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Environmental Durability of Aircraft Aluminum Alloy Skin Materials Cessna Aircraft Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Patni, K., author.
Conference Name:
General, Corporate & Regional Aviation Meeting & Exposition (1993-05-17 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1993
Summary:
This paper compares the environmental durability of currently used as well as some of the potential aircraft aluminum alloy skin materials. A simple test was developed to evaluate the environmental durability by simultaneous application of fatigue loads and aerated salt water attack. Alclad alloys showed excellent resistance to corrosion fatigue. On the other hand, 7475 alloy and new potential material 6013 alloy experienced inter-granular corrosion at the fatigue crack origin area. The test results also indicated the significance of corrosion preventive coatings to increase the age of aircraft
Notes:
Vendor supplied data
Publisher Number:
931229
Access Restriction:
Restricted for use by site license

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