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 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° 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:
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 provided. The sheet material is protected from corrosion and provides a nonslip or anti-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 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 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 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 μm.
The second metal deposition coating may be 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 stage than the second stage.
The second metal deposition coating may also be 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 that a surface produced in said first stage has a surface roughness less than a surface roughness produced in said second stage.
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 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 μm.
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 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 μm.
By providing a barrier coating of the above thickness, the advantage is provided 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:
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.
In a preferred embodiment the first metal deposition coating has a thickness of between 75 and 200 μm.
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.
In a preferred embodiment the second metal deposition coating is applied in a plurality of stages including a first stage and a second stage and wherein a surface produced in said first stage has a surface roughness less than a surface roughness produced in said second stage.
In another preferred embodiment the second metal deposition coating is applied to a thickness of between 150 and 300 μm.
In a preferred embodiment the barrier coating comprises an inorganic heat resistant coating material.
In another preferred embodiment the barrier coating comprises a potassium silicate coating material.
In a further preferred embodiment the barrier coating is applied to a thickness of between 5 and 25 μm.
According to a further aspect of the present invention there is provided a sheet material comprising:
In a preferred embodiment the steel comprises hardened steel.
In another preferred embodiment the steel comprises carbon manganese steel.
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.
According to a further aspect of the present invention there is provided an apparatus for applying a coating to a sheet of steel, the apparatus comprising:
By providing an apparatus described above, the advantage is provided that large surfaces of sheet material, for example the deck of an aircraft carrier, can be coated accurately and evenly producing a surface to a consistent standard.
In a preferred embodiment the applicator uses at least one of the metal deposition techniques of arc spray, wire spray, twin wire arc spray, air plasma and cold spray.
The apparatus may comprise a plurality of applicators for applying at least one first metal deposition coating and at least one second metal deposition coating to a sheet of steel.
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:
Referring to
The primary functions of the surface preparation (indicated at 14 on
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
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.
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 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 and 200 μm. 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, 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 and 300 μm 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 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 anti-skid surface. By slowing down and reducing the momentum of the particles in the second 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 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).
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 μm 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 35 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
The sheet material is suitable for use in any of the following applications, which 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 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 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.
| Number | Date | Country | Kind |
|---|---|---|---|
| 1410336.0 | Jun 2014 | GB | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/GB2015/051703 | 6/10/2015 | WO | 00 |