Patent Application
20170106473
The present disclosure concerns a pressure vessel and/or a method of cladding a pressure vessel.
Nuclear pressure vessels (e.g. reactor vessels) are generally large components, for example a typical pressure vessel would have a diameter in the region of at least 2 metres. A pressure vessel typically has a cylindrical central portion and domed ends (which may be referred to as heads). The pressure vessels are generally made from a low-carbon steel. To withstand the harsh environment of operation, the inner surface of the vessel needs to be coated with an inert material, for example with stainless steel or a nickel-based alloy.
Arc welding techniques such as metal inert gas (MIG) or tungsten inert gas (TIG) welding is used to coat the inner surface of the pressure vessels. The arc welding process introduces a high thermal input into the substrate (i.e. the material of the vessel being coated). This high thermal input means that the clad and substrate chemistries mix resulting in a diluted clad material on the inner surface of the vessel. To address this, multiple layers of clad material are deposited on the inner surface of the vessel. Each layer of clad needs to be individually inspected using a suitable non-destructive technique to ensure that no defects are present before welding the next layer of clad. Furthermore, it is typically necessary to machine the clad material once it has been deposited to achieve the required surface finish and chemistry suitable of the operational environment (e.g. high temperature and high pressure). This method of cladding a component is time consuming and expensive.
According to a first aspect there is provided a method of cladding a pressure vessel having an internal diameter (e.g. at the widest part) greater than or equal to 1 m (e.g. greater than or equal to 2 m). The method comprises laser cladding an inner surface of the vessel, wherein the laser cladding follows a helical path.
The helical path may be defined such that adjacent loops of clad overlap by approximately 40 to 70%, e.g. 60%.
The method may comprise rotating and axially moving the vessel to define the helical path.
Alternatively, a head of the cladding machine may be manipulated to define the helical path. Further alternatively, the head and the vessel may be manipulated to define the helical path, for example the vessel may be rotated and the head may be moved axially.
The method may comprise positioning a vessel on a support frame. The support frame may comprise rollers arranged to manipulate the vessel (e.g. to rotate and/or axially move the vessel).
The vessel may not be pre-heated before being clad. For example, just before (or at the start) of the cladding process the temperature of the vessel may be considered to be at room temperature (e.g. 10 to 40° C.).
The method may comprise providing a metallic powder, melting said powder, and depositing said powder on the inner surface of the vessel.
Alternatively the source of cladding material used to clad the internal surface may be a wire.
The method may comprise using a vacuum to remove excess powder from the vessel.
The method may comprise providing a powder removal device to generate the vacuum. The device may comprise a housing and a plurality of holes. The device may be configured such that excess powder is removed via the holes and is directed to a location removed from the vessel.
Once the inner surface of the component has been clad, the method may comprise moving a laser over the surface of the component to reduce the surface roughness. The laser may be the laser used to clad the vessel.
The method may comprise adding additional insulation to a head of the laser cladding equipment used to clad the vessel.
The vessel may be a cylinder having a length greater than or equal to approximately 1 m. Alternatively, the vessel may be dome shaped.
According to a second aspect there is provided a method of producing a pressure vessel for use in a nuclear power generation plant, the method comprising providing a vessel, and cladding the vessel using the method according to the first aspect.
The pressure vessel may be a reactor vessel or a heat exchanger.
According to a third aspect there is provided a pressure vessel made by the method according to the second aspect.
According to a fourth aspect there is provided a method of cladding a pressure vessel having an internal diameter (e.g. at the widest part) greater than or equal to 1 m (e.g. greater than or equal to 2 m). The method comprises providing the vessel at room temperature; and laser cladding an inner surface of the vessel.
That is, the method does not comprise the step of pre-heating the vessel before laser cladding.
The vessel may be a vessel for a nuclear power plant, e.g. a reactor or a heat exchanger.
The skilled person will appreciate that except where mutually exclusive, a feature described in relation to any one of the above aspects may be applied mutatis mutandis to any other aspect. Furthermore except where mutually exclusive any feature described herein may be applied to any aspect and/or combined with any other feature described herein.
Embodiments will now be described by way of example only, with reference to the Figures, in which:
Referring to
Referring to
The pressure vessel in this example is made from a low-carbon steel and has a coating of stainless steel on the inner (or internal) surface of the vessel. In alternative embodiments the inner surface of the pressure vessel may be coated with a nickel-based alloy.
Referring now to
The vessel support 32 includes a frame 36 and a plurality of rollers 38. The frame 36 supports the vessel to maintain the vessel in the desired position. The rollers 38 are arranged so that they are able to manipulate the vessel, including rotating the vessel. The vessel support 32 may be connected to a control unit 40. The control unit 40 may be used to control the manipulation of the vessel via the support vessel and/or the operation of the cladding machine.
The control unit 40 may comprise any suitable circuitry to cause performance of the methods described herein. The control unit may comprise: at least one application specific integrated circuit (ASIC); and/or at least one field programmable gate array (FPGA); and/or single or multi-processor architectures; and/or sequential (Von Neumann)/parallel architectures; and/or at least one programmable logic controllers (PLCs); and/or at least one microprocessor; and/or at least one microcontroller, to perform the methods.
By way of an example, the control unit 40 may comprise at least one processor 42 and at least one memory 44. The memory 44 may store a computer program 46 comprising computer readable instructions that, when read by the processor 40, causes performance of the methods described herein. The computer program may be software or firmware, or may be a combination of software and firmware.
The processor 40 may include at least one microprocessor and may comprise a single core processor, or may comprise multiple processor cores (such as a dual core processor or a quad core processor).
The memory 44 may be any suitable non-transitory computer readable storage medium, data storage device or devices, and may comprise a hard disk and/or solid state memory (such as flash memory). The memory 44 may be permanent non-removable memory, or may be removable memory (such as a universal serial bus (USB) flash drive).
The cladding machine is of the type commercially available and includes a head 34 that applies the cladding to the surface of a component. Referring to
Referring again to
The head 34 is connected to a manipulator 50. The manipulator may include a jib or a column. In some examples the manipulator includes an articulated arm that may be connected to either a jib or column.
A powder supply 52 is provided. In this example the powder supply is remote from the head. Flexible piping is used to transport powder from the powder supply to the head.
A laser source 54 is provided. In this example, the laser source is remote from the head. Optical cables are used to transmit the laser beam to the component via the head 34.
A powder removal device 56 is also provided. Referring to
The method of cladding the cylindrical part 24 of the vessel 22 (shown in
The cylindrical part 24 of the vessel 22 is positioned on the vessel support 32. When the cylindrical part is position on the vessel it is at room temperature. No heat treatment of the component takes place. The inventors have surprisingly found that the vessel does not need heating before the laser cladding process, e.g. using the following described method, without the need to preheat. This is contrary to what is currently done in the art, and goes against the prejudice in the art.
Once the part 24 is in position, the head 34 is moved to a start position that is inside the bore of the cylindrical part 24. The cladding process is then commenced.
During the cladding process, metal powder is blown through the nozzle 45 along the annular passageway 46 by an inert gas, e.g. argon. A laser beam is fired through the central portion 47 of the nozzle. The laser beam melts the metal powder whilst it is in transit to the substrate to be clad, this means that the majority of the powder is heated (and molten) before it reaches the surface of the cylindrical part 24, the remainder of the powder is melted on the surface.
In the present example, the powder spot has a diameter of approximately 1 cm, but it will be understood by the person skilled in the art that the diameter of the powder spot can vary depending on the set up of the cladding machine and the specific arrangement of the nozzle.
During the cladding process, the vessel support 32 rotates the cylindrical part and moves the cylindrical part axially, in this way a helix of cladding is deposited on the inner surface of the cylindrical part, as illustrated in
During the cladding process, the powder removal device is used to remove any loose powder from the inner side of the cylindrical part. For example, this may be powder that has not been melted and has fallen from an upper surface of the cylindrical part to a lower surface of the cylindrical part as the cylindrical part is rotated.
The laser cladding process may take place in a single run, or alternatively, for larger components the laser cladding process may be done in several stages. Generally if using welding techniques it is undesirable to start and stop the cladding process, but when laser cladding is used, the point at which the stop-start occurs is not unacceptably affected because the process means that there will always be more material at the point of the restart. Furthermore, during the overlap of the restart position (due to each pass of cladding deposit overlapping) the heat from the laser has been found to smooth the cladding in the stop-start region.
It has been found that optionally the laser of the head 34 can be run over the cladding once cladding has been completed. In this way the clad surface can be smoothed. However, the surface finish of the laser cladding is smoother than a comparable welded clad surface and as such for some applications no surface post-processing (such as smoothing with a laser or machining) may be necessary.
The size the cylindrical part is much greater and cladding of the internal surface is more complex that parts from other industries that are clad using laser cladding.
For example, the size of the component means that the cladding process is in continuous operation for a longer period of time than for other components. In addition to the size of the component, cladding of the internal surface of the component also poses technical challenges because of laser reflections, heat management, and powder nozzle blockages. The present inventors have found that it has been possible to overcome these challenges using the described method.
Laser cladding of the inner surface of the pressure vessel is advantageous over conventional processes such as TIG and MIG welding because not as much heat is put into the surface, which means that dilution is significantly reduced. In some examples, it is expected that dilution could reach less than 4%. This means that only a single layer of cladding needs to be provided, compared to the multiple layers of the prior art. Use of only a single layer of cladding means that process time can be reduced both in terms of production and inspection. Furthermore, the laser clad surface does not need machining, saving more production time.
Cladding along a helical path reduces the number of stop-starts compared to other cladding patterns that could be used. Furthermore, cladding along a helical path means that the temperature of the parent material (the cylindrical part) is more consistent at the point where the cladding is deposited, compared to other options of cladding paths. The process “sees” the parent material as an infinite heat sink which means that the dilution is more consistent. Furthermore, there is a steady state inter-pass temperature which helps to reduce cracking.
Removing the need for preheating large components such as the described pressure vessel before cladding means that manufacturing times can be reduced and the capital costs involved in manufacturing large pressure vessels for nuclear power plants can be reduced.
Adding additional insulation to the head further helps with heat management and reduces blockages in the nozzle.
The method of cladding a pressure vessel has been described with reference to the cylindrical part, but it will be appreciated that a similar method could be used to clad the dome ends of the pressure vessel.
One example of laser cladding has been described, but other laser cladding equipment may be used and in this alternative equipment the features of the head may be different and/or wire may be used as the source material instead of powder.
It will be understood that the invention is not limited to the embodiments above-described and various modifications and improvements can be made without departing from the concepts described herein. Except where mutually exclusive, any of the features may be employed separately or in combination with any other features and the disclosure extends to and includes all combinations and sub-combinations of one or more features described herein.
| Number | Date | Country | Kind |
|---|---|---|---|
| 1518351.0 | Oct 2015 | GB | national |
