AU2015273296B2 - A method of coating a sheet of steel - Google Patents
A method of coating a sheet of steel Download PDFInfo
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- AU2015273296B2 AU2015273296B2 AU2015273296A AU2015273296A AU2015273296B2 AU 2015273296 B2 AU2015273296 B2 AU 2015273296B2 AU 2015273296 A AU2015273296 A AU 2015273296A AU 2015273296 A AU2015273296 A AU 2015273296A AU 2015273296 B2 AU2015273296 B2 AU 2015273296B2
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- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
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- 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
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/08—Metallic material containing only metal elements
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- 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
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
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- 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
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- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
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- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
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- 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
- C23C4/131—Wire arc spraying
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- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Inorganic Chemistry (AREA)
- Coating By Spraying Or Casting (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Coating With Molten Metal (AREA)
Abstract
A method of coating a sheet of steel is disclosed. The method includes preparing a surface of the sheet of steel by grit blasting with brown fused alumina. A first metal deposition coating, including aluminium, is applied and then a second metal deposition coating, including aluminium and a least one first doping material,is applied to the first coating. Finally a barrier coating including potassium silicate is applied to the second metal deposition coating.
Description
A METHOD OF COATING A SHEET OF STEEL
The present invention relates to a method of coating a sheet of steel and to a coating for a sheet of steel and relates particularly, but not exclusively, to a method of coating a surface of a weight bearing sheet of steel for use on an aircraft carrier.
Ships, such as aircraft carriers, are commonly made from steel including the uppermost deck surface that acts as the aircrafts' takeoff and landing runway. These deck surfaces are commonly protected by applying a layer of organic paint. However, such paint is unable to withstand the gas-wash produced during the takeoff and landing of aircraft that use jet engines to facilitate a vertical takeoff or landing or short takeoff and 0 vertical landing (STOVL). This gas-wash can result in a change of surface temperature from ambient to 2000°C causing a patch of the paintwork to be burnt away on each such manoeuvre. Such damage then makes a deck surface vulnerable to corrosion.
A surface coating is required that is able to deal with the rapid change in temperature including starting from ambient temperatures in a range of -50° C to +50° 5 C. The coating must provide a nonslip or anti-skid surface allowing it to be safely walked on, it must be sufficiently robust to withstand the force applied to it during takeoff and landing and be easily repairable in the event of damage.
Preferred embodiments of the present invention seek to overcome the above described disadvantages of the prior art.
According to an aspect of the present invention there is provided a method of coating a sheet of steel comprising the steps:preparing a surface of a sheet of steel that is to be coated;
applying a first metal deposition coating to said sheet of steel, said first coating comprising aluminium;
applying a second metal deposition coating to said first coating, said second coating comprising aluminium and at least one first doping material; and applying a barrier coating to said second metal deposition coating wherein said second metal deposition coating is applied in a plurality of stages including a first stage and a second stage and wherein a particle accelerator used in the 30 coating applications operates so as to accelerate the particles more in the first stage than the second stage so that a surface produced in said first stage has a surface roughness less than a surface roughness produced in said second stage.
By applying, to a sheet of steel, a first coating of aluminium, a second coating of aluminium plus a doping material and a barrier coating, a series of advantages are 35 provided. The sheet material is protected from corrosion and provides a nonslip or anti2
2015273296 24 Mar 2020 skid surface which is safe to walk on and provide suitable friction resistant surface to operate an aircraft from. The surface can be painted and yet is sufficiently resistant to rapid changes in temperatures that the gas wash from a vertical takeoff aircraft will not damage the surface or the steel. The surface also provides sufficient frictional resistance 5 to allow the takeoff on landing of other aircraft.
In a preferred embodiment the surface of said sheet of steel is prepared by grit blasting.
By grit blasting the steel surface a substantially oxide free and suitably rough surface is created which ensures a secure bond between the steel of the sheet material 0 and the aluminium of the first coating.
In another preferred embodiment grit blasting uses a grit comprising brown fused alumina which is suitably angular and robust to provide the required profile to optimise adhesion of the aluminium of the first coating.
In a preferred embodiment the first coating further comprises at least one second doping material which enhances the corrosion resistance of the first coating and/or facilitates the ease of repair.
In another preferred embodiment second doping material comprises at least one of zinc, molybdenum, gallium, tin and indium. The addition of the dopants extends the life of the sacrificial characteristics of the first coating layer in marine environments and 0 increases the compatibility of the first coating with the repair regime.
In a further preferred embodiment first metal deposition coating is applied to a thickness of between 75 and 200 pm.
In a preferred embodiment the first doping material comprises at least one of titanium, chromium, manganese, boron, aluminium oxide, titanium oxide, chromium 25 oxide, manganese oxide, boron oxide, boron nitride, boron carbide and tungsten carbide.
By applying the second metal deposition coating in a plurality of stages with lower acceleration of the particles in the second stage thereby leading to greater roughness of the resulting surface, the advantage is provided that the bond between the first metal deposition coating and the second metal deposition coating are secure (due to the 30 increased particle velocity on impact in the first stage) but the uppermost surface of the second metal deposition coating is sufficiently rough (due to decreased particle velocity on impact in the second stage) to assist in the provision of a nonslip or anti-skid surface.
In another preferred embodiment the second metal deposition coating is applied to a thickness of between 150 and 300 pm.
2015273296 24 Mar 2020
In a preferred embodiment the barrier coating comprises an inorganic heat resistant coating material.
By using an inorganic heat resistant coating material for the barrier coating, the advantage is provided that the barrier coating assists in the protection of the first and 5 second metal deposition coatings and the high temperatures, resultant from jet gas wash, do not damage the barrier coating. As a result, the coating of the present invention can be regarded as intumescent.
In another preferred embodiment the barrier coating comprises a potassium silicate coating material.
A potassium silicate coating provides the above described advantages and can be applied at a convenient thickness.
In a further preferred embodiment the barrier coating is applied to a thickness of between 5 and 25 pm.
By providing a barrier coating of the above thickness, the advantage is provided 5 that the barrier coating follows, and substantially reproduces, the profile of second metal deposition coating thereby assisting in the creation of the nonslip surface.
In a preferred embodiment at least one of said first and second metal deposition coatings are applied using at least one of the metal deposition techniques of arc spray, wire spray, twin wire arc spray, air plasma and cold spray.
According to another aspect of the present invention there is provided a coating for a sheet of steel, the coating comprising:a first metal deposition coating comprising aluminium and applied to a prepared surface of a sheet of steel;
a second metal deposition coating comprising aluminium and at least one 25 first doping material and applied to said first metal deposition coating;
a barrier coating applied to said second metal deposition coating wherein said second metal deposition coating is applied in a plurality of stages including a first stage and a second stage and wherein a particle accelerator used in the coating applications operates so as to accelerate the particles more in the first 30 stage than the second stage so that a surface produced in said first stage has a surface roughness less than a surface roughness produced in said second stage..
The first coating may further comprise at least one second doping material.
The second doping material may comprise at least one of zinc, molybdenum, Gallium, tin and indium.
2015273296 24 Mar 2020
The first doping material may comprise at least one of titanium, chromium, manganese, boron, aluminium oxide, titanium oxide, chromium oxide, manganese oxide, boron oxide, boron nitride, boron carbide and tungsten carbide.
According to a further aspect of the present invention there is provided a sheet 5 material comprising:a sheet of steel material; and a coating as set out above applied to said sheet of steel material.
According to another aspect of the present invention there is provided an article comprising at least one sheet material as set out above.
In a preferred embodiment the sheet material forms a weight bearing surface.
In another preferred embodiment the article is any of a helicopter landing platform, a submarine, an oil rig, a chemical processing plant, an energy production plant, a shipping container and a munitions box.
Preferred embodiments of the present invention will now be described, by way of example only, and not and in any limitative sense with reference to the accompanying drawings in which:Figure 1 is a flowchart showing a method of the present invention;
Figure 2 is a schematic sectional representation of a sheet material and coating of the present invention;
Figure 3 is a micrograph image of a prepared surface of sheet material used in the present invention;
Figure 4 is a micrograph of a cross-section of a prepared surface of sheet material used in the present invention;
Figure 5 is a micrograph of a cross-section of a prepared surface of sheet material not suitable for use in the present invention;
Figure 6 is a flowchart showing a method of the present invention;
Figure 7 is a perspective view of an apparatus for applying the coating of present invention; and
Figure 8 is another perspective view of the apparatus of figure 7.
Referring to figures 1 and 2, a method of applying a coating 10 onto a sheet of steel 12 is undertaken in a series of steps set out in figures 1 and 6, with figure 1 representing a simplified version of the more complete process shown in figure 6. At the start of the process a sheet of steel material 12 is prepared in order to receive the coating that will be applied to at least one surface thereof. The thickness of the sheet of steel is dependent upon the application for which it is to be used and is therefore not a constraint
2015273296 24 Mar 2020 or limitation of this invention. Furthermore, the term sheet refers to a single or multiple sheets of steel that are joined together and it is not a limitation of this invention that the sheets form a planar or substantially planar surface. The purpose of the coating is to create a protective nonslip or anti-skid surface to the steel. The steel is for use in any 5 suitable weight bearing situation carrying the weight of, for example, a person, vehicle or aircraft.
The primary functions of the surface preparation (indicated at 14 on figures 1 and 6) are to expose a substantially oxide free surface of the steel and to create sufficient surface roughness to ensure secure bonding between the steel 12 and coating 10. An 0 example of such a surface preparation technique is grit blasting (indicated at 16) in which a grit, preferably brown fused alumina, is accelerated in a stream of compressed air at a pressure of greater than 80 psi and directed at the sheet steel at an angle between 45° and 90° to the surface being prepared.
An inspection takes place at step 18 and a pass or fail is determined at step 20.
The step of inspection may include examining a micrograph of the prepared surface and an acceptable surface micrograph at 100 times magnification is shown in figure 3 with the sharp edges shown therein providing an indication of a surface that will create a good bond to the coating that will be applied thereto. Figures 4 and 5 are also micrographs (at 100 times magnification) showing a cross-section of the grit blasted surface. Figure 4 shows 0 an example of an acceptable grit blasted surface and figure 5 shows an example of an unacceptable surface due to having insufficient roughness. The table below set out the preferred critical roughness parameters for the blasted surface, the roughness being measured using roughness measuring techniques familiar to a person skilled in the art.
| Parameter | Description | Acceptable Range (pm) |
| Ra | The mean of the absolute values and describes the average roughness | > 4 (normally 4- 5.5) |
| Rp | The maximum peak height | > 15 |
| Rku | The average sharpness of the peaks | > 3 |
| R.sm | The mean width of the profile peak elements | < 500 |
| Rt | The maximum peak to valley height in the sampling length | 30 - 60 |
Prior to the grit blasting at step 16, other surface preparation techniques may be applied. These include degreasing and paint removal and the latter may be undertaken using grit blasting but with another grit such as shot or aggregate. The surface may also be tested for grease and for the presence of chloride using a chloride indicator tape or similar techniques familiar to a person skilled in the art.
2015273296 24 Mar 2020
Following the surface preparation in step 14, metal deposition is undertaken at step 22. This metal deposition is undertaken in two different coatings with two different compositions of metal being deposited consecutively onto the steel 12. A first metal deposition coating 24 is applied at step 25 and comprises at least aluminium. The first 5 metal deposition coating 24 may include a doping component, including, but not limited to, metals such as zinc, molybdenum, gallium, tin and indium The first metal deposition coating 24 is applied by arc spraying although other metal deposition/spraying processes are also acceptable including, but not limited to, wire spray, twin wire arc spray, air plasma and cold spray. The first metal deposition coating typically has a thickness of between 75 0 and 200 pm. The first metal deposition coating is preferably applied as a series of layers bypassing the spray gun over the same surface a number of times.
Once the first metal deposition coating 24 has been applied a second metal deposition coating 26 is applied (at step 27) on top of the first coating 24. The second metal deposition coating comprises aluminium and at least one other doping component, 5 including, but not limited to, metals such as titanium, chromium, manganese, boron, aluminium oxide, titanium oxide, chromium oxide, manganese oxide, boron oxide, boron nitride, boron carbide and tungsten carbide. The second metal deposition coating 26 is applied using any of the same techniques used to apply the first metal deposition coating 24. The second metal deposition coating typically has a thickness of between 150 0 and 300 pm and is applied in two stages. The two stages preferably use the same metal combination but can be distinguished by a difference in the acceleration of the metal particles from the spray gun as the spray is applied. In the first stage of the application, producing the first stage 28 of second coating 26, the spray particles are accelerated from the spray gun at a faster rate than those producing the second stage 30 of second coating 5 26. In the first stage the increased momentum of the fast-moving particles results in secure adhesion between the second coating 26 and first coating 24 and high density. However, the resultant temporary surface (indicated at 32) at the end of the first stage of the second coating does not have sufficient roughness to provide a good nonslip or antiskid surface. By slowing down and reducing the momentum of the particles in the second 30 stage (by reducing the pressure of the accelerant gas in the spray gun by roughly half) a rougher surface (indicated at 34) is produced.
Once the first and second metal deposition coatings have been applied and inspection takes place at step 29 and a pass fail is determined at step 31. The inspection can include a visual inspection, surface roughness measurements and a bend test (where 35 a sample of steel, not forming part of the main surface being protected, is taken and bent using a predetermined force around a predetermined diameter to ensure good adhesion between the metal deposition coatings and the steel).
2015273296 24 Mar 2020
The coating 10 is completed by the application (at step 33) of a barrier coating 36. The barrier coating is an inorganic heat resistant material such as a potassium silicate sealant. The sealant acts as a barrier preventing oxidisation of the aluminium and is applied in a layer that is thinner than the first and second metal deposition coatings at between 5 and 25 pm thick. This thickness is sufficiently small that the roughness of the upper surface 34 of the second metal deposition coating 26 is retained thereby providing a good nonslip surface. The barrier coating can be applied by brush, roller, spray gun (HVLP, High velocity, low pressure) or dipping for smaller surfaces. The barrier coating 36 can include a pigment in order to provide a base coat colour as required.
Once the barrier coating has been applied a final inspection step takes place at and a pass fail is determined at 37. If required, further barrier coatings containing other pigments to produce other colours can be applied to the surface of the barrier coating to give line marking or other demarcation as required.
Spray guns of the type described above can be operated manually to apply the metal deposition coatings. However, when working over large surface areas it is preferable to use a robotic device of the type shown in figures 7 and 8. The apparatus includes a frame 50 which is placed onto sheet material 12 and is manoeuvrable via wheels 52. An applicator, in the form of spray gun 54, is provided to apply the first metal deposition coating and the second metal deposition coating in consecutive applications. However, the applicator could alternatively include two or more spray guns to apply the separate metal deposition coatings and most preferably includes three spray guns. The first spray gun applies the first metal deposition coating, the second spray gun applies the first stage of the second metal deposition coating and the third gun applies the second stage of the second metal deposition coating. The applicator is moved relative to frame 50 using an 25 applicator moving means in the form of robotic arm 56. It will be apparent to person skilled in the art that other applicator moving means could be used to control the movement of the applicator relative to the frame, such as a flat-bed scanner. The movement of the robotic arm 56 and use of the spray gun 54 is controlled by a processor (not shown). The processor enables the even application of the coatings and can ensure 30 that at the edges of the patch of coating 10 (see figure 8) are feathered, by controlling the speed of movement of the arm and/or rate of deposition of the metal coating, so that patches of coating 10 can be separately formed and a consistent coating be applied to the whole surface of the sheet steel material 12.
The sheet material is suitable for use in any of the following applications, which 35 are provided by way of example only and not as a definitive list, a helicopter landing platform, a submarine, an oil rig, a chemical processing plant, an energy production plant, a shipping container and a munitions box. It is generally the case that the application in
2015273296 24 Mar 2020 which the coating is being applied to the sheet of steel is already built when the coating is applied. For example, if the coating is being applied to the deck of an aircraft carrier, the coating is applied once the ship has been constructed.
It will be appreciated by persons skilled in the art that the above embodiments 5 have been described by way of example only and not in any limitative sense, and that various alterations and modifications are possible without departure from the scope of the protection which is defined by the appended claims.
Claims (5)
1. A method of coating a sheet of steel comprising the steps:- preparing a surface of a sheet of steel that is to be coated;
applying a first metal deposition coating to said sheet of steel, said first 5 coating comprising aluminium;
applying a second metal deposition coating to said first coating, said second coating comprising aluminium and a least one first doping material; and applying a barrier coating to said second metal deposition coating wherein said second metal deposition coating is applied in a plurality of stages including a 0 first stage and a second stage and wherein a particle accelerator used in the coating applications operates so as to accelerate the particles more in the first stage than the second stage so that a surface produced in said first stage has a surface roughness less than a surface roughness produced in said second stage.
2. A method according to claim 1, wherein said surface of said sheet of steel is 5 prepared by grit blasting.
3. A method according to claim 2, wherein said grit blasting uses a grit comprising brown fused alumina.
4. A method according to any preceding claim, wherein said first coating further comprises at least one second doping material.
0 5. A method according to claim 4, wherein said second doping material comprises at least one of zinc, molybdenum, Gallium, tin and indium.
6. A method according to any preceding claim, wherein said first metal deposition coating is applied to a thickness of between 75 and 200 pm.
7. A method according to any preceding claim, wherein said first doping material 25 comprises at least one of titanium, chromium, manganese, boron, aluminium oxide, titanium oxide, chromium oxide, manganese oxide, boron oxide, boron nitride, boron carbide and tungsten carbide.
8. A method according to any preceding claim, wherein said second metal deposition coating is applied to a thickness of between 150 and 300 pm.
30 9. A method according to any preceding claim, wherein said barrier coating comprises an inorganic heat resistant coating material.
10. A method according to any preceding claim, wherein said barrier coating comprises a potassium silicate coating material.
2015273296 24 Mar 2020
11. A method according to any preceding claim, wherein said barrier coating is applied to a thickness of between 5 and 25 pm.
12. A method according to any preceding claim, wherein at least one of said first and second metal deposition coatings are applied using at least one of the metal deposition
5 techniques of arc spray, wire spray, twin wire arc spray, air plasma and cold spray.
13. A coating for a sheet of steel, the coating comprising:- a first metal deposition coating comprising aluminium and applied to a prepared surface of a sheet of steel;
a second metal deposition coating comprising aluminium and at least one 0 first doping material and applied to said first metal deposition coating;
a barrier coating applied to said second metal deposition coating wherein said second metal deposition coating is applied in a plurality of stages including a first stage and a second stage and wherein a particle accelerator used in the coating applications operates so as to accelerate the particles more in the first
5 stage than the second stage so that a surface produced in said first stage has a surface roughness less than a surface roughness produced in said second stage.
14. A coating according to claim 13, wherein said first coating further comprises at least one second doping material.
15. A coating according to claim 14, wherein said second doping material comprises 0 at least one of zinc, molybdenum, Gallium, tin and indium.
16. A coating according to anyone of claims 13 to 15, wherein said first doping material comprises at least one of titanium, chromium, manganese, boron, aluminium oxide, titanium oxide, chromium oxide, manganese oxide, boron oxide, boron nitride, boron carbide and tungsten carbide.
25 17. A sheet material comprising:a sheet of steel material; and a coating according to any of claims 13 to 16 applied to said sheet of steel material.
18. An article comprising at least one sheet material according to claim 17.
30 19. An article according to claim 18, wherein said sheet material forms a weight bearing surface.
20. An article according to claim 18 or 19, wherein said article is any of a helicopter landing platform, a submarine, an oil rig, a chemical processing plant, an energy production plant, a shipping container and a munitions box.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1410336.0 | 2014-06-10 | ||
| GB1410336.0A GB2529608B (en) | 2014-06-10 | 2014-06-10 | A method of coating a sheet of steel |
| PCT/GB2015/051703 WO2015189612A2 (en) | 2014-06-10 | 2015-06-10 | A method of coating a sheet of steel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
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| EP (1) | EP3155138B1 (en) |
| CN (1) | CN107155334B (en) |
| AU (1) | AU2015273296B2 (en) |
| CA (1) | CA2951204C (en) |
| GB (2) | GB2529608B (en) |
| PT (1) | PT3155138T (en) |
| SG (1) | SG11201610389TA (en) |
| WO (1) | WO2015189612A2 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US9335296B2 (en) | 2012-10-10 | 2016-05-10 | Westinghouse Electric Company Llc | Systems and methods for steam generator tube analysis for detection of tube degradation |
| DE102019116363A1 (en) | 2019-06-17 | 2020-12-17 | Benteler Automobiltechnik Gmbh | Method for the production of an armor component for motor vehicles |
| US11935662B2 (en) | 2019-07-02 | 2024-03-19 | Westinghouse Electric Company Llc | Elongate SiC fuel elements |
| KR102523509B1 (en) | 2019-09-19 | 2023-04-18 | 웨스팅하우스 일렉트릭 컴퍼니 엘엘씨 | Apparatus and Method of Use for Performing In Situ Adhesion Testing of Cold Spray Deposits |
| CN110760777A (en) * | 2019-11-29 | 2020-02-07 | 国网山东省电力公司电力科学研究院 | A kind of preparation method of zinc-aluminum alloy powder core wire for arc spraying |
| CN112226723B (en) * | 2020-10-20 | 2021-11-16 | 西安交通大学 | Preparation method of aluminum-containing alloy coating in atmospheric atmosphere |
| BE1031323B1 (en) | 2023-02-03 | 2024-09-16 | Sichem | CERAMIC FOR HEAT EXCHANGER |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| EP1091020A1 (en) * | 1999-10-04 | 2001-04-11 | General Electric Company | A method of applying a bond coating and a thermal barrier coating on a metal substrate, and related articles |
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| US3855444A (en) * | 1968-12-16 | 1974-12-17 | M Palena | Metal bonded non-skid coating and method of making same |
| US4987003A (en) * | 1988-03-04 | 1991-01-22 | Alcan International Limited | Production of aluminum matrix composite coatings on metal structures |
| US5034358A (en) * | 1989-05-05 | 1991-07-23 | Kaman Sciences Corporation | Ceramic material and method for producing the same |
| JPH0673529A (en) * | 1991-06-06 | 1994-03-15 | Nisshin Steel Co Ltd | Vapor deposition double layer plated steel sheet |
| RU2049827C1 (en) * | 1991-09-03 | 1995-12-10 | Мила Шлемовна Штейбух | Method for producing multilayer coating |
| US5863617A (en) * | 1997-08-21 | 1999-01-26 | Harsco Technologies Corporation | Portable metal bonded anti-slip coating application process |
| CN1297688C (en) * | 2000-05-30 | 2007-01-31 | 杰富意钢铁株式会社 | Organic coating covered steel sheet and manufacturing method thereof |
| CA2421520A1 (en) * | 2000-09-22 | 2002-03-28 | General Electric Company | Combinatorial coating systems and methods |
| CN1166459C (en) * | 2002-11-21 | 2004-09-15 | 西安交通大学 | Mold Manufacturing Method Combining Metal Spraying and Brush Plating |
| JP2004317732A (en) * | 2003-04-15 | 2004-11-11 | Seiko Epson Corp | Substrate with recess, microlens substrate, transmission screen and rear projector |
| CN2812303Y (en) * | 2005-03-09 | 2006-08-30 | 南开大学 | Equipment for nano-oxide nesa preparation by means of ultrasonic rapid deposition |
| US7554052B2 (en) * | 2005-07-29 | 2009-06-30 | Applied Materials, Inc. | Method and apparatus for the application of twin wire arc spray coatings |
| US20070190354A1 (en) * | 2006-02-13 | 2007-08-16 | Taylor Thomas A | Low thermal expansion bondcoats for thermal barrier coatings |
| US8293035B2 (en) * | 2006-10-12 | 2012-10-23 | Air Products And Chemicals, Inc. | Treatment method, system and product |
| CN102021586A (en) * | 2009-09-15 | 2011-04-20 | 鞍钢股份有限公司 | A kind of production method of single-sided coated steel plate and single-sided coated steel plate |
| CN101724737B (en) * | 2009-12-25 | 2011-12-21 | 机械科学研究总院先进制造技术研究中心 | Steel plate hot forming method based on anti-oxidation coating and production line for implementing same |
| CN101906604B (en) * | 2010-07-30 | 2013-01-23 | 江苏中矿大正表面工程技术有限公司 | Rare earth aluminum alloy wire for thermal spraying |
| US8887532B2 (en) * | 2010-08-24 | 2014-11-18 | Corning Incorporated | Glass-forming tools and methods |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| EP1091020A1 (en) * | 1999-10-04 | 2001-04-11 | General Electric Company | A method of applying a bond coating and a thermal barrier coating on a metal substrate, and related articles |
Also Published As
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| GB201700406D0 (en) | 2017-02-22 |
| EP3155138B1 (en) | 2018-12-05 |
| CN107155334B (en) | 2019-12-03 |
| CA2951204C (en) | 2020-11-17 |
| CA2951204A1 (en) | 2015-12-17 |
| US20170114438A1 (en) | 2017-04-27 |
| AU2015273296A1 (en) | 2017-02-02 |
| SG11201610389TA (en) | 2017-01-27 |
| GB2542088A (en) | 2017-03-08 |
| GB201410336D0 (en) | 2014-07-23 |
| GB2529608A (en) | 2016-03-02 |
| GB2529608B (en) | 2018-07-18 |
| EP3155138A2 (en) | 2017-04-19 |
| CN107155334A (en) | 2017-09-12 |
| PT3155138T (en) | 2019-05-03 |
| WO2015189612A2 (en) | 2015-12-17 |
| WO2015189612A3 (en) | 2016-02-25 |
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