4.3 Article

Enhancing the Environmentally Assisted Cracking Resistance of Aircraft Quality Al Alloy of Type AA7075 Stiffened with Polymer Matrix Composite Using Cerium Chloride Inhibitor

Journal

TRANSACTIONS OF THE INDIAN INSTITUTE OF METALS
Volume 71, Issue 12, Pages 3021-3027

Publisher

SPRINGER INDIA
DOI: 10.1007/s12666-018-1403-z

Keywords

Aluminum alloy; Polymer matrix composite; Cerium chloride; Inhibitor; Stress corrosion; Asymmetric stiffener

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This study explores a methodology to raise environmentally assisted cracking resistance of alclad Al-Zn-Mg-Cu (AA7075) alloy, used in aircraft structures, stiffened with polymer matrix composite asymmetric patch in order to suppress growth of fatigue cracks. Fracture mechanics studies of adhesively bonded center-pre-cracked Al alloy specimens having stiffeners were carried out in 3.5 wt% sodium chloride environment to understand the effect of cerium chloride inhibitor on the threshold stress intensity for stress corrosion cracking as well as the second-stage (steady-state) crack growth rate. It was observed that in the peak- and the two-step-aged tempers, the crack growth rate of the alloy reduced by two and a half, and four times, respectively, while the threshold stress intensity increased by 14-15% due to the addition of 1000 ppm of this inhibitor. The study offers a method to enhance significantly life of aging aircrafts stiffened with polymer matrix composite.

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