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Contamination and Surface Preparation Effects on Composite BondingResults presented here demonstrate the effect of several prebond surface contaminants (hydrocarbon, machining fluid, latex, silicone, peel ply residue, release film) on bond quality, as measured by fracture toughness and failure modes of carbon fiber reinforced epoxy substrates bonded in secondary and co-bond configurations with paste and film adhesives. Additionally, the capability of various prebond surface property measurement tools to detect contaminants and potentially predict subsequent bond performance of three different adhesives is also shown. Surface measurement methods included water contact angle, Dyne solution wettability, optically stimulated electron emission spectroscopy, surface free energy, inverse gas chromatography, and Fourier transform infrared spectroscopy with chemometrics analysis. Information will also be provided on the effectiveness of mechanical and energetic surface treatments to recover a bondable surface after contamination. The benefits and drawbacks of the various surface analysis tools to detect contaminants and evaluate prebond surfaces after surface treatment were assessed as well as their ability to correlate to bond performance. Surface analysis tools were also evaluated for their potential use as in-line quality control of adhesive bonding parameters in the manufacturing environment.
Document ID
20170006189
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Kutscha, Eileen O.
(Boeing Research and Technology Seattle, WA, United States)
Vahey, Paul G.
(Boeing Research and Technology Seattle, WA, United States)
Belcher, Marcus A.
(Boeing Research and Technology Seattle, WA, United States)
VanVoast, Peter J.
(Boeing Research and Technology Seattle, WA, United States)
Grace, William B.
(Boeing Research and Technology Seattle, WA, United States)
Blohowiak, Kay Y.
(Boeing Research and Technology Seattle, WA, United States)
Palmieri, Frank L.
(NASA Langley Research Center Hampton, VA, United States)
Connell, John W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
July 6, 2017
Publication Date
May 22, 2017
Subject Category
Composite Materials
Report/Patent Number
NF1676L-26032
Report Number: NF1676L-26032
Meeting Information
Meeting: SAMPE 2017
Location: Seattle, WA
Country: United States
Start Date: May 22, 2017
End Date: May 25, 2017
Sponsors: Society for the Advancement of Materials and Process Engineering
Funding Number(s)
WBS: WBS 826611.04.07.03.05
Distribution Limits
Public
Copyright
Public Use Permitted.
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