Nanostructured Coatings for Corrosion Protection of Aluminum Alloys

  Dr. Robert A. Mantz
Air Force Research Laboratory, Materials and Manufacturing Directorate
WPAFB , OH   45433-7750
Phone:  937-255-2199 / Fax:  937-255-2176
Email:  robert.mantz@wpafb.af.mil

Abstract:  The aging U.S. Air Force legacy aircraft fleet (e.g., KC-135, C-130, F-15, etc.) has a well-documented corrosion problem.  Corrosion protection of aluminum-skinned aircraft and development of improved environmentally benign surface treatments for aluminum aerospace alloys are high priority topics for U.S. Air Force and the aerospace industry.  Current coating systems for aircraft corrosion protection are based on a surface treatment, primer, and topcoat.  These coating systems generally utilize a chromated conversion coating (CCC) surface treatment (e.g., Alodine 1200S) and a solvent-borne epoxy-polyamide primer that is pigmented with a strontium chromate inhibitor.  Chemical conversion coatings on aluminum alloys are intended to perform dual functions – to promote adhesion and to improve corrosion resistance of the subsequent organic coating. While traditional chromate-based conversion coatings are very efficient and offer many valuable coating properties, increasing environmental regulations restrict the use of chromates due to the toxicity of hexavalent chromium.  The U.S. Department of Health and Human Services released the 9th Report on Carcinogens (January 2001) in which hexavalent chromium compounds, including the most widely used chromate corrosion inhibitor, strontium chromate, are listed as known human carcinogens.  In addition, OSHA and the FDA all have restrictive exposure limits on hexavalent chromium compounds.  OSHA recently proposed new guidelines reducing the permissible exposure limit from 52 to 1 mg/m3.

Both environmental and toxicity issues are compounded by the fact that these coating system are replaced every 6-8 years on average.  The size of the aging legacy fleet of AA2024-T3 skinned aircraft is rather large and the current trend is to greatly extend these aircraft projected lifetimes, as much as four times the original estimate.  Given the toxic waste products and the environmental impact of the de-paint/paint cycle, the Air Force has a specific need for a chromate free coating systems that can provide long-term environmentally benign corrosion protection.  The Air Force Research Laboratory is developing environmentally benign alternatives to the traditional chromated aircraft coating for aircraft corrosion protection, targeted to a 30+ year performance life cycle.

Cleaning and surface pretreatment are critical steps in protecting aerospace alloys from corrosion.  One promising solution to this complex problem is based on the use of organofunctional silanes and the principles of sol-gel chemistry.  Organosilanes are relatively environmentally friendly chemicals and work well for improving adhesion at the metal/coating interface, providing better corrosion protection.  These materials have been used to engineer nanostructured ceramic coatings for corrosion protection of aluminum aerospace alloys. This advanced hybrid approach is called the Self-assembled NanoPhase (SNAP) coating process.  The approach starts with hydrolysis and condensation reactions of silanes to generate nanomaterials with epoxy functionalities in-situ. The nanomaterials are then crosslinked using epoxy/amine chemistry to form a thin film (1 µm).  The hybrid coatings made by SNAP process are essentially nanocomposite materials and have been demonstrated as a viable alternative for chromate conversion coatings providing exceptional corrosion resistance and long-term coating performance.