铝
铝合金
合金
汽车工业
材料科学
冶金
工程类
航空航天工程
作者
R. Jones,Jan Čížek,Ondřej Kovářı́k,Andrew Siao Ming Ang,Victor K. Champagne
标识
DOI:10.1016/j.addlet.2022.100026
摘要
Scalmalloy® has been proposed for use as additively manufactured (AM) replacement aluminium alloy parts for civil and military aircraft, and for AM aluminium parts for use in satellites and space structures. This study builds on the results of a prior investigation to reveal that Scalmalloy® has a crack growth curve similar to those associated with aluminium alloys AA5754 and AA6061-T6, which are widely used in the automotive industry and in maritime vessels. The R = 0.1 da/dN versus ΔK curve for small naturally occurring cracks in LPBF Scalmalloy® is also predicted and the additive manufacturing community is challenged to undertake testing to validate or disprove this prediction.
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