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Effect of thermal exposure, forming, and welding on high-temperature, dispersion-strengthened aluminum alloy: Al-8Fe-1V-2SiThe feasibility of applying conventional hot forming and welding methods to high temperature aluminum alloy, Al-8Fe-1V-2Si (FVS812), for structural applications and the effect of thermal exposure on mechanical properties were determined. FVS812 (AA8009) sheet exhibited good hot forming and resistance welding characteristics. It was brake formed to 90 deg bends (0.5T bend radius) at temperatures greater than or equal to 390 C (730 F), indicating the feasibility of fabricating basic shapes, such as angles and zees. Hot forming of simple contoured-flanged parts was demonstrated. Resistance spot welds with good static and fatigue strength at room and elevated temperatures were readily produced. Extended vacuum degassing during billet fabrication reduced porosity in fusion and resistance welds. However, electron beam welding was not possible because of extreme degassing during welding, and gas-tungsten-arc welds were not acceptable because of severely degraded mechanical properties. The FVS812 alloy exhibited excellent high temperature strength stability after thermal exposures up to 315 C (600 F) for 1000 h. Extended billet degassing appeared to generally improve tensile ductility, fatigue strength, and notch toughness. But the effects of billet degassing and thermal exposure on properties need to be further clarified. The manufacture of zee-stiffened, riveted, and resistance-spot-welded compression panels was demonstrated.
Document ID
19910022886
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kennedy, J. R.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Gilman, P. S.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Zedalis, M. S.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Skinner, D. J.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Peltier, J. M.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.26:187575
NASA-CR-187575
RE-787
Report Number: NAS 1.26:187575
Report Number: NASA-CR-187575
Report Number: RE-787
Accession Number
91N32200
Funding Number(s)
PROJECT: RTOP 505-63-50-02
CONTRACT_GRANT: NAS1-18533
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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