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Service evaluation of aluminum-brazed titanium (ABTi)Long term creep-rupture, flight service and jet engine exhaust tests on aluminum-brazed titanium (ABTi), originally initiated under the DOT/SST follow-on program, were completed. These tests included exposure to natural airline service environments for up to 6 years. The results showed that ABTi has adequate corrosion resistance for long time commercial airplane structural applications. Special precautions are required for those sandwich structures designed for sound attenuation that utilize perforated skins. ABTi was also shown to have usable creep-rupture strength and to be metallurgically stable at temperatures up to 425 C (800 F).
Document ID
19810013599
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Elrod, S. D.
(Boeing Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1981
Publication Information
Publisher: NASA
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-CR-3418
D6-48609
Report Number: NASA-CR-3418
Report Number: D6-48609
Accession Number
81N22129
Funding Number(s)
CONTRACT_GRANT: NAS1-13681
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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