WO2018047444A1 - Roll outer layer material for hot rolling and composite roll for hot rolling - Google Patents
Roll outer layer material for hot rolling and composite roll for hot rolling Download PDFInfo
- Publication number
- WO2018047444A1 WO2018047444A1 PCT/JP2017/023663 JP2017023663W WO2018047444A1 WO 2018047444 A1 WO2018047444 A1 WO 2018047444A1 JP 2017023663 W JP2017023663 W JP 2017023663W WO 2018047444 A1 WO2018047444 A1 WO 2018047444A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- roll
- outer layer
- hot rolling
- rolling
- layer material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B27/00—Rolls, roll alloys or roll fabrication; Lubricating, cooling or heating rolls while in use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/08—Casting in, on, or around objects which form part of the product for building-up linings or coverings, e.g. of anti-frictional metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
- B22D13/02—Centrifugal casting; Casting by using centrifugal force of elongated solid or hollow bodies, e.g. pipes, in moulds rotating around their longitudinal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/16—Casting in, on, or around objects which form part of the product for making compound objects cast of two or more different metals, e.g. for making rolls for rolling mills
-
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
-
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
-
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B27/00—Rolls, roll alloys or roll fabrication; Lubricating, cooling or heating rolls while in use
- B21B27/02—Shape or construction of rolls
- B21B27/03—Sleeved rolls
- B21B27/032—Rolls for sheets or strips
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D5/00—Heat treatments of cast-iron
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/38—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for roll bodies
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C37/00—Cast-iron alloys
Definitions
- the present invention relates to a composite roll for hot rolling, and more particularly to a roll outer layer material for hot rolling and a composite roll for hot rolling suitable for use in a hot rolling finish mill of a steel plate.
- Patent Document 1 discloses that C: 1.5 to 3.5%, Ni: 5.5% or less, Cr: 5.5 to 12.0%, Mo : 2.0 to 8.0%, V: 3.0 to 10.0%, Nb: 0.5 to 7.0%, and Nb and V include Nb, V and C content.
- a rolling roll outer layer material that satisfies a specific relationship and further contains a ratio of Nb and V within a specific range has been proposed. Thereby, even if the centrifugal casting method is applied, segregation of hard carbides in the outer layer material is suppressed, and the outer layer material of the roll for rolling is excellent in wear resistance and crack resistance.
- Patent Document 2 C: 1.5 to 3.5%, Cr: 5.5 to 12.0%, Mo: 2.0 to 8.0%, V: 3.0 to 10.0 %, Nb: 0.5 to 7.0%, and Nb and V, the contents of Nb, V and C satisfy a specific relationship, and the ratio of Nb to V is within a specific range
- a roll outer layer material for rolling containing so as to have been proposed.
- Patent Document 3 discloses that C: 2.2 to 2.6%, Cr: 5.0 to 8.0%, Mo: 4.4 to 6.0%, V: 5 Adjust the C, Mo, V, and Nb contents so that Mo + V and C-0.24V-0.13Nb are within the specified range.
- the present invention has been made in view of the above circumstances, and while ensuring the wear resistance, reducing the pit-like wrinkles on the roll surface, the roll outer layer material for hot rolling and the hot It aims at providing the composite roll for rolling.
- the present inventors investigated in detail the location of the occurrence of pit-like wrinkles formed on the surface of the hot rolling roll.
- the pit-shaped soot is formed by cracks generated from eutectic carbides (mainly M 2 C, M 6 C, M 7 C 3 and M 23 C 6 carbides) propagating through the base structure. It was clarified that the shape was lost. Therefore, in order to reduce pit-like wrinkles, it is considered effective to reduce the propagation speed of cracks propagating through the base structure in addition to focusing on conventional carbide types and sizes. Was completed.
- the casting temperature was 1450 ° C. to 1530 ° C., and the centrifugal force was such that the outer peripheral portion of the ring-shaped roll material had a gravity multiple of 180 G.
- quenching and tempering were performed, and the hardness was HS 78-86.
- the quenching treatment was performed by heating to a heating temperature of 1070 ° C. and air cooling. Further, the tempering treatment was performed twice or three times depending on the components at a temperature of 530 to 570 ° C. so that the amount of retained austenite was less than 10% by volume.
- a hot-rolled fatigue test piece (outer diameter 60 mm ⁇ , wall thickness 10 mm) was taken from the obtained ring-shaped roll material, and the fatigue resistance of the hot rolling work roll in an actual machine was evaluated with good reproducibility in JP 2010-101752.
- a hot rolling fatigue test was conducted to show that it was possible.
- As the fatigue test piece a notch (depth t: 1.2 mm, circumferential length L: 0.8 mm) as shown in FIG. 1 was used at two locations on the outer peripheral surface, and a 0.2 mm ⁇ wire was used. It was introduced by the electric discharge machining (wire cut) method. Further, the end of the rolling surface of the fatigue test piece was chamfered with 1.2C.
- the hot-rolling fatigue test was performed by a two-spindle rolling sliding method of a test piece having a notch (hot-rolling fatigue test piece) and a heated counterpart material. That is, as shown in FIG. 1, a test piece (hot rolled fatigue test piece) 1 was rotated at 700 rpm while being cooled with cooling water 2, and the rotating test piece 1 was heated to 800 ° C. by a high frequency induction heating coil 3. While the mating piece (material: S45C, outer diameter: 190 mm ⁇ , width: 15 mm) 4 was pressed with a load of 980 N, it was rolled at a slip ratio of 9%.
- the structure of the obtained ring-shaped roll material was observed.
- tissue observation a 10 ⁇ 10 ⁇ 5 mm (5 mm is the thickness direction of the ring) tissue observation specimen is taken at an arbitrary position within 10 mm from the outer surface of the ring-shaped roll material, and the 10 ⁇ 10 mm surface is a mirror surface Polishing was performed, and corrosion was performed with nital (5% by volume nitric acid + ethanol) for about 10 seconds.
- a measurement test piece (5 mm ⁇ 10 mm ⁇ 5 mm) at an arbitrary position within 10 mm from the outer surface of the obtained ring-shaped roll material
- the surface of 5 mm ⁇ 10 mm was mirror-polished and EBSD measurement was performed.
- the measurement was performed by electron beam backscatter diffraction (EBSD) in an area of 10000 ⁇ m 2 or more at an acceleration voltage of 15 kV and a step size of 0.1 ⁇ m.
- EBSD electron beam backscatter diffraction
- a boundary line is drawn at a position where the azimuth difference between adjacent measurement points is 15 ° or more, and as shown in FIG. 12, the region surrounded by the boundary line is a single crystal, and the major axis is 5 ⁇ m or more on the measurement surface.
- the minor axis of 20 crystals was measured and the average value was calculated.
- FIG. 3 shows the relationship with + (% Ni)
- FIG. 4 shows the relationship between the hot-rolled fatigue life and the minor axis of tempered martensite or bainite.
- FIG. 3 shows that (% C ⁇ % V ⁇ 0.177 ⁇ % Nb ⁇ 0.129 ⁇ % Cr ⁇ 0.099 ⁇ % Mo ⁇ 0.063 ⁇ % W ⁇ 0.033) + (% Ni) is 0. It can be seen that when it is 0.05 or more or 4.0 or less, the hot-rolled fatigue life is remarkably improved.
- V, Cr, Mo, Nb, and W are elements that are easy to produce carbides.
- (% C-% V ⁇ 0.177-% Nb ⁇ 0.129-% Cr ⁇ 0.099-% Mo ⁇ 0 .063-% W ⁇ 0.033) represents the amount of carbon dissolved in the matrix.
- the present invention has been completed based on the above findings, and the gist thereof is as follows.
- C 2.0 to 3.0%
- Si 0.2 to 1.0%
- Mn 0.2 to 1.0%
- Cr 4.0 to 7.0%
- Mo 3.0 to 6.5%
- V 5.0 to 7.5%
- Nb 0.5 to 3.0%
- Ni 0.05 to 3.0%
- Co 0.2 -5.0%
- W 0.5-5.0%
- the contents of C, Cr, Mo, V, Nb, Ni, W satisfy the following formula (1)
- the balance Fe and It has a composition consisting of inevitable impurities, and 85% or more of the base structure is a tempered martensite and / or bainite structure, and the minor axis of the tempered martensite or bainite is 0.5 to 3.0 ⁇ m.
- Roll outer layer material for hot rolling 0.05 ⁇ (% C ⁇ % V ⁇ 0.177 ⁇ % Nb ⁇ 0.129 ⁇ % Cr ⁇ 0.099 ⁇ % Mo ⁇ 0.063 ⁇ % W ⁇ 0.033) + (% Ni) ⁇ 4 .0 (1)
- % C,% V,% Nb,% Cr,% Mo,% W, and% Ni are the contents (mass%) of each element.
- the present invention it is possible to manufacture a hot rolling roll outer layer material and a hot rolling composite roll in which the propagation speed of cracks is significantly reduced.
- surface damage due to hot rolling such as rough skin and missing edges can be suppressed, and there is an effect that continuous rolling distance can be extended and roll life can be improved.
- FIG. 1 shows the configuration of the testing machine used in the hot rolling fatigue test, the outer periphery of the hot rolling fatigue test specimen (fatigue test specimen), and the hot rolling fatigue test specimen (fatigue specimen) It is explanatory drawing which shows typically the shape and dimension of the notch introduced into the surface.
- FIG. 2 is a diagram showing a result of measuring the outer layer material for hot rolling according to the embodiment of the present invention by EBSD.
- FIG. 3 shows the hot-rolled fatigue life in the hot-rolled fatigue test and (% C-% V ⁇ 0.177-% Nb ⁇ 0.129-% Cr ⁇ 0.099-% Mo ⁇ 0.063-% W ⁇ 0 .033) + (% Ni).
- FIG. 4 is a diagram showing the relationship between the hot-rolled fatigue life in the hot-rolled fatigue test and the minor axis of tempered martensite or bainite.
- the roll outer layer material for hot rolling of the present invention is manufactured by a known casting method such as a centrifugal casting method or a continuous casting overlaying method, and can be used as it is as a ring roll or a sleeve roll, but for hot finish rolling. It is preferably used as an outer layer material of a composite roll for hot rolling.
- the composite roll for hot rolling according to the present invention includes an outer layer and an inner layer welded and integrated with the outer layer.
- An intermediate layer may be disposed between the outer layer and the inner layer. That is, instead of the inner layer welded and integrated with the outer layer, an intermediate layer welded and integrated with the outer layer and an inner layer welded and integrated with the intermediate layer may be used.
- the composition of the inner layer and the intermediate layer is not particularly limited, but the inner layer is spheroidal graphite cast iron (ductile iron) or forged steel, and the intermediate layer is a high carbon material of C: 1.5 to 3.0% by mass. Is preferred.
- C 2.0 to 3.0% C forms a solid solution to increase the base hardness and combines with a carbide forming element to form a hard carbide, thereby improving the wear resistance of the roll outer layer material.
- the amount of eutectic carbide varies depending on the C content. Eutectic carbides affect the rolling service characteristics. For this reason, if the C content is less than 2.0%, the amount of eutectic carbide is insufficient, the frictional force during rolling increases, rolling becomes unstable, and the amount of C dissolved in the base structure is low. Reduces rolling fatigue resistance during heat resistance.
- C is limited to a range of 2.0 to 3.0%.
- the content is 2.1 to 2.8%.
- Si 0.2 to 1.0%
- Si is an element that acts as a deoxidizer and improves the castability of the molten metal.
- a content of 0.2% or more is required.
- Si is limited to 0.2 to 1.0%.
- the content is 0.3 to 0.7%.
- Mn 0.2 to 1.0%
- Mn is an element having the effect of fixing S as MnS and detoxifying S, and partly dissolving in the base structure and improving the hardenability.
- a content of 0.2% or more is required.
- Mn is limited to 0.2 to 1.0%.
- the content is 0.3 to 0.8%.
- Cr 4.0 to 7.0% Cr combines with C to mainly form eutectic carbides, improves wear resistance, reduces friction with the steel sheet during rolling, reduces roll surface damage, and stabilizes rolling. It is an element having In order to obtain such an effect, the content of 4.0% or more is required. On the other hand, if the content exceeds 7.0%, coarse eutectic carbides increase, and fatigue resistance is lowered. For this reason, Cr is limited to the range of 4.0 to 7.0%. Preferably, the content is 4.3 to 6.5%.
- Mo 3.0 to 6.5%
- Mo is an element that combines with C to form a hard carbide and improves wear resistance.
- Mo dissolves in hard MC-type carbides in which V, Nb, and C are bonded, strengthens the carbides, and also dissolves in eutectic carbides to increase the fracture resistance of these carbides. Through such an action, Mo improves the wear resistance and fatigue resistance of the outer roll layer material.
- the content of 3.0% or more is required.
- Mo-based hard and brittle carbides are produced, which reduces the rolling fatigue resistance during heat resistance and lowers the fatigue resistance. For this reason, Mo is limited to the range of 3.0 to 6.5%.
- the content is 3.5 to 6.0%.
- V 5.0-7.5%
- V is an important element in the present invention in order to combine wear resistance and fatigue resistance as a roll.
- V forms extremely hard carbide (MC type carbide), improves wear resistance, and effectively acts to sever and disperse eutectic carbide, thereby improving rolling fatigue resistance during heat resistance. Further, it is an element that remarkably improves fatigue resistance as a roll outer layer material. Such an effect becomes remarkable when the content is 5.0% or more.
- the content exceeds 7.5%, the MC type carbides are coarsened, so that various properties of the rolling roll are made unstable. For this reason, V is limited to the range of 5.0 to 7.5%.
- the content is 5.2 to 7.0%.
- Nb 0.5 to 3.0%
- Nb improves the wear resistance, particularly fatigue resistance, through the action of strengthening the MC type carbide by solid solution in the MC type carbide and increasing the fracture resistance of the MC type carbide.
- Nb and Mo are dissolved in the carbide, the improvement in wear resistance and further fatigue resistance becomes significant.
- Nb is an element which has the effect
- Nb also has the effect of suppressing segregation during centrifugal casting of MC type carbide. Such an effect becomes remarkable when the content is 0.5% or more.
- Nb is limited to a range of 0.5 to 3.0%.
- the content is 0.8 to 1.5%.
- Ni 0.05-3.0%
- Ni is an element that dissolves in the matrix, lowers the transformation temperature of austenite during heat treatment, and improves the hardenability of the matrix. In order to acquire such an effect, 0.05% or more of content is required. On the other hand, if the content exceeds 3.0%, the transformation temperature of austenite becomes too low and the hardenability is improved, so that austenite tends to remain after heat treatment. When austenite remains, the rolling fatigue resistance during hot rolling is reduced, for example, cracks are generated during hot rolling. Therefore, Ni is limited to the range of 0.05 to 3.0%. Even if the cooling rate during the heat treatment is slow, it is preferably 0.2 to 3.0% from the viewpoint of ease of operation that the crystal size of the matrix structure can be made fine.
- Co 0.2-5.0%
- Co is an element that has a function of solid-dissolving in the matrix, strengthening the matrix, particularly at high temperatures, and improving fatigue resistance. In order to obtain such an effect, a content of 0.2% or more is required. On the other hand, even if the content exceeds 5.0%, the effect is saturated and an effect commensurate with the content cannot be expected, which is economically disadvantageous. Therefore, Co is limited to the range of 0.2 to 5.0%. Preferably, it is 0.5 to 3.0%.
- W 0.5-5.0%
- W is an element having a function of solid-dissolving in the matrix, strengthening the matrix at a high temperature and improving fatigue resistance, and forming M 2 C or M 6 C-based carbides, and wear resistance. To improve. In order to acquire such an effect, 0.5% or more of content is required. On the other hand, if the content exceeds 5.0%, not only the effect is saturated, but also coarse M 2 C or M 6 C-based carbides are formed, and the rolling fatigue resistance during heat resistance is reduced. For this reason, W is limited to a range of 0.5 to 5.0%. Preferably, it is 1.0 to 3.5%.
- C, Cr, Mo, V, Nb, Ni, and W are contained in the above-described range, and further adjusted and contained so as to satisfy the following expression (1).
- % C,% V,% Nb,% Cr,% Mo,% W, and% Ni are the contents (mass%) of each element.
- V, Cr, Mo, Nb, and W are elements that are easy to produce carbides.
- (% C-% V ⁇ 0.177-% Nb ⁇ 0.129-% Cr ⁇ 0.099-% Mo ⁇ 0.063- % W ⁇ 0.033) represents the amount of carbon dissolved in the base. Therefore, (% C-% V ⁇ 0.177-% Nb ⁇ 0.129-% Cr ⁇ 0.099-% Mo ⁇ 0.063-% W ⁇ 0.033) + (% Ni) It is the sum of the amount of dissolved carbon and the amount of Ni, and by adjusting this value to an appropriate range, a roll outer layer material having a slow crack propagation speed in the base and an excellent hot-rolled fatigue life can be obtained.
- the balance other than the above components is composed of Fe and inevitable impurities.
- the base structure is tempered martensite and / or bainite structure, and it is preferable that the minor axis of tempered martensite or bainite is 0.5 to 3.0 ⁇ m.
- the base structure contains 85% or more of tempered martensite and / or bainite structure. It is more preferable that it is contained 90% or more from the viewpoint of property.
- a retained austenite and / or pearlite are mentioned.
- it may be controlled by repeating the cooling process after heating and holding at 500 to 570 ° C.
- the minor axis of tempered martensite or bainite in a component system in which the minor axis of tempered martensite or bainite is smaller than 0.5 ⁇ m, the transformation temperature becomes too low, and it becomes difficult to reduce the amount of retained austenite even if tempering is repeated. Cracking during hot rolling due to austenite may occur, and the hot rolling fatigue resistance is reduced.
- the minor axis of tempered martensite or bainite exceeds 3.0 ⁇ m, the crack propagation rate of the base structure is high, and the rolling fatigue resistance during heat resistance decreases. Therefore, it is preferable to limit the minor axis of tempered martensite or bainite of the base structure to a range of 0.5 to 3.0 ⁇ m.
- the thickness is preferably in the range of 0.5 to 2.0 ⁇ m.
- the components and the cooling rate may be controlled so that the transformation temperature of the matrix is in the range of 200 to 400 ° C.
- the roll outer layer material is preferably produced by a known centrifugal casting method or a casting method such as a continuous casting overlay method. Needless to say, the present invention is not limited to these methods.
- a molten mold having the above-described roll outer layer material composition is applied to a rotating mold whose inner surface is coated with a refractory material mainly composed of zircon or the like in a thickness of 1 to 5 mm. It is poured and centrifugally cast so as to have a predetermined thickness.
- the number of rotations of the mold is preferably in the range of 120 to 220 G in the gravity multiple applied to the outer surface of the roll.
- the mold rotation and stand the mold After the outer layer or the intermediate layer is completely solidified, it is preferable to stop the mold rotation and stand the mold, and then statically cast the inner layer material to form a composite roll. Thereby, the inner surface side of the roll outer layer material is redissolved to form a composite roll in which the outer layer and the inner layer, or the outer layer and the intermediate layer, and the intermediate layer and the inner layer are welded and integrated.
- the inner layer it is preferable to use spheroidal graphite cast iron, worm-like graphite cast iron (CV cast iron), etc. excellent in castability and mechanical properties for the inner layer to be statically cast.
- the outer layer and the inner layer are integrally welded, so that the component of the outer layer material is mixed in the inner layer by about 1 to 8%.
- carbide forming elements such as Cr and V contained in the outer layer material are mixed into the inner layer, the inner layer is weakened. For this reason, it is preferable to suppress the mixing rate of the outer layer component into the inner layer to less than 6%.
- the intermediate layer when forming the intermediate layer, it is preferable to use graphite steel, high carbon steel, hypoeutectic cast iron or the like as the intermediate layer material.
- the intermediate layer and the outer layer are integrally welded in the same manner, and the outer layer component is mixed in the intermediate layer in the range of 10 to 95%. From the viewpoint of suppressing the amount of the outer layer component mixed into the inner layer, it is important to reduce the amount of the outer layer component mixed into the intermediate layer as much as possible.
- the composite roll for hot rolling of the present invention is preferably subjected to heat treatment after casting.
- heat treatment it is preferable to perform the step of heating to 950 to 1100 ° C. by air cooling or blast air cooling, and further the step of cooling after heating and holding at 500 to 570 ° C. is performed twice or more.
- the cooling rate in accordance with the components so that the transformation temperature is in the range of 200 to 400 ° C., it is possible to obtain the above-mentioned preferred minor axis size.
- the amount of tempered martensite and / or bainite in the base structure changes depending on the number of repetitions of the cooling step after heating and holding at 500 to 570 ° C., 85% or more of the base structure is tempered martensite and / or Alternatively, the number of repetitions may be set so as to be bainite.
- the preferred hardness of the composite roll for hot rolling of the present invention is 79 to 88 HS (Shore hardness), and more preferred is 80 to 86 HS. If the hardness is lower than 80 HS, the wear resistance is deteriorated. Conversely, if the hardness exceeds 86 HS, cracks formed on the surface of the hot rolling roll during hot rolling are difficult to remove by grinding. It is preferable to adjust the heat treatment temperature and heat treatment time after casting so that such hardness can be stably secured.
- the melt of the roll outer layer material composition shown in Table 1 was melted in a high-frequency induction furnace and made into a ring-shaped test material (ring roll; outer diameter: 250 mm ⁇ , width: 65 mm, wall thickness: 55 mm) by centrifugal casting.
- the casting temperature was 1450 to 1530 ° C., and the centrifugal force was such that the outer peripheral portion of the ring-shaped roll material was 180 G in the multiple of gravity.
- the quenching temperature is reheated to 1070 ° C., air-cooled, and quenching quenching and tempering are performed at a temperature of 530 to 570 ° C. so that the residual austenite amount is less than 10% by volume.
- Vickers hardness HV50 is measured with a Vickers hardness tester (test force: 50 kgf (490 N)) in accordance with the provisions of JIS Z 2244, and Shore hardness HS is calculated with a JIS conversion table. Converted. The measurement points were 10 points each, the maximum value and the minimum value were deleted, the average value was calculated, and the hardness of the test material.
- the hot rolling fatigue test method was as follows. A hot rolling fatigue test piece (outer diameter 60 mm ⁇ , wall thickness 10 mm, chamfered) was collected from the obtained ring-shaped test material. In the hot rolling fatigue test piece, notches (depth t: 1.2 mm, circumferential length L: 0.8 mm) as shown in FIG. 1 are provided at two locations on the outer peripheral surface (positions 180 ° apart). And introduced by an electric discharge machining (wire cut) method using a 0.20 mm ⁇ wire. As shown in FIG. 1, the hot rolling fatigue test was performed by a two-disk sliding rolling method between a test piece and a counterpart material.
- the test piece 1 was rotated at 700 rpm while being cooled with cooling water 2, and the rotating test piece 1 was heated to 800 ° C. with the high frequency induction heating coil 3 (material: S45C, outer diameter: 190 mm ⁇ , width: 15 mm). , C1 chamfer) 4 was brought into contact with a load of 980 N while rolling at a slip ratio of 9%. And it rolled until the two notches 5 introduced into the hot rolling fatigue test piece 1 broke, each rolling rotation speed until each notch broke was calculated
- tissue observation a 10 ⁇ 10 ⁇ 5 mm (5 mm is the thickness direction of the ring) tissue observation specimen is taken at an arbitrary position within 10 mm from the outer surface of the ring-shaped roll material, and the 10 ⁇ 10 mm surface is a mirror surface Polishing was performed, and corrosion was performed with nital (5% by volume nitric acid + ethanol) for about 10 seconds.
- the short diameter (short axis length) of tempered martensite or bainite is obtained by taking an EBSD measurement test piece (5 mm ⁇ 10 mm ⁇ 5 mm) from an arbitrary position within 10 mm from the outer surface of the obtained ring-shaped roll material, A surface of 5 mm ⁇ 10 mm was mirror-polished and determined by EBSD measurement. EBSD measurement was performed in an area of 10000 ⁇ m 2 or more at an acceleration voltage of 15 kV and a step size of 0.1 ⁇ m. Using the obtained data, as shown in FIG.
- a boundary line is drawn at a position where the azimuth difference between adjacent measurement points is 15 ° or more, and the region surrounded by the boundary line is taken as one crystal, and the measurement surface Above, the minor axis of 20 crystals whose major axis is 10 ⁇ m or more was measured, and the average value was calculated.
- the hot-rolled fatigue life was remarkably increased, and an excellent hot-rolled fatigue life exceeding 350,000 times was exhibited.
- the structure observation it was confirmed that 85% or more of the base structure was tempered martensite and / or bainite structure.
- the present invention it is possible to manufacture a composite roll for hot rolling in which the propagation speed of cracks is significantly reduced. As a result, surface damage due to hot rolling such as rough skin and missing edges can be suppressed, so that the effect of extending the continuous rolling distance and improving the roll life can also be obtained.
- Test piece hot rolled fatigue test piece
- Cooling water High frequency induction heating coil 4
- Opposite piece 5 Notch
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Reduction Rolling/Reduction Stand/Operation Of Reduction Machine (AREA)
- Heat Treatment Of Articles (AREA)
Abstract
Description
本発明は、熱間圧延用複合ロールに係り、とくに、鋼板の熱間圧延仕上げミル用として好適な熱間圧延用ロール外層材および熱間圧延用複合ロールに関する。 The present invention relates to a composite roll for hot rolling, and more particularly to a roll outer layer material for hot rolling and a composite roll for hot rolling suitable for use in a hot rolling finish mill of a steel plate.
近年、鋼板の熱間圧延技術の進歩につれてロールの使用環境は苛酷化しており、また、高強度鋼板や薄肉品など圧延負荷の大きな鋼板の生産量も増加している。このため、圧延用ワークロールには圧延面の疲労に起因した肌荒れや欠落ち疵が発生することが多くなり、これまで以上に耐肌荒れ性と耐欠落ち性への要求が強くなっている。現在、熱間圧延では数%量のVを添加することにより硬質炭化物を多量に形成させて、耐摩耗性を向上させたハイス系ロールが多用されている。 In recent years, with the progress of hot rolling technology for steel plates, the usage environment of rolls has become severe, and the production volume of steel plates with high rolling load such as high-strength steel plates and thin-walled products has also increased. For this reason, the work roll for rolling often has rough skin and chipping due to fatigue of the rolling surface, and the demand for rough skin resistance and chipping resistance is stronger than ever. At present, high-speed rolls in which a large amount of hard carbide is formed by adding several percent of V in hot rolling to improve wear resistance are frequently used.
このようなハイス系ロールの外層材として、例えば、特許文献1には、C:1.5~3.5%、Ni:5.5%以下、Cr:5.5~12.0%、Mo:2.0~8.0%、V:3.0~10.0%、Nb:0.5~7.0%を含み、かつ、NbおよびVを、Nb、VおよびCの含有量が特定の関係を満足し、さらにNbとVの比が特定の範囲内となるように含有する圧延用ロール外層材が提案されている。これにより、遠心鋳造法を適用しても外層材における硬質炭化物の偏析が抑制され、耐摩耗性と耐クラック性に優れた圧延用ロール外層材となるとしている。また、特許文献2には、C:1.5~3.5%、Cr:5.5~12.0%、Mo:2.0~8.0%、V:3.0~10.0%、Nb:0.5~7.0%を含み、かつ、NbおよびVを、Nb、VおよびCの含有量が特定の関係を満足し、さらにNbとVの比が特定の範囲内となるように含有する圧延用ロール外層材が提案されている。これにより、遠心鋳造法を適用しても外層材における硬質炭化物の偏析が抑制され、耐摩耗性と耐クラック性が向上し、熱間圧延の生産性向上に大きく貢献するとしている。
As an outer layer material of such a high-speed roll, for example,
一方で、熱間圧延製品の品質向上と生産性向上の観点から、熱間圧延用ロールの使用環境は苛酷化しており、鋼板の連続圧延量が増加している。さらに、熱間圧延製品の表面品質への要求も厳しくなっている。そのため、摩耗よりも肌荒れといったロール表面の疲労損傷を抑制することが大きな課題となってきた。このような課題に対して、特許文献3には、C:2.2~2.6%、Cr:5.0~8.0%、Mo:4.4~6.0%、V:5.3~7.0%、Nb:0.6~1.3%を、Mo+V、C-0.24V-0.13Nbが特定範囲内となるようにC、Mo、V、Nb含有量を調整して、熱間圧延環境下でのロール表層の耐疲労性に優れるとした遠心鋳造製複合ロールが提案されている。また、特許文献4には、C:1.3~2.2%、Si:0.3~1.2%、Mn:0.1~1.5%、Cr:2.0~9.0%、Mo:9.0%以下、V:4.0~15.0%、およびW:20.0%以下、Ni:5.0%以下、Co:10.0%以下のうちいずれか1種または2種以上を含有し残部実質的にFeおよび不可避的不純物からなり、その組織中に分散する炭化物のサイズが特定の範囲内となる圧延用ロール外層材が提案されている。特許文献4では、粗大な炭化物として形成しやすい共晶炭化物量を低減することで、ピット状の疵を軽減することが可能としている。
On the other hand, from the viewpoint of improving the quality and productivity of hot-rolled products, the usage environment of hot-rolling rolls has become severe, and the amount of continuous rolling of steel sheets has increased. Furthermore, the requirements for the surface quality of hot-rolled products are becoming stricter. Therefore, it has become a big subject to suppress fatigue damage on the roll surface such as rough skin rather than wear. For such a problem,
しかしながら、近年の圧延技術は圧延鋼板の高品質化と高級化に向けて目覚しいスピードで進歩を遂げている。同時に、圧延に対し低コスト化も厳しく追及されることから、ロールの使用環境はますます厳しい。このため、従来までの炭化物のみに着目したロール材質の設計では、ピット状の疵の発生を軽減できない場合が出てきた。 However, the rolling technology in recent years has made remarkable progress toward high quality and high quality rolled steel sheets. At the same time, the rolling environment is becoming increasingly severe because of the rigorous pursuit of cost reduction for rolling. For this reason, in the conventional roll material design focusing only on carbides, the occurrence of pit-like wrinkles has sometimes been reduced.
本発明は、上記事情を鑑みてなされたものであり、耐摩耗性を確保するとともに、ロール表面のピット状の疵を軽減させ、耐肌荒れ性に優れた熱間圧延用ロール外層材および熱間圧延用複合ロールを提供することを目的とする。 The present invention has been made in view of the above circumstances, and while ensuring the wear resistance, reducing the pit-like wrinkles on the roll surface, the roll outer layer material for hot rolling and the hot It aims at providing the composite roll for rolling.
本発明者らは、熱間圧延用ロール表面に形成されたピット状の疵の発生箇所を詳細に調査した。その結果、ピット状の疵は、共晶炭化物(主としてM2C系、M6C系、M7C3系およびM23C6系炭化物)から発生したクラックが基地組織を伝播することでピット状に欠け落ちることを明らかにした。そこで、ピット状の疵を軽減するためには、従来までの炭化物種類、サイズに着目することに加えて、基地組織を伝播するクラックの伝播速度を低減させることが有効であると考え、本発明を完成させた。すなわち、ロール外層材の耐熱間転動疲労性と基地組織サイズに影響する各種要因について研究した結果、各元素の成分範囲の調整、および、各元素が特定の関係を満足するように各元素の含有量を調整することにより、熱間圧延時の耐疲労性が著しく向上するという、従来にない知見を得た。さらに、基地組織サイズを制御することにより、より熱間圧延時の耐疲労性が著しく向上するという知見も得た。 The present inventors investigated in detail the location of the occurrence of pit-like wrinkles formed on the surface of the hot rolling roll. As a result, the pit-shaped soot is formed by cracks generated from eutectic carbides (mainly M 2 C, M 6 C, M 7 C 3 and M 23 C 6 carbides) propagating through the base structure. It was clarified that the shape was lost. Therefore, in order to reduce pit-like wrinkles, it is considered effective to reduce the propagation speed of cracks propagating through the base structure in addition to focusing on conventional carbide types and sizes. Was completed. In other words, as a result of studying various factors that affect the rolling fatigue resistance and base structure size of the outer layer material of the roll, adjustment of the component range of each element, and each element to satisfy a specific relationship The present inventors have obtained an unprecedented knowledge that fatigue resistance during hot rolling is remarkably improved by adjusting the content. Furthermore, the knowledge that fatigue resistance at the time of hot rolling is remarkably improved by controlling the size of the base structure was also obtained.
まず、本研究の基礎となった実験結果について説明する。質量%で、Si:0.1~1.5%、Mn:0.1~1.5%とし、C:1.6~3.5%、Cr:3.5~9.0%、Mo:2.1~7.0%、V:4.1~8.5%、Nb:0.3~4.6%、Ni:0.02~3.6%、Co:0.3~8.0%、W:0.2~8.0%の範囲で変化させ、残部Feおよび不可避的不純物からなる組成の溶湯を、高周波誘導炉で溶解し、ロール外層材に相当するリング状ロール材(外径:250mmφ、幅:65mm、肉厚:55mm)を遠心鋳造法により鋳造した。なお、鋳込み温度は1450℃~1530℃とし、遠心力はリング状ロール材の外周部が重力倍数で180Gとなるようにした。鋳造後、焼入れ処理、焼戻処理を施し、硬さをHS 78~86とした。なお、焼入れ処理は、加熱温度:1070℃に加熱し、空冷する処理とした。また、焼戻処理は、温度:530~570℃で、残留オーステナイト量が体積%で10%未満になるように、成分によって2または3回実施した。 First, the experimental results that became the basis of this research will be explained. In mass%, Si: 0.1 to 1.5%, Mn: 0.1 to 1.5%, C: 1.6 to 3.5%, Cr: 3.5 to 9.0%, Mo : 2.1 to 7.0%, V: 4.1 to 8.5%, Nb: 0.3 to 4.6%, Ni: 0.02 to 3.6%, Co: 0.3 to 8 0.0%, W: A ring-shaped roll material corresponding to the roll outer layer material by changing the range of 0.2 to 8.0% and melting the molten metal having the balance Fe and inevitable impurities in a high-frequency induction furnace (Outer diameter: 250 mmφ, width: 65 mm, wall thickness: 55 mm) was cast by a centrifugal casting method. The casting temperature was 1450 ° C. to 1530 ° C., and the centrifugal force was such that the outer peripheral portion of the ring-shaped roll material had a gravity multiple of 180 G. After casting, quenching and tempering were performed, and the hardness was HS 78-86. The quenching treatment was performed by heating to a heating temperature of 1070 ° C. and air cooling. Further, the tempering treatment was performed twice or three times depending on the components at a temperature of 530 to 570 ° C. so that the amount of retained austenite was less than 10% by volume.
得られたリング状ロール材から熱延疲労試験片(外径60mmφ、肉厚10mm)を採取して、特開2010-101752にて実機における熱間圧延用作業ロールの耐疲労性を再現よく評価できることを示した熱延疲労試験を実施した。なお、疲労試験片には、図1に示すようなノッチ(深さt:1.2mm、周方向長さL:0.8mm)を外周面の2箇所に、0.2mmφのワイヤを用いた放電加工(ワイヤカット)法で導入した。また、疲労試験片の転動面の端部には1.2Cの面取りを施した。 A hot-rolled fatigue test piece (outer diameter 60 mmφ, wall thickness 10 mm) was taken from the obtained ring-shaped roll material, and the fatigue resistance of the hot rolling work roll in an actual machine was evaluated with good reproducibility in JP 2010-101752. A hot rolling fatigue test was conducted to show that it was possible. As the fatigue test piece, a notch (depth t: 1.2 mm, circumferential length L: 0.8 mm) as shown in FIG. 1 was used at two locations on the outer peripheral surface, and a 0.2 mmφ wire was used. It was introduced by the electric discharge machining (wire cut) method. Further, the end of the rolling surface of the fatigue test piece was chamfered with 1.2C.
熱延疲労試験は、図1に示すように、ノッチを有する試験片(熱延疲労試験片)と加熱された相手材との2円盤の転がりすべり転動方式で行った。すなわち、図1に示すように試験片(熱延疲労試験片)1を冷却水2で水冷しながら700rpmで回転させ、回転する該試験片1に、高周波誘導加熱コイル3により800℃に加熱した相手片(材質:S45C、外径:190mmφ、幅:15mm)4を荷重980Nで押し当てながら、すべり率:9%で転動させた。熱延疲労試験片1に導入した2つのノッチ5が折損するまで転動させ、各ノッチが折損するまでの転動回転数をそれぞれ求め、その平均値を熱延疲労寿命とした。そして、熱延疲労寿命が350千回を超える場合を熱延疲労寿命が著しく優れると評価した。
As shown in FIG. 1, the hot-rolling fatigue test was performed by a two-spindle rolling sliding method of a test piece having a notch (hot-rolling fatigue test piece) and a heated counterpart material. That is, as shown in FIG. 1, a test piece (hot rolled fatigue test piece) 1 was rotated at 700 rpm while being cooled with cooling water 2, and the rotating
また、得られたリング状ロール材について、組織観察を行った。組織観察は、リング状ロール材の外表面から10mm内部の任意の位置において、10×10×5mm(5mmはリングの肉厚方向)の組織観察試験片を採取し、10×10mmの面を鏡面研磨して、ナイタール(5体積%硝酸+エタノール)で10秒程度腐食し、光学顕微鏡を用いて行った。 The structure of the obtained ring-shaped roll material was observed. For tissue observation, a 10 × 10 × 5 mm (5 mm is the thickness direction of the ring) tissue observation specimen is taken at an arbitrary position within 10 mm from the outer surface of the ring-shaped roll material, and the 10 × 10 mm surface is a mirror surface Polishing was performed, and corrosion was performed with nital (5% by volume nitric acid + ethanol) for about 10 seconds.
また、焼戻しマルテンサイトまたはベイナイトの短径(短軸長さ)を測定するため、得られたリング状ロール材の外表面から10mm内部の任意の位置において、測定試験片(5mm×10mm×5mm)を採取して、5mm×10mmの面を鏡面研磨し、EBSD測定を実施した。加速電圧15kV、ステップサイズ0.1μmで、10000μm2以上の領域の電子線後方散乱回折法(EBSD)により、測定を行った。隣接する測定点との方位差が15°以上の箇所に境界線を引き、図12に示すように、境界線で囲まれた領域を一つの結晶として、測定面上で、長径が5μm以上の20個の結晶の短径を測定し、その平均値を算出した。 Moreover, in order to measure the short diameter (short axis length) of tempered martensite or bainite, a measurement test piece (5 mm × 10 mm × 5 mm) at an arbitrary position within 10 mm from the outer surface of the obtained ring-shaped roll material The surface of 5 mm × 10 mm was mirror-polished and EBSD measurement was performed. The measurement was performed by electron beam backscatter diffraction (EBSD) in an area of 10000 μm 2 or more at an acceleration voltage of 15 kV and a step size of 0.1 μm. A boundary line is drawn at a position where the azimuth difference between adjacent measurement points is 15 ° or more, and as shown in FIG. 12, the region surrounded by the boundary line is a single crystal, and the major axis is 5 μm or more on the measurement surface. The minor axis of 20 crystals was measured and the average value was calculated.
得られた結果について、熱延疲労寿命と(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)との関係を図3に示し、熱延疲労寿命と焼戻しマルテンサイトまたはベイナイトの短径との関係を図4に示す。 Regarding the obtained results, the hot rolling fatigue life and (% C-% V × 0.177-% Nb × 0.129-% Cr × 0.099-% Mo × 0.063-% W × 0.033) FIG. 3 shows the relationship with + (% Ni), and FIG. 4 shows the relationship between the hot-rolled fatigue life and the minor axis of tempered martensite or bainite.
図3から、(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)が0.05以上または4.0以下になると、熱延疲労寿命が著しく向上していることが分かる。ここで、V、Cr、Mo、Nb、Wは炭化物を造りやすい元素であり、(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)は基地に固溶している炭素量を表す。そのため、(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)は基地に固溶している炭素量とNi量の和であり、この値を適正な範囲に調整することで、基地中のクラックの伝播速度が遅い、熱延疲労寿命の優れるロール外層材が得られる。また、上記成分範囲を満足し、且つ基地組織の焼戻しマルテンサイトまたはベイナイトの結晶サイズを図4に示す範囲内に制御することにより、熱延疲労寿命を著しく向上させることが可能となる。 FIG. 3 shows that (% C−% V × 0.177−% Nb × 0.129−% Cr × 0.099−% Mo × 0.063−% W × 0.033) + (% Ni) is 0. It can be seen that when it is 0.05 or more or 4.0 or less, the hot-rolled fatigue life is remarkably improved. Here, V, Cr, Mo, Nb, and W are elements that are easy to produce carbides. (% C-% V × 0.177-% Nb × 0.129-% Cr × 0.099-% Mo × 0 .063-% W × 0.033) represents the amount of carbon dissolved in the matrix. Therefore, (% C-% V × 0.177-% Nb × 0.129-% Cr × 0.099-% Mo × 0.063-% W × 0.033) + (% Ni) It is the sum of the amount of dissolved carbon and the amount of Ni, and by adjusting this value to an appropriate range, a roll outer layer material having a slow crack propagation speed in the base and an excellent hot-rolled fatigue life can be obtained. Further, by satisfying the above component range and controlling the crystal size of the tempered martensite or bainite in the matrix structure within the range shown in FIG. 4, the hot-rolled fatigue life can be remarkably improved.
本発明は上記の知見に基づき完成されたものであり、その要旨は次のとおりである。
[1]質量%で、C:2.0~3.0%、Si:0.2~1.0%、Mn:0.2~1.0%、Cr:4.0~7.0%、Mo:3.0~6.5%、V:5.0~7.5%、Nb:0.5~3.0%、Ni:0.05~3.0%、Co:0.2~5.0%、W:0.5~5.0%を含有し、かつC、Cr、Mo、V、Nb、Ni、Wの含有量が下記(1)式を満足し、残部Feおよび不可避的不純物からなる組成を有し、基地組織の85%以上が焼戻しマルテンサイトおよび/またはベイナイト組織であり、焼戻しマルテンサイトまたはベイナイトの短径は0.5~3.0μmであることを特徴とする熱間圧延用ロール外層材。
0.05≦(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)≦4.0 (1)
ここで、%C、%V、%Nb、%Cr、%Mo、%W、%Niは、各元素の含有量(質量%)である。
[2]外層と内層が溶着一体化してなる熱間圧延用複合ロールであって、前記外層が[1]に記載の熱間圧延用ロール外層材からなることを特徴とする熱間圧延用複合ロール。
The present invention has been completed based on the above findings, and the gist thereof is as follows.
[1] By mass%, C: 2.0 to 3.0%, Si: 0.2 to 1.0%, Mn: 0.2 to 1.0%, Cr: 4.0 to 7.0% , Mo: 3.0 to 6.5%, V: 5.0 to 7.5%, Nb: 0.5 to 3.0%, Ni: 0.05 to 3.0%, Co: 0.2 -5.0%, W: 0.5-5.0%, and the contents of C, Cr, Mo, V, Nb, Ni, W satisfy the following formula (1), and the balance Fe and It has a composition consisting of inevitable impurities, and 85% or more of the base structure is a tempered martensite and / or bainite structure, and the minor axis of the tempered martensite or bainite is 0.5 to 3.0 μm. Roll outer layer material for hot rolling.
0.05 ≦ (% C−% V × 0.177−% Nb × 0.129−% Cr × 0.099−% Mo × 0.063−% W × 0.033) + (% Ni) ≦ 4 .0 (1)
Here,% C,% V,% Nb,% Cr,% Mo,% W, and% Ni are the contents (mass%) of each element.
[2] A hot-rolling composite roll in which an outer layer and an inner layer are welded and integrated, wherein the outer layer is made of the hot-rolling roll outer layer material described in [1]. roll.
本発明によれば、クラックの伝播速度が著しく低減した熱間圧延用ロール外層材および熱間圧延用複合ロールを製造することが可能となる。その結果、肌荒れや欠落ちなどの熱間圧延による表面損傷を抑制でき、連続圧延距離の延長やロール寿命の向上を達成できるという効果もある。 According to the present invention, it is possible to manufacture a hot rolling roll outer layer material and a hot rolling composite roll in which the propagation speed of cracks is significantly reduced. As a result, surface damage due to hot rolling such as rough skin and missing edges can be suppressed, and there is an effect that continuous rolling distance can be extended and roll life can be improved.
本発明の熱間圧延用ロール外層材は、公知の遠心鋳造法あるいは連続鋳掛け肉盛法等の鋳造法により製造され、そのままリングロール、スリーブロールとすることもできるが、熱間仕上げ圧延用として好適な、熱間圧延用複合ロールの外層材として適用される。また、本発明の熱間圧延用複合ロールは、外層と、該外層と溶着一体化した内層とからなる。なお、外層と内層との間に中間層を配してもよい。すなわち、外層と溶着一体化した内層に代えて、外層と溶着一体化した中間層および該中間層と溶着一体化した内層としてもよい。本発明では、内層、中間層の組成はとくに限定されないが、内層は球状黒鉛鋳鉄(ダクタイル鋳鉄)や鍛鋼、中間層は、C:1.5~3.0質量%の高炭素材とすることが好ましい。 The roll outer layer material for hot rolling of the present invention is manufactured by a known casting method such as a centrifugal casting method or a continuous casting overlaying method, and can be used as it is as a ring roll or a sleeve roll, but for hot finish rolling. It is preferably used as an outer layer material of a composite roll for hot rolling. The composite roll for hot rolling according to the present invention includes an outer layer and an inner layer welded and integrated with the outer layer. An intermediate layer may be disposed between the outer layer and the inner layer. That is, instead of the inner layer welded and integrated with the outer layer, an intermediate layer welded and integrated with the outer layer and an inner layer welded and integrated with the intermediate layer may be used. In the present invention, the composition of the inner layer and the intermediate layer is not particularly limited, but the inner layer is spheroidal graphite cast iron (ductile iron) or forged steel, and the intermediate layer is a high carbon material of C: 1.5 to 3.0% by mass. Is preferred.
まず、本発明の熱間圧延用複合ロールの外層(外層材)の組成限定理由について説明する。なお、以下、質量%は、とくに断らない限り、単に%と記す。 First, the reasons for limiting the composition of the outer layer (outer layer material) of the composite roll for hot rolling according to the present invention will be described. In the following, mass% is simply written as% unless otherwise specified.
C:2.0~3.0%
Cは、固溶して基地硬さを増加させるとともに、炭化物形成元素と結合し硬質炭化物を形成し、ロール外層材の耐摩耗性を向上させる作用を有する。C含有量に応じて共晶炭化物量が変化する。共晶炭化物は圧延使用特性に影響する。このため、C含有量が2.0%未満では、共晶炭化物量が不足し、圧延時の摩擦力が増加し圧延が不安定となるとともに、基地組織中に固溶するC量が低いため、耐熱間転動疲労性を低下させる。一方、3.0%を超える含有は、炭化物の粗大化や共晶炭化物量を過度に増加させ、ロール外層材を硬質、脆化させて、疲労亀裂の発生・成長を促進し、耐疲労性を低下させる。このため、Cは2.0~3.0%の範囲に限定する。なお、好ましくは、2.1~2.8%である。
C: 2.0 to 3.0%
C forms a solid solution to increase the base hardness and combines with a carbide forming element to form a hard carbide, thereby improving the wear resistance of the roll outer layer material. The amount of eutectic carbide varies depending on the C content. Eutectic carbides affect the rolling service characteristics. For this reason, if the C content is less than 2.0%, the amount of eutectic carbide is insufficient, the frictional force during rolling increases, rolling becomes unstable, and the amount of C dissolved in the base structure is low. Reduces rolling fatigue resistance during heat resistance. On the other hand, the content exceeding 3.0% excessively increases the coarsening of carbide and the amount of eutectic carbide, hardens and embrittles the roll outer layer material, promotes the generation and growth of fatigue cracks, and fatigue resistance. Reduce. For this reason, C is limited to a range of 2.0 to 3.0%. Preferably, the content is 2.1 to 2.8%.
Si:0.2~1.0%
Siは、脱酸剤として作用するとともに、溶湯の鋳造性を向上させる元素である。このような効果を得るためには、0.2%以上の含有を必要とする。一方、1.0%を超えて含有しても、効果が飽和し含有量に見合う効果が期待できなくなり経済的に不利となり、さらには、基地組織を脆化させる場合もある。このため、Siは0.2~1.0%に限定する。なお、好ましくは、0.3~0.7%である。
Si: 0.2 to 1.0%
Si is an element that acts as a deoxidizer and improves the castability of the molten metal. In order to obtain such an effect, a content of 0.2% or more is required. On the other hand, if the content exceeds 1.0%, the effect is saturated and an effect commensurate with the content cannot be expected, which is economically disadvantageous, and further, the base structure may become brittle. For this reason, Si is limited to 0.2 to 1.0%. Preferably, the content is 0.3 to 0.7%.
Mn:0.2~1.0%
Mnは、SをMnSとして固定し、Sを無害化する作用を有するとともに、一部は基地組織に固溶し、焼入れ性を向上させる効果を有する元素である。このような効果を得るためには0.2%以上の含有を必要とする。一方、1.0%を超えて含有しても、効果が飽和し含有量に見合う効果が期待できなくなり、さらには材質を脆化する場合もある。このため、Mnは0.2~1.0%に限定する。なお、好ましくは、0.3~0.8%である。
Mn: 0.2 to 1.0%
Mn is an element having the effect of fixing S as MnS and detoxifying S, and partly dissolving in the base structure and improving the hardenability. In order to obtain such an effect, a content of 0.2% or more is required. On the other hand, even if the content exceeds 1.0%, the effect is saturated and an effect commensurate with the content cannot be expected, and further, the material may become brittle. For this reason, Mn is limited to 0.2 to 1.0%. Preferably, the content is 0.3 to 0.8%.
Cr:4.0~7.0%
Crは、Cと結合して主に共晶炭化物を形成し、耐摩耗性を向上させるとともに、圧延時に鋼板との摩擦力を低減し、ロールの表面損傷を軽減させ、圧延を安定化させる作用を有する元素である。このような効果を得るためには4.0%以上の含有を必要とする。一方、7.0%を超える含有は、粗大な共晶炭化物が増加するため、耐疲労性を低下させる。このため、Crは4.0~7.0%の範囲に限定する。なお、好ましくは、4.3~6.5%である。
Cr: 4.0 to 7.0%
Cr combines with C to mainly form eutectic carbides, improves wear resistance, reduces friction with the steel sheet during rolling, reduces roll surface damage, and stabilizes rolling. It is an element having In order to obtain such an effect, the content of 4.0% or more is required. On the other hand, if the content exceeds 7.0%, coarse eutectic carbides increase, and fatigue resistance is lowered. For this reason, Cr is limited to the range of 4.0 to 7.0%. Preferably, the content is 4.3 to 6.5%.
Mo:3.0~6.5%
Moは、Cと結合して硬質な炭化物を形成し、耐摩耗性を向上させる元素である。また、Moは、V、NbとCが結合した硬質なMC型炭化物中に固溶して、炭化物を強化するとともに、共晶炭化物中にも固溶し、それら炭化物の破壊抵抗を増加させる。このような作用を介してMoは、ロール外層材の耐摩耗性、耐疲労性を向上させる。このような効果を得るためには、3.0%以上の含有を必要とする。一方、6.5%を超える含有は、Mo主体の硬脆な炭化物が生成し、耐熱間転動疲労性を低下させ、耐疲労性を低下させる。このため、Moは3.0~6.5%の範囲に限定する。なお、好ましくは、3.5~6.0%である。
Mo: 3.0 to 6.5%
Mo is an element that combines with C to form a hard carbide and improves wear resistance. In addition, Mo dissolves in hard MC-type carbides in which V, Nb, and C are bonded, strengthens the carbides, and also dissolves in eutectic carbides to increase the fracture resistance of these carbides. Through such an action, Mo improves the wear resistance and fatigue resistance of the outer roll layer material. In order to obtain such an effect, the content of 3.0% or more is required. On the other hand, if the content exceeds 6.5%, Mo-based hard and brittle carbides are produced, which reduces the rolling fatigue resistance during heat resistance and lowers the fatigue resistance. For this reason, Mo is limited to the range of 3.0 to 6.5%. Preferably, the content is 3.5 to 6.0%.
V:5.0~7.5%
Vは、ロールとしての耐摩耗性と耐疲労性とを兼備させるために、本発明において重要な元素である。Vは、極めて硬質な炭化物(MC型炭化物)を形成し、耐摩耗性を向上させるとともに、共晶炭化物を分断、分散晶出させることに有効に作用し、耐熱間転動疲労性を向上させ、ロール外層材としての耐疲労性を顕著に向上させる元素である。このような効果は、5.0%以上の含有で顕著となる。一方、7.5%を超える含有は、MC型炭化物を粗大化させるため、圧延用ロールの諸特性を不安定にする。このため、Vは5.0~7.5%の範囲に限定する。なお、好ましくは、5.2~7.0%である。
V: 5.0-7.5%
V is an important element in the present invention in order to combine wear resistance and fatigue resistance as a roll. V forms extremely hard carbide (MC type carbide), improves wear resistance, and effectively acts to sever and disperse eutectic carbide, thereby improving rolling fatigue resistance during heat resistance. Further, it is an element that remarkably improves fatigue resistance as a roll outer layer material. Such an effect becomes remarkable when the content is 5.0% or more. On the other hand, if the content exceeds 7.5%, the MC type carbides are coarsened, so that various properties of the rolling roll are made unstable. For this reason, V is limited to the range of 5.0 to 7.5%. Preferably, the content is 5.2 to 7.0%.
Nb:0.5~3.0%
Nbは、MC型炭化物に固溶してMC型炭化物を強化し、MC型炭化物の破壊抵抗を増加させる作用を介し、耐摩耗性、とくに耐疲労性を向上させる。NbとMoとがともに、炭化物中に固溶されることにより、耐摩耗性とさらには耐疲労性の向上が顕著となる。また、Nbは、共晶炭化物の分断を促進させ、共晶炭化物の破壊を抑制する作用を有し、ロール外層材の耐疲労性を向上させる元素である。また、NbはMC型炭化物の遠心鋳造時の偏析を抑制する作用を併せ有する。このような効果は、0.5%以上の含有で顕著となる。一方、含有量が3.0%を超えると、溶湯中でのMC型炭化物の成長が促進され、耐熱間転動疲労性を悪化させる。このため、Nbは0.5~3.0%の範囲に限定する。なお、好ましくは、0.8~1.5%である。
Nb: 0.5 to 3.0%
Nb improves the wear resistance, particularly fatigue resistance, through the action of strengthening the MC type carbide by solid solution in the MC type carbide and increasing the fracture resistance of the MC type carbide. When both Nb and Mo are dissolved in the carbide, the improvement in wear resistance and further fatigue resistance becomes significant. Moreover, Nb is an element which has the effect | action which promotes the division | segmentation of a eutectic carbide and suppresses destruction of a eutectic carbide, and improves the fatigue resistance of a roll outer layer material. Nb also has the effect of suppressing segregation during centrifugal casting of MC type carbide. Such an effect becomes remarkable when the content is 0.5% or more. On the other hand, if the content exceeds 3.0%, the growth of MC type carbide in the molten metal is promoted, and the rolling fatigue resistance during heat resistance is deteriorated. Therefore, Nb is limited to a range of 0.5 to 3.0%. Preferably, the content is 0.8 to 1.5%.
Ni:0.05~3.0%
Niは、基地中に固溶し、熱処理中のオーステナイトの変態温度を低下させ、基地の焼入れ性を向上させる元素である。このような効果を得るためには、0.05%以上の含有を必要とする。一方、3.0%を超えて含有すると、オーステナイトの変態温度が低くなりすぎ、且つ焼入れ性が向上するため、熱処理後にオーステナイトが残留しやすくなる。オーステナイトが残留すると、熱間圧延中にクラックが発生するなど、耐熱間転動疲労性を低下させる。そのため、Niは0.05~3.0%の範囲に限定する。なお、熱処理中の冷却速度が遅くても、基地組織の結晶サイズを微細にすることが可能となるという、操業し易さから、好ましくは0.2~3.0%である。
Ni: 0.05-3.0%
Ni is an element that dissolves in the matrix, lowers the transformation temperature of austenite during heat treatment, and improves the hardenability of the matrix. In order to acquire such an effect, 0.05% or more of content is required. On the other hand, if the content exceeds 3.0%, the transformation temperature of austenite becomes too low and the hardenability is improved, so that austenite tends to remain after heat treatment. When austenite remains, the rolling fatigue resistance during hot rolling is reduced, for example, cracks are generated during hot rolling. Therefore, Ni is limited to the range of 0.05 to 3.0%. Even if the cooling rate during the heat treatment is slow, it is preferably 0.2 to 3.0% from the viewpoint of ease of operation that the crystal size of the matrix structure can be made fine.
Co:0.2~5.0%
Coは、基地中に固溶し、とくに高温において基地を強化して、耐疲労性を向上させる作用を有する元素である。このような効果を得るためには、0.2%以上の含有を必要とする。一方、5.0%を超えて含有しても、効果が飽和し、含有量に見合う効果が期待できなくなり、経済的に不利となる。このため、Coは0.2~5.0%の範囲に限定する。なお、好ましくは、0.5~3.0%である。
Co: 0.2-5.0%
Co is an element that has a function of solid-dissolving in the matrix, strengthening the matrix, particularly at high temperatures, and improving fatigue resistance. In order to obtain such an effect, a content of 0.2% or more is required. On the other hand, even if the content exceeds 5.0%, the effect is saturated and an effect commensurate with the content cannot be expected, which is economically disadvantageous. Therefore, Co is limited to the range of 0.2 to 5.0%. Preferably, it is 0.5 to 3.0%.
W:0.5~5.0%
Wは、基地中に固溶し、とくに高温において基地を強化して、耐疲労性を向上させる作用を有する元素であり、且つM2CまたはM6C系の炭化物を形成し、耐摩耗性を向上させる。このような効果を得るためには、0.5%以上の含有を必要とする。一方、5.0%を超えて含有すると、効果が飽和するだけでなく、粗大なM2CまたはM6C系の炭化物が形成され、耐熱間転動疲労性を低下させる。このため、Wは0.5~5.0%の範囲に限定する。なお、好ましくは、1.0~3.5%である。
W: 0.5-5.0%
W is an element having a function of solid-dissolving in the matrix, strengthening the matrix at a high temperature and improving fatigue resistance, and forming M 2 C or M 6 C-based carbides, and wear resistance. To improve. In order to acquire such an effect, 0.5% or more of content is required. On the other hand, if the content exceeds 5.0%, not only the effect is saturated, but also coarse M 2 C or M 6 C-based carbides are formed, and the rolling fatigue resistance during heat resistance is reduced. For this reason, W is limited to a range of 0.5 to 5.0%. Preferably, it is 1.0 to 3.5%.
本発明では、C、Cr、Mo、V、Nb、Ni、Wを、上記した範囲で含有し、さらに、下記(1)式を満足するように調整して含有する。
0.05≦(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)≦4.0 (1)
ここで、%C、%V、%Nb、%Cr、%Mo、%W、%Niは、各元素の含有量(質量%)である。
In the present invention, C, Cr, Mo, V, Nb, Ni, and W are contained in the above-described range, and further adjusted and contained so as to satisfy the following expression (1).
0.05 ≦ (% C−% V × 0.177−% Nb × 0.129−% Cr × 0.099−% Mo × 0.063−% W × 0.033) + (% Ni) ≦ 4 .0 (1)
Here,% C,% V,% Nb,% Cr,% Mo,% W, and% Ni are the contents (mass%) of each element.
(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)について、上記(1)式を満足するように調整することにより、折損転動数が顕著に増加し、耐熱間転動疲労性が顕著に向上する。(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)は、耐熱間転動疲労性向上の駆動力となる重要なファクターであり、上記(1)式の範囲を外れると、耐熱間転動疲労性が劣化する。V、Cr、Mo、Nb、Wは炭化物を造りやすい元素であり、(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)は基地に固溶している炭素量を表す。そのため、(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)は基地に固溶している炭素量とNi量の和であり、この値を適正な範囲に調整することで、基地中のクラックの伝播速度が遅い、熱延疲労寿命の優れるロール外層材が得られる。このため、本発明では(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)について、上記(1)式を満足するように調整する。 (% C−% V × 0.177−% Nb × 0.129−% Cr × 0.099−% Mo × 0.063−% W × 0.033) + (% Ni) above (1) By adjusting so as to satisfy the formula, the number of breakage rolling is remarkably increased, and the rolling fatigue resistance during heat resistance is remarkably improved. (% C-% V x 0.177-% Nb x 0.129-% Cr x 0.099-% Mo x 0.063-% W x 0.033) + (% Ni) is rolling during heat resistance It is an important factor that becomes a driving force for improving fatigue resistance, and if it falls outside the range of the above formula (1), the rolling fatigue resistance during heat resistance deteriorates. V, Cr, Mo, Nb, and W are elements that are easy to produce carbides. (% C-% V × 0.177-% Nb × 0.129-% Cr × 0.099-% Mo × 0.063- % W × 0.033) represents the amount of carbon dissolved in the base. Therefore, (% C-% V × 0.177-% Nb × 0.129-% Cr × 0.099-% Mo × 0.063-% W × 0.033) + (% Ni) It is the sum of the amount of dissolved carbon and the amount of Ni, and by adjusting this value to an appropriate range, a roll outer layer material having a slow crack propagation speed in the base and an excellent hot-rolled fatigue life can be obtained. Therefore, in the present invention, (% C−% V × 0.177−% Nb × 0.129−% Cr × 0.099−% Mo × 0.063−% W × 0.033) + (% Ni) Is adjusted to satisfy the above expression (1).
上記した成分以外の残部は、Feおよび不可避的不純物からなる。 The balance other than the above components is composed of Fe and inevitable impurities.
また、本発明では、基地組織の85%以上が焼戻しマルテンサイトおよび/またはベイナイト組織であり、焼戻しマルテンサイトまたはベイナイトの短径が0.5~3.0μmとなるようにすることが好ましい。残留オーステナイトやパーライト組織の分率が多いと、耐熱間転動疲労性が低下するため、基地組織中に焼戻しマルテンサイトおよび/またはベイナイト組織が85%以上含まれることが好ましく、耐熱間転動疲労性の観点から90%以上含まれることがより好ましい。なお、残部としては、残留オーステナイトおよび/またはパーライトが挙げられる。なお、基地組織の85%以上を焼戻しマルテンサイトおよび/またはベイナイトとするためには、500~570℃に加熱保持した後、冷却する工程の繰り返し回数により制御すればよい。 In the present invention, 85% or more of the base structure is tempered martensite and / or bainite structure, and it is preferable that the minor axis of tempered martensite or bainite is 0.5 to 3.0 μm. When the fraction of retained austenite and pearlite structure is large, the rolling fatigue resistance during heat resistance decreases, so that it is preferable that the base structure contains 85% or more of tempered martensite and / or bainite structure. It is more preferable that it is contained 90% or more from the viewpoint of property. In addition, as a remainder, a retained austenite and / or pearlite are mentioned. In order to make 85% or more of the matrix structure tempered martensite and / or bainite, it may be controlled by repeating the cooling process after heating and holding at 500 to 570 ° C.
また、焼戻しマルテンサイトまたはベイナイトの短径が0.5μmよりも小さくなるような成分系では、変態温度が低くなりすぎ、焼戻しを繰り返し行っても残留オーステナイト量を低くすることが困難になり、残留オーステナイトを起因とした熱間圧延中のクラックの発生が生じる可能性があり、耐熱間転動疲労性が低下する。また、焼戻しマルテンサイトまたはベイナイトの短径が3.0μmを超えると、基地組織のクラック伝播速度が速く、耐熱間転動疲労性が低下する。そのため、基地組織の焼戻しマルテンサイトまたはベイナイトの短径を0.5~3.0μmの範囲に限定することが好ましい。耐熱間転動疲労性の観点から好ましくは0.5~2.0μmの範囲である。また、この短径を得るためには、基地の変態温度が200~400℃の範囲となるように、成分および冷却速度を制御すればよい。 In addition, in a component system in which the minor axis of tempered martensite or bainite is smaller than 0.5 μm, the transformation temperature becomes too low, and it becomes difficult to reduce the amount of retained austenite even if tempering is repeated. Cracking during hot rolling due to austenite may occur, and the hot rolling fatigue resistance is reduced. On the other hand, if the minor axis of tempered martensite or bainite exceeds 3.0 μm, the crack propagation rate of the base structure is high, and the rolling fatigue resistance during heat resistance decreases. Therefore, it is preferable to limit the minor axis of tempered martensite or bainite of the base structure to a range of 0.5 to 3.0 μm. From the viewpoint of rolling fatigue resistance during heat resistance, the thickness is preferably in the range of 0.5 to 2.0 μm. In order to obtain this minor axis, the components and the cooling rate may be controlled so that the transformation temperature of the matrix is in the range of 200 to 400 ° C.
つぎに、本発明の熱間圧延用複合ロールの好ましい製造方法について説明する。 Next, a preferred method for producing the composite roll for hot rolling according to the present invention will be described.
本発明では、ロール外層材の製造方法は、公知の遠心鋳造法あるいは連続鋳掛け肉盛法等の鋳造法により製造されることが好ましい。なお、本発明では、これらの方法に限定されないことは言うまでもない。 In the present invention, the roll outer layer material is preferably produced by a known centrifugal casting method or a casting method such as a continuous casting overlay method. Needless to say, the present invention is not limited to these methods.
遠心鋳造法でロール外層材を鋳造する場合、まず、内面にジルコン等を主材とした耐火物が1~5mm厚で被覆された、回転する鋳型に、上記したロール外層材組成の溶湯を、所定の肉厚となるように、注湯し、遠心鋳造する。ここで、鋳型の回転数は、ロールの外表面に印加される重力倍数が120~220Gの範囲とすることが好ましい。そして、中間層を形成する場合には、ロール外層材の凝固途中あるいは完全に凝固したのち、鋳型を回転させながら、中間層組成の溶湯を注湯し、遠心鋳造することが好ましい。外層あるいは中間層が完全に凝固したのち、鋳型の回転を停止し鋳型を立ててから、内層材を静置鋳造して、複合ロールとすることが好ましい。これにより、ロール外層材の内面側が再溶解され外層と内層、あるいは外層と中間層、中間層と内層とが溶着一体化した複合ロールとなる。 When casting a roll outer layer material by the centrifugal casting method, first, a molten mold having the above-described roll outer layer material composition is applied to a rotating mold whose inner surface is coated with a refractory material mainly composed of zircon or the like in a thickness of 1 to 5 mm. It is poured and centrifugally cast so as to have a predetermined thickness. Here, the number of rotations of the mold is preferably in the range of 120 to 220 G in the gravity multiple applied to the outer surface of the roll. When the intermediate layer is formed, it is preferable that the outer layer layer material is solidified during solidification or completely solidified, and then the molten metal having the intermediate layer composition is poured and centrifugally cast while rotating the mold. After the outer layer or the intermediate layer is completely solidified, it is preferable to stop the mold rotation and stand the mold, and then statically cast the inner layer material to form a composite roll. Thereby, the inner surface side of the roll outer layer material is redissolved to form a composite roll in which the outer layer and the inner layer, or the outer layer and the intermediate layer, and the intermediate layer and the inner layer are welded and integrated.
なお、静置鋳造される内層は、鋳造性と機械的性質に優れた球状黒鉛鋳鉄、いも虫状黒鉛鋳鉄(CV鋳鉄)などを用いることが好ましい。遠心鋳造製ロールは、外層と内層が一体溶着されているため、外層材の成分が1~8%程度内層に混入する。外層材に含まれるCr、V等の炭化物形成元素が内層へ混入すると、内層を脆弱化する。このため、外層成分の内層への混入率は6%未満に抑えることが好ましい。 In addition, it is preferable to use spheroidal graphite cast iron, worm-like graphite cast iron (CV cast iron), etc. excellent in castability and mechanical properties for the inner layer to be statically cast. In the centrifugal casting roll, the outer layer and the inner layer are integrally welded, so that the component of the outer layer material is mixed in the inner layer by about 1 to 8%. When carbide forming elements such as Cr and V contained in the outer layer material are mixed into the inner layer, the inner layer is weakened. For this reason, it is preferable to suppress the mixing rate of the outer layer component into the inner layer to less than 6%.
また、中間層を形成する場合は、中間層材として、黒鉛鋼、高炭素鋼、亜共晶鋳鉄等を用いることが好ましい。中間層と外層とは同じように一体溶着されており、外層成分が中間層へ10~95%の範囲で混入する。内層への外層成分の混入量を抑える観点から、外層成分の中間層への混入量はできるだけ低減しておくことが肝要となる。 Further, when forming the intermediate layer, it is preferable to use graphite steel, high carbon steel, hypoeutectic cast iron or the like as the intermediate layer material. The intermediate layer and the outer layer are integrally welded in the same manner, and the outer layer component is mixed in the intermediate layer in the range of 10 to 95%. From the viewpoint of suppressing the amount of the outer layer component mixed into the inner layer, it is important to reduce the amount of the outer layer component mixed into the intermediate layer as much as possible.
本発明の熱間圧延用複合ロールは、鋳造後、熱処理を施されることが好ましい。熱処理は、950~1100℃に加熱し空冷あるいは衝風空冷する工程と、さらに500~570℃に加熱保持した後、冷却する工程を2回以上行うことが好ましい。この時、変態温度が200~400℃の範囲になるように、成分に応じて冷却速度を調整することによって、前述の好適な短径サイズを得ることが可能となる。また、500~570℃に加熱保持した後、冷却する工程の繰り返し回数によって、基地組織中の焼戻しマルテンサイトおよび/またはベイナイトの量が変化するため、基地組織の85%以上が焼戻しマルテンサイトおよび/またはベイナイトになるように繰り返し回数を設定すればよい
なお、本発明の熱間圧延用複合ロールの好ましい硬さは、79~88HS(ショア硬さ)、より好ましい硬さは80~86HSである。80HSよりも硬さが低いと、耐摩耗性が劣化し、逆に硬さが86HSを超えると、熱間圧延中に熱間圧延用ロール表面に形成されたクラックを研削により除去し難くなる。このような硬さを安定して確保できるように、鋳造後の熱処理温度、熱処理時間を調整することが好ましい。
The composite roll for hot rolling of the present invention is preferably subjected to heat treatment after casting. In the heat treatment, it is preferable to perform the step of heating to 950 to 1100 ° C. by air cooling or blast air cooling, and further the step of cooling after heating and holding at 500 to 570 ° C. is performed twice or more. At this time, by adjusting the cooling rate in accordance with the components so that the transformation temperature is in the range of 200 to 400 ° C., it is possible to obtain the above-mentioned preferred minor axis size. In addition, since the amount of tempered martensite and / or bainite in the base structure changes depending on the number of repetitions of the cooling step after heating and holding at 500 to 570 ° C., 85% or more of the base structure is tempered martensite and / or Alternatively, the number of repetitions may be set so as to be bainite. The preferred hardness of the composite roll for hot rolling of the present invention is 79 to 88 HS (Shore hardness), and more preferred is 80 to 86 HS. If the hardness is lower than 80 HS, the wear resistance is deteriorated. Conversely, if the hardness exceeds 86 HS, cracks formed on the surface of the hot rolling roll during hot rolling are difficult to remove by grinding. It is preferable to adjust the heat treatment temperature and heat treatment time after casting so that such hardness can be stably secured.
表1に示すロール外層材組成の溶湯を、高周波誘導炉で溶解し遠心鋳造法により、リング状試験材(リングロール;外径:250mmφ、幅:65mm、肉厚:55mm)とした。なお、鋳込み温度は1450~1530℃とし、遠心力はリング状ロール材の外周部が重力倍数で180Gとなるようにした。鋳造後、焼入れ温度:1070℃に再加熱し、空冷して、焼入れる焼入れ処理、焼戻処理は、温度:530~570℃で、残留オーステナイト量が体積%で10%未満になるように、成分によって2または3回実施し、且つ、硬さを78~86HSに調整した。得られたリング状試験材から、硬さ試験片、熱間転動疲労試験片およびEBSD測定用試験片を採取して、硬さ試験、熱間転動疲労試験および組織観察試験を実施した。 The melt of the roll outer layer material composition shown in Table 1 was melted in a high-frequency induction furnace and made into a ring-shaped test material (ring roll; outer diameter: 250 mmφ, width: 65 mm, wall thickness: 55 mm) by centrifugal casting. The casting temperature was 1450 to 1530 ° C., and the centrifugal force was such that the outer peripheral portion of the ring-shaped roll material was 180 G in the multiple of gravity. After casting, the quenching temperature is reheated to 1070 ° C., air-cooled, and quenching quenching and tempering are performed at a temperature of 530 to 570 ° C. so that the residual austenite amount is less than 10% by volume. Performed 2 or 3 times depending on the ingredients and the hardness was adjusted to 78-86 HS. From the obtained ring-shaped test material, a hardness test piece, a hot rolling fatigue test piece, and a test piece for EBSD measurement were collected, and a hardness test, a hot rolling fatigue test, and a structure observation test were performed.
得られた硬さ試験片について、JIS Z 2244 の規定に準拠して、ビッカース硬さ計(試験力:50kgf(490N))でビッカース硬さHV50を測定し、JIS換算表でショア硬さHSに換算した。なお、測定点は各10点とし、最高値、最低値を削除して平均値を算出し、その試験材の硬さとした。 About the obtained hardness test piece, Vickers hardness HV50 is measured with a Vickers hardness tester (test force: 50 kgf (490 N)) in accordance with the provisions of JIS Z 2244, and Shore hardness HS is calculated with a JIS conversion table. Converted. The measurement points were 10 points each, the maximum value and the minimum value were deleted, the average value was calculated, and the hardness of the test material.
熱間転動疲労試験方法は次の通りとした。得られたリング状試験材から熱間転動疲労試験片(外径60mmφ、肉厚10mm、面取り有)を採取した。熱間転動疲労試験片には、図1に示すようなノッチ(深さt:1.2mm、周方向長さL:0.8mm)を外周面の2箇所(180°離れた位置)に、0.20mmφのワイヤを用いた放電加工(ワイヤカット)法で導入した。熱間転動疲労試験は、図1に示すように、試験片と相手材との2円盤すべり転動方式で行った。試験片1を冷却水2で水冷しながら700rpmで回転させ、回転する該試験片1に、高周波誘導加熱コイル3で800℃に加熱した相手片(材質:S45C、外径:190mmφ、幅:15mm、C1面取り)4を荷重980Nで接触させながら、すべり率:9%で転動させた。そして、熱間転動疲労試験片1に導入した2つのノッチ5が折損するまで転動させ、各ノッチが折損するまでの転動回転数をそれぞれ求め、その平均値を熱延疲労寿命とした。そして、熱延疲労寿命が350千回を超える場合を熱延疲労寿命が著しく優れると評価した。
The hot rolling fatigue test method was as follows. A hot rolling fatigue test piece (outer diameter 60 mmφ, wall thickness 10 mm, chamfered) was collected from the obtained ring-shaped test material. In the hot rolling fatigue test piece, notches (depth t: 1.2 mm, circumferential length L: 0.8 mm) as shown in FIG. 1 are provided at two locations on the outer peripheral surface (positions 180 ° apart). And introduced by an electric discharge machining (wire cut) method using a 0.20 mmφ wire. As shown in FIG. 1, the hot rolling fatigue test was performed by a two-disk sliding rolling method between a test piece and a counterpart material. The
組織観察は、リング状ロール材の外表面から10mm内部の任意の位置において、10×10×5mm(5mmはリングの肉厚方向)の組織観察試験片を採取し、10×10mmの面を鏡面研磨して、ナイタール(5体積%硝酸+エタノール)で10秒程度腐食し、光学顕微鏡を用いて行った。 For tissue observation, a 10 × 10 × 5 mm (5 mm is the thickness direction of the ring) tissue observation specimen is taken at an arbitrary position within 10 mm from the outer surface of the ring-shaped roll material, and the 10 × 10 mm surface is a mirror surface Polishing was performed, and corrosion was performed with nital (5% by volume nitric acid + ethanol) for about 10 seconds.
焼戻しマルテンサイトまたはベイナイトの短径(短軸長さ)は、得られたリング状ロール材の外表面から10mm内部の任意の位置からEBSD測定試験片(5mm×10mm×5mm)を採取して、5mm×10mmの面を鏡面研磨し、EBSD測定により求めた。加速電圧15kV、ステップサイズ0.1μmで、10000μm2以上の領域のEBSD測定を行った。得られたデータを用いて、図2に示すように、隣接する測定点との方位差が15°以上の箇所に境界線を引き、境界線で囲まれた領域を一つの結晶として、測定面上で、長径が10μm以上の20個の結晶の短径を測定し、その平均値を算出した。 The short diameter (short axis length) of tempered martensite or bainite is obtained by taking an EBSD measurement test piece (5 mm × 10 mm × 5 mm) from an arbitrary position within 10 mm from the outer surface of the obtained ring-shaped roll material, A surface of 5 mm × 10 mm was mirror-polished and determined by EBSD measurement. EBSD measurement was performed in an area of 10000 μm 2 or more at an acceleration voltage of 15 kV and a step size of 0.1 μm. Using the obtained data, as shown in FIG. 2, a boundary line is drawn at a position where the azimuth difference between adjacent measurement points is 15 ° or more, and the region surrounded by the boundary line is taken as one crystal, and the measurement surface Above, the minor axis of 20 crystals whose major axis is 10 μm or more was measured, and the average value was calculated.
得られた結果を表2に示す。 Table 2 shows the results obtained.
本発明例では熱延疲労寿命は著しく増加しており、350千回を超える優れた熱延疲労寿命を示した。また、組織観察の結果、本発明例はいずれも基地組織の85%以上が焼戻しマルテンサイトおよび/またはベイナイト組織であることを確認した。 In the examples of the present invention, the hot-rolled fatigue life was remarkably increased, and an excellent hot-rolled fatigue life exceeding 350,000 times was exhibited. As a result of the structure observation, it was confirmed that 85% or more of the base structure was tempered martensite and / or bainite structure.
したがって、本発明によれば、クラックの伝播速度が著しく低減した熱間圧延用複合ロールを製造することが可能となる。その結果、肌荒れや欠落ちなどの熱間圧延による表面損傷を抑制できるため、連続圧延距離の延長やロール寿命の向上を達成できるという効果も得られる。 Therefore, according to the present invention, it is possible to manufacture a composite roll for hot rolling in which the propagation speed of cracks is significantly reduced. As a result, surface damage due to hot rolling such as rough skin and missing edges can be suppressed, so that the effect of extending the continuous rolling distance and improving the roll life can also be obtained.
1 試験片(熱延疲労試験片)
2 冷却水
3 高周波誘導加熱コイル
4 相手片
5 ノッチ
1 Test piece (hot rolled fatigue test piece)
2 Cooling
Claims (2)
Si:0.2~1.0%、
Mn:0.2~1.0%、
Cr:4.0~7.0%、
Mo:3.0~6.5%、
V:5.0~7.5%、
Nb:0.5~3.0%、
Ni:0.05~3.0%、
Co:0.2~5.0%、
W:0.5~5.0%
を含有し、かつC、Cr、Mo、V、Nb、Ni、Wの含有量が下記(1)式を満足し、残部Feおよび不可避的不純物からなる組成を有し、基地組織の85%以上が焼戻しマルテンサイトおよび/またはベイナイト組織であり、焼戻しマルテンサイトまたはベイナイトの短径は0.5~3.0μmであることを特徴とする熱間圧延用ロール外層材。
0.05≦(%C-%V×0.177-%Nb×0.129-%Cr×0.099-%Mo×0.063-%W×0.033)+(%Ni)≦4.0 (1)
ここで、%C、%V、%Nb、%Cr、%Mo、%W、%Niは、各元素の含有量(質量%)である。 % By mass, C: 2.0 to 3.0%,
Si: 0.2 to 1.0%,
Mn: 0.2 to 1.0%,
Cr: 4.0 to 7.0%,
Mo: 3.0 to 6.5%,
V: 5.0-7.5%,
Nb: 0.5 to 3.0%,
Ni: 0.05 to 3.0%,
Co: 0.2-5.0%
W: 0.5-5.0%
And the content of C, Cr, Mo, V, Nb, Ni, W satisfies the following formula (1), has a composition consisting of the remainder Fe and inevitable impurities, and is 85% or more of the base structure Is a tempered martensite and / or bainite structure, the tempered martensite or bainite having a minor axis of 0.5 to 3.0 μm.
0.05 ≦ (% C−% V × 0.177−% Nb × 0.129−% Cr × 0.099−% Mo × 0.063−% W × 0.033) + (% Ni) ≦ 4 .0 (1)
Here,% C,% V,% Nb,% Cr,% Mo,% W, and% Ni are the contents (mass%) of each element.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1020197004864A KR102234330B1 (en) | 2016-09-07 | 2017-06-28 | Outer roll material for hot rolling and composite roll for hot rolling |
| CN201780050783.6A CN109641250B (en) | 2016-09-07 | 2017-06-28 | Roll outer layer material for hot rolling and composite roll for hot rolling |
| JP2017552525A JP6292362B1 (en) | 2016-09-07 | 2017-06-28 | Roll outer layer material for hot rolling and composite roll for hot rolling |
| BR112019003360-2A BR112019003360B1 (en) | 2016-09-07 | 2017-06-28 | OUTER LAYER MATERIAL OF HOT ROLLING CYLINDER AND COMPOSITE CYLINDER FOR HOT ROLLING |
| EP17848389.7A EP3479915B1 (en) | 2016-09-07 | 2017-06-28 | Roll outer layer material for hot rolling and composite roll for hot rolling |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2016-174329 | 2016-09-07 | ||
| JP2016174329 | 2016-09-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2018047444A1 true WO2018047444A1 (en) | 2018-03-15 |
Family
ID=61561802
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2017/023663 Ceased WO2018047444A1 (en) | 2016-09-07 | 2017-06-28 | Roll outer layer material for hot rolling and composite roll for hot rolling |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP3479915B1 (en) |
| JP (1) | JP6292362B1 (en) |
| KR (1) | KR102234330B1 (en) |
| CN (1) | CN109641250B (en) |
| TW (1) | TWI655295B (en) |
| WO (1) | WO2018047444A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2020022989A (en) * | 2018-08-08 | 2020-02-13 | 日立金属株式会社 | Outer layer material of centrifugal casting compound roll for rolling and centrifugal casting compound roll for rolling |
| JP2022178535A (en) * | 2021-05-20 | 2022-12-02 | Jfeスチール株式会社 | Roll outer layer material for hot rolling and composite roll for hot rolling |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000109951A (en) * | 1998-08-05 | 2000-04-18 | Kawasaki Steel Corp | High strength hot rolled steel sheet excellent in stretch flangeability and method for producing the same |
| JP2005246391A (en) * | 2004-03-01 | 2005-09-15 | Nippon Steel Corp | 3-layer composite sleeve roll |
| JP2015193015A (en) * | 2014-03-31 | 2015-11-05 | 日立金属株式会社 | Composite roll for rolling and manufacturing method thereof |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2715199B2 (en) | 1990-10-01 | 1998-02-18 | 川崎製鉄株式会社 | Roll outer layer material for rolling |
| JP2715205B2 (en) | 1990-11-21 | 1998-02-18 | 川崎製鉄株式会社 | Roll outer layer material for rolling |
| JP3962838B2 (en) | 1998-08-03 | 2007-08-22 | 日立金属株式会社 | Hot rolling roll |
| CN100485075C (en) * | 2007-04-03 | 2009-05-06 | 西安交通大学 | A high-carbon high-vanadium high-speed steel composite roll and heat treatment method thereof |
| JP5136138B2 (en) | 2008-03-18 | 2013-02-06 | Jfeスチール株式会社 | Centrifugal cast composite roll for hot rolling |
| CN101831590B (en) * | 2009-03-10 | 2011-07-06 | 江苏东冶轧辊有限公司 | High-boron low-alloy high-speed steel roll and preparation method thereof |
| SE535101C2 (en) * | 2010-01-11 | 2012-04-17 | Sandvik Intellectual Property | music String |
| JP6036698B2 (en) * | 2011-09-21 | 2016-11-30 | 日立金属株式会社 | Centrifugal cast composite roll for hot rolling and manufacturing method thereof |
| ES2562625T3 (en) * | 2011-11-21 | 2016-03-07 | Hitachi Metals, Ltd. | Centrifugally cast composite roller and its production method |
| JP5862526B2 (en) * | 2012-09-13 | 2016-02-16 | Jfeスチール株式会社 | Roll outer layer material for hot rolling and composite roll for hot rolling |
| JP5949596B2 (en) * | 2013-03-01 | 2016-07-06 | Jfeスチール株式会社 | Roll outer layer material for hot rolling, and composite roll for hot rolling |
| JP5768947B2 (en) * | 2013-05-02 | 2015-08-26 | 日立金属株式会社 | Composite roll for hot rolling made by centrifugal casting |
| BR112016004075B1 (en) * | 2013-09-25 | 2020-03-24 | Hitachi Metals, Ltd. | COMPOSITE HOT LAMINATION CYLINDER CASTED BY CENTRIFUGATION |
| CN104018076B (en) * | 2014-06-25 | 2016-06-15 | 武汉钢铁(集团)公司 | A kind of high temperature resistant reinforcing bar and production method |
-
2017
- 2017-06-28 JP JP2017552525A patent/JP6292362B1/en active Active
- 2017-06-28 KR KR1020197004864A patent/KR102234330B1/en active Active
- 2017-06-28 CN CN201780050783.6A patent/CN109641250B/en active Active
- 2017-06-28 WO PCT/JP2017/023663 patent/WO2018047444A1/en not_active Ceased
- 2017-06-28 EP EP17848389.7A patent/EP3479915B1/en active Active
- 2017-07-11 TW TW106123209A patent/TWI655295B/en active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000109951A (en) * | 1998-08-05 | 2000-04-18 | Kawasaki Steel Corp | High strength hot rolled steel sheet excellent in stretch flangeability and method for producing the same |
| JP2005246391A (en) * | 2004-03-01 | 2005-09-15 | Nippon Steel Corp | 3-layer composite sleeve roll |
| JP2015193015A (en) * | 2014-03-31 | 2015-11-05 | 日立金属株式会社 | Composite roll for rolling and manufacturing method thereof |
Non-Patent Citations (1)
| Title |
|---|
| See also references of EP3479915A4 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2020022989A (en) * | 2018-08-08 | 2020-02-13 | 日立金属株式会社 | Outer layer material of centrifugal casting compound roll for rolling and centrifugal casting compound roll for rolling |
| JP7063180B2 (en) | 2018-08-08 | 2022-05-09 | 日立金属株式会社 | Outer layer material of centrifugal casting composite roll for rolling, and centrifugal casting composite roll for rolling |
| JP2022178535A (en) * | 2021-05-20 | 2022-12-02 | Jfeスチール株式会社 | Roll outer layer material for hot rolling and composite roll for hot rolling |
| JP7400771B2 (en) | 2021-05-20 | 2023-12-19 | Jfeスチール株式会社 | Hot rolling roll outer layer material and hot rolling composite roll |
Also Published As
| Publication number | Publication date |
|---|---|
| BR112019003360A2 (en) | 2019-06-04 |
| JPWO2018047444A1 (en) | 2018-09-06 |
| EP3479915A1 (en) | 2019-05-08 |
| EP3479915B1 (en) | 2021-07-21 |
| EP3479915A4 (en) | 2019-08-07 |
| KR20190029716A (en) | 2019-03-20 |
| CN109641250B (en) | 2020-11-03 |
| TW201812028A (en) | 2018-04-01 |
| JP6292362B1 (en) | 2018-03-14 |
| CN109641250A (en) | 2019-04-16 |
| KR102234330B1 (en) | 2021-03-30 |
| TWI655295B (en) | 2019-04-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP5949596B2 (en) | Roll outer layer material for hot rolling, and composite roll for hot rolling | |
| JP5136138B2 (en) | Centrifugal cast composite roll for hot rolling | |
| EP2770073B1 (en) | Roll surface-layer material for hot rolling with excellent fatigue resistance produced by centrifugal casting, and composite roll for hot rolling produced through centrifugal casting | |
| JP6474038B2 (en) | Composite roll for continuous casting and overlay casting | |
| JP2016180167A (en) | Consecutive tinkering padding casting-made composite roll for rolling | |
| JP5703718B2 (en) | Outer layer material and composite roll made of centrifugal cast for hot rolling | |
| JP5434276B2 (en) | Centrifugal cast composite roll for hot rolling | |
| JP6292362B1 (en) | Roll outer layer material for hot rolling and composite roll for hot rolling | |
| JP2003073767A (en) | Roll outer layer material for hot rolling and composite roll for hot rolling | |
| JP5516545B2 (en) | Centrifugal cast roll outer layer material for hot rolling with excellent fatigue resistance and composite roll made of centrifugal cast for hot rolling | |
| JP2002220635A (en) | Single layer sleeve roll for hot rolling by centrifugal casting | |
| JP6669109B2 (en) | Roll outer layer material for hot rolling and composite roll for hot rolling | |
| JP5434249B2 (en) | Centrifugal cast composite roll for hot rolling | |
| JP5867143B2 (en) | Centrifugal cast roll outer layer material for hot rolling excellent in fatigue resistance, centrifugal cast composite roll for hot rolling, and production method thereof | |
| JP5327342B2 (en) | Centrifugal cast roll outer layer material for hot rolling with excellent fatigue resistance and composite roll made of centrifugal cast for hot rolling | |
| JP5867144B2 (en) | Centrifugal cast roll outer layer material for hot rolling excellent in fatigue resistance, centrifugal cast composite roll for hot rolling, and production method thereof | |
| JP7400771B2 (en) | Hot rolling roll outer layer material and hot rolling composite roll | |
| JP4260670B2 (en) | Adamite roll for hot rolling | |
| KR20210082226A (en) | Outer layer material for hot rolling and composite roll for hot rolling |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WWE | Wipo information: entry into national phase |
Ref document number: 2017552525 Country of ref document: JP |
|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 17848389 Country of ref document: EP Kind code of ref document: A1 |
|
| ENP | Entry into the national phase |
Ref document number: 2017848389 Country of ref document: EP Effective date: 20190204 |
|
| ENP | Entry into the national phase |
Ref document number: 20197004864 Country of ref document: KR Kind code of ref document: A |
|
| REG | Reference to national code |
Ref country code: BR Ref legal event code: B01A Ref document number: 112019003360 Country of ref document: BR |
|
| NENP | Non-entry into the national phase |
Ref country code: DE |
|
| ENP | Entry into the national phase |
Ref document number: 112019003360 Country of ref document: BR Kind code of ref document: A2 Effective date: 20190219 |