Abstract

For more than six decades, chromic acid anodizing has been the main step in the surface treatment of aluminum for adhesively bonded aircraft structures. Soon this process, known for producing a readily adherent oxide with an excellent corrosion resistance, will be banned by strict international environmental and health regulations. Replacing this traditional process in a high-demanding and high-risk industry such as aircraft construction requires an in-depth understanding of the underlying adhesion and degradation mechanisms at the oxide/resin interface resulting from alternative processes. The relationship between the anodizing conditions in sulfuric and mixtures of sulfuric and phosphoric acid electrolytes and the formation and durability of bonding under various environmental conditions was investigated. Scanning electron microscopy was used to characterize the oxide features. Selected specimens were studied with transmission electron microscopy coupled with energy-dispersive X-ray spectroscopy to measure resin concentration within structurally different porous anodic oxide layers as a function of depth. Results show that there are two critical morphological aspects for strong and durable bonding. First, a minimum pore size is pivotal for the formation of a stable interface, as reflected by the initial peel strengths. Second, the increased surface roughness of the oxide/resin interface caused by extended chemical dissolution at higher temperature and higher phosphoric acid concentration is crucial to assure bond durability under water ingress. There is, however, an upper limit to the beneficial amount of anodic dissolution above which bonds are prone for corrosive degradation. Morphology is, however, not the only prerequisite for good bonding and bond performance also depends on the oxides’ chemical composition.

Highlights

  • Long-term service of adhesively bonded aircraft structures relies upon the durability of adhesion between the aluminum substrates and the adhesive

  • The results in this study demonstrate that the anodizing conditions are crucial in determining the adhesive bond strength and durability

  • The most dominant parameters that determine the final morphology of the oxide are the electrolyte composition and the anodizing temperature

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Summary

INTRODUCTION

Long-term service of adhesively bonded aircraft structures relies upon the durability of adhesion between the aluminum substrates and the adhesive. Industrial and scientific research has greatly contributed to our understanding of the changes that take place during surface treatments of aluminum and its alloys, as well as the influence of different processing parameters.[4] the excellent adhesion and corrosion resistance that is achieved by the complete Cr(VI)-based pre-treatment process currently applied by the European aerospace industry is not duplicated.[5] Since strict international environmental and health regulations announced the near future ban of Cr(VI), its replacement has become a critical and timely issue.[6] Reviewing the literature to date, the high strength of these bonded structures is attributed to the accumulated effect of two main mechanisms: (1) mechanical interlocking and (2) chemical interactions and physical interactions between the oxide and the organic resin.[7,8,9] their extent and role remains unclear. More aggressive coupled with energy-dispersive X-ray spectroscopy (EDS) and anodizing conditions that include phosphoric acid and higher related to its resulting bonding performance measured using temperatures cause such extended dissolution that collapses the floating roller peel tests

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