US20240316622A1 - Continuous casting process of metal - Google Patents
Continuous casting process of metal Download PDFInfo
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- US20240316622A1 US20240316622A1 US18/736,509 US202418736509A US2024316622A1 US 20240316622 A1 US20240316622 A1 US 20240316622A1 US 202418736509 A US202418736509 A US 202418736509A US 2024316622 A1 US2024316622 A1 US 2024316622A1
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- continuous casting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
- B22D11/11—Treating the molten metal
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
- B22D11/103—Distributing the molten metal, e.g. using runners, floats, distributors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
- B22D11/108—Feeding additives, powders, or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/14—Plants for continuous casting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/16—Controlling or regulating processes or operations
- B22D11/22—Controlling or regulating processes or operations for cooling cast stock or mould
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/50—Pouring-nozzles
- B22D41/58—Pouring-nozzles with gas injecting means
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
Definitions
- the present invention relates to a continuous casting process.
- the invention relates to a continuous casting process, called Hollow Jet Casting, in which powder is injected into a hollow jet of metal.
- the term metal will be understood in the rest of the text as including pure metals or metal alloys.
- the continuous casting of steel is a well-known process. It consists in pouring a liquid metal from a ladle into a tundish intended to regulate the flow and then, after this tundish, in pouring the metal into the upper part of a water-cooled bottomless copper mould undergoing a vertical reciprocating movement.
- the solidified semi finished product is extracted from the lower part of the mould by rollers.
- the liquid steel is introduced into the mould by means of a tubular duct called a nozzle placed between the tundish and the mould.
- a powder can be injected in the center of the hollow jet created by the refractory dome.
- This injection technique is disclosed in the document EP 0 605 379 B1.
- This powder injection aims to create an additional cooling of the liquid steel by the melting of the metallic powder or to modify the composition of the steel during casting by addition of other metallic elements such as ferro-alloys.
- the powder can be transported via a mechanical screw feeder and is fed by gravity in a hole going through the refractory dome. Generally, the hole goes through one of the support arms of the dome intended for securing the dome to the vertical tubular member.
- An object of the present invention is to provide a continuous casting process in which plugging of the powder injection means is avoided and powder can be injected during the full casting sequence.
- the present invention provides a continuous casting process of a steel semi-product comprising a step of casting using a hollow jet nozzle located between a tundish and a continuous casting mould.
- the nozzle includes, in its upper part, a dome for deflecting the liquid metal arriving at the inlet of said nozzle towards the internal wall of the nozzle, thus defining an internal volume with no liquid metal and a simultaneous step of injection of powder through a hole of the dome, said powder having a particle size of 200 ⁇ m or less and said dome including first means to inject said powder without any contact with said dome and second means to avoid sticking or sintering of said powder onto said first means.
- the process may also include the following features:
- the present invention further provides continuous casting equipment as defined above.
- FIG. 1 represents a section view of continuous casting equipment as previously referred as hollow jet nozzle according to the prior art.
- FIG. 2 represents a section view of the dome according to a first embodiment of the invention.
- FIG. 2 also represents a section view A-A of the injection tube.
- FIG. 3 represents a section view of the dome according to a second embodiment of the invention.
- FIG. 4 represents a section view of the dome according to a third embodiment of the invention.
- FIG. 5 represents a section view of the dome according to a fourth embodiment of the invention.
- the present invention relates to a continuous casting process in which a flow of liquid metal is poured from a tundish into a ingot mould through the hollow jet nozzle (HJN).
- a hole is made through the dome 2 of the HJN, and in particular through one of the support arm 7 of the dome 2 , to allow the injection of powder in the melt, as already known from the prior art.
- the metallic powder flowing through the hole is in direct contact with the refractory dome that is at a very high temperature (up to 1200° C.).
- Inventors have discovered that despite the very short contact time between the particles and the refractory material, it is sufficient to gradually stick the particles together and to sinter them.
- a cluster of sintered powder is then formed after some minutes of casting and can lead to the full plugging of the powder injector. For example, an injection hole of 20 mm diameter is fully plugged after about 10 minutes of casting when using an iron powder with a size range between 100 and 180 ⁇ m.
- first means are provided to prevent a direct contact between the dome 2 at high temperature (approximately between 100° and 1300° C.) and the powder during injection.
- Said first means comprise a hollow body 12 , for example, extending inside the hole 6 of the dome 2 , the powder being injected inside the hollow body 12 during casting.
- This hollow body 12 may have any suitable shape as long as it creates a physical barrier between the dome 2 and the powder.
- the hollow body may be a tube with a circular section; it can be made of a refractory material or metal such as low carbon steel.
- the inner diameter of said tube depends on the powder flow rate to be injected and can, for example, range from 8 to 30 mm for a powder flow rate between 1 and 7 kg/min.
- second means are provided for preventing the sticking and sintering of the powder inside the hollow body. They are described in FIGS. 2 to 5 in different embodiments. These second means according to the different embodiments allow reducing the surface temperature of the inner wall of the hollow body 12 and thereby reducing the heating of the powder.
- the second means may be a second device that is a cooling device, for example.
- said hollow body 12 has a double wall 13 cooled by gas.
- the gas inlet and outlet in the double wall 13 are respectively illustrated by dashed arrows in FIG. 2 .
- the external and internal walls can have, for example, a thickness of 2 mm and the thickness of the gas film in the double wall can be of about 1.5 mm.
- the gas can be nitrogen or any other suitable gas and circulates usually in the double wall with a flow rate ranging from 10 to 30 m 3 /h. In a preferred embodiment said gas circulates in closed loop in order to avoid any gas injection inside the nozzle which could disturb the liquid steel flow and the good working of the casting equipment.
- the hollow body 12 can also be wrapped in an insulating layer 14 to create a thermal barrier between the hollow body 12 and the refractory dome 2 .
- the continuous casting equipment can also be provided with means for measuring the temperature and the gas flow rate at the inlet and outlet of the cooling device.
- the powder feeder 11 which is preferably a screw feeder, is disposed above the dome 2 .
- the hollow body 12 has the shape of a bent tube and the powder feeder 11 is partly located into said hollow body 12 inside the dome 2 .
- the hollow body 12 with a shape of the bent tube can also goes through a support arm 7 of the dome 2 and the powder feeder 11 is partly located into said hollow body 12 and goes through said support arm 7 . This configuration allows gaining space to reduce the size of the equipment.
- the hollow body 12 is rotary mounted about the longitudinal axis of the hole.
- the rotation of the hollow body 12 allows creating shear stresses on the particles in order to avoid their possible sintering or sticking on the hollow body 12 and to obtain a cooling of the hollow body 12 by the heat exchange between this latter and the powder.
- the hollow body 12 as illustrated in FIG. 4 , is a double wall hollow body as previously described, but in another embodiment, not illustrated, it could be a single tube without gas circulation. As in the previous embodiments, said hollow body 12 can be isolated from the refractory dome 2 by an insulating layer 14 .
- the hollow body 12 is mounted in such a way that it may vibrate in the hole.
- the vibration applied to the hollow body 12 allows avoiding the formation of powder clusters inside the hollow body.
- the vibration can be generated by a mechanical vibrator, by ultrasounds or by other adequate means 15 creating high frequency vibrations, between 50 and 500 HZ.
- the hollow body 12 can also be wrapped with an insulating layer 14 to reduce the inner surface temperature of the hollow body 12 .
- the powder feeder 11 is located above the dome 2 but in another embodiment, not illustrated, it could be located into the hollow body 12 having a shape of a bent tube.
- the insulating layers can be made up of ceramic fibers which are resistant to high temperatures, such as 1300° C.
- the powder used for injection can be of any type, i.e. metallic or ceramic, or a mixture of different powder types.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Continuous Casting (AREA)
- Powder Metallurgy (AREA)
- Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
- Control And Other Processes For Unpacking Of Materials (AREA)
- Auxiliary Devices For And Details Of Packaging Control (AREA)
- Electric Connection Of Electric Components To Printed Circuits (AREA)
Abstract
A continuous casting process of a steel semi-product is provided. The process includes a step of casting using a hollow jet nozzle located between a tundish and a continuous casting mould. The nozzle includes, in its upper part, a dome for deflecting the liquid metal arriving at the inlet of the nozzle towards the internal wall of the nozzle, defining an internal volume with no liquid metal. A simultaneous step of injecting powder through a hole of the dome occurs. The powder has a particle size of 200 μm or less. The dome includes a first device to inject the powder without any contact with the dome and a second device to avoid sticking or sintering of the powder onto the first device.
Description
- The present invention relates to a continuous casting process. In particular, the invention relates to a continuous casting process, called Hollow Jet Casting, in which powder is injected into a hollow jet of metal. The term metal will be understood in the rest of the text as including pure metals or metal alloys.
- The continuous casting of steel is a well-known process. It consists in pouring a liquid metal from a ladle into a tundish intended to regulate the flow and then, after this tundish, in pouring the metal into the upper part of a water-cooled bottomless copper mould undergoing a vertical reciprocating movement. The solidified semi finished product is extracted from the lower part of the mould by rollers. The liquid steel is introduced into the mould by means of a tubular duct called a nozzle placed between the tundish and the mould.
- Document EP 0 269 180 B1 describes a specific continuous casting process called “Hollow Jet Casting” in which the liquid metal is poured onto the top of a dome made of a refractory material. The shape of this dome causes the metal to flow towards its periphery, the flow being deflected towards the internal wall of the nozzle or of an intermediate vertical tubular member. Said intermediate vertical tubular member can be a
copper tube 3 cooled by awater jacket 4 as illustrated inFIG. 1 and topped by arefractory ring 5. What is thus created, in the central part of the nozzle beneath the tundish member, is a volume without any liquid metal within which it is possible to carry out additions via an injection channel. The device thus described is referred to as a “Hollow Jet Nozzle (HJN)”. - A powder can be injected in the center of the hollow jet created by the refractory dome. This injection technique is disclosed in the document EP 0 605 379 B1. This powder injection aims to create an additional cooling of the liquid steel by the melting of the metallic powder or to modify the composition of the steel during casting by addition of other metallic elements such as ferro-alloys. As disclosed in
document EP 2 099 576 B1, the powder can be transported via a mechanical screw feeder and is fed by gravity in a hole going through the refractory dome. Generally, the hole goes through one of the support arms of the dome intended for securing the dome to the vertical tubular member. - However problems occur when powder with a size range of 200 μm or less is injected. Indeed after a short time injection means are plugged and injection cannot be longer performed.
- An object of the present invention is to provide a continuous casting process in which plugging of the powder injection means is avoided and powder can be injected during the full casting sequence.
- The present invention provides a continuous casting process of a steel semi-product comprising a step of casting using a hollow jet nozzle located between a tundish and a continuous casting mould. The nozzle includes, in its upper part, a dome for deflecting the liquid metal arriving at the inlet of said nozzle towards the internal wall of the nozzle, thus defining an internal volume with no liquid metal and a simultaneous step of injection of powder through a hole of the dome, said powder having a particle size of 200 μm or less and said dome including first means to inject said powder without any contact with said dome and second means to avoid sticking or sintering of said powder onto said first means.
- In further preferred embodiments, taken alone or in combination, the process may also include the following features:
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- said first means comprise a hollow body;
- said hollow body comprises a double wall in which gas is circulating;
- said gas is nitrogen;
- a powder feeder is partly disposed in the hollow body;
- the powder feeder goes through a support arm of the dome;
- said second means comprise means for rotating the hollow body about its longitudinal axis;
- said second means comprise means for vibrating the hollow body inside the hole;
- said means for vibrating the hollow body comprise a mechanical vibrator or an ultrasound vibrator;
- an insulating layer is disposed inside the hole between the dome and the hollow body to create a thermal barrier;
- said insulating layer comprises ceramic fibers;
- said hollow body is a tube with a circular section;
- the inner diameter of said tube ranges from 8 to 30 mm.
- The present invention further provides continuous casting equipment as defined above.
- Other features and advantages of the invention will become apparent on reading the following detailed description given solely by way of non-limiting example, with reference to the appended figures in which:
-
FIG. 1 represents a section view of continuous casting equipment as previously referred as hollow jet nozzle according to the prior art. -
FIG. 2 represents a section view of the dome according to a first embodiment of the invention.FIG. 2 also represents a section view A-A of the injection tube. -
FIG. 3 represents a section view of the dome according to a second embodiment of the invention. -
FIG. 4 represents a section view of the dome according to a third embodiment of the invention. -
FIG. 5 represents a section view of the dome according to a fourth embodiment of the invention. -
- (1) Tundish
- (2) Refractory dome
- (3) Copper tube
- (4) Water cooling jacket
- (5) Refractory ring
- (6) Hole
- (7) Support arm
- (8) Submerged entry nozzle
- (9) Mould
- (10) Powder container
- (11) Powder feeder
- (12) Hollow body
- (13) Double wall
- (14) Insulating layer
- (15) Vibration means
- The present invention relates to a continuous casting process in which a flow of liquid metal is poured from a tundish into a ingot mould through the hollow jet nozzle (HJN). A hole is made through the
dome 2 of the HJN, and in particular through one of thesupport arm 7 of thedome 2, to allow the injection of powder in the melt, as already known from the prior art. - During the injection, the metallic powder flowing through the hole is in direct contact with the refractory dome that is at a very high temperature (up to 1200° C.). Inventors have discovered that despite the very short contact time between the particles and the refractory material, it is sufficient to gradually stick the particles together and to sinter them. A cluster of sintered powder is then formed after some minutes of casting and can lead to the full plugging of the powder injector. For example, an injection hole of 20 mm diameter is fully plugged after about 10 minutes of casting when using an iron powder with a size range between 100 and 180 μm.
- With particles of a powder having a size of 200 μm or more, the problem does not occur, as particles do not stick together in the lapse of time during which they are in direct contact with the refractory dome.
- According to the invention, first means are provided to prevent a direct contact between the
dome 2 at high temperature (approximately between 100° and 1300° C.) and the powder during injection. Said first means comprise ahollow body 12, for example, extending inside thehole 6 of thedome 2, the powder being injected inside thehollow body 12 during casting. Thishollow body 12 may have any suitable shape as long as it creates a physical barrier between thedome 2 and the powder. For example, as illustrated inFIGS. 2 to 5 for different embodiments of the invention, the hollow body may be a tube with a circular section; it can be made of a refractory material or metal such as low carbon steel. The inner diameter of said tube depends on the powder flow rate to be injected and can, for example, range from 8 to 30 mm for a powder flow rate between 1 and 7 kg/min. - In addition to said first means, second means are provided for preventing the sticking and sintering of the powder inside the hollow body. They are described in
FIGS. 2 to 5 in different embodiments. These second means according to the different embodiments allow reducing the surface temperature of the inner wall of thehollow body 12 and thereby reducing the heating of the powder. The second means may be a second device that is a cooling device, for example. - In a first embodiment of the present invention as illustrated in
FIG. 2 , saidhollow body 12 has adouble wall 13 cooled by gas. The gas inlet and outlet in thedouble wall 13 are respectively illustrated by dashed arrows inFIG. 2 . The external and internal walls can have, for example, a thickness of 2 mm and the thickness of the gas film in the double wall can be of about 1.5 mm. The gas can be nitrogen or any other suitable gas and circulates usually in the double wall with a flow rate ranging from 10 to 30 m3/h. In a preferred embodiment said gas circulates in closed loop in order to avoid any gas injection inside the nozzle which could disturb the liquid steel flow and the good working of the casting equipment. In addition to this gas cooling, thehollow body 12 can also be wrapped in an insulatinglayer 14 to create a thermal barrier between thehollow body 12 and therefractory dome 2. The continuous casting equipment can also be provided with means for measuring the temperature and the gas flow rate at the inlet and outlet of the cooling device. - In
FIG. 2 , thepowder feeder 11, which is preferably a screw feeder, is disposed above thedome 2. In another embodiment thehollow body 12 has the shape of a bent tube and thepowder feeder 11 is partly located into saidhollow body 12 inside thedome 2. As illustrated inFIG. 3 thehollow body 12 with a shape of the bent tube can also goes through asupport arm 7 of thedome 2 and thepowder feeder 11 is partly located into saidhollow body 12 and goes through saidsupport arm 7. This configuration allows gaining space to reduce the size of the equipment. - Trials performed with casting equipment according to this first embodiment of the present invention and with injection of powder having particles size ranging between 100 and 200 μm, for example, have shown a drastic improvement of the duration of the injection without any plugging problem.
- In another embodiment of the invention as illustrated in
FIG. 4 , thehollow body 12 is rotary mounted about the longitudinal axis of the hole. The rotation of thehollow body 12 allows creating shear stresses on the particles in order to avoid their possible sintering or sticking on thehollow body 12 and to obtain a cooling of thehollow body 12 by the heat exchange between this latter and the powder. Thehollow body 12, as illustrated inFIG. 4 , is a double wall hollow body as previously described, but in another embodiment, not illustrated, it could be a single tube without gas circulation. As in the previous embodiments, saidhollow body 12 can be isolated from therefractory dome 2 by an insulatinglayer 14. - In another embodiment of the invention as illustrated in
FIG. 5 , thehollow body 12 is mounted in such a way that it may vibrate in the hole. The vibration applied to thehollow body 12 allows avoiding the formation of powder clusters inside the hollow body. The vibration can be generated by a mechanical vibrator, by ultrasounds or by other adequate means 15 creating high frequency vibrations, between 50 and 500 HZ. Thehollow body 12 can also be wrapped with an insulatinglayer 14 to reduce the inner surface temperature of thehollow body 12. - In this embodiment the
powder feeder 11 is located above thedome 2 but in another embodiment, not illustrated, it could be located into thehollow body 12 having a shape of a bent tube. - For all embodiments, the insulating layers can be made up of ceramic fibers which are resistant to high temperatures, such as 1300° C.
- The powder used for injection can be of any type, i.e. metallic or ceramic, or a mixture of different powder types.
Claims (20)
1. A continuous casting process of a steel semi-product comprising:
casting, using a hollow jet nozzle located between a tundish and a continuous casting mould, the nozzle including, in an upper part, a dome for deflecting liquid metal arriving at an inlet of the nozzle towards an internal wall of the nozzle, thereby defining an internal volume with no liquid metal; and
injecting, simultaneously, powder through a hole of the dome, the powder having a particle size of 200 μm or less, the dome including a first device to inject the powder without any contact with the dome, the first device including a hollow body, and a second device to apply mechanical stresses to the powder particles in contact with the hollow body.
2. The continuous casting process according to claim 1 , wherein the hollow body is rotated about a longitudinal axis.
3. The continuous casting process according to claim 1 , wherein the second device vibrates the hollow body inside the hole.
4. The continuous casting process according to claim 3 , wherein the second device includes a mechanical vibrator or an ultrasound vibrator.
5. The continuous casting process according to claim 3 , wherein the second device vibrates the hollow body inside the hole at a frequency between 50 and 500 HZ.
6. The continuous casting process according to claim 1 , wherein the second device includes an insulating layer disposed inside the hole between the dome and the hollow body to create a thermal barrier, the first device being surrounded by the insulating layer.
7. The continuous casting process according to claim 6 , wherein the insulating layer includes ceramic fibers.
8. The continuous casting process according to claim 6 , wherein the insulating layer extends at least over a length of the hole, the length being taken along a longitudinal axis of the hole
9. The continuous casting process according to claim 1 , wherein the hollow body is a tube with a circular section.
10. The continuous casting process according to claim 9 , wherein an inner diameter of the tube ranges from 8 to 30 mm.
11. The continuous casting process according to claim 1 , wherein a powder feeder is partly disposed in the hollow body.
12. The continuous casting process according to claim 11 , wherein the powder feeder goes through a support arm of the dome.
13. The continuous casting process according to claim 1 , wherein said hollow body comprises a double wall, and the process comprises, during the injecting, circulating a cooling gas inside the double wall via an inlet on an end of the double wall and exhausting the cooling gas from the double wall via an outlet on said end of the double wall.
14. The continuous casting process according to claim 13 , wherein the double wall further comprises an outer wall and an inner wall, the powder being in contact with an internal surface of the inner wall during the injecting.
15. The continuous casting process according to claim 14 , wherein an external surface of the inner wall and an internal surface of the outer wall define a gas input channel and a gas outlet channel, the gas circulating in the gas input channel in a first direction and the gas circulating in the gas outlet channel in a second direction opposite to the first direction.
16. The continuous casting process according to claim 15 , wherein the gas circulating in the gas input channel is in contact with the external surface of the inner wall and with the internal surface of the outer wall, and the gas circulating in the gas outlet channel is in contact with the external surface of the inner wall and with the internal surface of the outer wall.
17. The continuous casting process according to claim 15 , further comprising a plurality of transverse walls extending radially from the inner wall to the outer wall.
18. The continuous casting process according to claim 14 , wherein the outer wall of the double wall is made of one material and has an external surface, the external surface of the outer wall being arranged away from an inner surface of the hole of the dome, the external surface of the outer wall and the inner surface of the hole of the dome delimiting between them a space.
19. The continuous casting process according to claim 13 , wherein the cooling gas circulates in the double wall with a flow rate ranging from 10 to 30 m3/h.
20. The continuous casting process according to claim 13 , wherein the inlet and the outlet of the double wall are arranged out of the dome.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US18/736,509 US20240316622A1 (en) | 2012-03-28 | 2024-06-06 | Continuous casting process of metal |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/IB2012/000628 WO2013144668A1 (en) | 2012-03-28 | 2012-03-28 | Continuous casting process of metal |
| US201514385046A | 2015-01-23 | 2015-01-23 | |
| US18/736,509 US20240316622A1 (en) | 2012-03-28 | 2024-06-06 | Continuous casting process of metal |
Related Parent Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/IB2012/000628 Division WO2013144668A1 (en) | 2012-03-28 | 2012-03-28 | Continuous casting process of metal |
| US14/385,046 Division US12157165B2 (en) | 2012-03-28 | 2012-03-28 | Continuous casting process of metal |
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| US20240316622A1 true US20240316622A1 (en) | 2024-09-26 |
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| US14/385,046 Active 2033-07-07 US12157165B2 (en) | 2012-03-28 | 2012-03-28 | Continuous casting process of metal |
| US18/736,509 Pending US20240316622A1 (en) | 2012-03-28 | 2024-06-06 | Continuous casting process of metal |
| US18/748,604 Pending US20240335873A1 (en) | 2012-03-28 | 2024-06-20 | Continuous casting process of metal |
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|---|---|
| US (3) | US12157165B2 (en) |
| EP (1) | EP2830792B1 (en) |
| JP (1) | JP5893796B2 (en) |
| KR (2) | KR20160125529A (en) |
| CN (1) | CN104220190B (en) |
| AU (1) | AU2012375161C1 (en) |
| BR (1) | BR112014023711B1 (en) |
| CA (2) | CA2868147C (en) |
| ES (1) | ES2727252T3 (en) |
| HU (1) | HUE043371T2 (en) |
| IN (1) | IN2014DN08195A (en) |
| MX (1) | MX361679B (en) |
| PL (1) | PL2830792T3 (en) |
| RU (1) | RU2608253C2 (en) |
| UA (1) | UA110573C2 (en) |
| WO (1) | WO2013144668A1 (en) |
| ZA (1) | ZA201406486B (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| DE102015116517A1 (en) * | 2015-09-29 | 2017-03-30 | Thyssenkrupp Ag | Apparatus and method for the continuous production of a band-shaped metallic workpiece |
| CN111451462B (en) * | 2020-04-09 | 2021-09-28 | 苏州大学 | Method for refining solidification structure of continuous casting billet by utilizing submerged nozzle to spray magnesium powder |
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| JPS49333Y1 (en) * | 1970-09-18 | 1974-01-08 | ||
| SU416149A1 (en) | 1971-09-21 | 1974-02-25 | ||
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| GB2096032A (en) * | 1981-04-07 | 1982-10-13 | Mitsubishi Steel Mfg | Continuously casting lead-containing steel |
| SU986588A1 (en) | 1981-04-13 | 1983-01-07 | Всесоюзный Научно-Исследовательский Институт Литейного Машиностроения,Литейной Технологии И Автоматизации Литейного Производства "Вниилитмаш" | Apparatus for modifying liquid metal |
| US4520861A (en) * | 1983-11-18 | 1985-06-04 | Republic Steel Corporation | Method and apparatus for alloying continuously cast steel products |
| DE3508618A1 (en) * | 1985-03-29 | 1986-09-18 | Vasipari Kutató és Fejlesztö Vállalat, Budapest | BLOWING TREATMENT FOR TREATING METAL MELT IN MILL PLANTS |
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| KR200166037Y1 (en) | 1999-07-28 | 2000-02-15 | 한국중공업주식회사 | Device for preventing reoxidation of molten steel in bottom-pouring ingot |
| EP1452252A1 (en) | 2003-02-28 | 2004-09-01 | Hubert Dipl.-Ing. Sommerhofer | Continuous casting method |
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| KR100749026B1 (en) * | 2006-06-23 | 2007-08-13 | 주식회사 포스코 | Continuous casting apparatus using melt mold flux |
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| EP2047926A1 (en) * | 2007-10-10 | 2009-04-15 | Ugine & Alz France | Method of manufacturing stainless steels comprising fine carbonitrides, and product obtained from this method |
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| AU2012375161C1 (en) | 2016-11-24 |
| JP2015514585A (en) | 2015-05-21 |
| WO2013144668A1 (en) | 2013-10-03 |
| HUE043371T2 (en) | 2019-08-28 |
| KR20160125529A (en) | 2016-10-31 |
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| MX2014011705A (en) | 2014-12-08 |
| EP2830792B1 (en) | 2019-02-20 |
| ZA201406486B (en) | 2016-07-27 |
| CA2868147A1 (en) | 2013-10-03 |
| US20150158078A1 (en) | 2015-06-11 |
| CA2999637C (en) | 2020-07-07 |
| PL2830792T3 (en) | 2019-08-30 |
| CA2868147C (en) | 2018-05-29 |
| EP2830792A1 (en) | 2015-02-04 |
| RU2014143201A (en) | 2016-05-20 |
| RU2608253C2 (en) | 2017-01-17 |
| AU2012375161A1 (en) | 2014-10-02 |
| KR20140129321A (en) | 2014-11-06 |
| BR112014023711B1 (en) | 2019-06-11 |
| AU2012375161B2 (en) | 2016-07-14 |
| IN2014DN08195A (en) | 2015-05-01 |
| CN104220190B (en) | 2018-08-28 |
| CN104220190A (en) | 2014-12-17 |
| US20240335873A1 (en) | 2024-10-10 |
| MX361679B (en) | 2018-12-13 |
| WO2013144668A9 (en) | 2013-12-12 |
| JP5893796B2 (en) | 2016-03-23 |
| CA2999637A1 (en) | 2013-10-03 |
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