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复合材料贴片修补内部穿透裂纹的粘弹性分析
引用本文:陈保兴,张相周.复合材料贴片修补内部穿透裂纹的粘弹性分析[J].航空学报,1989,10(7):338-345.
作者姓名:陈保兴  张相周
作者单位:西北工业大学 (陈保兴),西北工业大学(张相周)
摘    要: 本文研究用复合材料贴片修补含裂纹弹性板件的强度分析问题,着重考虑贴片或胶粘剂的各种粘弹性性质。获得了裂纹尖端应力强度因子及其随时间的变化关系,论述了复合材料贴片修补技术对结构强度的影响与作用。

关 键 词:裂纹  复合材料贴片  粘弹性  
收稿时间:1988-06-08;

VISCOELASTIC ANALYSIS OF CRACKED PLATES REPAIRED WITH COMPOSITE PATCHES
Northwestern Polytechnical University Chen BaoXing Zhang Xiangzhou.VISCOELASTIC ANALYSIS OF CRACKED PLATES REPAIRED WITH COMPOSITE PATCHES[J].Acta Aeronautica et Astronautica Sinica,1989,10(7):338-345.
Authors:Northwestern Polytechnical University Chen BaoXing Zhang Xiangzhou
Institution:Northwestern Polytechnical University Chen BaoXing Zhang Xiangzhou
Abstract:In this article the strength analysis of cracked plates repaired with composite patches is investigated. Emphasis is laid on the consideration of various viscoelastic behaviors of patches or adhesives. By taking the forces in the repaired zone as basic unknowns, the problem is formulated exactly and the stress intensity factors at crack tips are obtained in closed form for point bond cases. For full and partial bond cases, the problem is reduced to a Fredholm integral equat on of the first or second kind, depending on whether the effect of the adhesives is excluded or included in the consideration. Through numerical solution of the Fredholm integral equations, the variation of the stress intensity factors with respect to time is obtained and presented in graphical and tabular forms for various patch sizes, viscoelastic models, locations of the patches and bonded ranges. The results indicate that the stress intensity factors increase progressively with time, or, the reinforcement effect of patches on cracked plates decays monotonously due to the viscoelastic behavior of patches or adhesives. This paper shows that the viscoelastic effect should be taken into account in the strength analysis of cracked structures repaired by composite patches and provides the idealized models, basic equations and solution methods for the problem.
Keywords:crack  composite patch  viscoelastisity    
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