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Evaluation of high-temperature structural adhesives for extended serviceCandidate high-temperature stable resin formulations were evaluated for adhesive properties when bonded to titanium treated with various surface preparations. The adhesive formulations included LARC-13, NR150 A2, NR150 B2, NR056X, FM-34, HR-602, and polyphenylquinoxaline. Eight titanium surface preparations were compared for resulting bond strength with the candidate adhesives. After initial evaluation, three adhesive systems (comprised of adhesive, primer, and titanium surface preparation) were selected for further screening. The screening (still in progress) includes cure-cycle optimization and bond properties from 219 K (-65 F) to 505 K (450 F), after isothermal aging at 505 K (450 F) up to 15,000 hours, and after humidity aging at 322 K 9120 F)/ 95 percent R. H. for up to 2000 hours. Larger-area bond capability of the three adhesive system can be demonstrated by fabrication of 30.5 cm (12 in) square titanium honeycomb sandwich and metal-to-metal bonded panels.
Document ID
19810009487
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hendricks, C. L.
(Boeing Aerospace Co. Seattle, WA, United States)
Hill, S. G.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1980
Publication Information
Publication: NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2,
Subject Category
Nonmetallic Materials
Accession Number
81N18010
Funding Number(s)
CONTRACT_GRANT: NAS1-15605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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