Copper cooling plate with wear resistant inserts, for a blast furnace

Abstract

A cooling plate for use in a blast furnace is described. The cooling plate contains a copper body having an inner face containing ribs parallel therebetween, having first extremities opposite therebetween and separated by grooves having second extremities opposite therebetween. At least one of these ribs contains at least one housing located between its first extremities and containing at least one insert made of a wear resistant material that increases locally the wear resistance of this rib.

Claims

1. A cooling plate for a blast furnace, said cooling plate comprising a copper body having an inner face having a plurality of parallel ribs separated by grooves, the ribs having first extremities facing laterally away from the copper body, the grooves having second extremities facing laterally away from the copper body, wherein at least one of said ribs includes at least one housing located between said first extremities and including at least one insert made of a wear resistant ceramic that increases locally the wear resistance of said at least one of said ribs, a base of the at least one housing being on a plane vertically spaced apart from a base of the groove.

2. A cooling plate for a blast furnace, said cooling plate comprising a copper body having an inner face having a plurality of parallel ribs separated by grooves, the ribs extending vertically away from the copper body, the ribs having first extremities facing laterally away from the copper body, the grooves having second extremities facing laterally away from the copper body, wherein at least one of said ribs includes at least one housing located between said first extremities and including at least one insert made of a wear resistant material that increases locally the wear resistance of said at least one of said ribs, a base of the at least one housing being on a plane vertically spaced apart from a base of the groove, said at least one housing having a cavity holding said at least one insert.

3. The cooling plate according to claim 2, wherein said insert is a wear-resistant steel or cast iron.

4. The cooling plate according to claim 1, wherein said wear resistant ceramic of said insert is silicon carbide, an extruded silicon carbide or other refractory material with good resistant to spalling and high hardness.

5. The cooling plate according to claim 1, wherein said at least one housing is a slot comprising an insert.

6. The cooling plate according to claim 1, wherein said at least one housing is a threaded hole in which a bolt, defining said at least one insert, is screwed.

7. A cooling plate for a blast furnace, said cooling plate comprising a copper body having an inner face having a plurality of parallel ribs separated by grooves, the ribs having first extremities facing laterally away from the copper body, the grooves having second extremities facing laterally away from the copper body, wherein at least one of said ribs includes at least one housing located between said first extremities and including at least one insert made of a wear resistant material that increases locally the wear resistance of said at least one of said ribs, wherein at least one of said grooves comprises at least a part of a multilayer protrusion extending between said second extremities and comprising at least one layer made of said wear resistant material that increases locally the wear resistance of neighboring ribs.

8. The cooling plate according to claim 7, wherein said multilayer protrusion comprises a first layer made of a material providing a heat shield, and a second layer made of said wear resistant material and set on top of said first layer.

9. The cooling plate according to claim 8, wherein said material of said first layer is chosen from a group consisting of a high conductivity metal copper and a copper alloy.

10. The cooling plate according to claim 8, wherein said multilayer protrusion is associated to a single groove.

11. The cooling plate according to claim 10, wherein said multilayer protrusion further comprises a third layer sandwiched between said first and second layers and made of a material having a hardness intended for increasing hardness of said multilayer protrusion.

12. The cooling plate according to claim 11, wherein said third layer is made of a ceramic.

13. The cooling plate according to claim 8, wherein the first and second layers of said multilayer protrusion are respectively associated to two neighboring grooves.

14. The cooling plate according to claim 13, wherein said first layer of said multilayer protrusion comprises a slot extending between said second extremities and comprising an additional insert made of a material having a hardness intended for increasing hardness of said first layer.

15. The cooling plate according to claim 14, wherein said additional insert is made of a ceramic or of a wear-resistant and/or heat-resistant steel.

16. The cooling plate according to claim 1, wherein said inner face of said copper body comprises ribs having at least two different heights.

17. The cooling plate according to claim 1, wherein said grooves have a dovetail cross-section.

18. The cooling plate according to claim 12, wherein said ceramic comprises SiC or extruded SiC.

19. A blast furnace comprising a cooling plate according to claim 1.

20. The cooling plate according to claim 2 wherein said cavity is a slot holding said at least one insert.

21. The cooling plate according to claim 2, wherein said cavity is a threaded hole in which a bolt, defining said at least one insert, is screwed.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Other characteristics and advantages of the invention will emerge clearly from the description of it that is given below by way of an indication and which is in no way restrictive, with reference to the appended figures in which:

(2) FIG. 1 illustrates schematically, in a perspective view, a part of a first example of an embodiment of a cooling plate according to the present invention,

(3) FIG. 2 illustrates schematically, in a cross section view, a part of a second example of an embodiment of a cooling plate according to the present invention,

(4) FIG. 3 illustrates schematically, in a cross section view, a variant of the cooling plate illustrated in FIG. 2,

(5) FIG. 4 illustrates schematically, in a cross section view, a part of a third example of an embodiment of a cooling plate according to the present invention,

(6) FIG. 5 illustrates schematically, in a cross section view, a part of a fourth example of an embodiment of a cooling plate according to the present invention, and

(7) FIG. 6 illustrates schematically, in a cross section view, a part of a fifth example of an embodiment of a cooling plate according to the present invention.

DETAILED DESCRIPTION

(8) The present invention provides a cooling plate (or stave) 1 that can be used in a blast furnace and presenting an increased wear resistance.

(9) An example of an embodiment of a cooling plate (or stave) 1 according to the present invention is illustrated in FIG. 1. Such a cooling plate (or stave) 1 is intended to be mounted on an inner wall of a blast furnace.

(10) As illustrated, a cooling plate (or stave) 1 according to the present invention comprises a copper body 2 having an inner (or hot) face 3 comprising several ribs 4-j parallel therebetween. These ribs 4-j have two first extremities 6 opposite therebetween and are separated by grooves 5 having two second extremities 7 opposite therebetween. Once the cooling plate 1 is mounted on the blast furnace inner wall, its ribs 4-j and grooves 5 are arranged horizontally. In this case, the copper body 2 comprises an outer face 14 that is opposite to its inner face 3 and fixed to the inner wall blast furnace. So, the inner face 3 is the body face that can be in contact with the very hot material and gas present inside the blast furnace.

(11) For instance, and as illustrated in FIGS. 3 to 6, the grooves 5 may have a dovetail cross-section in order to optimize anchorage of a process generated accretion layer 15 when they do not comprise an optional multilayer protrusion 10 (described below). But, the ribs 4-j and grooves 5 may have other cross-section shapes. Thus, and as illustrated in FIGS. 1 and 2, they may have a rectangular cross-section, for instance.

(12) More, and as illustrated in the non-limiting example of FIG. 1, the inner face 3 of the copper body 2 may comprise ribs 4-j having at least two different heights h1 and h2. This option allows optimizing anchorage of refractory bricks 15. In the example of FIG. 1, first ribs 4-1 (j=1) have a first height h1 and second ribs 4-2 (j=2), defined between first ribs 4-1, have a second height h2 that is smaller than the first height h1. But, as illustrated in the other examples of embodiment of FIGS. 2 to 6, the copper body 2 may comprise ribs 4-1 having the same height.

(13) Still more, and as illustrated in FIGS. 2 and 3, the copper body 2 comprises preferably internal channels 16 in which a cooling fluid flows.

(14) As illustrated in FIGS. 1 to 6, at least one of the ribs 4-j comprises at least one housing 8 located between its first extremities 6 and comprising at least one insert 9 made of a wear resistant material that increases locally the wear resistance of the rib 4-j.

(15) Thanks to the rib inserts 9, the wear resistance of the ribs 4-j can be appreciably increased which allows avoiding an early erosion of their material (i.e. copper or copper alloy).

(16) In the non-limiting example of FIG. 1, only the first ribs 4-1 comprise at least one housing 8 comprising at least one insert 9. This is due to the fact that the second height h2 of the second ribs 4-2 is too small to allow definition of the housing(s) 8.

(17) For instance, the wear resistant material of the insert 9 may be a metal or a ceramic. This wear resistant metal may be, for instance, a steel or cast iron, preferably a refractory grade (for example a heat-resistant casting steel such as GX40CrSi13 in which the chemical composition comprises, the contents being expressed as weight percentages: 0.3%≤C≤0.5%, 1%≤Si≤2.5%, 12≤Cr≤14%, Mn≤1%, Ni≤1%, P≤0.04%, S≤0.03% and Mo≤0.5%) or a wear-resistant steel able to work at high temperatures. The wear resistant ceramic may be, for instance, a silicon carbide (SiC), extruded silicon carbide (higher thermal conductivity) or other refractory material with good resistance to spalling and high hardness.

(18) When at least one rib 4-j comprises at least one housing 8, each housing 8 may be a slot comprising at least one insert 9. This is notably the case in the examples illustrated in FIGS. 1 to 3. It is important to notice that a rib 4-j may comprise only one slot 8 extending between its first extremities 6, possibly from one first extremity 6 to the opposite one (as illustrated), or at least two slots 8 defined between its first extremities 6, preferably along a same axis. Moreover each slot 8 may comprise one or more inserts 9 placed one after the other. Each slot 8 may be defined by machining, for instance by means of a drill bit.

(19) In certain embodiments, each housing 8 may be a threaded hole in which a bolt, defining an insert 9, is screwed. It is important to notice that a rib 4-j may comprise only one threaded hole 8 defined between its first extremities 6, or at least two threaded holes 8 defined between its first extremities 6, preferably along a same axis. Each threaded hole 8 may be defined by machining, for instance by means of a drill bit. Preferably, the holes 8, and therefore the bolts 9, are installed in front of cooling channels 16 to protect the bolts 9 and reduce their number. In this case, bolts 9 are not only well connected with copper (through the threads), but also well cooled.

(20) As illustrated in FIGS. 4 to 6, in addition, at least one of the grooves 5 of the copper body 2 may comprise at least a part of a multilayer protrusion 10 extending between its second extremities 7 and comprising at least one layer 12 made of the wear resistant material that increases locally the wear resistance of the neighboring ribs 4-j.

(21) So, in such an embodiment, one or several ribs 4-j comprise(s) at least one housing 8 located between its/their first extremities 6 and comprising at least one insert 9 made of a wear resistant material, and one or several grooves 5 comprise(s) at least a part of a multilayer protrusion 10 extending between its second extremities 7 and comprising at least one layer 12 made of a wear resistant material.

(22) Thanks to the multilayer protrusions 10 (located into grooves 5), the speed and pressure exerted by the descending burden on the stave are appreciably decreased, which allows avoiding an early erosion of their material (i.e. copper or copper alloy) and of the stave body. In other words, the protrusions allows generating an area of low material movement to minimize wear.

(23) The wear resistant material of each layer 12 is preferably the same as the one of an insert 9. So, it may be a metal or a ceramic as described above for the insert 9.

(24) When at least one groove 5 comprises at least a part of a multilayer protrusion 10, the latter 10 may comprise a first layer 11 made of a material having a high thermal conductivity, and a second layer 12 made of the wear resistant material and set on top of this first layer 11. This is notably the case in the examples illustrated in FIGS. 4 to 6. In contrast to the previous embodiment (illustrated in FIGS. 1 to 3), this embodiment allows an adaptation of a conventional cooling plate without any machining phase.

(25) The first layer 11 having a high thermal conductivity is laid in the lowest position of the multilayer protrusion 10 to act as a heat shield, because the thermal load is coming mainly from hot gas streams flowing upwards. For instance, the material of this first layer 11 may be a high conductivity metal copper or a copper alloy. The second layer 12 is made of the wear resistant material and laid on top of the first layer 11 to protect it from an early erosion. As mentioned before, this second layer 12 can be made of wear-resistant steel, cast iron or ceramic.

(26) Also for instance, and as illustrated in FIGS. 4 and 5, each multilayer protrusion 10 may be associated to a single groove 5. In other word a part of each multilayer protrusion 10 is located into a single groove 5 while the remaining part of this multilayer protrusion 10 extends beyond this single groove 5.

(27) In this case, each multilayer protrusion 10 may further comprise a third layer 13 sandwiched between the first 11 and second 12 layers and made of a ceramic material having a very high hardness intended for increasing the wear resistance of the whole protrusion.

(28) In the example of FIG. 4, each third layer 13 is in contact with a part of the inner face 3 that delimitates the base of its associated groove 5, while in the example of FIG. 5, each third layer 13 is separated by a protruding part of the underlying first layer 11 from the part of the inner face 3 that delimitates the base of its associated groove 5. The alternative shown in FIG. 4 can be installed on the stave from the front side, while the alternative displayed in FIG. 5 can only be installed sideways inside the groove. The advantage of this latter embodiment is the higher stability of the set in case the brittle ceramic piece would be broken in pieces.

(29) For instance, each third layer 13 may be made of a high-hardness ceramic such as SiC or extruded SiC. A ceramic can be used here because it is sandwiched and therefore protected from impact of falling material and independent of the cooling plate bending that can be induced by a thermal expansion.

(30) In a variant of an embodiment illustrated in FIG. 6, the first 11 and second 12 layers of each multilayer protrusion 10 may be respectively associated to two neighboring grooves 5. In other words, a part of the first layer 11 of a multilayer protrusion 10 is located into a first groove 5, while the remaining part of this first layer 11 extends beyond this first groove 5, and a part of the second layer 12 of this multilayer protrusion 10 is located into a second groove 5 located near the first groove 5, while the remaining part of this second layer 12 extends beyond this second groove 5. So, the first layer 11 in the lower part takes the heat load towards the copper body 2, while the second layer 12 on top protects the associated first layer 11 from wear.

(31) In this case, and as illustrated in the non-limiting example of FIG. 6, the first layer 11 of each multilayer protrusion 10 may comprise a slot 17 extending between the second extremities 7 and comprising an additional insert 18. This additional insert 18, embedded in a first layer 11, is made of a material having a hardness intended for increasing hardness of this first layer 11. For instance, and as illustrated in the non-limiting example of FIG. 6, the face of the first layer 11, in which is defined (or machined) the slot 17, may be inclined to send the gas outwards and also to help the burden flow smoothly into the “pockets” that are built with the protrusions 10.

(32) Also for instance, and as illustrated in FIG. 6, each other slot 17, and therefore the associated other insert 18, may have a dovetail cross-section.

(33) Also for instance, each other insert 18 may be made of a ceramic such as SiC or a steel (wear-resistant, heat-resistant of a combination of both). Other implementations to increase the hardness of the layer 11 can be used. For example, each slot 17 may be a threaded hole in which a bolt, defining an insert 18, is screwed.

(34) It is important to note that in an embodiment where the cooling plate 1 comprises also multilayer protrusions 10, the grooves 5 in which these multilayer protrusions 10 are located may depend on the shape and/or dimensions of the blast furnace. For instance, in the example illustrated in FIGS. 4 and 5 a multilayer protrusion 10 may be located every three grooves 5. But, in other embodiments, a multilayer protrusion 10 may be located every two or four or even five grooves 5.

(35) As illustrated in FIGS. 4 to 6, in an embodiment where the cooling plate 1 comprises multilayer protrusions 10, the ribs 4-j delimiting the grooves 5 comprising these multilayer protrusions 10 or embedded into multilayer protrusions 10 do not really need to comprise housing(s) 8 comprising insert(s) 9, because they are already protected by these multilayer protrusions 10. So, preferably only ribs 4-j not located in the vicinity of a multilayer protrusion 10 comprise housing(s) 8 comprising insert(s) 9.