US20170144270A1 - Method for producing a corrosion-inhibiting or adhesion-promoting coating - Google Patents

Method for producing a corrosion-inhibiting or adhesion-promoting coating Download PDF

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US20170144270A1
US20170144270A1 US15/127,248 US201515127248A US2017144270A1 US 20170144270 A1 US20170144270 A1 US 20170144270A1 US 201515127248 A US201515127248 A US 201515127248A US 2017144270 A1 US2017144270 A1 US 2017144270A1
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substrate
corrosion
dopant
inhibiting
particles
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Barry TWOMEY
Kenneth STANTON
John O'Donoghue
Kevin Roche
Joseph MOHAN
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EnBIO Ltd
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EnBIO Ltd
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C11/00—Selection of abrasive materials or additives for abrasive blasts
    • B24C11/005—Selection of abrasive materials or additives for abrasive blasts of additives, e.g. anti-corrosive or disinfecting agents in solid, liquid or gaseous form
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C1/00—Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C1/00—Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods
    • B24C1/08—Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods for polishing surfaces, e.g. smoothing a surface by making use of liquid-borne abrasives
    • B24C1/086—Descaling; Removing coating films
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C11/00—Selection of abrasive materials or additives for abrasive blasts
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00—Coating starting from inorganic powder
    • C23C24/02—Coating starting from inorganic powder by application of pressure only
    • C23C24/04—Impact or kinetic deposition of particles
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/134—Plasma spraying
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/18—After-treatment

Definitions

  • the present invention relates to surface treatment techniques in the field of materials science.
  • Abrasion may be defined as the action or process of scraping or grazing something, or of wearing something down by friction; the action or fact of becoming worn down in this way.
  • the bombardment of metal surfaces with abrasive materials is finding an increasing number of technical applications in recent years.
  • Techniques such as grit blasting, shot blasting, sand blasting, and micro abrasion fall under this category of surface treatment techniques.
  • an abrasive material, shot or grit is mixed with a fluid and delivered at high velocity to impinge the surface to be treated.
  • the technique used to deliver the abrasive material can be classified as wet or dry depending on the choice of fluid medium used to deliver the abrasive to the surface, usually water and air respectively.
  • the abrasive can be propelled at the surface using a spinning wheel or paddle using a wheelblast machine. As the wheel turns, the abrasive particles are accelerated and directed toward the target where they impact and abrade as per standard fluid abrasion systems. These systems do not require any fluid or compressed gas to propel the particles at the surface.
  • the generic term “abrasive bombardment” is used to refer to all such techniques in this specification. These techniques are different to shot peen techniques which bombard a surface with rounded particles to alter the stress level in the substrate or to induce a dimpled surface texture without producing significant material abrasion. (For the avoidance of any uncertainty, though, it will be appreciated that abrasive bombardment techniques can potentially alter the stress level in the surface of the substrate, as well as producing material abrasion.)
  • abrasive bombardment includes metal cutting, surface cleaning and the pre-treatment of surfaces to induce desirable texture (surface roughness) for the purposes of enhanced adhesion of further coating materials.
  • HA coated implants are desirable because of the biomimetic properties of the apatite layer but an optimum bonding strength between the titanium surface and the apatite layer is also necessary.
  • Choi et al. (KR 2003-0078480) refer to the use of a single calcium phosphate particle as a grit blasting media for the purposes of embedding the grit in the surface of dental implants but particles in excess of 190 ⁇ m are disclosed.
  • U.S. Pat. No. 6,502,442 refers to the use of sintered HA as the abrasive using water as the fluid medium. Some impregnation of the HA was achieved in this instance as the HA was thermally processed.
  • Muller et al. disclosed blasting particles comprising calcium phosphate contained in a glassy matrix.
  • Other disclosures e.g., U.S. Pat. Nos. 4,752,457 and 6,210,715 describe methods for the manufacture of calcium phosphate micro-spheres usually comprising a polymer component and complex methods of manufacturing the same, but their effectiveness as blasting media was not elucidated.
  • the RocatecTM system for the silicization of metallic and other surfaces also uses individual particles having multiple components. This technology is used extensively in the dental arena. In this instance an alumina particle having an outer adherent layer of silica is propelled at a pre-roughened surface and upon impact the local heat generated in the vicinity of the impact causes the shattered silica outer layer to become fused to the surface through a process referred to as ceramicization.
  • Bru-Magniez et al. (U.S. Pat. No. 6,431,958) have disclosed hard abrasive materials with multiple stratified layers for use in blasting abrasive bombardment techniques to modify surfaces.
  • the purpose of the process was to embed or otherwise attach the stratified layer around the abrasive particles to the surface being treated.
  • the outer layer comprises at least one polymer while the core ceramic material of choice is an oxide, carbide, nitride, or carbonitride.
  • Lange et al. (U.S. Pat. No. 6,468,658) have disclosed a particle composed of a core base material and an outer adherent layer of titanium dioxide for blasting purposes.
  • abrasive bombardment for the purposes of surface modification are to be found in the biomedical sector such as for example the use of micro abrasion to clean the oxide slag from the struts of laser machined coronary stents and the impregnation of the surfaces of pacemakers and defibrillators with silica to increase the adhesion of further polymer coatings to the device.
  • a commonality among these examples is the use of a single type of solid particle in the fluid stream. This may be a pre-treatment step in advance of subsequent coating.
  • U.S. Pat. No. 3,754,976 offers a different approach in which two separate particles are used.
  • the patent describes a process for metal plating which comprises spraying a mixture of metallic powder and small peening particles at high velocity against a surface, said velocity being sufficient to impact and bond said metallic powder onto said surface to form a laminate layer of metal.
  • the process is limited to a combination of a non-abrasive, shot peening particles and metallic powders.
  • U.S. Pat. No. 4,552,784 offers a similar approach, wherein a stream of shot peening particles are combined with a stream of rapidly solidified metal powder particles such that upon impacting the substrate, the metal powder is deposited as a laminate layer upon the metal surface.
  • U.S. Pat. No. 4,753,094 describes a process which comprises spraying a stream of molybdenum disulfide powder mixed with steel shot at a predetermined velocity against the substrate, the velocity being sufficient, when impacting the substrate, to bond minute plate-like particles of molybdenum disulfide to the substrate and form a friction reducing surface thereon.
  • the process makes no mention of abrasive particles and the steel shot used is typically used in the non-abrasive shot peen process.
  • U.S. Pat. No. 8,119,183 and WO 2008/033867 disclose an alternate strategy wherein the abrasive blasting and coating deposition are carried out simultaneously by combining the flow of abrasive and flow of coating precursor (dopant) into a single step to modify the surface of a metal implant.
  • the abrasive is used to remove the oxide layer and bind the dopant to the metal in a single step, thus providing a new method to alter the metal surface of a medical and a range of biologically relevant dopants were described for this coating process.
  • the dopant species are used to improve the biomedical properties of the surface of the device. No corrosion resistant dopants were considered, as the materials used to manufacture medical implants are naturally resistant to corrosion and do not require corrosion protective coatings.
  • a substrate may be susceptible to corrosion, due to the presence of corrosive species in the vicinity of the substrate (for example during use of the substrate, or during subsequent processing or storage of the substrate, etc.). There is therefore a desire to provide a corrosion-inhibiting surface treatment to such a substrate.
  • corrosion-inhibiting should be interpreted broadly, to encompass treatments that reduce the susceptibility of the substrate to corrosion, as well as those which prevent corrosion altogether.
  • Conversion coatings are routinely used to protect metal components in industries such as aerospace, marine, petrochemicals and many others.
  • a conversion coating is a treatment of a metal substrate wherein at least part of the surface is converted into the coating with a chemical or electro-chemical process. Examples include chromate conversion coatings, phosphate conversion coatings and anodizing. The most common reasons for applying conversion coatings are to enhance corrosion protection, to change the surface colour, to increase the surface hardness or to deposit a primer layer on the surface to enhance adhesion of a subsequent layer.
  • Chromate conversion coatings have dominated the corrosion coating market in a number of sectors, but these coatings are diminishing in popularity due to the negative environmental impact of the chromate conversion process, largely due to the toxicity of the hexavalent chromium used in the coating process. This has led to a gradual increase in the significance of phosphate coatings, and particularly zinc phosphate coatings.
  • phosphate conversion coating is a complex process that involves a significant number of steps and involves a multi-stage surface treatment strategy.
  • the first step involves cleaning the surface. This can be accomplished by various methods including immersion in solvents, etching agents, acids, bases, degreasing agents and physical cleaning of the surface using ultrasonic tanks or physical abrasion, using techniques such as grit blasting. Many of these processes involve dangerous or toxic chemicals and are carried out at elevated temperatures.
  • the surface may be then further activated.
  • This can be a physical activation using grit blasting or mechanical abrasion which disrupts the native oxide layer, roughens the surface and leaves active sites available for subsequent binding to the conversion coating during a subsequent step.
  • the surface can be activated using chemical means. For example, pre-treating the surface with colloidal titanium compounds immediately prior to the application of the conversion coating is popular for zinc phosphate coatings. Other compounds like dilute solutions of cupric or nickel sulphates, oxalic acid and polyphosphonates help in increasing the number of initial nuclei formed during the subsequent phosphating step and these pre-treatments yield thin and compact phosphate coatings of fine-grained nature.
  • the activation step can involve a combination of initial grit blasting followed by subsequent chemical activation.
  • Actual phosphate deposition is a standalone processing step and is typically carried out using wet chemical solutions.
  • the substrate is usually immersed in a bath of chemicals.
  • the composition of these baths vary from manufacturer to manufacturer, but all typically contain dilute phosphoric acid based solutions containing alkali metal/heavy metal ions in them alongside suitable accelerators.
  • These baths are typically heated to enhance the rate of reaction and optimise the surface finish.
  • the chemical concentrations of reactants and waste products within the bath steadily alters as the chemical reactions proceed and the bath has to be rigorously monitored and adjusted to maintain optimum performance. For larger parts, the physical size of the component can make chemical baths prohibitively large, complex and difficult to control.
  • a spray phosphating process is used. Although largely similar to the wet chemical bath method, the chemical solution is instead sprayed on to the metal surface and allowed to react.
  • the components are usually washed, dried and then sent for further processing which may include deposition of additional layers, sealants, passivation treatments or paints.
  • the overall phosphating process is slow, complex, requires considerable thermal input and uses harsh, toxic chemicals.
  • mechanically-bonded coatings these are coatings which are bonded to the underlying substrate by mechanical interlocking between the coating and the underlying substrate, rather than being formed as a consequence of the surface of the substrate undergoing a chemical or electro-chemical reaction.
  • a coating that is to be mechanically bonded to the substrate conventionally the surface of the substrate is subjected to a separate pre-treatment process, to roughen the surface of the substrate. This produces, on the microscopic scale, a large number of crevices, depressions or other regions of unevenness in the surface of the substrate, into which the subsequently-applied coating can interlock.
  • Such a roughening process is typically performed by sandblasting, after which the roughened surface is then cleaned.
  • the coating is then applied in a separate process, e.g. by spraying.
  • a separate process e.g. by spraying.
  • the use of separate sandblasting, cleaning and spraying processes in this manner is time consuming and there is a desire to make such a process more efficient.
  • Adhesion-Promoting Coatings (Including Primer Layers)
  • adhesion-promoting refers to coatings which are applied to a substrate to enhance the adhesive character of the surface of the substrate—i.e. to enable, promote or improve the adhesion of the substrate to another material or article with which the coated substrate subsequently comes into contact; or to enable, promote or improve the adhesion of a subsequently-deposited layer to the substrate (the coating thereby serving as a primer layer in respect of the subsequently-deposited layer).
  • a primer layer is a coating that is formed on the surface of a substrate. A subsequent coating is then applied to the primer layer. The primer layer is selected so as to bond well to the substrate, and such that the subsequently-applied coating bonds well to the primer layer. Thus, the primer layer acts as an intermediate layer between the substrate and the subsequently-applied coating, with an overall effect of better bonding between the subsequently-applied coating and the substrate than would be achieved if the primer layer were not present.
  • an adhesion-promoting coating can be formed as a conversion coating or a mechanically-bonded coating on an underlying substrate. In either case, the problems discussed above in relation to conversion coatings and mechanically-bonded coatings (in the context of corrosion inhibition) remain equally applicable.
  • a method of treating a metal substrate comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the metal substrate, to impregnate the surface of the metal substrate with the dopant; wherein the dopant comprises a corrosion-inhibiting species such as to form a corrosion-inhibiting conversion coating at the surface of the metal substrate.
  • metal substrate as used herein should be interpreted broadly, to encompass not only substrates made of substantially pure metals, or of alloys, but also substrates made of composite materials having a metallic component, such as metal matrix composites.
  • the action of the abrasive particles on the surface of the metal substrate aids the impregnation of the corrosion-inhibiting dopant particles into the surface of the metal substrate.
  • the corrosion-inhibiting species is chemically bonded to the substrate.
  • a method of treating a metal substrate comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the metal substrate, to impregnate the surface of the metal substrate with the dopant; wherein the dopant comprises a corrosion-inhibiting species that forms a mechanically-bonded corrosion-inhibiting coating on the surface of the metal substrate.
  • the action of the abrasive particles on the surface of the metal substrate aids the impregnation of the corrosion-inhibiting dopant particles into the surface of the substrate, and also causes folds or twists to be produced at the interface between the substrate and the coating, thereby enhancing the degree of mechanical bonding between the substrate and the coating, and the overall bond strength.
  • Such a process is particularly applicable to substrate materials on which a conversion coating cannot be formed, and provides a way of producing a corrosion-inhibiting coating in a manner that can be readily employed to treat both large and small components, is simple to use, and does not require a multi-step treatment process.
  • the nature of the coating is such that no laminate layer of the dopant results.
  • the method may further comprise removing a metal oxide from a surface of the metal substrate by abrasive blasting, thereby exposing the metal surface; and substantially simultaneously delivering the particles comprising the corrosion-inhibiting dopant from at least one fluid jet to the metal surface to impregnate the surface of the substrate with the dopant.
  • the physical process of the abrasive particles impinging on the surface of the metallic material acts to remove the surface oxide and substantially simultaneously embeds the dopant particles into or onto the surface.
  • the abrasive blasting process can alter the microstructure of the underlying metal, compacting the surface and imparting compressive forces into the metal. This surface compressive stress can also help to reduce stress corrosion cracking as it counteracts the tensile forces that are necessary for crack propagation.
  • the removal of the passivating metal oxide layer exposes a reactive metal underneath.
  • sufficient energy can be released to chemically bond the coating to the substrate.
  • the bond formed by the combination of abrasive and dopant can increase the adhesion and/or durability of the dopant material.
  • the abrasive may also churn and twist the substrate surface such that the dopant is physically mixed into the surface and is not just present as an external surface layer.
  • the deposit contains very little evidence of the abrasive particle. Instead, the substrate surface appears to be preferentially doped with the corrosion-inhibiting material. The abrasive materials appear to bounce off the surface with minimal abrasive grit impregnating the surface. In general, over 90% of the deposit is made up of the corrosion resistant material and less than 10% is derived from the abrasive. In some cases over 99% of the deposit is made up of the corrosion resistant material and less than 1% is derived from the abrasive particles.
  • the layer of corrosion-inhibiting material may be used as a final surface finish which acts as a corrosion resistant layer.
  • the corrosion-inhibiting material may be further covered with one or more additional coating layer(s) to enhance the corrosion resistance (and/or scratch resistance) of the surface.
  • These one or more additional different layer(s) may be applied by spraying, painting, dipping, vapor deposition or any suitable method to apply the subsequent layer(s).
  • the corrosion-inhibiting material may act as a primer onto which these additional layer(s) are able to adhere, thereby enhancing the adhesion strength of the subsequent layer(s) to the substrate metal. Adjusting the abrasive properties, dopant properties or blast conditions can alter the surface topography and chemistry of the deposited layer of corrosion resistant material, thereby optimising the primer surface to deliver improved primer performance.
  • the layer of corrosion-inhibiting material may be deposited over a repaired area on a metal surface.
  • certain repairs such as welding or brazing
  • the bare metal remains exposed and is susceptible to corrosion.
  • the application of a corrosion resistant material cannot be easily accomplished using traditional deposition techniques as field repairs generally occur in situations where complex wet chemical deposition techniques cannot be employed. As such, the repaired regions often suffer from excessive corrosion and can fail again.
  • a simple particle blasting process, as described herein, could be easily used in such a situation to apply a corrosion-inhibiting surface treatment that would protect the repaired region and extend the lifetime of the product.
  • the method disclosed herein offers a one step process which cleans and roughens the surface, while converting the native oxide layer into a corrosion resistant surface. This is accomplished without the use of thermal energy and does not require the use of harmful, toxic or corrosive chemicals.
  • the process is not limited by the size of the substrate and can be readily applied to large-scale engineering components such as pipeline sections, wind turbine components, civil engineering structures, external walls, marine components, automotive body parts or other such large metallic components that routinely suffer from corrosion.
  • the component is a tubular pipe and the coating is applied to the internal or external surface of the pipe. When applied to the internal surface of a pipe, the coating may reduce corrosion and also reduce friction when pumping liquids through the pipe.
  • the dopant is delivered in a gaseous carrier fluid, such as nitrogen, hydrogen, argon, helium, air, ethylene oxide, and combinations thereof.
  • a gaseous carrier fluid such as nitrogen, hydrogen, argon, helium, air, ethylene oxide, and combinations thereof.
  • the dopant is delivered in a liquid carrier fluid.
  • the liquid is also an etching liquid (basic or acidic).
  • the dopant is delivered in an inert environment.
  • the corrosion-inhibiting dopant material may be a chromate, phosphate, polymer (e.g. thermoset or thermoplastic), oxide or a nitride.
  • the dopant may be cerium oxide (ceria).
  • the coating is derived from a phosphate compound.
  • the phosphate may comprise a corrosion-inhibiting transition metal phosphate, such as iron phosphate, manganese phosphate or zinc phosphate, or combinations thereof. As the phosphate is not deposited by an electrochemical process, a range of materials can be incorporated into the surface by modifying the starting dopant powder.
  • the abrasive has a suitable property chosen from at least one of size, shape, hardness, and density to break an oxide layer on the metal substrate.
  • the abrasive has a Mohs hardness ranging from 0.1 to 10, such as a Mohs hardness ranging from 1 to 10, or a Mohs hardness ranging from 5 to 10.
  • the abrasive has a Mohs hardness ranging from 7 to 10.
  • the abrasive has a particle size ranging from 0.1 ⁇ m to 10000 ⁇ m, such as a particle size ranging from 1 ⁇ m to 5000 ⁇ m, or a particle size ranging from 50 ⁇ m to 500 ⁇ m.
  • the particle size of the abrasive is from 10 ⁇ m to 150 ⁇ m.
  • Abrasive materials to be used in this method include but are not limited to shot or grit made from silica, sand, alumina, zirconia, zirconate, barium titanate, calcium titanate, sodium titanate, titanium oxide, glass, biocompatible glass, diamond, silicon carbide, boron carbide, dry ice, boron nitride, calcium phosphate, calcium carbonate, metallic powders, carbon fibre composites, polymeric composites, titanium, stainless steel, hardened steel, carbon steel chromium alloys or any combination thereof.
  • the abrasive bombardment can be used to work harden the surface and this can interact synergistically with the corrosion-inhibiting dopant to limit stress corrosion cracking.
  • the degree of work hardening can be tailored by altering the abrasive properties. Altering the size, shape or chemistry of the abrasive can alter the effects on the substrate. While the surface is severely deformed and is chemically altered by the presence of the dopant, the layers underneath are also altered. While the dopant does not penetrate into this sub-surface zone, the bombardment process can alter the grain structure of the underlying metal. This zone can extend for 10-50 microns and the depth of this zone can be controlled by altering the particle size, hardness or velocity of the abrasive.
  • the pressure of the fluid jet will also be a factor in determining the impact energy of the abrasive.
  • the abrasive and dopant(s) do not have to be delivered to the surface through the same jet. They could be in any number of separate jets as long as they deliver the solid components to the surface at the substantially the same time, e.g., prior to reformation of any oxide layer. This allows a large amount of flexibility in optimizing the invention towards a specific need. For large substrates, multiple nozzles may be used to deliver abrasives and dopants to multiple points on the surface simultaneously, thereby accelerating the overall treatment rate.
  • the fluid jet is selected from wet blasters and abrasive water jet peening machines.
  • the at least one fluid jet operates at a pressure ranging from 0.5 to 100 bar, such as a pressure ranging from 1 to 30 bar, or a pressure ranging from 1 to 10 bar.
  • the at least one fluid jet is selected from dry blasters, wheel abraders, grit blasters, sand blasters, and micro-blasters. In one embodiment, the at least one fluid jet operates at a pressure ranging from 0.5 to 100 bar, such as a pressure ranging from 1 to 30 bar, or a pressure ranging from 3 to 10 bar.
  • blasting equipment can be used in conjunction with controlled motion such as CNC or robotic control.
  • the blasting can be performed in an inert environment.
  • the dopants and abrasives are contained in the same reservoir and are delivered to a surface from the same jet (nozzle).
  • the dopant is contained in one reservoir and abrasive contained in a separate reservoir, and multiple nozzles deliver the dopants and abrasives.
  • the multiple nozzles can take the form of a jet within a jet, i.e., the particles from each jet bombard the surface at the same incident angle.
  • the multiple nozzles are spatially separated so as to bombard the surface at different incident angles yet hit the same spot on the surface simultaneously.
  • the article to be treated is a metal, such as those metals chosen from pure metals, metal alloys, intermetallic compounds or mixtures thereof.
  • metals include iron, zinc, cadmium, tin, silver, titanium, titanium alloys (e.g., NiTi or nitinol), ferrous alloys, stainless steel and stainless steel alloys, carbon steel, carbon steel alloys, aluminum, aluminum alloys, nickel, nickel alloys, nickel titanium alloys, tantalum, tantalum alloys, niobium, niobium alloys, chromium, chromium alloys, cobalt, cobalt alloys, precious metals, and precious metal alloys.
  • a method of treating a substrate comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the substrate, to impregnate the surface of the substrate with the dopant; wherein the dopant comprises an adhesion-promoting species such as to form an adhesion-promoting coating at or on the surface of the substrate.
  • the adhesion-promoting species may form a conversion coating at the surface of the substrate.
  • adhesion-promoting species may be chemically bonded to the substrate.
  • the adhesion-promoting species may form a mechanically-bonded adhesion-promoting coating on the surface of the substrate.
  • the action of the abrasive particles on the surface of the substrate aids the impregnation of the adhesion-promoting dopant particles into the surface of the substrate.
  • the adhesion-promoting species forms a primer layer on the substrate, i.e. the adhesion-promoting species serves as a primer-forming species.
  • a primer-forming species may comprise a fluoropolymer such as PTFE, a perfluoroalkoxy material such as Teflon, polyvinylidene fluoride, perfluoropolyether, a perfluorinated elastomer, or polyvinylfluoride.
  • the primer-forming species may comprise a silane, siloxane, acrylate, epoxy, hydrogen bonded silicon compound or material which contains one or more vinyl, peroxyester, peroxide, acetate or carboxylate functional group.
  • One or more subsequent layers may be applied to the primer layer, such as a scratch-inhibiting layer, a corrosion-inhibiting layer, an adhesive layer, a non-stick surface or a solid low-friction layer (e.g. a fluoropolymer such as PTFE).
  • a scratch-inhibiting layer such as a scratch-inhibiting layer, a corrosion-inhibiting layer, an adhesive layer, a non-stick surface or a solid low-friction layer (e.g. a fluoropolymer such as PTFE).
  • the adhesion-promoting coating may be provided so as to improve the adhesion of the substrate to another material or article with which the coated substrate subsequently comes into contact.
  • the adhesion-promoting may comprise, for example, a silane, siloxane, acrylate, epoxy, hydrogen bonded silicon compound or material which contains one or more vinyl, peroxyester, peroxide, acetate or carboxylate functional group.
  • the second set of particles i.e. the abrasive particles
  • the second set of particles have an average particle size in the range of 1 ⁇ m to 150 ⁇ m, more preferably an average particle size in the range of 10 ⁇ m to 150 ⁇ m, and particularly preferably an average particle in the range of 50 ⁇ m to 150 ⁇ m.
  • the use of small abrasive particles of such dimensions gives rise to enhanced disruption of the surface of the substrate, thereby promoting penetration of the dopant particles into the substrate surface and intermixing of the dopant particles with the substrate surface.
  • the first set of particles i.e. the dopant particles
  • the first set of particles have an average particle size in the range of 1 ⁇ m to 100 ⁇ m.
  • the ratio of the first set of particles to the second set of particles is between 20:80 and 80:20 by weight.
  • the ratio of the first set of particles to the second set of particles is between 40:60 and 60:40 by weight.
  • the first and second sets of particles may be delivered without the use of a carrier fluid.
  • a method of treating a substrate comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the substrate, to impregnate the surface of the substrate with the dopant; wherein the dopant comprises a corrosion-inhibiting or adhesion-promoting species, such as to form a corrosion-inhibiting or adhesion-promoting coating at or on the surface of the substrate.
  • an article comprising a metal substrate having a corrosion-inhibiting conversion coating, the conversion coating comprising particles of a corrosion-inhibiting species that impregnate the surface of the metal substrate.
  • impregnation may be taken to mean a process wherein the dopant is present within the top 20 microns of the metal surface and is intimately intermixed with the metal.
  • the impregnated material may also extend onto or above the metal surface, but it is also to be found penetrating into the metal.
  • the dopant material is not formed as a laminate layer that sits solely on top of the metal substrate.
  • article as used herein should be interpreted broadly, to encompass a component part of a larger product, as well as an overall product.
  • an article comprising a metal substrate having a mechanically-bonded corrosion-inhibiting coating, the mechanically-bonded coating comprising particles of a corrosion-inhibiting species that impregnate the surface of the metal substrate.
  • an article comprising a substrate having an adhesion-promoting coating thereon, the adhesion-promoting coating comprising particles of an adhesion-promoting species that impregnate the surface of the substrate.
  • an article comprising a substrate having a corrosion-inhibiting or adhesion-promoting coating produced by a method in accordance with the first, second, third or fourth aspect of the invention.
  • FIGS. 1 a , 1 b and 1 c schematically illustrate a process for treating a metal substrate
  • FIGS. 2 a , 2 b and 2 c are schematic diagrams of three different nozzle configurations to deliver abrasive particles and dopant particles to a surface;
  • FIG. 3 is a schematic cross-sectional representation of a metal substrate having a corrosion-inhibiting conversion coating
  • FIG. 4 is a schematic cross-sectional representation of a metal substrate having a corrosion-inhibiting conversion coating on which a second layer has been formed;
  • FIG. 5 is a schematic cross-sectional representation of a substrate having an adhesion-promoting coating
  • FIG. 6 is a schematic cross-sectional representation of a substrate having an adhesion-promoting coating serving as a primer layer, onto which a subsequent coating has been formed;
  • FIG. 7 presents the results of lap-shear strength testing following various surface treatments on titanium (in respect of Example 5 discussed below).
  • the present embodiments provide a method of treating a substrate, the method comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the substrate, to impregnate the surface of the substrate with the dopant; wherein the dopant comprises a corrosion-inhibiting or adhesion-promoting species, such as to form a corrosion-inhibiting or adhesion-promoting coating at or on the surface of the substrate.
  • the action of the abrasive particles on the substrate causes a rough interface to be formed between the substrate material and the coating formed thereon. Furthermore, the degree of intermixing between the substrate and dopant species is such that no laminate layer of the dopant results.
  • the present embodiments may be subdivided into three main variants.
  • certain embodiments provide a method of treating a metal substrate, the method comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the metal substrate, to impregnate the surface of the metal substrate with the dopant; wherein the dopant comprises a corrosion-inhibiting species such as to form a corrosion-inhibiting conversion coating at the surface of the metal substrate.
  • other embodiments provide a method of treating a metal substrate, the method comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the metal substrate, to impregnate the surface of the metal substrate with the dopant; wherein the dopant comprises a corrosion-inhibiting species that forms a mechanically-bonded corrosion-inhibiting coating on the surface of the metal substrate.
  • a method of treating a substrate comprising: delivering substantially simultaneously a first set of particles comprising a dopant and a second set of particles comprising an abrasive from at least one fluid jet to a surface of the substrate, to impregnate the surface of the substrate with the dopant; wherein the dopant comprises an adhesion-promoting species such as to form (e.g. by conversion coating or mechanical bonding) an adhesion-promoting coating at or on the surface of the substrate.
  • WO 2008/033867 describes techniques for the substantially simultaneous deposition of first and second sets of particles.
  • WO 2008/033867 does not describe the dopant comprising a corrosion-inhibiting species such as to form a corrosion-inhibiting conversion coating or a mechanically-bonded corrosion-inhibiting coating at or on the surface of the metal substrate (as per the present first and second variants).
  • WO 2008/033867 also does not describe forming an adhesion-promoting coating at or on the surface of the substrate (as per the present third variant).
  • the first and second sets of particles are different from one another (i.e. the dopant species is different from the abrasive).
  • Embodiments of the present method are encompassed in but not limited to the schematic representation shown in FIGS. 1 a , 1 b and 1 c.
  • FIG. 1 a schematically shows a fluid jet (nozzle) 2 that delivers a stream 3 comprising a set of abrasive particles 4 substantially simultaneously with a set of dopant particles 6 .
  • the dopant particles 6 comprise a corrosion-inhibiting species.
  • Particle sets 4 and 6 bombard a surface 10 of a metal substrate 8 , to impregnate the surface of the metal substrate with the corrosion-inhibiting dopant.
  • a chemical or electro-chemical reaction may take place between the dopant species and the substrate material, resulting in the formation of a corrosion-inhibiting conversion coating at the surface of the metal substrate 8 .
  • the energy required to initiate these reactions may be provided by the impact of both sets of particles on the surface.
  • the abrasive particles may not necessarily partake directly in the chemical reaction, but their impact on the surface may provide the activation energy to initiate the conversion reaction.
  • a mechanically-bonded corrosion-inhibiting coating may be formed on the surface of the metal substrate, with some of the corrosion-inhibiting dopant particles mechanically interlocking with the surface of the substrate, the surface having been roughened by the action of the abrasive particles.
  • the formation of the corrosion-inhibiting coating may also involve a combination of both conversion coating and mechanical bonding of the dopant particles to the surface of the substrate.
  • the dopant particles that have been deposited are subjected to ongoing bombardment by the abrasive particles, repeatedly hammering the dopant particles onto and into the surface of the substrate, resulting in an intimate mixing of the substrate and dopant species and a high level of bonding and interlocking between the two, such that, at the corrosion-inhibiting coating, no laminate layer of the dopant results.
  • the surface 10 is a metal oxide layer.
  • the surface oxide layer is disrupted, and breaches in the oxide layer 10 result to expose a new surface 10 a of substrate 8 ( FIG. 1 b ).
  • the newly exposed surface is a metal surface.
  • the dopant particles 6 are integrated into the surface 10 of the substrate 8 ( FIG. 1 c ).
  • Such disruption of the oxide layer, to produce a newly exposed surface of metal is particularly applicable if a chemical or electro-chemical reaction is to take place between the dopant and substrate species, enabling the dopant species to react with the substrate metal (rather than the surface oxide layer).
  • disruption of the oxide layer is also beneficial if the coating is to be mechanically bonded to the substrate 8 .
  • the blasting equipment can be used in conjunction with controlled motion such as CNC (computer numerical control) or robotic control.
  • controlled motion such as CNC (computer numerical control) or robotic control.
  • the blasting can be performed in an inert environment.
  • the dopants and abrasives are contained in the same reservoir and are delivered to a surface from the same jet (nozzle).
  • the dopant is contained in one reservoir and abrasive contained in a separate reservoir, and multiple nozzles deliver the dopants and abrasives.
  • the multiple nozzles can take the form of a jet within a jet, i.e., the particles from each jet bombard the surface at the same incident angle.
  • the multiple nozzles are spatially separated so as to bombard the surface at different incident angles yet hit the same spot on the surface simultaneously.
  • FIGS. 2 a , 2 b and 2 c are schematic diagrams of three different nozzle configurations to deliver the dopants and abrasive to a surface: single nozzle ( FIG. 2 a ); multiple nozzles with dopants and abrasives delivered from separate reservoirs where one nozzle is situated within another nozzle ( FIG. 2 b ); and multiple, separate nozzles with dopants and abrasives delivered from separate reservoirs ( FIG. 2 c ). More specifically, FIG. 2 a shows a single nozzle 20 for delivering a single stream 23 of abrasive particles 24 and corrosion-inhibiting dopant particles 26 to a substrate 28 . FIG.
  • FIG. 2 b shows that multiple nozzles with dopants and abrasives delivered from separate reservoirs can be used, with FIG. 2 b illustrating one nozzle 30 for delivering a stream 33 of abrasive particles 24 situated within another nozzle 40 for delivering a stream 43 of corrosion-inhibiting dopant particles 26 , where streams 33 and 43 are coaxial.
  • Multiple, separate nozzles with dopants and abrasives delivered from separate reservoirs can also be used, as indicated in FIG. 2 c , which shows nozzles 30 and 40 , for delivering streams 33 and 43 of abrasive particles 24 and corrosion-inhibiting dopant particles 26 , respectively.
  • the distance D between the nozzle(s) and the substrate surface can be in the range of 0.1 mm to 100 mm, such as a range of 0.1 mm to 50 mm, or a range of 0.1 mm to 20 mm.
  • the angle of the nozzle to the surface can range from 10 degrees to 90 degrees, such as a range of 30 degrees to 90 degrees, or a range of 70 to 90 degrees.
  • dopant species More than one type of dopant species can be used. It will readily be appreciated that where more than one type of dopant is used, the dopants may be delivered from a single nozzle, or each type may respectively be delivered from a separate nozzle.
  • the layer of corrosion-inhibiting material 52 may be used as a final surface finish which acts as a corrosion resistant layer for the substrate 8 .
  • a corrosion resistant layer 52 may be formed as a conversion coating at the surface of the substrate 8 , or as a layer that is mechanically bonded to the substrate 8 .
  • the corrosion-inhibiting layer 52 may be further covered with one or more additional coating layer(s) 54 to enhance the corrosion resistance (and/or scratch resistance) of the surface.
  • These one or more layer(s) may be applied by spraying, painting, dipping, vapor deposition or any suitable method to apply the subsequent layer(s).
  • the corrosion-inhibiting material 52 may act as a primer onto which these additional layer(s) 54 are able to adhere, thereby enhancing the adhesion strength of the subsequent layer(s) 54 to the substrate metal 8 . Adjusting the abrasive properties, dopant properties or blast conditions can alter the surface topography and chemistry of the deposited layer of corrosion resistant material 52 , thereby optimising the primer surface to deliver improved primer performance.
  • an adhesion-promoting coating is also encompassed in but not limited to the schematic representation shown in FIGS. 1 a , 1 b and 1 c , in this case with the dopant particles 6 comprising an adhesion-promoting species.
  • Particle sets 4 and 6 bombard a surface 10 of a substrate 8 , which in some embodiments may be metal, but in others may be a non-metal (e.g. a polymer or ceramic) or a composite material, so as to impregnate the surface of the substrate 8 with the adhesion-promoting species.
  • the surface 10 may again comprise a metal oxide layer.
  • the surface oxide layer is disrupted, and breaches in the oxide layer 10 result to expose a new surface 10 a of substrate 8 ( FIG. 1 b ).
  • the newly exposed surface is a metal surface.
  • the adhesion-promoting dopant particles 6 are integrated into the surface 10 of the substrate 8 ( FIG. 1 c ).
  • Such disruption of the oxide layer, to produce a newly exposed surface of metal is particularly applicable if a chemical or electro-chemical reaction is to take place between the dopant and substrate species, enabling the dopant species to react with the substrate metal (rather than the surface oxide layer).
  • disruption of the oxide layer is also beneficial if the adhesion-promoting coating is to be mechanically bonded to the substrate 8 .
  • FIGS. 2 a , 2 b and 2 c three different possible nozzle configurations are illustrated schematically in FIGS. 2 a , 2 b and 2 c.
  • a chemical or electro-chemical reaction may take place between the adhesion-promoting species and the substrate material, resulting in the formation of an adhesion-promoting conversion coating at the surface of the substrate 8 .
  • a mechanically-bonded adhesion-promoting coating may be formed on the surface of the substrate, with some of the adhesion-promoting dopant particles mechanically interlocking with the surface of the substrate, the surface having been roughened by the action of the abrasive particles.
  • the formation of the adhesion-promoting coating may also involve a combination of both conversion coating and mechanical bonding of the dopant particles to the surface of the substrate.
  • the dopant particles that have been deposited are subjected to ongoing bombardment by the abrasive particles, repeatedly hammering the dopant particles onto and into the surface of the substrate, resulting in an intimate mixing of the substrate and dopant species and a high level of bonding and interlocking between the two, such that, at the adhesion-promoting coating, no laminate layer of the dopant results.
  • FIG. 5 shows a schematic cross-sectional representation of a substrate 8 having an adhesion-promoting coating 56 , formed either as a conversion coating at the surface of the substrate, or as a mechanically-bonded coating on the surface of the substrate.
  • the adhesion-promoting coating 56 may be deposited in an uncured or semi-cured form, for curing in a separate step using heat, radiation, moisture, etc., prior to the application of any subsequent coating.
  • Such curing may be performed in a localised manner (e.g. using localised infra-red curing).
  • the adhesion-promoting coating 56 may be provided so as to improve the adhesion of the substrate 8 to another material or article with which the coated substrate subsequently comes into contact. That is to say, the production of the adhesion-promoting coating 56 may be the only surface treatment process carried out on the substrate.
  • the adhesion-promoting coating 56 may alternatively serve as a primer layer, onto which a further coating 58 (or a plurality of subsequent coatings) may subsequently be applied.
  • the coating 58 may be, for example, a scratch-inhibiting coating, or a corrosion-inhibiting coating (to inhibit corrosion of the underlying substrate 8 ), or a solid low-friction or non-stick coating such as polytetrafluoroethylene (PTFE), or an adhesive layer to enable the underlying substrate 8 to be adhesively bonded to another article.
  • the coating 58 may comprise some other kind of fluoropolymer layer, a paint layer (e.g. epoxy paint), or a ceramic coating, etc.
  • fluoropolymer layers can also be applied to minimise the accumulation and deposition of unwanted scale, debris, asphaltenes, paraffins or debris which can impair the operation of the underlying substrate.
  • a fluoropolymer primer such as PTFE has been found to be especially beneficial as it allows the thick fluoropolymer coating to be effectively adhered to the substrate underneath. This was unexpected, as the first layer of fluoropolymer which impregnated the substrate would be expected to act as a release layer that would minimise the adhesion of subsequent layers.
  • the subsequently-applied coating 58 may be deposited in an uncured or semi-cured form, for curing in a separate step using heat, radiation, moisture, etc.
  • Such curing may be performed in a localised manner (e.g. using localised infra-red curing).
  • Abrasive species that may be used in any of the above variants of the present method (as a second set of particles, delivered substantially simultaneously with a first, different, set of particles comprising a dopant) include but are not limited to shot or grit made from silica, sand, alumina, zirconia, barium titanate, calcium titanate, sodium titanate, titanium oxide, glass, biocompatible glass, diamond, silicon carbide, boron carbide, dry ice, boron nitride, calcium phosphate, calcium carbonate, metallic powders, carbon fibre composites, polymeric composites, titanium, stainless steel, hardened steel, carbon steel chromium alloys or any combination thereof.
  • the abrasive particles preferably have a hardness of at least 7 on the Mohs scale.
  • the abrasive particles preferably have an average particle size (diameter) in the range of 1 ⁇ m to 150 ⁇ m, more preferably in the range of 10 ⁇ m to 150 ⁇ m, and particularly preferably in the range of 50 ⁇ m to 150 ⁇ m.
  • the use of small abrasive particles of such dimensions gives rise to enhanced disruption of the surface of the substrate, thereby promoting penetration of the dopant particles into the substrate surface and intermixing of the dopant particles with the substrate surface.
  • the dopant species is impregnated into the substrate such that no laminate layer of the dopant results.
  • corrosion-inhibiting dopant species that may be used in the present method (as a first set of particles, different from the second) include but are not limited to a chromate, phosphate, polymer (e.g. a thermoset or a thermoplastic), oxide or a nitride.
  • the dopant may be ceria.
  • the coating is derived from a phosphate compound.
  • the phosphate may comprise iron phosphate, manganese phosphate, zinc phosphate or combinations thereof. As the phosphate is not deposited by an electrochemical process, a range of materials can be incorporated into the surface by modifying the starting dopant powder.
  • the corrosion-inhibiting dopant species need not be a metal or a metal salt, which are inherently sacrificial in nature.
  • Polymer based dopants may be deposited which form a stable deposit on the substrate surface and prevent corrosion by inhibiting the build-up of corrosive materials on the surface or by physically isolating the corrosive species from the underlying substrate. Fluoropolymer, acrylate, acetate and epoxy based layers may all perform this function.
  • the dopant particles preferably have an average particle size (diameter) in the range of 1 ⁇ m to 100 ⁇ m.
  • the ratio of the dopant particles to the abrasive particles is between 20:80 and 80:20 by weight, and particularly preferably is between 40:60 and 60:40 by weight.
  • adhesion-promoting dopant species that may be used in the present method (as a first set of particles, different from the second) include but are not limited to fluoropolymers such as PTFE, perfluoroalkoxy materials such as Teflon, polyvinylidene fluoride, perfluoropolyethers, perfluorinated elastomers, polyvinylfluoride. They may also include silanes, siloxanes, acrylates, epoxys, hydrogen bonded silicon compounds or materials which contain one or more vinyl, peroxyester, peroxide, acetate or carboxylate functional group.
  • fluoropolymers such as PTFE, perfluoroalkoxy materials such as Teflon, polyvinylidene fluoride, perfluoropolyethers, perfluorinated elastomers, polyvinylfluoride. They may also include silanes, siloxanes, acrylates, epoxys, hydrogen bonded silicon compounds or materials which contain one or
  • the primer layer when forming an adhesion-promoting coating to serve as a primer layer for a polymer-based subsequent layer, the primer layer may be composed of the same materials as present within the subsequent layer.
  • PTFE or other fluoropolymers may be used as primer-forming dopant species for the improved adhesion of subsequent fluoropolymer layers.
  • the dopant particles preferably have an average particle size (diameter) in the range of 1 ⁇ m to 100 ⁇ m.
  • the ratio of the dopant particles to the abrasive particles is between 20:80 and 80:20 by weight, and particularly preferably is between 40:60 and 60:40 by weight.
  • Example 1 Deposition of Zinc Phosphate on a Range of Metal Substrates (Aluminium, Copper, Grade 2 and 5 Titanium, Hastelloy, Inconel, Magnesium, Mild Steel, Stainless Steel (316))
  • a series of metal substrates were obtained, made respectively of Aluminium, Copper, Grade 2 and 5 Titanium, Hastelloy, Inconel, Magnesium, Mild Steel and Stainless Steel (316).
  • Zinc phosphate powder ( ⁇ 5 microns average particle size) was mixed in equal volumetric proportions with alumina grit (100 micron average particle size) and then loaded into an Accuflow powder feeder. The powder was fed from there to a grit blast nozzle which was moved over the surface of the metal substrates and the powder was blasted at the surface at a pressure of 75 psi. Following blasting, the substrates were cleaned with compressed air to remove loose powder. All treated samples were visibly noted to have significant levels of zinc phosphate deposited on the surface.
  • Mild steel coupons and buttons were blasted with a mixture of zinc phosphate powder and alumina grit. Following deposition, the samples were analysed using EDX and both types of treated samples were found to have approximately 40% zinc phosphate present on the surface. The coated samples were then immersed in a 3.5% w/w NaCl solution. Untreated mild steel coupons and buttons were used as controls. After 72 hours, the untreated steel samples were visibly discoloured and the sample containers had a significant deposit of brown sediment which had settled to the bottom of the jar. The zinc phosphate treated samples showed no visible changes from their initial condition. There was no evidence of any deposit, any discolouration or any other visible signs of corrosion. The test was continued until day 7, with the untreated samples continuing to degrade while the zinc phosphate blasted samples remained largely unchanged, thereby confirming the protective corrosion-inhibiting properties of the abrasive blasting treatment.
  • Corrosion testing was carried out using a neutral salt fog cabinet as per ISO 9227.
  • a ‘T’ scribe was introduced to each sample using a carbide tip as per ISO 18782.
  • each sample was removed periodically and photographed to log the growth of corrosion from the scratch.
  • the samples were cleaned in deionised water to remove excess rust/corrosion on top of the sample prior to taking the photograph.
  • the width/growth of the corrosion from the scratch was measured using the freely available imageJ software.
  • Each coupon was removed from the salt fog cabinet at set intervals over a period of 56 days.
  • the width of the corrosion was measured using the imageJ software. A steel ruler was used to calibrate the scale.
  • the ‘Iron Phosphate’ and ‘Zinc Plated’ samples performed quite poorly.
  • the Zinc Plated sample exhibited significant delamination of the epoxy paint after 28 days and almost complete catastrophic failure after 56 days.
  • the Blank & Grit-Blasted coupons initially appeared to perform quite well and produced results that appeared superficially identical to the zinc phosphate coatings. However, when sectioned and examined in detail, it was evident that the depth of corrosion was much greater for these samples than for either of the zinc phosphate treatments. Both zinc phosphate treatments were noticeably better than the other commercial treatments.
  • the blasted zinc phosphate tie-layer was very close in performance to that of the commercial Dry Zinc Phosphate primer (which utilised a noticeably thicker coating).
  • Adhesion testing was then carried out using a modified version of ISO 2409.
  • samples prepared using the abrasively blasted pre-treatment yielded a value of 1, while the samples that were blasted with both abrasive and PTFE showed no effects and were therefore classified as 0.
  • the abrasively blasted samples were classified at level 2 to level 4, while the samples blasted with both abrasive and PTFE remained at classification 0 or 1, indicating significantly enhanced adhesion due to the PTFE primer.
  • the substrate in this case was grade V titanium. Five different surface treatments were then subjected to adhesion testing. These consisted of
  • CFRP carbon fibre reinforced plastic
  • the CFRP was Hexcel 8552/5H which was prepared for bonding using a wet peel ply (Henkel Hysol EA9895).
  • the adhesive was Cytec FM300 epoxy film adhesive (0.03 gsm weight) which was cured at 177 C for 1 hour at a pressure of 45 psi.
  • the samples were cooled to room temperature and then subjected to lap-shear testing, which was conducted in accordance with ISO 2243-1.
  • the specimens were 25 mm wide with a 12.5 mm adhesive overlap.
  • the lap-shear strength was calculated by dividing the force at failure by the overlap area. Four repetitions were performed for each surface treatment.
  • the present method has potential application across a wide range of industries, including but not limited to: large-scale engineering components such as pipeline sections; wind turbine components; civil engineering structures; external walls; marine components; automotive body parts; oil and gas industry components; and aerospace components.
  • large-scale engineering components such as pipeline sections; wind turbine components; civil engineering structures; external walls; marine components; automotive body parts; oil and gas industry components; and aerospace components.

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AU2015233403A1 (en) 2016-11-03
RU2016141061A (ru) 2018-04-27
KR20160135327A (ko) 2016-11-25
WO2015140327A1 (en) 2015-09-24
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