Journal of Japan Institute of Light Metals
Online ISSN : 1880-8018
Print ISSN : 0451-5994
ISSN-L : 0451-5994
Effect of the morphology of constituents and dispersoids on fracture toughness and fatigue crack propagation rate in 2024 aluminum alloys
Manabu NAKAITakehiko ETOH
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1995 Volume 45 Issue 11 Pages 677-681

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Abstract

Fracture toughness and fatigue crack propagation rate in 2024 alloys have been investigated through changing the morphologies of constituens and dispersoids. Fracture toughness is proportional to the square root of the spacing of constituents, mainly Cu2FeAl7 in 2024 alloys. Broadening the spacing from 58μm to 140μm, the fracture toughness increases by 18%. The fact that the dimple diameter becomes larger with increasing constituent spacing leads to the increase in fracture toughness. In a low ΔK region, the fatigue crack propagation rate becomes slower mainly by broadening the spacing of dispersoids, Cu2Mn3Al20. Broadening the spacing from 0.45μm to 0.64μm, the propagation rate decreases by 50%. In a high ΔK region, on the other hand, the propagation rate becomes slower mainly by broadening the spacing of constituents.

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