재능력적영향흔소。
Study on mechanism and crack arrest effect of tear strap is of the important significance for increasing the strength and efficiency of structure.The method based on progressive damage analysis and Finite Element Model is used to analyze the inhibition and mechanism of tear strap,the effects of different number of tear straps and the distribution of tear straps along the thickness on the residual strength of composite stiffened panel are discussed.The result shows that,the damage of skin is inhibited on the near of edge strip by 0°damage tear strap and maintain a history of loading,so bearing capacity of composite stiffened panel is improved,failure stress of skin increases by increase of ply number of 0°damage tear strap,for the same number of 0°damage tear strap,the different distribution along the thickness of skin is of a little influence for bearing capacity of structure.