Analysis of “Kiss” Bonds Between Composite Laminates

被引:0
|
作者
Scott L. Poveromo
James C. Earthman
机构
[1] University of California,Department of Chemical Engineering and Materials Science
[2] Irvine,undefined
来源
JOM | 2014年 / 66卷
关键词
Shear Strength; Composite Laminate; Ultrasonic Testing; Epoxy Adhesive; Bonding Surface;
D O I
暂无
中图分类号
学科分类号
摘要
One of the leading challenges to designing lightweight, cost-effective bonded structures is to detect low shear strength “kiss” bonds where no other defects such as voids and cracks exist. To develop a nondestructive testing method that is sensitive to kiss bonds, standards need to be fabricated with known strength values. In the current work, we attempt to create kiss bonds in between carbon fiber composite laminates that have been bonded with epoxy film adhesive and epoxy paste adhesive. Based on ultrasonic testing, when creating true kiss bonds using film adhesives, a complete disbond could not be avoided because of thermally induced stresses during the high-temperature cure. However, further work demonstrated that kiss bonds can be formed using room-temperature curable epoxy paste adhesives by creating an amine blush on the epoxy surface or applying a release agent on the bonding surfaces.
引用
收藏
页码:970 / 978
页数:8
相关论文
共 50 条
  • [31] Failure analysis of laminated composite skew laminates
    Kumar, Ajay
    Chakrabarti, Anupam
    PLASTICITY AND IMPACT MECHANICS, 2017, 173 : 1560 - 1566
  • [32] Multicontinuum failure analysis of composite structural laminates
    Mayes, JS
    Hansen, AC
    MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES, 2001, 8 (04): : 249 - 262
  • [33] Performance Analysis of Ply Orientation in Composite Laminates
    Kumari, N. B. V. Lakshmi
    Mehar, Afroz
    Abdulrahman, Mohammed
    Tatineni, Sheetal
    Shashank, Ellendula Venkateshwara
    Muthyala, Jonathan Ted
    MATERIALS TODAY-PROCEEDINGS, 2018, 5 (02) : 5984 - 5992
  • [34] Damping analysis of orthotropic composite materials and laminates
    El Mahi, Abderrahim
    Assarar, Mustapha
    Sefrani, Youssef
    Berthelot, Jean-Marie
    COMPOSITES PART B-ENGINEERING, 2008, 39 (7-8) : 1069 - 1076
  • [35] A THEORY FOR STRESS-ANALYSIS OF COMPOSITE LAMINATES
    VALISETTY, RR
    REHFIELD, LW
    AIAA JOURNAL, 1985, 23 (07) : 1111 - 1117
  • [36] Analysis of Allowable Assembly Forces for Composite Laminates
    Zhang, Tingyu
    Zhang, Chong
    Zhao, Jianshe
    Guo, Anru
    4TH INTERNATIONAL CONFERENCE ON ADVANCED MATERIALS RESEARCH AND MANUFACTURING TECHNOLOGIES (AMRMT 2019), 2019, 647
  • [37] COMPARATIVE ANALYSIS OF THE ENGINEERING CONSTANTS OF COMPOSITE LAMINATES
    Hudisteanu, Iuliana
    Taranu, Nicolae
    Entuc, Ioana-Sorina
    Maxineasa, Sebastian George
    REVISTA ROMANA DE MATERIALE-ROMANIAN JOURNAL OF MATERIALS, 2016, 46 (02): : 232 - 241
  • [38] A hierarchical iterative procedure for the analysis of composite laminates
    Mitchell, JA
    Reddy, JN
    COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2000, 181 (1-3) : 237 - 260
  • [39] Impact analysis of composite laminates with multiple delaminations
    Hu, N
    Sekine, H
    Fukunaga, H
    Yao, ZH
    INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1999, 22 (06) : 633 - 648
  • [40] ANALYSIS OF CREEP AND RELAXATION IN COMPOSITE LAMINATES WITH HOLES
    HWANG, IH
    LIN, KY
    AIAA/ASME/ASCE/AHS/ASC 30TH STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE, PTS 1-4: A COLLECTION OF TECHNICAL PAPERS, 1989, : 2064 - 2070