LANCE NOZZLE, METHOD FOR MANUFACTURING LANCE NOZZLE AND APPARATUS FOR MANUFACTURING LANCE NOZZLE
20170051370 ยท 2017-02-23
Assignee
Inventors
Cpc classification
B21J7/00
PERFORMING OPERATIONS; TRANSPORTING
F27D2003/169
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21K21/08
PERFORMING OPERATIONS; TRANSPORTING
F27D3/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22D25/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
F27D3/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21K21/08
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Provided is a method and an apparatus for manufacturing a lance nozzle comprising: a casting step for primarily manufacturing the lance nozzle comprising a plurality of discharge pipes, which discharge a gas supplied through an inlet to an outlet, and a front wall with a plurality of discharge holes, each of which is connected to the outlet of the discharge pipe; and a forging step for forming forging structure by forging a circumference of the discharge holes in a front surface of the front wall positioned on an opposite side to the discharge pipes.
Claims
1. A method for manufacturing a lance nozzle comprising: a casting step for primarily manufacturing the lance nozzle comprising a plurality of discharge pipes, which discharge a gas supplied through an inlet to an outlet, and a front wall with a plurality of discharge holes, each of which is connected to the outlet of the discharge pipe; and a forging step for forming forging structure by forging a circumference of the discharge holes in a front surface of the front wall positioned on an opposite side to the discharge pipes.
2. The method of claim 1, wherein in the casting step, a closing member is formed in the inside of the discharge pipe and parts other than a front portion of the discharge pipe are closed by the closing member, and in the forging step, a forging process is made in a state of forming the closing member.
3. The method of claim 2, further comprising: an opening step of opening the discharge pipe by eliminating the closing member, after the forging step.
4. The method of claim 1, further comprising: after the casting step and before the forging step, a rough machining step for rough machining the front surface of the lance nozzle.
5. The method of claim 4, further comprising: after the forging step, a finish machining step for eliminating a stair gap between the forging structure and portions other than the forging structure of the front surface via finish machining.
6. The method of claim 5, wherein a height of the forging structure is lower than a height of the front surface before the finish machining step.
7. The method of claim 1, wherein the forging step comprises forming the forging structure using a hammer with an external diameter larger than a diameter of the discharge holes.
8. An apparatus for manufacturing a lance comprising a plurality of discharge pipes, which discharge a gas supplied through an inlet to an outlet, and a front wall with a plurality of discharge holes, each of which is connected to the outlet of the discharge pipe, the apparatus comprising: a bed, on which the lance nozzle is installed and which supports the lance nozzle so that the front surface of the lance nozzle is towards an upper portion in keeping a horizontal state; a hammer installed on the bed and having an external diameter larger than a diameter of the discharge hole; and a hammer driving member for driving the hammer and forging a circumference of the discharge hole of the front surface.
9. The apparatus of claim 8, wherein the bed supports the lance nozzle in a state of being inserted into the inside of the front wall and have the same shape as the inside of the front wall.
10. The apparatus of claim 8, further comprising: a guide tip protruded from the lower surface of the hammer and having an external diameter smaller than a diameter of the discharge hole, the guide tip being positioned in the discharge hole when the lower surface of the hammer contacts with the front surface.
11. A lance nozzle comprising: a plurality of discharge pipes, which discharge a gas supplied through an inlet to an outlet; and a front wall with a plurality of discharge holes, each of which is connected to the outlet of the discharge pipe, wherein the front wall has forging structure and casting structure, and the forging structure is positioned on a circumference of the discharge hole and has a predetermined depth.
12. A method for manufacturing a lance nozzle comprising: a casting step for primarily manufacturing the lance nozzle via a casting process; and a forging step for forming forging structure by forging a circumference of discharge holes in a front surface of an outside front wall positioned on an opposite side to discharge pipes, using a lower surface of a hammer having an external diameter larger than a diameter of the discharge hole, wherein the lance nozzle comprises: an inside front wall forming a plurality of openings; a central pipe, a front end of which is closed by the inside front wall; an internal pipe coaxially arranged around of the central pipe, a cooling fluid is fed to an internal ring-shaped cavity formed between the internal pipe and the central pipe; an external pipe arranged coaxially around of the central pipe, the cooling fluid from the internal ring-shaped cavity is discharged to an external ring-shaped cavity formed between the internal pipe and the external pipe; the outside front wall positioned in the front of the central pipe with a plurality of discharge holes arranged in a row of the openings and closing the front end of the external pipe; a plurality of discharge pipes connected to the openings and the discharge holes and discharging gas supplied via the opening to the discharge holes.
13. The method of claim 12, wherein in the casting step, a closing member is formed in the inside of the discharge pipe and parts other than a front portion of the discharge pipe are closed by the closing member, and in the forging step, a forging process is made in a state of forming the closing member.
14. The method of claim 13, further comprising: an opening step of opening the discharge pipes by eliminating the closing member after the forging step.
Description
DESCRIPTION OF DRAWINGS
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
BEST MODE
[0029] Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to
[0030]
[0031] An internal pipe 5 is arranged around the central pipe 2 coaxially to the central pipe 2 and a ring-shaped cavity 6 is formed between the internal pipe 5 and the central pipe 2 so that the cooling fluid is fed in a direction of an arrow F.sub.1.
[0032] An external pipe 10 is arranged around the central pipe 2 coaxially to the central pipe 2 and a ring-shaped cavity 11 is formed between the internal pipe 5 and the external pipe 10 so that the cooling fluid is discharged to a direction of an arrow F.sub.2. The external pipe 10 is closed by a front wall 12, which faces a converter to be stirred and is subjected to threshold thermal stress. The cooling fluid flows a thermal exchange space 13 formed between the front wall 3 and the front wall 12 (F.sub.1, F.sub.3). The front wall 12 may preferably be manufactured by thermal conductive materials having a high heat transfer coefficient such as cupper to provide sufficient thermal exchange between the cooling fluid and the heated front wall 12. That is, the cooling fluid flowed from the cavity 6 bypasses discharge pipes 15 and flows into the thermal exchange space 13 via a passage 8 (F.sub.4), and flows towards the cavity 11 in a direction of the arrow F.sub.1.
[0033] In addition, the front wall 12 has discharge holes 14 arranged in a row of the openings 4 formed on the front wall 3, and the discharge pipes 15 are connected to the openings 4 and the discharge holes 14 so as to discharge the stirring gas (for example, oxygen) to the outside of the lance nozzle 1. The discharge pipes 15 inclines towards the outside to the front on a basis of the axis 19 and a front surface of the lance nozzle 1 is substantially perpendicular to central axes of the discharge pipes 15. Therefore, the front surface of the front wall 12 has a shape, which inclines towards the outside to the lower side on a basis of the axis 19. Also, the front wall 12 has a sink part 16 in the center, which is concave towards the passage 8, and a cooling fluid exhaust nozzle 9 is formed between the discharge pipes 15 and the internal pipe 5.
[0034]
[0035] First, the lance nozzle 1 may be manufactured as one unit via casting or be manufactured as two or more units and then be connected by welding. The casting has an advantage, which can mass-produce things having the same shape and the same size because the casting makes the same things by pouring a liquid into a mold. Particularly, the casting has an advantage, which can save the processing costs because it can easily manufacture products having a complicated shape.
[0036] Then, the lance nozzle 1 goes through rough machining and has surplus portion C (a thickness=about 10 mm) before finish machining in a state of completing the rough machining as illustrated in
[0037] At this time, a closing member 15a is formed in the inside of the discharge pipe 15 via the casting process and closes a portion of the inside of the discharge pipe 15. In the forging process, the closing member 15a prevents the discharge hole 14 or the discharge pipe 15 from deformation (for example, increasing a diameter). That is, in the forging process of the lance nozzle, only a portion of the front terminal of the discharge pipe 15 is partially hollowed and a portion of the inside of the discharge pipe 15 is closed. After the forging process is completed, the discharge pipe 15 is completely formed by eliminating the closing member 15a and thus opening the discharge pipe 15 as illustrated in
[0038] A guide tip 24 is protruded from the lower surface of the hammer 22 and has an external diameter smaller than the diameter of the discharge hole 14 after the forging process is completed. The guide tip 24 may have a trapezoidal shaped cross-section, the upper diameter of which is larger than the lower diameter. When the hammer 22 contacts with the front surface 12a, the guide tip 24 is inserted into the discharge hole 13 and guides the hammer 22 so as to accurately apply the compressive load to the circumference of the discharge hole 14.
[0039] As illustrated in
[0040] According to this embodiment of the present invention, both the advantage of the casting process and the advantage of the forging process can be utilized and at the same time, the disadvantage of the casting process can be compensated by the forging process while the disadvantage of the forging process can be compensated by the casting process. That is, the casting process is a process of melting metal and cooling/freezing the metal to the required shape and thus has the disadvantage that mechanical properties of the casting metal is inferior to the product made by the other process with the same materials because the structure of the casting metal has rough crystalline structure often referred to as a cast structure. Consequently, in a case of the lance nozzle 1 as described the above, there is a problem that the terminal side of the discharge pipes 15 (or the surroundings of the discharge holes 14) erupting the stirring gas is easily worn or damaged.
[0041] On the other hand, the forging process can improve the mechanical properties such as strength because it applies the compressive load or impact load to the material so as to densifying the metal structure compared with the casting process. Therefore, the forging process can extend the lance nozzle's lifetime but has a problem that a lot of time and costs is spent on the manufacturing.
[0042] Consequently, the present invention reduces the time and costs on the manufacturing by manufacturing primarily the lance nozzle via the casting process and at the same time, reinforces the terminal side of the discharge pipes 15 (or the surroundings of the discharge holes 14) easily worn or damaged by improving the mechanical properties via the forging process.
[0043]
[0044]
[0045]
TABLE-US-00001 TABLE 1 Wear test condition test standard ASTM G99, pin-on-disk sliding wear test pin, counterpart Al.sub.2O.sub.3 alumina ball disk, specimen applied load 100 N sliding speed 0.1 m/s sliding distance 100 m Temperature room temperature humidity 34%
[0046] As a result, as illustrated in
[0047]
[0048] The apparatus for manufacturing the lance nozzle 1 further comprises a support frame 29 and the support frame 29 is maintained in a fixed state. A support rod 26 is installed through the support frame 29 and the hammer 22 is fixed to the lower end of the support rod 26. The support rod 26 is operated by a separate driving device (not shown) and on the operation, the hammer 22 carries out the forging process by applying the compressive load (or the impact load) on the front surface of lance nozzle 1.
[0049] Specifically, the lance nozzle 1 is fixed on the bed so that the front surface 12a of the lance nozzle 1 is towards the upper portion and a torch heats the lance nozzle 1 up to the appropriate temperature for the forging process (for example, 500-750 C.). Thereafter, the bed 36 is moved to a body 30 and the position of the bed 36 is adjusted so that the discharge hole 14 of the lance nozzle 1 to be forged is positioned just below the hammer 22. If the position adjustment of the bed 36 is completed, the driving device (for example, a driving cylinder) is operated so as to carry out the forging process on the circumference of the discharge hole 14 using the hammer 22. And then, if the forging process is completed, the bed 36 is moved in the opposite direction of the body 36 and the lance nozzle 1 is removed from the bed 36.
[0050] Although the present invention is described in detail with reference to the exemplary embodiments, the invention may be embodied in many different forms. Thus, technical idea and scope of claims set forth below are not limited to the preferred embodiments.