SAE AMS 4330B Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged
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SAE AMS 4330B Document Information:
Title
Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged
SAE International
Publication Date:
Nov 1, 2004
Scope:
Form:
This specification covers an aluminum alloy in the form of plate.
Application:
These products have been typically used in aerospace applications
where low density is needed in
combination with moderate strength, high fatigue resistance, good
stress corrosion properties, and
improved stiffness, but usage is not limited to such applications.
Keywords:
-
Aluminum alloy
-
plate
-
solution heat treated
-
aging
-
2297-T87
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