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青山 高士; Choudhary, S.*; Pandaleon, A.*; Burns, J. T.*; Kokaly, M.*; Restis, J.*; Ross, J.*; Kelly, R. G.*
Corrosion, 81(6), p.609 - 621, 2025/06
被引用回数:1 パーセンタイル:46.46(Materials Science, Multidisciplinary)This study presents a new test method for inducing controlled corrosion damage within simulated fastener holes of aluminum alloys, aimed at pretreating fatigue test specimens. The method involves insulating the outer surface while exposing the fastener hole surface to electrolytes containing 0.66 M NaCl + 0.1 M AlCl
with varying concentrations of K
S
O
. The evolution of corrosion damage within the fastener hole was examined as a function of exposure duration, electrolyte composition, and volume, as well as the effect of galvanic coupling with a SS316 cathode. Results indicate that fissure depth increases with an increase in K
S
O
concentration but does not progress further after 24-48 hours of exposure in the chemical, or freely-corroding, exposure test. In contrast, galvanic coupling with a SS316 plate significantly accelerates corrosion, leading to much deeper fissures in a shorter time. The importance of electrolyte replenishment has been explored using electrochemical measurements, revealing the impact of evolving electrolyte chemistry. Beyond its application in fatigue specimen pretreatment, this method provides a simple yet effective approach for studying localized corrosion and evaluating mitigation strategies for fastener holes in aerospace structures.
Choudhary, S.*; 青山 高士; Pandaleon, A.*; Burns, J. T.*; Kokaly, M.*; Restis, J.*; Ross, J.*; Kelly, R. G.*
no journal, ,
This study introduces novel test methods for inducing controlled corrosion damage within fastener holes of aluminum alloys, providing a practical approach for pretreating fatigue test specimens. By selectively exposing the fastener hole surface to electrolytes containing 0.66 M NaCl+ 0.1 M AlCl
, and varying concentrations of K
S
O
, we have investigated the evolution of localized corrosion under both freely corroding and galvanically coupled conditions. Our findings highlight the role of oxidizer concentration, exposure duration, and electrolyte replenishment in fissure development, while demonstrating the significant acceleration of corrosion through galvanic coupling with a SS316 cathode. Beyond its immediate application in fatigue testing, this method offers broader utility for studying localized corrosion mechanisms within the fastener hole and evaluating mitigation strategies relevant to aerospace structures.