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Engineering Property Comparisons of Powder Metallurgy (PM) Alloy X7901-T7E69 and Ingot Metallurgy (IM) Alloy Forgings

机译:粉末冶金(pm)合金X7901-T7E69与铸锭冶金(Im)合金锻件的工程特性比较

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Fracture toughness and stress corrosion tests of aircraft aluminum alloys are summarized. Considerably better resistance to crack extension of the IM alloys 7075-T73 and 7050-T736 as compared to the PM alloy X7091-T7E69 is found in the fracture toughness tests for the same test orientation as applied in spectrum fatigue tests. This may be (part of) the explanation for the early static crack extension and the low fatigue crack propagation life with flight simulation loading of PM alloy X7091-T7E69 specimens. The stress corrosion tests under atmospheric conditions show a higher resistance to stress corrosion cracking for the PM alloy X7091-T7E69 than for the IM alloys.

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