Design of Corrosion Protective and Antistatic Hybrid Sol-Gel Coatings on 6XXX AlMgSi Alloys for Aerospace Application

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Resumen

An inorganic–organic coating based on glycidyl-functionalized silica and zirconia was synthesized by sol-gel technology to protect three types of AlMgSi (6XXX series) alloys against corrosion in aerospace applications. Different parameters such as the solid content, the organic/inorganic ratio of the sols and the deposition conditions were studied with the aim to achieve a tradeoff between the corrosion protection, antistatic performance and low vacuum-induced outgassing. Those parameters directly influence the thickness and the density of the coatings, and therefore the barrier effect against corrosion and the contact electrical resistance, which are affected in opposite ways. To obtain a low contact electrical resistance, silver nanowires (NW) with a high aspect ratio were loaded in the sol-gel matrix with the aim to create a conductive path through the hybrid coating with a low concentration of NWs. The coatings were adapted for AA6063, AA6061 and AA6082, and they all showed an outstanding anti-corrosion performance in different artificial weathering tests, whereas electrochemical impedance spectroscopy permitted the identification of the most critical parameters affecting water uptake. An antistatic performance was demonstrated by the low contact electrical resistance of the coated AA6061 and AA6063 alloys, although the incorporation of NWs showed a detrimental effect on the corrosion protection compared with the unloaded coating
Idioma originalInglés
Número de artículo441
Páginas (desde-hasta)441
Número de páginas1
PublicaciónCoatings
Volumen10
N.º5
DOI
EstadoPublicada - 30 abr 2020

Palabras clave

  • Corrosion protection
  • Hybrid sol-gel coating
  • Aerospace
  • Outgassing
  • AlMgSi
  • 6XXX

Project and Funding Information

  • Project ID
  • info:eu-repo/grantAgreement/EC/H2020/640143/EU/Flight Qualification of Deployable Radiator using Two Phase Technology /PEGASUS
  • Funding Info
  • This work has received funding from the European Union’s Horizon 2020 Research and Innovation Programme within the project PEGASUS under Grant Agreement no. 640143; from the European Space Agency within ESA ITI Programme under contract number 4000124218 (IRUCOAT4SPACE project) and from the Basque Government through FRONTIERS IV project (ELKARTEK 2018, KK-2018/00108).

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