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Laser Surface Preparation and Bonding of Aerospace Structural CompositesAdhesive bonds are critical to the integrity of built-up structures. Disbonds can often be detected but the strength of adhesion between surfaces in contact is not obtainable without destructive testing. Typically the number one problem in a bonded structure is surface contamination, and by extension, surface preparation. Standard surface preparation techniques, including grit blasting, manual abrasion, and peel ply, are not ideal because of variations in their application. Etching of carbon fiber reinforced plastic (CFRP) panels using a neodymium-doped yttrium aluminum garnet (Nd:YAG) laser appears to be a highly precise and promising way to both clean a composite surface prior to bonding and provide a bond-promoting patterned surface akin to peel ply without the inherent drawbacks from the same (i.e., debris and curvature). CFRP surfaces prepared using laser patterns conducive to adhesive bonding were compared to typical prebonding surface treatments through optical microscopy, contact angle goniometry, and post-bonding mechanical testing.
Document ID
20100021129
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Belcher, M. A.
(National Inst. of Aerospace Hampton, VA, United States)
Wohl, C. J.
(National Inst. of Aerospace Hampton, VA, United States)
Hopkins, J. W.
(NASA Langley Research Center Hampton, VA, United States)
Connell, J. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
May 17, 2010
Subject Category
Composite Materials
Report/Patent Number
NF1676L-9374
Meeting Information
Meeting: SAMPE 2010 Conference
Location: Seattle, WA
Country: United States
Start Date: May 17, 2010
End Date: May 20, 2010
Sponsors: Society for the Advancement of Materials and Process Engineering
Funding Number(s)
WBS: WBS 698259.02.07.07.04
Distribution Limits
Public
Copyright
Public Use Permitted.
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