NL2020368B1 - A component for an electric furnace - Google Patents
A component for an electric furnace Download PDFInfo
- Publication number
- NL2020368B1 NL2020368B1 NL2020368A NL2020368A NL2020368B1 NL 2020368 B1 NL2020368 B1 NL 2020368B1 NL 2020368 A NL2020368 A NL 2020368A NL 2020368 A NL2020368 A NL 2020368A NL 2020368 B1 NL2020368 B1 NL 2020368B1
- Authority
- NL
- Netherlands
- Prior art keywords
- component
- additive manufacturing
- component according
- alloys
- during
- Prior art date
Links
- 239000000463 material Substances 0.000 claims abstract description 56
- 238000004519 manufacturing process Methods 0.000 claims abstract description 50
- 239000000654 additive Substances 0.000 claims abstract description 39
- 230000000996 additive effect Effects 0.000 claims abstract description 39
- 238000007789 sealing Methods 0.000 claims abstract description 9
- 238000001816 cooling Methods 0.000 claims description 37
- 238000000034 method Methods 0.000 claims description 31
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 14
- 229910052802 copper Inorganic materials 0.000 claims description 14
- 239000010949 copper Substances 0.000 claims description 14
- 229910045601 alloy Inorganic materials 0.000 claims description 6
- 239000000956 alloy Substances 0.000 claims description 6
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 5
- 229910000975 Carbon steel Inorganic materials 0.000 claims description 3
- 229910000640 Fe alloy Inorganic materials 0.000 claims description 3
- 229910000963 austenitic stainless steel Inorganic materials 0.000 claims description 3
- 239000010962 carbon steel Substances 0.000 claims description 3
- 229910010293 ceramic material Inorganic materials 0.000 claims description 3
- 229910052914 metal silicate Inorganic materials 0.000 claims description 3
- 229910021471 metal-silicon alloy Inorganic materials 0.000 claims description 3
- 150000004760 silicates Chemical class 0.000 claims description 3
- 238000009413 insulation Methods 0.000 claims description 2
- 239000010410 layer Substances 0.000 claims 3
- 239000011247 coating layer Substances 0.000 claims 2
- 230000001419 dependent effect Effects 0.000 claims 2
- 239000000110 cooling liquid Substances 0.000 claims 1
- 239000000725 suspension Substances 0.000 claims 1
- 229910000859 α-Fe Inorganic materials 0.000 claims 1
- 238000005253 cladding Methods 0.000 description 11
- 238000010146 3D printing Methods 0.000 description 8
- 239000011800 void material Substances 0.000 description 7
- 238000005266 casting Methods 0.000 description 6
- 239000012809 cooling fluid Substances 0.000 description 6
- 238000005553 drilling Methods 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 238000005242 forging Methods 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 238000000149 argon plasma sintering Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000010894 electron beam technology Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000001465 metallisation Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- 239000011135 tin Substances 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910001021 Ferroalloy Inorganic materials 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000001010 compromised effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000009740 moulding (composite fabrication) Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D11/00—Arrangement of elements for electric heating in or on furnaces
- F27D11/08—Heating by electric discharge, e.g. arc discharge
- F27D11/10—Disposition of electrodes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/09—Mixtures of metallic powders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y70/00—Materials specially adapted for additive manufacturing
- B33Y70/10—Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y80/00—Products made by additive manufacturing
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B7/00—Heating by electric discharge
- H05B7/02—Details
- H05B7/10—Mountings, supports, terminals or arrangements for feeding or guiding electrodes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Ceramic Engineering (AREA)
- Civil Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structural Engineering (AREA)
- Materials Engineering (AREA)
- Optics & Photonics (AREA)
- Physics & Mathematics (AREA)
- Furnace Details (AREA)
Abstract
Description
OctrooicentrumPatent center
Θ 2020368Θ 2020368
(2?) Aanvraagnummer: 2020368(2?) Application number: 2020368
Aanvraag ingediend: 1 februari 2018 © Int. CL:Application submitted: 1 February 2018 © Int. CL:
B22F 1/00 (2018.01) B22F 3/105 (2018.01)B22F 1/00 (2018.01) B22F 3/105 (2018.01)
A COMPONENT FOR AN ELECTRIC FURNACEA COMPONENT FOR AN ELECTRIC FURNACE
57) A component (10) for an electric furnace forms part of a lower electrode assembly (100). The component comprises a body (26) which is made by an additive manufacturing method (28) utilising at least a first material (30). In an example embodiment, the component is a pressure ring segment. The component may also be in the form of a contact shoe (12), a biasing device (14), a hanging device (16, 18), a sealing device (20, 21), an insulating device (22) and a heat shield (24) forming part of the lower electrode assembly.57) A component (10) for an electric furnace forms part of a lower electrode assembly (100). The component comprises a body (26) which is made by an additive manufacturing method (28) utilizing at least a first material (30). In an example embodiment, the component is a pressure ring segment. The component may also be in the form of a contact shoe (12), a biasing device (14), a hanging device (16, 18), a sealing device (20, 21), an insulating device (22) and a heat shield (24) forming part of the lower electrode assembly.
NL B1 2020368NL B1 2020368
Dit octrooi is verleend ongeacht het bijgevoegde resultaat van het onderzoek naar de stand van de techniek en schriftelijke opinie. Het octrooischrift komt overeen met de oorspronkelijk ingediende stukken.This patent has been granted regardless of the attached result of the research into the state of the art and written opinion. The patent corresponds to the documents originally submitted.
P33486N L00/MEP33486N L00 / ME
Title: A COMPONENT FOR AN ELECTRIC FURNACETitle: A COMPONENT FOR AN ELECTRIC FURNACE
INTRODUCTION AND BACKGROUNDINTRODUCTION AND BACKGROUND
This invention relates to a component for an electric furnace and more particularly to a lower electrode component such as, but not limited to, a pressure ring segment, a contact plate, and other components forming part of the general lower electrode assembly including heat shields, bellows, hangers, brackets, seals and insulating devices. The invention further relates to a method of manufacturing the component.This invention relates to a component for an electric furnace and more particularly to a lower electrode component such as, but not limited to, a pressure ring segment, a contact plate, and other components forming part of the general lower electrode assembly including heat shields, bellows, hangers, brackets, seals and insulating devices. The invention further relates to a method of manufacturing the component.
Electric furnaces typically comprise a cylindrical electrode with lower electrode components such as pressure ring segments and contact plates or contact shoes arranged around the electrode. These components are generally made by conventional manufacturing techniques or methods by casting or forging a copper body from copper or a copper-based alloy and providing cooling passages within the body for circulating a cooling fluid, such as water. These internal cooling passages may be formed by drilling holes into the body, as is the case with a forged body, or by providing pre-formed pipes and casting the copper body around these pipes, as is the case with the cast body. When adopting the forged and drilled conventional manufacturing technique, the copper body is heated after drilling and bent into a curved shape to form the component, whereafter some of the holes are plugged, for example by welding, press-fitting or other means. The possible shapes and configurations of the cooling passages are limited when using the aforementioned forged manufacturing methods. When utilising the casting technique, greater flexibility in the body and cooling channel geometry is possible. But the casting technique produces a work piece with compromised mechanical properties due to the larger grain structures that are naturally formed during the process. Furthermore, fusion of the preformed pipes with the molten metal being cast is problematic. Defects on the metal-pipe boundary are common and lead to heat transfer retardation.Electric furnaces typically include a cylindrical electrode with lower electrode components such as pressure ring segments and contact plates or contact shoes arranged around the electrode. These components are generally made by conventional manufacturing techniques or methods by casting or forging a copper body from copper or a copper-based alloy and providing cooling passages within the body for circulating a cooling fluid, such as water. These internal cooling passages may be formed by drilling holes into the body, as is the case with a forged body, or by providing pre-formed pipes and casting the copper body around these pipes, as is the case with the cast body. When adopting the forged and drilled conventional manufacturing technique, the copper body is heated after drilling and are into a curved shape to form the component, whereafter some of the holes are plugged, for example by welding, press-fitting or other means. The possible shapes and configurations of the cooling passages are limited when using the aforementioned forged manufacturing methods. When using the casting technique, greater flexibility in the body and cooling channel geometry is possible. But the casting technique produces a work piece with compromised mechanical properties due to the larger grain structures that are naturally formed during the process. Furthermore, fusion of the preformed pipes with the molten metal being cast is problematic. Defects on the metal-pipe boundary are common and lead to heat transfer retardation.
The above forging and casting methods require multiple production stages including casting, forging, cooling pipe cutting, forming and welding, rough cutting, drilling, heating, bending, machining and welding. Hence, such an intensive multistage process requires many different machines and human skill sets to produce a final product. Each stage of manufacture introduces risk of non-conformity. The conventional manufacturing techniques typically take weeks to produce a single component.The above forging and casting methods require multiple production stages including casting, forging, cooling pipe cutting, forming and welding, rough cutting, drilling, heating, bending, machining and welding. Hence, such an intensive multi-stage process requires many different machines and human skill sets to produce a final product. Each stage of manufacture introduces risk or non-conformity. The conventional manufacturing techniques typically take weeks to produce a single component.
-2In use, the components are subjected to high temperatures in the furnace over years of operation. The necessity to cool these components in an electric furnace environment has necessitated the use of materials with superior thermal conductivities and relatively good mechanical properties, for which copper has become the preferred material of construction. With the use of copper to form the body of the component, even elevated temperatures that pose no risk to the component per se, do accelerate the phenomenon of creep. Creep deforms the copper body at elevated temperatures despite relatively low stresses, thereby reducing the geometrical accuracy of the component and impeding the component’s ability to perform its inherent function. To mitigate the impact of creep, two remedies are generally used. Firstly, by selecting specialised and often expensive copper alloys to increase softening temperature, to improve hardness and to extend creep life. Secondly, by increasing the cross-sectional area of the component, so that stress in the component, which is a function of area, is reduced. The latter option results in large and cumbersome components which are “oversized” to add creep resistance rather than to provide any significant thermal advantages.-2In use, the components are subject to high temperatures in the furnace over years of operation. The necessity to cool these components in an electric furnace environment has necessitated the use of materials with superior thermal conductivities and relatively good mechanical properties, for which copper has become the preferred material of construction. With the use of copper to form the body of the component, even elevated temperatures that pose no risk to the component per se, do accelerate the phenomenon of creep. Create deforms the copper body at elevated temperatures despite relatively low stresses, continuously reducing the geometric accuracy of the component and impeding the component's ability to perform its inherent function. To mitigate the impact of creep, two remedies are generally used. Firstly, by selecting specialized and often expensive copper alloys to increase softening temperature, to improve hardness and to extend creep life. Secondly, by increasing the cross-sectional area of the component, so that stress in the component, which is a function of area, is reduced. The latter option results in large and numerical components which are "oversized" to add creep resistance rather than provide any significant thermal advantages.
Hence, the known components and methods may not be suitable for at least some applications.Hence, the known components and methods may not be suitable for at least some applications.
OBJECT OF THE INVENTIONOBJECT OF THE INVENTION
Accordingly, it is an object of the present invention to provide a component for an electric furnace and a method of manufacturing the component, with which at least some of the above problems may be alleviated or which may provide a useful alternative for the known components and/or methods.Aw, it is an object of the present invention to provide a component for an electric furnace and a method of manufacturing the component, with which at least some of the above problems may be alleviated or which may provide a useful alternative to the known components and / or methods.
SUMMARY OF THE INVENTIONSUMMARY OF THE INVENTION
According to a first aspect of the invention there is provided a component for an electric furnace, the component comprising a body which is made by an additive manufacturing method utilising at least a first material.According to a first aspect of the invention there is provided a component for an electric furnace, the component including a body which is made by an additive manufacturing method utilizing at least a first material.
The component may be any one of, but not limited to, a pressure ring segment, a contact plate or a contact shoe, a bellows or biasing device, a hanger or hanging device, an insulating device and a heat shield.The component may be any one, but not limited to, a pressure ring segment, a contact plate or a contact shoe, a bellows or biasing device, a pendant or hanging device, an insulating device and a heat shield.
The component may form part of a lower electrode assembly for an electric furnace. The lower electrode assembly normally comprises the pressure ring segment, the contact plate,The component may form a part of a lower electrode assembly for an electric furnace. The lower electrode assembly normally comprises the pressure ring segment, the contact plate,
-3the biasing device, the hanging device, the heat shield, the insulating device and a sealing device such as a pressure ring tip seal.-3the biasing device, the hanging device, the heat shield, the insulating device and a sealing device such as a pressure ring tip seal.
The additive manufacturing method may comprise a “3D printing” technique including, but not limited to any one of: laser sintering, laser metal deposition or other associated methods and/or techniques, including, for example, the method known in the trade as “electron beam additive manufacturing” (EBAM®).The additive manufacturing method may include a "3D printing" technique including, but not limited to any one of: laser sintering, laser metal deposition or other associated methods and / or techniques, including, for example, the method known in the trade as “ electron beam additive manufacturing (EBAM®).
The body of the component may comprise a frame or skeleton for supporting a remainder of the body.The body of the component may comprise a frame or skeleton for supporting a remainder of the body.
The component, including the frame and the remainder of the body, may be made by forming sequential layers of the body during a single run of the additive manufacturing method.The component, including the frame and the remainder of the body, may be made by forming sequential layers of the body during a single run of the additive manufacturing method.
The remainder of the body may be made of the first material and the frame may be made of a second material.The remainder of the body may be made of the first material and the frame may be made of a second material.
The first and second materials may be metallic or a metal alloy.The first and second materials may be metallic or a metal alloy.
The first and second materials may be different from one another.The first and second materials may be different from one another.
The first material may be selectable from a group comprising copper and copper-based alloys including but not limited to alloys containing silver, nickel, chrome, zirconium, iron, silicon and tin.The first material may be selectable from a group including copper and copper-based alloys including but not limited to alloys containing silver, nickel, chrome, zirconium, iron, silicon and tin.
The second material may be selectable from a group comprising: carbon steel, ferritic and/or austenitic stainless steel and ferrous alloys including ferroalloys, etc.The second material may be selectable from a group including: carbon steel, ferritic and / or austenitic stainless steel and ferrous alloys including ferroalloys, etc.
The first and second materials may be fused to one another during the additive manufacturing method, for example by close proximity melting and re-solidification.The first and second materials may be fused to another during the additive manufacturing method, for example by close proximity melting and re-solidification.
The body of the component may at least partially be cladded by a cladding layer of a third material. The third material may be selectable from a group comprising ceramic material, metal alloys, silicates or silicon alloys etc. The cladding layer may be a heat insulating or heat dispersing layer.The body of the component may at least be partially cladded by a cladding layer or a third material. The third material may be selectable from a group including ceramic material, metal alloys, silicates or silicon alloys etc. The cladding layer may be a heat insulating or heat dispersing layer.
-4The cladding layer may be formed during the single run of the additive manufacturing method.-4 The cladding layer may be formed during the single run or the additive manufacturing method.
The body may define an internal cooling passage for a cooling fluid.The body may define an internal cooling passage for a cooling fluid.
The cooling passage may be provided by forming a void in the body of the component. The void may be formed during the single run of the additive manufacturing method.The cooling passage may be provided by forming a void in the body or the component. The void may be formed during the single run or the additive manufacturing method.
It will be appreciated that by utilising the additive manufacturing method, the dependence on conventional void formation is absent and the cooling passage may be created by forming a void of irregular shape.It will be appreciated that utilizing the additive manufacturing method, the dependence on conventional void formation is absent and the cooling passage may be created by forming a void or irregular shape.
The cooling passage may have a varying cross section along its length.The cooling passage may have a varying cross section along its length.
A plurality of cooling circuits may be formed which run separately and/or which combine with one another.A variety of cooling circuits may be formed which run separately and / or which combine with one another.
The cooling passage or the plurality of cooling circuits may have a predetermined internal geometry (e.g. spirals) which creates controlled turbulence of the cooling fluid for the benefit of heat transfer, etc.The cooling passage or the multiple of cooling circuits may have a predetermined internal geometry (e.g. spirals) which creates controlled turbulence or the cooling fluid for the benefit of heat transfer, etc.
According to a second aspect of the invention there is provided a method of manufacturing a component for an electric furnace, the method comprising utilising an additive manufacturing technique to form the component layer by layer, utilising at least a first material.According to a second aspect of the invention there is provided a method of manufacturing a component for an electric furnace, the method including utilizing an additive manufacturing technique to form the component layer by layer, utilizing at least a first material.
BRIEF DESCRIPTION OF THE ACCOMPANYING DIAGRAMSLETTER DESCRIPTION OF THE ACCOMPANYING DIAGRAMS
The invention will now further be described, by way of example only, with reference to the accompanying diagrams wherein:The invention will now be further described, by way of example only, with reference to the accompanying diagrams:
figure 1 is a diagrammatic perspective view of a lower electrode assembly of components for an electric furnace;figure 1 is a diagrammatic perspective view of a lower electrode assembly or components for an electric furnace;
figure 2is a diagrammatic perspective view of a pressure ring segment for the electric furnace;figure 2 is a diagrammatic perspective view of a pressure ring segment for the electric furnace;
figure 3is a diagrammatic representation of an additive manufacturing method showing the pressure ring segment in a partially completed form; and figure 4is a diagrammatic perspective view of the pressure ring segment, illustrating a frame and internal cooling channels.figure 3 is a diagrammatic representation of an additive manufacturing method showing the pressure ring segment in a partially completed form; and figure 4 is a diagrammatic perspective view of the pressure ring segment, illustrating a frame and internal cooling channels.
-5DESCRIPTION OF A PREFERRED EMBODIMENT OF THE INVENTION-5DESCRIPTION OF A PREFERRED EMBODIMENT OF THE INVENTION
An example embodiment of a component for an electric furnace forming part of a lower electrode assembly 100 (shown in figure 1) is generally designated by the reference numeral 10 in the figures.An example embodiment of a component for an electric furnace forming part of a lower electrode assembly 100 (shown in figure 1) is generally designated by the reference numeral 10 in the figures.
In the example embodiment, the component 10 is a pressure ring segment. The component may also be in the form of a contact shoe or contact plate 12, a biasing device or bellows 14, a hanging device 16, 18, a sealing device 20, 21, (such as a pressure ring tip seal 20 and a rope seal 21), a heat shield 24 or insulating device 22 forming part of the lower electrode assembly 100.In the example embodiment, the component 10 is a pressure ring segment. The component may also be in the form of a contact shoe or contact plate 12, a biasing device or bellows 14, a hanging device 16, 18, a sealing device 20, 21, (such as a pressure ring tip seal 20 and a rope seal 21), a heat shield 24 or insulating device 22 forming part of the lower electrode assembly 100.
Referring to figures 2 and 3, the component 10 comprises a body 26 which is made by an additive manufacturing method 28 utilising at least a first material 30. In figure 3 is shown the component 10 in a partially completed form, during the additive manufacturing method 28 and in figure 2 is shown the component 10 after the additive manufacturing method 28 is completed.Referring to figures 2 and 3, the component 10 comprises a body 26 which is made by an additive manufacturing method 28 utilizing at least a first material 30. Figure 3 shows the component 10 in a partially completed form, during the additive manufacturing method 28 and in figure 2 the component 10 is shown after the additive manufacturing method 28 is completed.
The additive manufacturing method 28 is preferably a “3D printing” technique including, but not limited to any one of: laser sintering, laser metal deposition or other associated methods and/or techniques including, for example, the method known in the trade as “electron beam additive manufacturing” (EBAM®). For explanatory purposes the term “3D printing” will be used as a synonym for any one of the aforementioned methods. A 3D printing apparatus 32 is provided for performing the additive manufacturing method 28.The additive manufacturing method 28 is preferably a "3D printing" technique including, but not limited to any one of: laser sintering, laser metal deposition or other associated methods and / or techniques including, for example, the method known in the trade as “ electron beam additive manufacturing (EBAM®). For explanatory purposes the term "3D printing" will be used as a synonym for any one of the aforementioned methods. A 3D printing apparatus 32 is provided for performing the additive manufacturing method 28.
Referring to figures 3 and 4, the body 26 of the component 10 comprises a skeleton or frame 34 for supporting a remainder 30 of the body 26. The remainder 30 of the body is made of the first material and the frame 34 is preferably made of a second material. The body 26 of the component 10 is at least partially cladded by a cladding layer 36 of a third material. The third material is preferably in the form of a heat insulating or heat dispersing material so that the cladding layer 36 provides resistance to heat transfer from an interior of the furnace to the component 10. The body 26 further defines an internal cooling passage 38 for a cooling fluid. Other insulating or sealing devices forming part of the lower electrode assembly 100 (shown in figure 1) may also be formed utilising the additive manufacturing method.Referring to figures 3 and 4, the body 26 of the component 10 comprises a skeleton or frame 34 for supporting a remainder 30 of the body 26. The remainder 30 of the body is made of the first material and the frame 34 is preferably made of a second material. The body 26 or the component 10 is at least partially cladded by a cladding layer 36 or a third material. The third material is preferably in the form of a heat insulating or heat dispersing material so that the cladding layer 36 provides resistance to heat transfer from an interior of the furnace to the component 10. The body 26 further defines an internal cooling passage 38 for a cooling fluid. Other insulating or sealing devices forming part of the lower electrode assembly 100 (shown in figure 1) may also be used utilizing the additive manufacturing method.
Referring to figure 3, the component 10, including the frame 34 and the remainder 30 of the body 26, is preferably made by forming sequential layers of the body. 3D printing apparatus 32 initiates the method 28 by depositing a first layer of the body 26. Sequential layers areReferring to figure 3, the component 10, including the frame 34 and the remainder 30 or the body 26, is preferably made by forming sequential layers of the body. 3D printing apparatus 32 initiates the method 28 by depositing a first layer of the body 26. Sequential layers are
-6then deposited by 3D printing apparatus in a layer by layer fashion, until the component 10 is completed. The sequential process of depositing layers from a first layer to a last layer of the body 26 may be referred to as a single run of the additive manufacturing method 28. During the single run, the frame 34, the remainder 30 of the body 26, the cladding layer 36 and the cooling passage 38 are formed. The 3D printing apparatus is configured to deposit the first material 30, the second material 34 and the third material 36. As indicated by the three arrows in figure 3, the first, second and third materials 30, 34 and 36 are welded, sintered or fused together, depending on the particular additive manufacturing method or technique utilised. The first, second and/or third materials may also be fused to one another or bound on a molecular or microscopic level during the additive manufacturing. The cooling passage 38 is provided by forming a void in the body 26 of the component during the single run of the additive manufacturing method 28.-6then deposited by 3D printing apparatus in a layer by layer fashion, until the component 10 is completed. The sequential process of depositing layers from a first layer to a last layer of the body 26 may be referred to as a single run of the additive manufacturing method 28. During the single run, the frame 34, the remainder 30 of the body 26, the cladding layer 36 and the cooling passage 38 are formed. The 3D printing apparatus is configured to deposit the first material 30, the second material 34 and the third material 36. As indicated by the three arrows in Figure 3, the first, second and third materials 30, 34 and 36 are welded, sintered or fused together, depending on the particular additive manufacturing method or technique utilized. The first, second and / or third materials may also be fused to one or another bound on a molecular or microscopic level during additive manufacturing. The cooling passage 38 is provided by forming a void in the body 26 or the component during the single run of the additive manufacturing method 28.
Referring to figure 4, the remainder 30 of the body 26 is shown in broken lines. The frame 34 preferably comprises a plurality of structural elements for supporting the remainder 30 of the body 26. The structural elements comprise pillars 34.1 and supporting members or ribs 34.2. An inlet 40 and an outlet 42 of the cooling passage 38, a plurality of fastening locations 44 and a sealing channel 46 are preferably also made of the second material 34 during the single run of the additive manufacturing method 28. Sealing devices 20, 21 and insulating device 22 (shown in figure 1) are preferably made separately and may also be made by a 3D printing technique.Referring to figure 4, the remainder 30 or the body 26 is shown in broken lines. The frame 34 preferably comprises a variety of structural elements for supporting the remainder 30 of the body 26. The structural elements comprise pillars 34.1 and supporting members or ribs 34.2. An inlet 40 and an outlet 42 of the cooling passage 38, a variety of fastening locations 44 and a sealing channel 46 are preferably also made of the second material 34 during the single run of the additive manufacturing method 28. Sealing devices 20, 21 and insulating device 22 (shown in figure 1) are preferably made separately and may also be made by a 3D printing technique.
The first and second materials 30, 34 are preferably metallic or a metal alloy. The first material 30 is selectable from a group comprising copper and copper-based alloys including but not limited to alloys containing silver, nickel, chrome, zirconium, iron, silicon and tin. The second material 34 is selectable from a group comprising: carbon steel, ferritic and austenitic stainless steel, etc. The third material 36 of the cladding layer is preferably a heat insulating or heat dispersive material and is selectable from a group comprising ceramic material, metal alloys, silicates or silicon alloys, etc.The first and second materials 30, 34 are preferably metallic or a metal alloy. The first material 30 is selectable from a group including copper and copper-based alloys including but not limited to alloys containing silver, nickel, chrome, zirconium, iron, silicon and tin. The second material 34 is selectable from a group including: carbon steel, ferritic and austenitic stainless steel, etc. The third material 36 or the cladding layer is preferably a heat insulating or heat dispersive material and is selectable from a group including ceramic material, metal alloys, silicates or silicon alloys, etc.
It will be appreciated that there are many variations in detail on the invention as herein defined and/or described without departing from the scope and spirit of this disclosure.It will be appreciated that there are many variations in detail on the invention as described and / or described without departing from the scope and spirit of this disclosure.
For example, the additive manufacturing of the pressure ring segment 10 is described above, however other components of the lower electrode assembly 100 may also be manufactured utilising the method 28. It will further be appreciated that different parts of the components may be manufactured separately and assembled together at a later stage, or manufacturedFor example, the additive manufacturing of the pressure ring segment 10 is described above, but other components of the lower electrode assembly 100 may also be manufactured utilizing the method 28. It will be further appreciated that different parts of the components may be manufactured separately and assembled together at a later stage, or manufactured
-7during the single run of the additive manufacturing method. The components may also be manufactured utilising only a single one of the first, second and third materials. Annealing of the body 26 may not be required after the component 10 is manufactured using the additive manufacturing method 28. By utilising the frame 34, creep of the remainder 30 of the body 26 is prevented or at least alleviated.-7during the single run or the additive manufacturing method. The components may also be manufactured utilizing only a single one of the first, second and third materials. Annealing of the body 26 may not be required after the component 10 is manufactured using the additive manufacturing method 28. By utilizing the frame 34, creep of the remainder 30 or the body 26 is prevented or at least alleviated.
It will further be appreciated that by utilising the method 28, many different shapes and configurations of the cooling passage 38 are possible. No drilling or plugging of the body 26 is required to form the cooling passage 38. As described above, the inlet 40 and outlet 42 of the cooling passage 38 may be formed from the second material 34, preferably stainless steel. Other parts of the cooling passage 38 may also be formed from the second material 34 or even from the third material 36. The cooling passage 38 may be in the form of a series cooling circuit, an example of which is illustrated in figure 4. Parallel cooling circuits or arrangements are also possible, wherein two or more inlets and two or more outlets are provided for the cooling fluid.It will be further appreciated that by utilizing the method 28, many different shapes and configurations of the cooling passage 38 are possible. No drilling or plugging of the body 26 is required to form the cooling passage 38. As described above, the inlet 40 and outlet 42 of the cooling passage 38 may be formed from the second material 34, preferably stainless steel. Other parts of the cooling passage 38 may also be formed from the second material 34 or even from the third material 36. The cooling passage 38 may be in the form of a series cooling circuit, an example or which is illustrated in figure 4. Parallel cooling circuits or arrangements are also possible, two or more inlets and two or more outlets are provided for the cooling fluid.
It will be appreciated that by utilising the additive manufacturing method, the dependence on conventional void formation is absent and the cooling passage 38 may be created by forming a void of irregular shape. The cooling passage 38 may have a varying cross section along its length. A plurality of cooling circuits (not shown) may be formed which run separately and/or which combine. The cooling passage 38 or the plurality of cooling circuits may have a predetermined internal geometry (e.g. spirals) which creates controlled turbulence of the cooling fluid for the benefit of heat transfer, etc.It will be appreciated that utilizing the additive manufacturing method, the dependence on conventional void formation is absent and the cooling passage 38 may be created by forming a void or irregular shape. The cooling passage 38 may have a varying cross section along its length. A variety of cooling circuits (not shown) may be formed which run separately and / or which combine. The cooling passage 38 or the multiple of cooling circuits may have a predetermined internal geometry (e.g. spirals) which creates controlled turbulence or the cooling fluid for the benefit of heat transfer, etc.
As described above, the cooling passage 38, frame 34 and cladding layer 36 are provided in the pressure ring segment 10. However, other cooling passages and/or frames and or cladding layers may be similarly provided in the other components of the lower electrode assembly 100, such as in the contact shoe or contact plate 12, in the biasing device or bellows 14, in the hanging device 16, 18, in the sealing device 20, 21, in the insulating device 22 and in the heat shield 24.As described above, the cooling passage 38, frame 34 and cladding layer 36 are provided in the pressure ring segment 10. However, other cooling passages and / or frames and or cladding layers may be similarly provided in the other components of the lower electrode assembly 100, such as in the contact shoe or contact plate 12, in the biasing device or bellows 14, in the hanging device 16, 18, in the sealing device 20, 21, in the insulating device 22 and in the heat shield 24.
It will yet further be appreciated that the invention provides several advantages over the prior art. Firstly, the components may be made using a single setup and may be completed in a single run of the additive manufacturing method. The manufacturing of the component may be completed in mere hours while prior art methods require weeks to complete.It will yet be further appreciated that the invention provides several advantages about the prior art. Firstly, the components may be made using a single setup and may be completed in a single run of the additive manufacturing method. The manufacturing of the component may be completed in more hours while prior art methods require weeks to complete.
-8Secondly, by utilising additive manufacturing, the first and second materials (which may be dissimilar metals) may be fused to one another and/or embedded in one another. Hence, the component may be given a desirable property of the first material 30 (such as the ability to cool rapidly and to protect the second material 34) while also imparting a desirable property of the second material 34 (such as strength and creep resistance) to the component 10. This symbiotic relationship on a metallurgical level between the first and second materials results in an improved component compared to prior art components.-8Secondly, by utilizing additive manufacturing, the first and second materials (which may be dissimilar metals) may be fused to one another and / or embedded in one another. Hence, the component may be given as a desirable property of the first material 30 (such as the ability to cool rapidly and to protect the second material 34) while also imparting a desirable property of the second material 34 (such as strength and creep resistance) to the component 10. This symbiotic relationship on a metallurgical level between the first and second materials results in an improved component compared to prior art components.
Thirdly, in addition to the first and second materials, the third material is preferably melted with and re-solidified to bind or bond to the first and/or second materials to form the cladding layer for thermal insulation, arch- or wear resistance. Utilising the additive manufacturing method, this cladding may be positioned accurately and efficiently on designated surfaces of the component utilising a microscopically fused bond that essentially extends the first and/or second materials.Thirdly, in addition to the first and second materials, the third material is preferably melted with and re-solidified to bond or bond to the first and / or second materials to form the cladding layer for thermal insulation, arch or wear resistance. Utilizing the additive manufacturing method, this cladding may be positioned accurately and efficiently on designated surfaces or the component utilizing a microscopically fused bond that essentially extends the first and / or second materials.
Fourthly, cooling of electric furnace equipment operating inside the furnace is paramount. Whilst the use of embedded cooling pipes in cast components or drilling and plugging in forged components has provided sufficient cooling to date, both have distinct lead time, complexity, geometry and inherent reliability drawbacks. With additive manufacturing, any shape, direction, number and/or cross-sectional area of cooling passages or channels may be introduced to specifically target high heat areas of the component without any need for the introduction of a plug, without the limitation of the fact that a drill cannot go around a corner and without the limitation of not being able to vary the drill’s cross-sectional area along the length of a drilled port, etc.Fourthly, cooling or electric furnace equipment operating inside the furnace is paramount. Whilst the use of embedded cooling pipes in cast components or drilling and plugging in forged components has provided sufficient cooling to date, both have distinct lead time, complexity, geometry and inherent reliability drawbacks. With additive manufacturing, any shape, direction, number and / or cross-sectional area or cooling passages or channels may be introduced to specifically target high heat areas of the component without any need for the introduction of a plug, without the limitation of the fact that a drill cannot go around a corner and without the limitation or not being able to vary the drill's cross-sectional area along the length of a drilled port, etc.
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL2020368A NL2020368B1 (en) | 2018-02-01 | 2018-02-01 | A component for an electric furnace |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL2020368A NL2020368B1 (en) | 2018-02-01 | 2018-02-01 | A component for an electric furnace |
Publications (1)
Publication Number | Publication Date |
---|---|
NL2020368B1 true NL2020368B1 (en) | 2019-08-12 |
Family
ID=61628430
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL2020368A NL2020368B1 (en) | 2018-02-01 | 2018-02-01 | A component for an electric furnace |
Country Status (1)
Country | Link |
---|---|
NL (1) | NL2020368B1 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005071335A2 (en) * | 2004-01-19 | 2005-08-04 | Metix (Pty) Limited | Arc furnace pressure ring assembly |
EP2998282A1 (en) * | 2014-09-18 | 2016-03-23 | Toto Ltd. | Process for producing reaction bonded silicon carbide member |
WO2016138997A1 (en) * | 2015-03-05 | 2016-09-09 | Linde Aktiengesellschaft | 3d-printed heating surface element for a plate heat exchanger |
EP3338598A2 (en) * | 2016-12-23 | 2018-06-27 | Vorwerk & Co. Interholding GmbH | Cooking vessel for a kitchen machine, kitchen machine and method of manufacturing a heating element |
-
2018
- 2018-02-01 NL NL2020368A patent/NL2020368B1/en not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005071335A2 (en) * | 2004-01-19 | 2005-08-04 | Metix (Pty) Limited | Arc furnace pressure ring assembly |
EP2998282A1 (en) * | 2014-09-18 | 2016-03-23 | Toto Ltd. | Process for producing reaction bonded silicon carbide member |
WO2016138997A1 (en) * | 2015-03-05 | 2016-09-09 | Linde Aktiengesellschaft | 3d-printed heating surface element for a plate heat exchanger |
EP3338598A2 (en) * | 2016-12-23 | 2018-06-27 | Vorwerk & Co. Interholding GmbH | Cooking vessel for a kitchen machine, kitchen machine and method of manufacturing a heating element |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Lee et al. | Effects of copper insert layer on the properties of friction welded joints between TiAl and AISI 4140 structural steel | |
JPWO2017069268A1 (en) | Resistance spot welding method | |
JPS6037162B2 (en) | Manufacturing method of clad metal pipe | |
Wang et al. | Interface structure and mechanical properties of Ti (C, N)-based cermet and 17-4PH stainless steel joint brazed with nickel-base filler metal BNi-2 | |
Mohammed et al. | Trend and development of semisolid metal joining processing | |
CA2983078C (en) | Laser sintered die surface for a tool | |
He et al. | Controlling residual stress and distortion of friction stir welding joint by external stationary shoulder | |
JP5033423B2 (en) | Heat treatment method in press fitting | |
NL2020368B1 (en) | A component for an electric furnace | |
Kuball et al. | Process design for the forming of semi-tubular self-piercing rivets made of high nitrogen steel | |
Lim et al. | Ti-6Al-4V/SUS316L dissimilar joints with ultrahigh joint efficiency fabricated by a novel pressure-controlled joule heat forge welding method | |
Shin et al. | Enhanced cooling channel efficiency of high-pressure die-casting molds with pure copper linings in cooling channels via explosive bonding | |
Santhoshsarang et al. | Additively manufactured high-performance conformally cooled H13 tool steel die insert for pressure die casting | |
Bouarroudj et al. | Improved performance of a heterogeneous weld joint of copper-steel AISI 1045 obtained by rotary friction using a metal powder insert | |
JP2005514522A (en) | Cold plate for metallurgical furnace and method of manufacturing such a cold plate | |
Lalvani et al. | A solid-state joining approach to manufacture of transition joints for high integrity applications | |
Eroglu et al. | Diffusion bonding between high chromium white iron and low carbon steel | |
RU2486043C1 (en) | Method of producing composite articles with inner cavities by explosion welding | |
JP2002121643A (en) | Steel for diecasting die, method for producing diecasting die composed by using the same and diecasting die | |
Behrens et al. | Compound forging of hybrid powder-solid-parts made of steel and aluminum | |
Shin et al. | Microstructure and mechanical properties of SKD61–Cu cooling channel fabricated via explosive welding | |
NL8103201A (en) | METHOD FOR GIVING HEAT TREATMENT TO METAL | |
Stuth et al. | New technological approach in fabrication of high purity Nickel wire | |
Kim et al. | Microstructure and mechanical properties of friction-welded S20C and SCM415H steels | |
JPS6064785A (en) | Pipe having corrosion- and wear-resistant inside wall layer and its production |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM | Lapsed because of non-payment of the annual fee |
Effective date: 20210301 |