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加载速率对复合材料粘接修理金属结构力学性能的影响 被引量:10

Loading rate effect on mechanical property of metallic structure repaired with bonded composite patch
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摘要 基于复合材料补片基体和胶层树脂黏弹性的特点,分别采用光固化和传统热固化方式制备了一系列不同树脂配方的试样,实验研究了树脂配方对修理结构应变率效应的影响,测定了复合材料粘接修理结构在不同加载速率下的力学性能。结果表明,树脂体系的交联度较低时,应变率效应更明显;加载速率的提高通常会使补片更好地发挥分担载荷的作用,但是也会导致变形协调能力的下降;这两个因素共同影响复合材料粘接结构的最终修理效率。加载速率对于复合材料粘接修理结构的破坏模式也有影响。 In light of the viscoelastic property of the adhesive and resin matrix of the composite patch, a series of specimens were prepared by UV curing and conventionally thermal curing methods. The effect of the resin formula on the strain rate was investigated. And the effect of the loading rate on the bonded composite repair structure was studied. Results show that the crosslinking degree of the resin is an important factor affecting the strain rate effect. The lower crosslinking degree may mean the more pronounced strain rate effect. The increase of the loading rate can enhance load-share fraction of the composite patch. However, the stress redistribution function of the composite and adhesive by deformation may be reduced. The loading rate can affect the failure modes of the bonded composite repair structure.
出处 《复合材料学报》 EI CAS CSCD 北大核心 2013年第2期220-225,共6页 Acta Materiae Compositae Sinica
基金 中国博士后科学基金(20110491882)
关键词 粘接修理 复合材料补片 加载速率 力学性能 光固化 bonded repair composite patch loading rate mechanical property UV curing
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  • 1Ali Al-Mansour,程小全,寇长河.单面贴补修理后层合板的拉伸性能[J].复合材料学报,2005,22(3):140-144. 被引量:20
  • 2游敏,郑勇,郑小玲,陈天明.XH-11型胶粘剂最佳固化工艺的研究[J].粘接,1995,16(2):22-24. 被引量:13
  • 3亚当斯R D 陈惠君译.工程结构中的胶接技术[M].北京:北京科学技术出版社,1991..
  • 4吕胜利,程起有,姚磊江,童小燕.损伤复合材料层板胶接修理的优化设计[J].机械强度,2007,29(4):598-600. 被引量:22
  • 5BAKER A A. Repair efficiency in fatigue-cracked aluminum components reinforced with boron/epoxy patches [J]. Fatigue Fract Eng Mater Struct, 1993, 16(2) :753--765.
  • 6BAKER A A, JONES R. Bonded repair of aircraft structures [J]. Dordrecht (The Netherlands) : Martinus-Nijhoff Publishers, 1988, 9(5):145--147.
  • 7BAKER A A, ROSE L R F, JONES R. Advances in the bonded composite repair of metallic aircraft structure [J]. Amsterdam: Elsevier,2002, 13(9) :213-214.
  • 8KUMAR A M, HAKEEM S A. Optimum design of symmetric composite patch repair to centre cracked metallic sheet [J]. Composite Structures, 2000, 49 (2) : 285- 292.
  • 9SCHUBBE J J, MALL S. Investigation of a cracked thick aluminum panel repaired with a bonded composite patch[J]. Eng Fracture Mechanics,1999, 63(1) :305-323.
  • 10RAO V V, SINGH R, MALHOTRA S K. Residual strength and fatigue life assessment of composite patch repaired specimens[J]. Compos Part B. Eng,1999, 30(6):621-627.

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