WO2019195129A1 - Apparatus and method for forming an article - Google Patents
Apparatus and method for forming an article Download PDFInfo
- Publication number
- WO2019195129A1 WO2019195129A1 PCT/US2019/025110 US2019025110W WO2019195129A1 WO 2019195129 A1 WO2019195129 A1 WO 2019195129A1 US 2019025110 W US2019025110 W US 2019025110W WO 2019195129 A1 WO2019195129 A1 WO 2019195129A1
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- WO
- WIPO (PCT)
- Prior art keywords
- layer
- nonconductive
- liquid formulation
- bushing
- article
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/10—Processes of additive manufacturing
- B29C64/106—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
- B29C64/124—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using layers of liquid which are selectively solidified
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/20—Apparatus for additive manufacturing; Details thereof or accessories therefor
- B29C64/205—Means for applying layers
- B29C64/218—Rollers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/20—Apparatus for additive manufacturing; Details thereof or accessories therefor
- B29C64/227—Driving means
- B29C64/241—Driving means for rotary motion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/20—Apparatus for additive manufacturing; Details thereof or accessories therefor
- B29C64/245—Platforms or substrates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/20—Apparatus for additive manufacturing; Details thereof or accessories therefor
- B29C64/264—Arrangements for irradiation
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/30—Auxiliary operations or equipment
- B29C64/386—Data acquisition or data processing for additive manufacturing
- B29C64/393—Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
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- 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
- B33Y10/00—Processes of additive manufacturing
-
- 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
- B33Y30/00—Apparatus for additive manufacturing; Details thereof or accessories therefor
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0003—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular electrical or magnetic properties, e.g. piezoelectric
- B29K2995/0005—Conductive
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0003—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular electrical or magnetic properties, e.g. piezoelectric
- B29K2995/0007—Insulating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/34—Electrical apparatus, e.g. sparking plugs or parts thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/34—Electrical apparatus, e.g. sparking plugs or parts thereof
- B29L2031/3412—Insulators
-
- 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
- B33Y50/00—Data acquisition or data processing for additive manufacturing
- B33Y50/02—Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
-
- 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
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B17/00—Insulators or insulating bodies characterised by their form
- H01B17/26—Lead-in insulators; Lead-through insulators
- H01B17/28—Capacitor type
Definitions
- the present application generally relates to forming articles using additive manufacturing and more particularly, but not exclusively, to forming articles such as, e.g., condenser bushings, bulk-type bushings or other articles, using an additive manufacturing process.
- Condenser bushings e.g., for transformers and other devices, remain an area of interest.
- Some existing systems have various shortcomings, drawbacks and
- the manufacturing of the condenser bushing may be performed in shorter time periods. Accordingly, there remains a need for further contributions in this area of technology.
- One embodiment of the present invention is a unique method for forming an article of manufacturing using additive manufacturing. Another embodiment is a method for forming a condenser or bulk-type bushing using additive manufacturing. Another embodiment is a unique apparatus. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for articles of manufacture, including condenser bushings and bulk-type bushings. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
- FIG. 1 schematically illustrates some aspects of a non-limiting example of a system for manufacturing an article, such as a condenser bushing, using an additive manufacturing process in accordance with an embodiment of the present invention.
- FIG. 2 is a flowchart depicting some aspects of a non-limiting example of a method for forming an article of manufacture, e.g., a condenser bushing, using additive manufacturing in accordance with an embodiment of the present invention.
- FIG. 3 schematically illustrates some aspects of an expanded view of an article being formed, depicting a sub layer of a nonconductive liquid formulation being cured in accordance with an embodiment of the present invention.
- FIG. 4 schematically illustrates some aspects of non-limiting example of an article formed using an additive manufacturing process in accordance with an embodiment of the present invention.
- FIG. 5 schematically illustrates some aspects of a non-limiting example of a section view of the article of FIG. 4 in accordance with an embodiment of the present invention.
- FIGS. 6A-6C schematically illustrate some aspects of a non-limiting example of an article formed using an additive manufacturing process wherein the length of the conductive layers along the axis of rotation varies, e.g., to provide electric field grading, in accordance with an embodiment of the present invention.
- FIGS. 7 A and 7B schematically illustrate some aspects of a non-limiting example of an article formed using an additive manufacturing process, wherein the shape of the article is not a body of revolution, in accordance with an embodiment of the present invention.
- FIGS. 8A and 8B schematically illustrate some aspects of a non-limiting example of an article formed using an additive manufacturing process, wherein the shape of the article is not a body of revolution, in accordance with an embodiment of the present invention.
- FIG. 9A-9C schematically illustrate some aspects of a non-limiting example of an article formed using an additive manufacturing process, wherein cured nonconductive segments are separated from each other by an air gap in accordance with an embodiment of the present invention.
- FIGS. 10A and 10B schematically illustrate some aspects of a non-limiting example of an article formed using an additive manufacturing process, wherein a single continuous conductive layer in the form of a spiral is employed in accordance with an embodiment of the present invention.
- article 12 may be, for example, a transformer bushing or another type of condenser bushing or bulk-type bushing having a cylindrical conductor 14 at its core.
- conductor 14 may not be cylindrical, but rather, other shapes may be employed.
- conductor 14 have a hexagonal and/or other cross- sectional shape(s) in place of the circular cross-sectional shape of a cylinder.
- conductor 14 may be solid or may be hollow or may be solid in some portions and hollow in other portions.
- Article 12 may be constructed for use or as part of an electrical system, such as a low, medium or high voltage electrical system or electrical distribution system, e.g., for use in or with a transformer, switchgear and/or other electrical system components.
- article 12 may be another type of article of manufacture, e.g., other than a condenser bushing.
- System 10 includes a controller 16, a rotational stage 18, and an energy source 20 disposed at a first production station 22.
- Energy source 20 may be used for curing a photocurable polymer, monomer, oligomer and/or other liquid formulation, and/or may be used for melting, and/or may be used for providing a reaction trigger, and/or may be used for other purposes.
- Some embodiments include a second production station 24 having a material application system 26.
- Such embodiments may include a transfer mechanism 28 constructed to move the article 12 being formed (and in some embodiments, rotational stage 18) between first production station 22 and second production station 24 during the manufacturing of article 12, e.g., so that production operations may be alternatingly performed by first production station 22 and second production station 24.
- transfer mechanism 28 may also be constructed to move the article 12 being formed (and in some embodiments, rotational stage 18) to other production stations for the performance of other manufacturing operations, e.g., cleaning, drying and/or other operations.
- Other embodiments may alternatively include a material application system 30 at production stage 22, e.g., in place of material application system 26.
- shielding 32 may be positioned to avoid contamination of first production station 22.
- Controller 16 includes a processor 34 coupled to a memory device 36, such as a non-transitory computer readable storage medium readable by a processor and storing program instructions 38 for execution by the processor 34.
- memory device 36 may obtain program instructions 38 from another non-transitory computer readable storage medium readable by a processor and storing program instructions 38 for execution by a processor, e.g., via downloading by wired or wireless or optical connection.
- Controller 16 is communicatively coupled to rotational stage 18, energy source 20, material application system 26, transfer mechanism 28, and in embodiments so equipped, material applications system 30.
- controller 16 e.g., processor 34, executes program instructions 38 to perform the various acts described herein.
- Process flow begins at block 102.
- a mandrel e.g., conductor 14, which may or may not be cylindrical, is mounted on rotational stage 18.
- Rotational stage 18 is operative to rotate the mandrel and the article 12 being formed about a horizontal axis of rotation 40, which extends perpendicular to the plane of view of FIG. 1.
- environmental conditions in production station 22, and in some embodiments, production station 24, are controlled to achieve desired levels and are stabilized at the desired levels, e.g., within a desired tolerance band, for example, to maintain desired properties of formulation 46 for the formation of nonconductive layers 50 and/or to maintain desired properties of the conductive material for the formation of conductive layers 52 (formulation 46, nonconductive layers 50 and conductive layers 52 are described below).
- the ambient gas composition, humidity, temperature and pressure are controlled to achieve desired levels and stabilized at the desired levels in production station 22, and in some embodiments, in production station 24.
- the levels in production station 24 may or may not be the same as in production station 22.
- the ambient humidity, temperature and pressure may be controlled and stabilized by, for example, equipment such as humidifiers, heaters and chillers.
- the ambient gas composition may be controlled and stabilized by use of, among other things, for example, bottled gas, gas separation modules, vents, filters, atmospheric recyclers and/or other means to maintain a desired gas composition in production station 22, and in some embodiments, production station 24.
- the environmental conditions may be controlled (and stabilized) by processor 34.
- the environmental conditions may be controlled (and stabilized) by one or more other processors or controllers, with or without human intervention, or may be controlled (and stabilized) by human input.
- processor 34 executes program instructions 38 to rotate the article 12 being formed about horizontal axis 40.
- the rotation is in a counterclockwise direction 42.
- the rotation is continuous at a constant angular speed or velocity.
- the rotation may be intermittent and/or may have a changing angular speed or velocity.
- article 12 being formed is partially submerged or immersed in a bath 44 of a liquid formulation 46.
- Liquid formulation 46 may be a polymer, a monomer and/or an oligomer, or a liquid formulation containing a polymer, monomer, oligomer or a combination thereof.
- liquid formulation 46 may include a photoinitiator.
- Liquid formulation 46 may be cured into a solid condition by application of the appropriate type and amount of energy, e.g., photonic energy.
- liquid formulation 46 is photocurable, i.e. , is subject to photoinduced hardening using a particular wavelength/frequency of electromagnetic radiation or light.
- a cured liquid formulation 46 is a solid.
- liquid formulation 46 is electrically nonconductive, i.e., is insulating. In other embodiments, liquid formulation 46 may be electrically conductive.
- liquid formulation 46 may be cured by, for example, an energy dose of ultraviolet light in some embodiments, or blue light in other embodiments or light of one or more other frequencies in other
- liquid formulation 46 may be curable by an energy dose of infrared radiation or infrared light.
- the liquid formulation 46 may contain solid particles or additives such as S1O2 and/or AI2O3 and/or one or more other materials.
- a linear stage 45 may be used to maintain a desired degree of immersion of the article 12 being formed in bath 44.
- the bath 44 level of liquid formulation 46 may be maintained by means not shown, e.g., a float valve and a pump.
- the rotation of the article 12 being formed in bath 44 entrains a quantity of the liquid formulation 46 onto article 12.
- the liquid formulation achieves a mean film thickness (radial thickness), H, along the article 12 being formed, and is cured by energy source 20 delivering a curing energy dose to the liquid formulation 46.
- the energy dose delivered by energy source 20 may be
- electromagnetic radiation which may be of one or more specific wavelengths, a range of wavelengths or a combination of discrete wavelengths and ranges of wavelengths.
- Non-limiting examples include an energy dose of ultraviolet light in some embodiments, or blue light in other embodiments or light of one or more other frequencies in other embodiments.
- liquid formulation 46 may be curable by an energy dose of infrared radiation or infrared light.
- film or sub layer thickness H of liquid formulation 46 is depicted.
- the film or sub layer thickness H i.e., the radial thickness
- the film or sub layer thickness H varies with the radius R of the article 12 being formed, the speed of rotation of the article 12 being formed (i.e., the angular velocity), and the density and viscosity of liquid formulation 46.
- Equation 1 may be used to approximate the radial thickness H:
- Equation 1 Equation 1 where m is liquid viscosity of the liquid formulation 46, W is the rotational or angular speed of article 12, p is liquid density of the liquid formulation 46, g is gravitational acceleration, R is the radius of the article 12 being formed, and H is the coating mean thickness (radial thickness) for the liquid formulation 46 on the outside of the article 12 being formed.
- system 10 applies liquid formulation 46 and achieves a desired radial thickness H of formulation 46 prior to curing, but without the use of scraper blades, rollers or other mechanical means to achieve the desired radial thickness H for curing.
- other approaches may be employed to obtain a desired radial thickness H may be utilized.
- scraper blades or rollers or other features or means may be employed to obtain a desired radial thickness H.
- the liquid formulation 46 may be applied, for example, by painting it on the article 12 being formed, by brushing, spray coating or dripping liquid formulation 46 onto the article 12 being formed, with or without the use of scraper blades, rollers or other means to obtain the desired radial thickness H.
- processor 34 executes program instructions 38 to control a rate of rotation of the article 12 being formed to achieve a desired radial thickness H of a sub layer of uncured liquid formulation 46 at a desired rotational location on the object, e.g., based on Equation 1 and calibrations of angular velocity and radial thickness H.
- the controlled rate of rotation may include adjustments to account for the increasing radius of the article 12 being formed as nonconductive (insulating) and conductive layers are added to the article 12 being formed, e.g., via additive manufacturing. In some embodiments, e.g., in some bulk-type bushings, only nonconductive layers may be applied.
- processor 34 executes program instructions 38 to direct energy source 20 to provide a curing energy dose onto the object at a desired rotational location, e.g., where the radial thickness H of the liquid formulation 46 is at a desired value.
- a curing energy dose is an energy dose configured and sufficient to cure and solidify a sub layer of desired radial thickness H, e.g., sub layer 48.
- the radial thickness of any given sub layer of liquid formulation 46 may be, for example, in the range of 0.02 mm to 3.0 mm. That is, a film or liquid sub layer having a radial thickness in the range of 0.02 mm to 3.0 mm may be cured into a solid sub layer 48 of liquid formulation 46.
- energy source 20 is or includes a digital light processor.
- energy source 20 may be any light/energy source capable of delivering radiant energy to cure the desired radial thickness H of liquid formulation 46, for example, one or more banks or arrays of light emitting diodes (LEDs), one or more lasers, such as line lasers and/or other lasers, and/or lamps, and/or one or more other suitable radiant light/energy sources.
- LEDs light emitting diodes
- lasers such as line lasers and/or other lasers, and/or lamps, and/or one or more other suitable radiant light/energy sources.
- the radiant energy produced by energy source 20 is transformed, enhanced and/or controlled by routing it through a mask, digital micro-mirror devices (DMDs), optical filters and/or lenses to produce the desired geometry of nonconductive sub layers 48 and nonconductive layers 50 (layers 50 of liquid formulation 46 are described below), and ultimately of the formed article 12.
- Energy source 20 may be constructed to provide the radiant energy in terms of ultraviolet light in some embodiments, or blue light in other embodiments or light of one or more other frequencies in other embodiments. In still other embodiments, infrared radiation or infrared light may be used.
- processor 34 executes program instructions directing energy source 20 to vary its output along the horizontal axis of rotation 40.
- energy source 20 may vary a length along the horizontal axis to which the energy dose is applied. Accordingly, the length of one cured liquid formulation 46 sub layer 48 or layer 50 along the horizontal axis of rotation 40 may be different than the length of another cured sub layer 48 or layer 50 along the horizontal axis of rotation 40.
- processor 34 executes program instructions directing energy source 20 to cure only desired segments along horizontal axis of rotation 40, e.g., such that cured segments along horizontal axis of rotation 40 may be generated and spaced apart along horizontal axis of rotation 40 by uncured segments, resulting in an article 12 having cured nonconductive segments separated from each other by an air gaps, and having overhung portions (e.g., as illustrated in FIGS. 9A-9C).
- the size or length along horizontal axis of rotation 40 of the cured and uncured segments may vary with the needs of the particular application.
- processor 34 executes program instructions to selectively control the output of energy source 20, e.g., controlling when it is turned on and when it is turned off or modulating its output, e.g., in the form of pulse width modulation, to achieve a shape of article 12 that is not a body of revolution, e.g., as illustrated in FIGS. 7A, 7B, 8A and 8B.
- processor 34 executes program instructions 38 to determine whether a desired radial thickness 54 of a cured
- nonconductive liquid formulation 46 layer 50 has been achieved.
- the radial thickness of nonconductive layer 50, and/or of one or more nonconductive sub layers 48 in some embodiments can be determined by image analysis (e.g. via 2D and/or 3D image and/or video processing), mechanical and/or optical physical measurements.
- the number of sub layers 48 of a layer 50 may be multiplied by the thickness of each sub layer 48 in order to determine whether the desired radial thickness 54 of the layer 50 has been achieved. If not process flow returns to block 104, and repeats the processes of blocks 104-108, building one or more sub layers 48 upon the initial sub layer 48 until a desired radial thickness of the cured formulation 46 layer 50 has been achieved. If so, process flow proceeds to block 112.
- a cured nonconductive layer 50 of liquid formulation 46 may be formed of a single sub layer 48 of cured nonconductive liquid formulation 46, whereas in other embodiments, a plurality of sub layers 48 of cured nonconductive liquid formulation 46 may be built up to achieve a single layer 50 of cured nonconductive liquid formulation 46.
- a“layer” of cured nonconductive liquid formulation 46 defines the separation distance between conductive layers 52 or between a conductive layer 52 and conductor 14.
- the radial distance between conductive layers 52 defines the radial thickness 54 of a layer 50, with the exception of the outermost nonconductive layer, which may have any desired radial thickness.
- processor 34 executes program instructions to determine whether the desired number of alternating nonconductive and conductive layers has been achieved. If so, process flow proceeds to block 118, and the process ends. If not, process flow proceeds to block 114.
- processor 34 executes program instructions to form or add a conductive layer 52, e.g., over all or part of the currently outermost nonconductive layer 50.
- processor 34 also executes program instructions to vary the length of conductive layer 52 along horizontal axis of rotation 40, wherein the length of conductive layers 52 may be different, i.e. , so that some conductive layers 52 are longer and/or shorter than others, e.g., to provide an electric field gradient to an article 12 in the form of a condenser bushing.
- processor 34 executes program instructions to direct transfer mechanism 28 to remove the article 12 being formed (and in some embodiments, rotational stage 18) from bath 44 and first production station 22 after achieving a desired nonconductive layer radial thickness, and deliver it to second production station 24 for the addition of a conductive layer by material application system 26.
- Material application system 26 is constructed to deposit a conductive layer onto the cured nonconductive layer.
- the article 12 being formed may be cleaned prior or subject to another procedure prior to the application of conductive layer 52.
- the volume of the article 12 being immersed in bath 44 may be modified, e.g., so that the entire article 12 being formed may be cured prior to the application of conductor layer 52.
- Material application system 26 may include a linear stage in order to allow material application system 26 to maintain a desired distance from the article 12 being formed.
- material application system 26 is a roller to transfer conductive material to the article 12 being formed, i.e. , transfer a conductive layer 52, in the form of a foil or paint, such as a carbon black paint.
- material application system 26 may be an inkjet engine operative to print the conductive layer onto the non-conductive layer (or onto a previous conductive layer).
- material application system 26 may be an electro-deposition system constructed to deposit a conductive layer over a nonconductive layer or over a previous conductive layer.
- the conductive layer 52 may also or alternatively be formed of a metallic paint, a metallic liquid, an epoxy and/or formulation 46.
- the metallic paint, metallic liquid, epoxy and/or formulation 46 may include or be formed partially of a conductive material, such as silver, carbon, carbon black, zinc, nickel, aluminum and/or copper, for example, or may have such materials distributed throughout the base of such paint, liquid, epoxy and/or formulation 46.
- the metallic paint and/or metallic liquid may be formed completely or substantially completely out of a conductive material, such as silver, carbon, carbon black, zinc, nickel, aluminum and/or copper, for example, or may have such materials distributed throughout the base of such metallic paint and/or metallic liquid.
- conductive layer 52 may be added by material application system 30 in first production station 22, wherein the conductive layer is added rotationally downstream of the provision of the curing energy dose during continuous rotation by rotational stage 18.
- the description of material application system 26 and conductive layer 52 materials applies equally to material application system 30.
- material application system 30 applies conductive layer 52 to a cured portion of the article 12 being formed, in some embodiments, the article 12 being formed does not need to be removed from bath 44 during the application of conductive layer 52 by material application system 30. In other embodiments, linear stage 45 may be used to lift article 12 from bath 44 prior to or during the application of one or more conductive layers 52.
- processor 34 executes program instructions to determine whether conductive layer 52 has a desired radial thickness 56. For example, one or more measurements may be taken to determine if conductive layer 52 has the desired radial thickness. Examples of measurements may include the radial thickness of conductive layer 52 being determined by image analysis (e.g. via 2D and/or 3D image and/or video processing), and/or mechanical, optical and/or physical measurements. In some embodiments, e.g., where conductive layer 52 is built from a plurality of sub layers of the conductive material, the number of sub layers may be multiplied by the thickness of each sub layer in order to determine whether the desired radial thickness 56 of a conductive layer 52 of has been achieved. In another example, the program
- instructions might call for more than one conductive layer 52 to be added, and the determination may be or may include a determination as to whether the count of the desired number of conductive layers or sub layers has been reached. If not, process flow proceeds back to block 114 for the addition of another conductive layer 52. If so, process flow proceeds back to block 104. Blocks 104-116 are repeated until at block 112, processor 34 executes program instructions to determine whether the desired number of alternating nonconductive and conductive layers has been achieved, and the result of the determination is that the desired number of alternating nonconductive and conductive layers.
- FIGS. 6A-6C some aspects of a non-limiting example of an article 12 formed using an additive manufacturing process e.g., as described herein, are schematically illustrated, wherein the length of the conductive layers 52 along the axis of rotation varies, e.g., to provide electric field grading, in accordance with an additive manufacturing process e.g., as described herein, are schematically illustrated, wherein the length of the conductive layers 52 along the axis of rotation varies, e.g., to provide electric field grading, in accordance with an
- FIG. 6B illustrates an example of the length of the conductive layers 52 along the horizontal axis 40 being varied, e.g., so that the radially innermost conductive layer has a greater length than each succeeding next outer conductive layer 52.
- FIGS. 7 A and 7B some aspects of a non-limiting example of an article 12 formed using an additive manufacturing process e.g., as described herein, are schematically illustrated, wherein the shape of article 12 is not a body of revolution, in accordance with an embodiment of the present invention.
- FIGS. 8A and 8B some aspects of a non-limiting example of an article 12 formed using an additive manufacturing process e.g., as described herein, are schematically illustrated, wherein the shape of article 12 is not a body of revolution, in accordance with an embodiment of the present invention.
- FIGS. 9A-9C schematically illustrate some aspects of a non-limiting example of an article 12 formed using an additive manufacturing process, e.g., as described herein, wherein cured nonconductive segments 58 are separated from each other by air gap 60 in accordance with an embodiment of the present invention.
- Nonconductive segments 58 include extensions 62 that extend from a main body 64 of article 12.
- Main body 64 of the illustrated embodiment is formed of alternating nonconductive layers 50 and conductive layers 52, with a nonconductive layer 50 disposed about the radially outermost conductive layer 52.
- Nonconductive segments 58 and extensions 62 are integral with main body 64 and form a unitary structure with main body 64.
- each extension 62 includes an overhang portion 66 that overhangs the balance of extensions 62.
- Overhang portions 66 are integral with extensions 62 and form a unitary structure therewith. Although supported tangentially or diagonally by the balance of extension 62, there is no direct radial support for each overhang portion 66, i.e. , no structural support that is perpendicular to horizontal axis of rotation 40 and disposed between overhang portions 66 and main body 64. Rather, overhang portions 66 are cantilevered off extensions 62. Nonconductive segments 58 and extensions 62 with overhang portions 66 may form, for example, a weather shed (a bushing shed) for a condenser bushing in some embodiments, or for a bulk-type bushing in other embodiments.
- a weather shed a bushing shed
- FIGS. 10A and 10B some aspects of a non-limiting example of an article 12 formed using an additive manufacturing process, e.g., as described herein, are illustrated in a wherein accordance with an embodiment of the present invention.
- a single continuous conductive layer 52 is formed as a spiral 68.
- spiral 68 may be discontinuous.
- spiral 68 may be formed of a plurality of conductive layers 52 arranged as a discontinuous spiral, which may or may not include circumferential overlap of adjacent conductive layers 52, e.g., depending upon the embodiment.
- Embodiments of the present invention include a method for forming an article of manufacture using additive manufacturing, comprising: (a) rotating an object
- the method further comprises forming the article as a bulk-type bushing.
- the cured liquid formulation layer is a nonconductive layer, further comprising (d) forming a conductive layer over at least part of the nonconductive layer.
- the method further comprises forming the article as a condenser bushing.
- the method further comprises a transfer mechanism removing the object from the bath after achieving the desired cured liquid formulation layer radial thickness; rotating the object about the horizontal axis; and applying the conductive layer over the at least part of the nonconductive layer.
- the conductive layer material is added rotationally downstream of the provision of the energy dose during continuous rotation by the first rotational stage.
- the method further comprises repeating (a), (b) and (c) until a desired radial thickness of a second nonconductive layer is achieved.
- the method further comprises repeating (d), (a), (b) and (c) until a desired number of alternating nonconductive and conductive layers have been achieved.
- the method further comprises varying a length along the horizontal axis of selected conductive layers. In a yet still further refinement, the method further comprises operating a linear stage to maintain a desired degree of submersion of the object in the bath.
- the method further comprises varying a length along the horizontal axis to which the energy dose is applied.
- the method further comprises varying an output of the energy source to achieve a shape of the article that is not a body of revolution.
- the method further comprises forming an overhang on the article.
- the method further comprises repeating (a), (b) and (c) to form a weather shed on the article.
- Embodiments of the present invention include a method for forming a condenser bushing using additive manufacturing, comprising: (a) rotating an object about an axis of revolution using a first rotational stage, (b) applying a photocurable nonconductive liquid formulation sub layer to the object; (c) directing an energy source to provide an energy dose onto the object at a desired rotational location, wherein the energy dose is configured to cure and solidify the sub layer; repeating (a), (b) and (c) until a desired radial thickness of a cured liquid formulation layer is a achieved; (d) forming a
- the method further comprises varying a length along the axis of rotation of selected conductive layers. In another refinement, the method further comprises varying a length along the axis of rotation along which the energy dose is applied.
- the method further comprises varying an output of the energy source to achieve a shape of the article that is not a body of revolution.
- Embodiments of the present invention include an apparatus, comprising: a non- transitory computer readable storage medium readable by a processor and storing program instructions for execution by the processor to: (a) rotate an object continuously about a horizontal axis using a first rotational stage, wherein the object is partially submerged in a bath of energy curable liquid formulation during the rotation; (b) control a rate of rotation of the object to achieve a desired radial thickness of a sub layer of uncured liquid formulation at a desired rotational location on the object; (c) direct an energy source to provide an energy dose onto the object at a desired rotational location, wherein the energy dose is configured to cure and solidify the sub layer; and repeat (a), (b) and (c) until a desired radial thickness of a cured liquid formulation layer is a achieved.
- the cured liquid formulation layer is a nonconductive layer
- the non-transitory computer readable storage medium readable by the processor further stores program instructions for execution by the processor to (d) add a conductive layer over at least part of the nonconductive layer.
- the non-transitory computer readable storage medium readable by the processor further stores program instructions for execution by the processor to: direct a transfer mechanism to remove the object from the bath after achieving the desired cured liquid formulation layer radial thickness; rotate the object about the horizontal axis; and apply the conductive layer over the at least part of the nonconductive layer.
- the non-transitory computer readable storage medium readable by the processor further stores program instructions for execution by the processor to: add the conductive layer material rotationally downstream of the provision of the energy dose during continuous rotation by the first rotational stage.
- the non-transitory computer readable storage medium readable by the processor further stores program instructions for execution by the processor to: repeat (a), (b) and (c) until a desired radial thickness of a second nonconductive layer is achieved.
- the non-transitory computer readable storage medium readable by the processor further stores program instructions for execution by the processor to: repeat (d), (a), (b) and (c) until a desired number of alternating nonconductive and conductive layers have been achieved.
- Embodiments of the present invention include a method for forming a bushing using additive manufacturing, comprising: (a) rotating an object about an axis of revolution using a first rotational stage, (b) applying a photocurable nonconductive liquid formulation sub layer to the object; (c) directing an energy source to provide an energy dose onto the object at a desired rotational location, wherein the energy dose is configured to cure and solidify the sub layer; and repeating (a), (b) and (c) until a desired radial thickness of a cured liquid formulation layer is a achieved, wherein the bushing is a bulk-type bushing.
- Embodiments of the present invention include a bushing, comprising: a conductor; and a photocurable nonconductive formulation disposed about the conductor and operative to insulate the conductor.
- the bushing is a bulk-type bushing.
- the bushing further comprises a conductive layer disposed about the nonconductive layer, wherein the bushing is a condenser bushing.
- the terms“mounted,”“connected,” “supported,” and“coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and“coupled” are not restricted to physical or mechanical connections or couplings.
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Abstract
Description
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Priority Applications (6)
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JP2020554519A JP7043625B2 (en) | 2018-04-06 | 2019-04-01 | Equipment and methods for forming articles |
BR112020017556-0A BR112020017556B1 (en) | 2018-04-06 | 2019-04-01 | METHOD FOR FORMING AN ARTICLE OF MANUFACTURING USING ADDITIVE MANUFACTURING |
EP19781800.8A EP3774327B1 (en) | 2018-04-06 | 2019-04-01 | Apparatus and method for forming an article |
CA3094386A CA3094386C (en) | 2018-04-06 | 2019-04-01 | Apparatus and method for forming an article |
KR1020207028356A KR102366094B1 (en) | 2018-04-06 | 2019-04-01 | Apparatus and method for forming articles |
CN201980022492.5A CN111971169A (en) | 2018-04-06 | 2019-04-01 | Apparatus and method for forming articles |
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US15/946,999 US10937572B2 (en) | 2018-04-06 | 2018-04-06 | Apparatus and method for forming an article |
US15/946,999 | 2018-04-06 |
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US (1) | US10937572B2 (en) |
EP (1) | EP3774327B1 (en) |
JP (1) | JP7043625B2 (en) |
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CN (1) | CN111971169A (en) |
BR (1) | BR112020017556B1 (en) |
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JP6751595B2 (en) * | 2016-06-02 | 2020-09-09 | 株式会社ミマキエンジニアリング | Modeling equipment and modeling method |
CA3136654C (en) * | 2019-04-17 | 2024-04-23 | Origin Laboratories, Inc. | Method for regulating temperature at a resin interface in an additive manufacturing process |
US11376798B2 (en) | 2019-08-02 | 2022-07-05 | Stratasys, Inc. | Method for interlayer feedback control and failure prevention in an additive manufacturing process |
US20230041971A1 (en) * | 2019-12-30 | 2023-02-09 | Hitachi Energy Switzerland Ag | Condenser bushing |
EP3991945A1 (en) * | 2020-10-30 | 2022-05-04 | Fundació Eurecat | 3d printing device and 3d printing method |
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- 2019-04-01 WO PCT/US2019/025110 patent/WO2019195129A1/en active Application Filing
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Publication number | Publication date |
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CA3094386C (en) | 2023-02-21 |
BR112020017556B1 (en) | 2024-02-06 |
EP3774327A4 (en) | 2022-03-30 |
KR102366094B1 (en) | 2022-02-23 |
BR112020017556A2 (en) | 2020-12-22 |
CA3094386A1 (en) | 2019-10-10 |
EP3774327A1 (en) | 2021-02-17 |
CN111971169A (en) | 2020-11-20 |
KR20200128712A (en) | 2020-11-16 |
BR112020017556A8 (en) | 2022-10-18 |
EP3774327B1 (en) | 2023-07-12 |
JP2021520308A (en) | 2021-08-19 |
US10937572B2 (en) | 2021-03-02 |
JP7043625B2 (en) | 2022-03-29 |
US20190311822A1 (en) | 2019-10-10 |
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