AU2011203288B2 - Rotary hearth furnace - Google Patents

Rotary hearth furnace Download PDF

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AU2011203288B2
AU2011203288B2 AU2011203288A AU2011203288A AU2011203288B2 AU 2011203288 B2 AU2011203288 B2 AU 2011203288B2 AU 2011203288 A AU2011203288 A AU 2011203288A AU 2011203288 A AU2011203288 A AU 2011203288A AU 2011203288 B2 AU2011203288 B2 AU 2011203288B2
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circumference side
hearth
inner circumference
refractory
side corner
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AU2011203288A1 (en
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Sumito Hashimoto
Hiroshi Sugitatsu
Masahiko Tetsumoto
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Kobe Steel Ltd
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Kobe Steel Ltd
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Abstract

PROBLEM TO BE SOLVED: To provide a rotary hearth furnace which has a simple furnace structure in which the 5 furnace is not damaged even if the furnace is operated for a long term while presenting general equations capable of adequately determining a thermal expansion margin in the rotary hearth furnace. SOLUTION: Between the corner refractory of the outer 10 circumference side or the inner circumference side and the refractory, or between the refractories, a radius direction thermal expansion margin X defined by the following equation 2 is set, and if a width of the outer circumference side corner refractory 7 is given as A and a height of the hearth 15 curb casting 11 of the corner refractory 7 is given as B, the following equation 1 is satisfied: X + A < 4 (A2 + B2) : Equation 1 X = ([XO =] a distance between an outer end part of an outer circumference side hearth curb casting 11 and an inner 20 end part of an inner circumference side hearth curb casting 12 at an operation temperature) - ([X1 =) a total of lengths of a plurality of refractories 6 and corner refractories 7 and 8 in a radius direction at a room temperature) Equation 2

Description

I AUSTRALIA Patents Act 1990 KABUSHIKI KAISHA KOBE SEIKO SHO COMPLETE SPECIFICATION STANDARD PATENT Invention Title: Rotary hearth furnace The following statement is a full description of this invention including the best method of performing it known to us:- - 2 ROTARY HEARTH FURNACE Technical Field The present invention relates to a rotary hearth 5 furnace, and more particularly, relates to a rotary hearth furnace capable of preventing a furnace refractory from falling down by reducing effect due to thermal expansion of a furnace material. This application is a divisional application of 10 Australian Patent Application No. 2006300385 which is a national phase application from International Application No. PCT/JP2006/320176 filed 10 October 2006 which claims priority to and benefit of Japanese Patent Application No. 2005-296746, filed 11 October 2005. The full disclosures of 15 these applications is incorporated herein by reference. Background Art A rotary hearth furnace includes an outer circumference wall, an inner circumference wall, and a rotary hearth which 20 is arranged between the walls. The rotary hearth includes an annular hearth frame, a hearth heat insulating material which is arranged on the hearth frame, and a refractory which is arranged on the hearth heat insulating material. Such a rotary hearth is rotated by a driving mechanism. 25 With respect to the driving mechanism, for example, there are a gear mechanism in which a pinion gear driven by a rotary shaft provided to a lower part of the furnace engages with a rack rail which is circumferentially fixed to a bottom part of the hearth frame, and a mechanism in which a 30 plurality of drive wheels provided to the bottom part of the hearth frame drive on a track which is circumferentially -3 provided on a floor. The rotary hearth furnace which has such a structure is used for metal heating process of a steel billet and the like or combustion process of flammable waste, for example. 5 In recent years, methods of producing reduced iron from iron oxide by using the rotary hearth furnace have attracted notice. Hereinafter, with reference to a schematic view illustrating a known rotary hearth furnace illustrated in 10 Fig. 5, an example of reduced iron production process by the rotary hearth furnace will be described. (1) Powdered iron oxide (iron ore, electric furnace dust, etc.) and powdered carbonaceous reducing agents (coal, cokes, etc.) are mixed and palletized to form green pellets. 15 (2) The green pellets are heated up to such a temperature area that combustible volatile components generated from the pellets may not ignite to remove contained moisture to obtain dry pellets (raw material 29). (3) The dry pellets (raw material 29) are supplied 20 into a rotary hearth furnace 26 using a suitable charging unit 23. Then, a pellet layer which has a thickness of about one to two pellets is formed on a rotary hearth 21. (4) The pellet layer is radiant heated for reduction by combustion of a burner 27 installed to an upper part of 25 the inside of the furnace to metalize.
- 4 (5) The metalized pellets are cooled by a cooler 28. The cooling is performed, for example, by directly spraying gas on the pellets or indirectly cooling by a cooling water jacket. By cooling the pellets, mechanical strength 5 endurable for handling at a time of discharge and after the discharge is obtained. Then, the cooled pellets are discharged by a discharge unit 22. (6) After the metalized pellets (reduced iron 30) are discharged, the dry pellets (raw material 29) are 10 immediately charged and by repeating the above process, reduced iron is produced. The rotary hearth furnace has a lower part heat insulation structure that is composed of an annular hearth frame, a heat insulation material layer which is arranged on 15 the hearth frame, and a refractory layer which is arranged on the heat insulation material layer. To an outer circumference side and an inner circumference side of the rotary hearth, an outer circumference side corner refractory and an inner circumference side corner refractory are 20 arranged through hearth curb castings respectively. At a time of operation of the rotary hearth furnace, to an upper part of the lower part heat insulation structure which is surrounded by the outer circumference side and the inner circumference side corner refractories of the rotary 25 hearth, surface materials such as a mixture of dolomite, -5 iron ore, iron oxide (iron ore, electric furnace dust, etc.), carbonaceous reducing agents (coal, cokes, etc), or a material to be processed are charged and reduction process is performed. 5 Accordingly, due to the difference among these materials which constitute the rotary hearth, interference among the lower part heat insulation structure, the corner refractories, and the surface materials becomes complicated, and in some cases, the corner refractories or the lower part 10 heat insulation structure may be damaged. Especially, although there is no problem on the surface material during construction of the rotary hearth furnace before the rotary hearth furnace is operated, once the rotary hearth furnace is operated and continuously used for 15 a long period, the dolomite and the iron ore accumulates, solidifies, and becomes unified. The unified dolomite and iron ore often circularly solidifies at a furnace outer circumference part and sometimes the solidified material is formed all over the furnace. If the rotary hearth furnace 20 is cooled after the furnace surface is unified as described above, the refractories and the heat insulating materials are contracted and this causes gaps or cracks. To the layer of the dolomite and the iron ore which is to be a surface layer, it is not possible to intentionally 25 provide an expansion margin, and thus, cracks at points - 6 where the cracks most likely to occur and contracts by itself. If the surface layer is heated up again, the surface layer does not always return to the state before the cooling, there are many parts affected by external force due 5 to thermal expansion. The external force due to the thermal expansion acts not only in a circumferential direction, but acts in a radius direction. On the other hand, the hearth frame is structured to contract, however, when heated again, as a matter of course, 10 because the hearth frame is heated up from an upper part, during nonsteady temperature increase to a steady state in the furnace temperature, a phenomenon that only members in the upper part expand occurs. By the phenomenon, the corner refractory provided at an end part of the inner 15 circumference side or the outer circumference side of the rotary hearth is pushed, and may fall to the outside of the furnace, may be floated, or a fixing metallic material may be damaged. Known examples in which the above-described problems have been improved are described with reference to 20 Figs. 6 and 7. Fig. 6 is a fragmentary plane view illustrating a hearth structure of a known rotary hearth furnace. In the hearth structure, an annular rotary hearth 52 is arranged between an inner circumference wall and an outer 25 circumference wall, and an intermediate part of the rotary - 7 hearth 52 in an inner-outer direction is constituted of a refractory castable layer 55. On at least one of the inner circumference side or the outer circumference side of the refractory castable layer 55, a plurality of rows of 5 refractory bricks 73 and 74 are adjacently arranged in the inner-outer direction to form predetermined gaps 57 and 58 between the rows of refractory bricks 73 and 74. Moreover, a rotary hearth furnace according to another known example is described with reference to fragmentary 10 schematic view 7 illustrating a cross section of the rotary hearth furnace. The rotary hearth furnace includes a hearth central body 35 which has a rotatable hearth frame 32, a heat insulating brick 33 which is arranged on the hearth frame 32, and a castable refractory 34 which is arranged on 15 the heat insulating brick 33. The rotary hearth furnace is constituted of refractories, and includes a hearth inner outer circumference position determination part 37 which is arranged on the hearth frame 32. In the rotary hearth furnace, to an inner-outer 20 circumference part of the heat insulating brick 33 of the hearth central body 35, a step part 38 is formed using the same heat insulating brick and an expansion margin 39 is provided between the heat insulating brick which forms the step part 38 and the castable refractory 34 which is 25 arranged inside of the step part 38. The expansion margin - 8 39 is provided in a size of 25 mm or more, preferably, 30 mm. To the hearth inner-outer circumference position determination part 37, a castable refractory 40 is provided. To an outer circumference of the castable refractory 40, an 5 L-shaped metallic material 41 which is fixed to the hearth frame 32 is arranged. On the castable refractory 40, a position determination refractory 42 which is formed by layering an inorganic fiber heat insulating material is provided. The position determination refractory 42 is fixed 10 to the castable refractory 40. However, in the conventional rotary hearth furnace described with reference to Fig. 6, there is no specific description how much the size of the gaps 57 and 58 formed as the thermal expansion margins should be. 15 On the other hand, in the known example described with reference to Fig. 7, the specific size of the expansion margin 39 is described. However, the size of the expansion margin 39 is the size compensated according to the calculation if the width of the castable refractory 34 is 20 2825 mm, it is not possible to apply the known example to a case in which a size of a furnace or a material constituting the furnace is different. Accordingly, the known example cannot be a guiding technique which shows how to determine the expansion margin. Further, in any of the above 25 described known examples, there is a problem that the -9 furnace structures are too complicated and therefore, the construction is difficult and the costs increase. In the rotary hearth furnace, at a time of heating, the temperature increases to 500 CO or more, and in some 5 cases, increases to 600 C* or more. Then, by external force due to thermal expansion which acts on the corner refractories, force in a lateral direction acts on the corner refractory hearth curb castings which supports the corner refractories. Accordingly, it is necessary to use 10 expensive alloy, for example, alloy corresponding to ASTM HH, for the corner refractory hearth curb castings. However, there is a problem that the alloy is short in the life. Any discussion of documents, acts, materials, devices, 15 articles or the like which has been included in the present specification is not to be taken as an admission that any or all of these matters form part of the prior art base or were common general knowledge in the field relevant to the present invention as it existed before the priority date of 20 each claim of this application. Throughout this specification the word "comprise", or - 10 variations such as "comprises" or "comprising", will be understood to imply the inclusion of a stated element, integer or step, or group of elements, integers or steps, but not the exclusion of any other element, integer or step, 5 or group of elements, integers or steps. Disclosure of Invention In consideration of the above, the inventors have diligently studied about expansion/contraction process of 10 the hearth structure of the rotary hearth furnace. As a result, the inventors found that by modifying the structure of the corner refractory, it is possible to prevent damage of the hearth, to prevent the corner refractory from falling to the outside the hearth, or being floated, and 15 made the present invention. According to the present invention, there is provided a rotary hearth furnace in which a rotary hearth being arranged between an outer circumference wall and an inner circumference wall includes an annular hearth frame, a 20 hearth heat insulating material arranged on the hearth frame, a plurality of refractories arranged on the hearth - 11 heat insulating material, an outer circumference side corner refractory arranged to an outer circumference part of the rotary hearth through a first hearth curb casting, and an inner circumference side corner refractory arranged 5 to an inner circumference part of the rotary hearth through a second hearth curb casting. In the rotary hearth furnace, the inner circumference side corner refractory is divided into a plurality of pieces in the circumferential direction, a circumferential direction thermal expansion margin Y is 10 set between the divided inner circumference side corner refractory pieces, and while the circumferential direction thermal expansion margin Y is defined by the following equation 5: Y = ([a total of] lengths of inner circumference side 15 corner refractories contacting the second hearth curb casting at a contact surface side at an operation temperature) - (a total of lengths of each of divided inner circumference side corner refractories contacting the second hearth curb casting at a contact surface side at a 20 room temperature) : Equation 5, - 12 an inner circumference length Li and an outer circumference length L2 of the one divided inner circumference side corner refractory satisfy the following equation 3: 5 L 2 > Li+ 2y : Equation 3 wherein y = Y/n and n denotes the number of pieces of the divided inner circumference side corner refractory. Brief Description of the Drawings 10 Fig. 1 is a vertical sectional view illustrating a rotary hearth furnace according to an embodiment of the present invention. Fig. 2 is a partially enlarged cross sectional view illustrating an enlarged vicinity of an outer circumference 15 side corner refractory illustrated in Fig. 1. Fig. 3 is a view corresponding to Fig. 2 illustrating a state in a case in which a surface material expands. Fig. 4 is a schematic fragmentary plane view of an inner circumference side corner refractory for explaining a 20 basis of the equation 3. Fig. 5 is a schematic view illustrating a known rotary - 13 hearth furnace. Fig. 6 is a fragmentary plane view illustrating a furnace in a known rotary hearth furnace. Fig. 7 is a fragmentary plane view schematically 5 illustrating a conventional rotary hearth furnace. Best Mode for Carrying Out the Invention Hereinafter, a best mode for carrying out the invention will be described in detail with reference to drawings. 10 Fig. 1 illustrates an embodiment of a rotary hearth furnace according to the present invention. The drawing is a vertical sectional view of a rotary hearth furnace according to the embodiment. A rotary hearth furnace 1 includes an outer circumference wall 2, an inner 15 circumference wall 3, and an annular rotary hearth 10 arranged between the walls. The rotary hearth 10 is rotated by a driving device (not shown). The rotary hearth 10 includes an annular hearth frame 4, a hearth heat insulating material 5 which is arranged on the 20 hearth frame 4, and a plurality of refractories 6 which are arranged on the hearth heat insulating material 5. The hearth heat insulating material 5 and the refractories 6 constitute a lower part heat insulation structure 13. To an outer end part of the rotary hearth 10, an outer 25 circumference side corner refractory 7 is arranged on the - 14 hearth heat insulating material 5 through an outer circumference side hearth curb casting 11. To an inner end part of the rotary hearth 10, an inner circumference side corner refractory 8 is arranged on the hearth heat 5 insulating material 5 through an inner circumference side hearth curb casting 12. A large number of refractories 6 are aligned between the outer circumference side corner refractory 7 and the inner circumference side corner refractory 8 in a radius direction and circumferential 10 direction. The outer circumference side corner refractory 7 and the inner circumference side corner refractory 8 are taller than the refractories 6 respectively and protrude upwardly higher than upper surfaces of the refractories 6. Accordingly, if operation of the rotary hearth furnace 1 is 15 repeated, a surface material 9 such as a material to be processed which is introduced into the rotary hearth furnace 1 accumulates on the refractories 6, and the area between the outer circumference side corner refractory 7 and the inner circumference side corner refractory 8 is covered with 20 the surface material 9. Between the outer circumference side or the inner circumference side corner refractory 7 or 8 and the refractory 6, or between each of the refractories 6, a radius direction thermal expansion margin X is set. 25 Specifically, to at least one or more gap between the outer - 15 circumference side corner refractory 7 and the most outer circumference side refractory 6, between each of the refractories 6 adjacent in the radius direction, and between the inner circumference side corner refractory 8 and the 5 most inner circumference side refractory 6, a thermal expansion margin is set, and the total is set as the radius direction thermal expansion margin X. The radius direction thermal expansion margin X is defined as the following equation 2. 10 X = ([XO =] a distance between an outer end part of an outer circumference side hearth curb casting 11 and an inner end part of an inner circumference side hearth curb casting 12 at an operation temperature) - ([X1 =] a total of lengths of a plurality of refractories 6 and the corner refractories 15 7 and 8 in a radius direction at a room temperature) Equation 2 Wherein "a distance between an outer end part of the outer circumference side hearth curb casting 11 and an inner end part of the inner circumference side hearth curb casting 20 12 at an operation temperature" denotes a distance between an outer end part of the outer circumference side hearth curb casting 11 and an inner end part of the inner circumference side hearth curb casting 12. The outer end part of the outer circumference side hearth curb casting 11 25 is the most outer circumference side part of the hearth curb - 16 casting 11 and the inner end part of the inner circumference side hearth curb casting 12 is the most inner circumference side part of the hearth curb casting 12. Moreover, "a total of lengths of the plurality of refractories 6 and the corner 5 refractories 7 and 8 in a radius direction at a room temperature" denotes a total of lengths of the plurality of refractories 6 (refractory group) aligned in line in the radius direction and the outer circumference side corner refractory 7 and the inner circumference side corner 10 refractory 8 in the radius direction. The radius direction thermal expansion margin X is, if a width of the outer circumference side corner refractory 7 is given as A and a height of the outer circumference side hearth curb casting 11 is given as B, set to satisfy the 15 following equation 1: X + A < 4 (A 2 + B 2 ) Equation 1 The denotation of the equation 1 is described with reference to Figs. 2 and 3. Fig. 2 is a partially enlarged cross sectional view 20 illustrating an enlarged vicinity of the outer circumference side corner refractory 7 illustrated in Fig. 1 and Fig. 3 is a view illustrating a state in which the surface material 9 thermally expands and pushes the outer circumference side corner refractory 7. 25 As illustrated in Figs. 2 and 3, the outer - 17 circumference side corner refractory 7 is placed on the outer circumference side hearth curb casting 11 and can tilt in an outer circumference direction with an upper end part a of the outer end part of the outer circumference side hearth 5 curb casting 11 as a fulcrum. Here, the "tilt" denotes, in the case in which the outer circumference side corner refractory 7 is pushed in the outer circumference direction by thermal expansion of the surface material 9, due to reaction of the outer circumference side hearth curb casting 10 11 fixed on the lower part heat insulation structure 13, the outer circumference side corner refractory 7 tilts with the upper end part a of the outer end part of the outer circumference side hearth curb casting 11 as the fulcrum. Now, as in Fig. 2, a case in which between an outer 15 circumference surface 14 of the most outer side refractory 6 and the outer circumference side corner refractory 7, the radius direction thermal expansion margin X is set is described. The outer circumference side hearth curb casting 11 includes a bottom part Ila on which the outer 20 circumference side corner refractory 7 is placed and an outer wall part llb which upwardly extends from an outer end part of the bottom part lla. If the surface material 9 accumulated on the refractories 6 thermally expands, the outer end part of the surface material 9 pushes the outer 25 circumference side corner refractory 7 to the outside. Then, - 18 the outer circumference side corner refractory 7 tilts with the upper end of the outer wall part lb a as the fulcrum a. Here, a length of a straight line which connects the fulcrum a and an inner end part b in a lower end part of the 5 outer circumference side corner refractory 7 is defined as C. Then, with tilting movement of the outer circumference side corner refractory 7, in order to prevent outer circumference side corner refractory 7 from falling down by the inner end part b comes in contact with the outer circumference surface 10 14 of the refractory 6, the radius direction thermal expansion margin X and the width A of the outer circumference side corner refractory 7 are required to be in a relation to satisfy the following equation 6: X + A < C : Equation 6 15 On the other hand, according to the theorem of three squares, the size C can be calculated according to the following equation 7: C = N (A 2 + B 2 ) : Equation 7 wherein N denotes a square root of the equation in 20 the parentheses. Then, from the equations 6 and 7, the following equation 1 is given: X + A < 4 (A 2 + B 2 ) : Equation 1 To explain simply, as illustrated in Fig. 2, the case 25 in which the radius direction thermal expansion margin X is - 19 set between the outer circumference surface 14 of the most outer circumference side refractory 6 and the outer circumference side corner refractory 7 has been described. However, in an actual furnace structure, the radius 5 direction thermal expansion margin X is, as defined by the equation 2, an accumulation value of gaps formed between the plurality of refractories 6. In this case, even if the outer circumference side corner refractory 7 is pushed and tilted by the thermal 10 expansion of the surface material 9, the inner end part b comes in contact with the outer circumference surface 14 of the refractory 6. Then, the refractory 6 is pushed to the inner circumference side and absorbed by the gaps between the refractories. Accordingly, problems such as the damage 15 of the furnace material or falling down of the outer circumference side corner refractory 7 to the outside of the furnace will not occur. Then, thermal expansion of the rotary hearth 10 in the circumferential direction is described. At the outer 20 circumference side of the rotary hearth 10, effect of the thermal expansion in the circumferential direction is not large, however, at the inner circumference side, because effect of the thermal expansion in the circumferential direction is large, in the rotary hearth furnace 1 according 25 to the embodiment, the rotary hearth furnace 1 is structured - 20 as described below. That is, the inner circumference side corner refractory 8 is divided into a plurality of pieces in the circumferential direction. Between the divided inner 5 circumference side corner refractories 8, a circumferential direction thermal expansion margin Y is set as defined by the following equation 5. In other words, between the divided inner circumference side corner refractories 8, a gap corresponding to the circumferential direction thermal 10 expansion margin Y is set. Y = (a total of lengths of inner circumference side corner refractories between a hearth curb casting at a contact surface side at an operation temperature) - (a total of lengths of each of divided inner circumference side 15 corner refractories between a hearth curb casting at a contact surface side at a room temperature) : Equation 5 Wherein, "a total of lengths of inner circumference side corner refractories between a hearth curb casting at a contact surface side at an operation temperature" 20 corresponds to a length in the circumferential direction of the inner circumference side corner refractory 8 between the hearth curb casting 12 at the contact surface side. Moreover, "a total of lengths of each of divided inner circumference side corner refractories between a hearth curb 25 casting at a contact surface side at a room temperature" - 21 corresponds to a total of lengths of each of divided inner circumference side corner refractories 8 in the circumferential direction of the inner circumference side. Further, the circumferential direction thermal 5 expansion margin Y is set, in a relation between one inner circumference length Ll and one outer circumference length L2 of the inner circumference side corner refractory 8 which is divided in the circumferential direction, to satisfy the following equations 3 and 4: 10 L 2 > Li + 2y : Equation 3 y = Y/n : Equation 4 wherein n denotes the number of pieces of divided inner circumference side corner refractories 8. Fig. 4 is a schematic fragmentary plane view of the 15 inner circumference side corner refractory 8 for explaining a basis of the above equation 3. As clearly understood by the drawing, the equation 4 denotes the gap y between the inner circumference side corner refractories 8 adjacent to each other among the divided inner circumference side corner 20 refractories. The inner circumference length Li and the outer circumference length L2 of the inner circumference side corner refractory 8 are such lengths illustrated in Fig. 4. In a case in which the surface material 9 is heated up 25 and thermally expands, most of external force in the radius - 22 direction due to the thermal expansion acts in the outer circumference direction. However, in the vicinity of the inner circumference side corner refractory 8, on the contrary, most of external force in the radius direction due 5 to the thermal expansion acts in the inner circumference direction. Accordingly, as illustrated in Fig. 4, also in the inner circumference side corner refractory 8, the external force in the arrow direction illustrated in the drawing acts from the outer circumference side. Because the 10 divided inner circumference side corner refractory 8 has a fan-shape, as long as the above equation 3 is satisfied, by contacting with adjacent other the inner circumference side corner refractories 8a and 8b, the movement to the inside in the radius direction is prevented. 15 With respect to the above-described furnace structure of the rotary hearth furnace 1 according to the embodiment, working at a time of operation is described with reference to Figs. 1 to 4. When construction of the furnace structure of the 20 rotary hearth furnace 1 is completed and operation is started, first, thesurface material charged into the rotary hearth 10 is heated up. Then, the surface material 9 thermally expands in the radius direction. By the thermal expansion, the outer circumference side corner refractory 7 25 is pushed to the outer circumference side and tilts as - 23 illustrated in Fig. 3. However, because the inner end part b of the outer circumference side corner refractory 7 comes in contact with the outer circumference surface 14 of the most outside refractory 6, the outer circumference side 5 corner refractory 7 is prevented from falling. On the other hand, the inner circumference side corner refractory 8 is, during warm-up period in the initial stage of operation, pushed to the inner circumference side by the thermal expansion of the surface material 9. However, 10 because the inner circumference side corner refractories 8 is arranged to satisfy the equation 3, in the end, the inner circumference side corner refractory 8 comes in contact with the adjacent inner circumference side corner refractories 8a and 8b and comes in a state being held. After the moment, 15 in the surface material 9, as the temperature increases, the external force due to the thermal expansion in the radius direction acts to the outer circumference side. Accordingly, it is possible to prevent the inner circumference side corner refractory 8 from displacing to the outside of the 20 furnace or falling down. Then, the heat of the heated surface material 9 transmits to the refractory 6 in the lower layer by heat conduction, and if the refractory 6 is heated up, the refractory 6 also thermally expands in the radius direction. 25 Accordingly, the lower part of the outer circumference side - 24 corner refractory 7 is pushed and the tilt of the outer circumference side corner refractory 7 returns to the original and returns to the normal state. By the above-described furnace structure, even if the 5 force to push the inner circumference side corner refractory 8 to the inside in the radius direction acts by the thermal expansion, as long as the circumferential direction thermal expansion margin Y between the divided inner circumference side corner refractories 8 allows, the inner circumference 10 side corner refractories 8 are allowed to move to the inside and if the thermal expansion further proceeds, by the divided inner circumference side corner refractories 8 come in contact with each other, the movement of the inner circumference side corner refractories 8 is prevented. As a 15 result, the external force acts on the inner circumference side hearth curb casting 12 decreases, the life of the inner circumference side hearth curb casting 12, whose life has conventionally been one or two years, is elongated, and there was no problem in a test taken after two year had 20 passed. Further, because the inner circumference side corner refractories 8 contact with adjacent inner circumference side corner refractories 8a and 8b and comes in the state being held from a point after temperature increase, the inner circumference side hearth curb casting 25 12 is used only for a purpose of positioning of the inner - 25 circumference side corner refractories 8, and it is not necessary to form the inner circumference side hearth curb casting 12 by alloy which has high rigidity. As described above, the rotary hearth furnace 1 5 according to the embodiment includes the annular hearth frame 4, the hearth heat insulating material 5 which is arranged on the hearth frame 4, the plurality of refractories 6 which are arranged on the hearth heat insulating material 5, and the corner refractories 7 and 8 10 which are arranged to the outer circumference side and the inner circumference side of the rotary hearth 10 through the hearth curb castings 11 and 12 respectively. Between the corner refractory 7 or 8 of the outer circumference side or the inner circumference side and the refractory 6, or 15 between each of the refractories 6, the radius direction thermal expansion margin X is set. While the radius direction thermal expansion margin X is defined by the equation 2, in the relation between the width A of the outer circumference side corner refractory 7 and the height B of 20 the outer circumference side hearth curb casting 11, the equation 1 is satisfied. Accordingly, with the simple structure, the damage of the furnace is prevented and the outer circumference side corner refractory is prevented from falling to the outside of the furnace or floating due to 25 thermal expansion.
- 26 Further, in the rotary hearth furnace 1 according to the embodiment, while the outer circumference side corner refractory 7 is divided into the plurality of pieces in the circumferential direction, with the upper end part of the 5 outer circumference hearth curb casting 11 as the fulcrum a, the outer circumference side corner refractory 7 can tilt in the outer circumference direction. Accordingly, even if the outer circumference side corner refractory 7 tilts to the outside due to the thermal expansion of the surface material 10 9, the outer circumference side corner refractory 7 comes in contact with the refractory 6 of the inside, and prevented from further tilting. Thus, it is prevented that the outer circumference side corner refractory 7 falls down or the hearth curb casting 11 which supports the outer 15 circumference side corner refractory 7 is damaged. Moreover, in the rotary hearth furnace 1 according to the embodiment, the inner circumference side corner refractory 8 is divided into the plurality of pieces in the circumferential direction and the circumferential direction 20 thermal expansion margin Y is set between the divided inner circumference side corner refractories and in the relation between the inner circumference length Ll and the outer circumference length L2 of the inner circumference side corner refractory 8, the equations 3 and 4 are satisfied. 25 Accordingly, due to the thermal expansion of the surface - 27 material 9, even if the inner circumference side corner refractory 8 receives force from the surface material 9, by inner circumference side corner refractories contact with each other, it is possible to prevent the inner 5 circumference side corner refractories 8 and the inner circumference side hearth curb casting 12 from falling to the outside of the furnace or being damaged. That is, in the embodiment, while the radius direction thermal expansion margin X which satisfies the equation 1 is 10 set, in the inner circumference side of the rotary hearth 10, the circumferential direction thermal expansion margin Y which satisfies the equation 4 is set to the inner circumference side corner refractories, when the surface material 9 thermally expands, while further thermal 15 expansion to the inner circumference side is prevented by the adjacent inner circumference corner refractories come in contact with each other, by the thermal expansion of the surface material 9 to the outer circumference side due to the thermal expansion, even if the outer circumference side 20 corner refractory 7 tilts, by coming in contact with the refractories 6, the inner circumference side corner refractory 7 is prevented from falling down. In the embodiment, in the rotary hearth 10, while the radius direction thermal expansion margin X is set, in the 25 inner circumference side, the circumferential direction - 28 thermal expansion margin Y is set, however, the present invention is not limited to the structure. For example, in a case in which the surface material 9 of the outer circumference side of the rotary hearth furnace 10 is 5 especially easily heated, etc., while the radius direction thermal expansion margin X is set, the circumferential direction thermal expansion margin Y may not be set in the inner circumference side. Alternatively, for example, in a case in which the surface material 9 of the inner 10 circumference side is especially easily heated, etc., while the circumferential direction thermal expansion margin Y is set in the inner circumference side, the radius direction thermal expansion margin X may not be set. Hereinafter, features of the embodiment are described 15 below. (1) Between the corner refractory of the outer circumference side or the inner circumference side and the refractory, or between each of the refractories, the radius direction thermal expansion margin X is set. While the 20 radius direction thermal expansion margin X is defined by the equation 2, in the relation between the width A of the outer circumference side corner refractory and the height B of the outer circumference side hearth curb casting, the equation 1 is satisfied. Accordingly, the damage of the 25 furnace is prevented and the outer circumference side corner - 29 refractory is prevented from falling to the outside of the furnace or floating due to thermal expansion. (2) While the outer circumference side corner refractory is divided into the plurality of pieces in the 5 circumferential direction, with the upper end part in the outer end part of the hearth curb casting of the outer circumference side corner refractory as the fulcrum, the outer circumference side corner refractory can tilt in the outer circumference direction. Accordingly, even if the 10 outer circumference side corner refractory tilts to the outside due to the thermal expansion of the surface material, the outer circumference side corner refractory comes in contact with the refractory of the inside, and prevented from further tilting. Thus, it is prevented that the outer 15 circumference side corner refractory falls down or the hearth curb casting which supports the outer circumference side corner refractory is damaged. (3) While the inner circumference side corner refractory is divided into the plurality of pieces in the 20 circumferential direction and the circumferential direction thermal expansion margin Y is set between the divided inner circumference side corner refractories. While the circumferential direction thermal expansion margin Y is defined by the following equation 5, the inner circumference 25 length Ll and the outer circumference length L2 of the one - 30 divided inner circumference side corner refractory satisfy the following equation 3:
L
2 > Li + 2y : Equation 3 wherein y = Y/n and n denotes the number of pieces of 5 divided inner circumference side corner refractories. Y = ([a total of] lengths of inner circumference side corner refractories between a hearth curb casting at a contact surface side at an operation temperature) - (a total of lengths of each of divided inner circumference side 10 corner refractories between a hearth curb casting at a contact surface side at a room temperature) : Equation 5 Accordingly, due to the thermal expansion of the surface material, even if the inner circumference side corner refractory receives force from the surface material, 15 by inner circumference side corner refractories contact with each other, it is possible to prevent the inner circumference side corner refractories and the inner circumference side hearth curb casting from falling to the outside of the furnace or being damaged. 20 Industrial Applicability The present invention is applicable to a rotary hearth furnace in which a rotary hearth which is arranged between an outer circumference wall and an inner circumference wall 25 includes an annular hearth frame, a hearth heat insulating - 31 material arranged on the hearth frame, a plurality of refractories arranged on the hearth heat insulating material, an outer circumference side corner refractory arranged to an outer circumference part of the rotary hearth through a 5 hearth curb casting, and an inner circumference side corner refractory arranged to an inner circumference part of the rotary hearth through a hearth curb casting.

Claims (2)

1. A rotary hearth furnace in which a rotary hearth being arranged between an outer circumference wall and an inner circumference wall includes an annular hearth frame, a hearth 5 heat insulating material arranged on the hearth frame, a plurality of refractories arranged on the hearth heat insulating material, an outer circumference side corner refractory arranged to an outer circumference part of the rotary hearth through a first hearth curb casting, and an 10 inner circumference side corner refractory arranged to an inner circumference part of the rotary hearth through a second hearth curb casting; wherein the inner circumference side corner refractory is divided into a plurality of pieces in the circumferential 15 direction, a circumferential direction thermal expansion margin Y is set between the divided inner circumference side corner refractory pieces, and while the circumferential direction thermal expansion margin Y is defined by the following equation 5, an inner circumference length Ll and an 20 outer circumference length L2 of the one divided inner circumference side corner refractory satisfy the following equation 3: L
2 > L 1 + 2y : Equation 3 wherein y = Yin and n denotes the number of pieces of the 25 divided inner circumference side corner refractory, Y = ([a total of] lengths of inner circumference side corner refractories contacting the second hearth curb casting at a contact surface side at an operation temperature) - (a total of lengths of each of divided inner circumference side 30 corner refractories contacting the second hearth curb casting at a contact surface side at a room temperature) : Equation 5
AU2011203288A 2005-10-11 2011-07-05 Rotary hearth furnace Ceased AU2011203288B2 (en)

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JP2005-296746 2005-10-11
AU2006300385A AU2006300385B2 (en) 2005-10-11 2006-10-10 Rotary hearth furnace
AU2011203288A AU2011203288B2 (en) 2005-10-11 2011-07-05 Rotary hearth furnace

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AU2011203288B2 true AU2011203288B2 (en) 2012-02-02

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