Clad steel plate with excellent thermal conductivity
10562084 ยท 2020-02-18
Assignee
Inventors
Cpc classification
B32B15/011
PERFORMING OPERATIONS; TRANSPORTING
B21B1/38
PERFORMING OPERATIONS; TRANSPORTING
B32B3/263
PERFORMING OPERATIONS; TRANSPORTING
B32B3/28
PERFORMING OPERATIONS; TRANSPORTING
B21B1/26
PERFORMING OPERATIONS; TRANSPORTING
B32B15/01
PERFORMING OPERATIONS; TRANSPORTING
B21D22/02
PERFORMING OPERATIONS; TRANSPORTING
B32B3/02
PERFORMING OPERATIONS; TRANSPORTING
B32B2250/40
PERFORMING OPERATIONS; TRANSPORTING
B32B3/30
PERFORMING OPERATIONS; TRANSPORTING
B21B1/28
PERFORMING OPERATIONS; TRANSPORTING
International classification
B21B1/38
PERFORMING OPERATIONS; TRANSPORTING
B32B15/01
PERFORMING OPERATIONS; TRANSPORTING
B32B3/26
PERFORMING OPERATIONS; TRANSPORTING
B21D22/02
PERFORMING OPERATIONS; TRANSPORTING
B21B1/28
PERFORMING OPERATIONS; TRANSPORTING
B32B3/06
PERFORMING OPERATIONS; TRANSPORTING
B32B3/28
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Provided is a clad steel plate with excellent thermal conductivity that can be used suitably in cookware and the like. The present invention is a three-layer clad steel plate having a carbon steel base material and stainless steel mating material disposed respectively on both surface sides of the base material, wherein a plate thickness ratio L given by Equation (1) is 1.0-5.0 and at least one surface of the clad steel plate has a plurality of protrusions and recesses. Plate thickness ratio L=the plate thickness of the base material/the total thickness of the mating material . . . Equation (1) Here, the base material thickness and the mating material thickness are the thicknesses at the protrusions.
Claims
1. A three-layer clad steel plate comprising: a carbon steel base material; and stainless steel mating materials each disposed on either surface of the base material, a plate thickness ratio, L, represented by: the thickness of the base material/the total thickness of the mating materials, is a value from 1.0 to 5.0, a plurality of protruded portions and depressed portions being formed on at least one surface of the clad steel plate, wherein the thickness of the base material and the thicknesses of the mating materials are those at the protruded portions, the area of the plurality of protruded portions is 20 to 80% relative to the area of a surface of the clad steel plate on which the protruded portions are formed, and the plurality of protruded portions and depressed portions have a depression-protrusion difference of 0.02 mm or more to 0.2 mm or less in the plate thickness direction.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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PREFERRED MODE FOR CARRYING OUT THE INVENTION
(9) Below, the embodiments of the present invention will be described. The descriptions of these shall not limit the present invention.
(10) An embodiment of the present invention is a three-layer clad steel plate including: low carbon steel as a base material; and stainless steel as mating materials (hereinafter may also be referred to as outer layers) each disposed on either surface of the base material, in which a plate thickness ratio L defined as the thickness of the base material/the total thickness of the outer layers is 1.0 to 5.0 with regard to the thicknesses of the base material and the mating materials, and a plurality of protruded portions and depressed portions are formed on at least one surface of the clad steel plate.
(11) (Clad Steel Plate)
(12) The three-layer clad steel plate according to an embodiment of the present invention (hereinafter may also be referred to as the three-layer clad steel plate) may be manufactured mainly via hot rolling, annealing, and cold rolling. Specifically, metal plates as raw materials of the three layers are laminated, and a release material such as Ni foil is further laminated on the both sides of these, which is then placed inside a bag made of a foil or thin sheet of a metal having oxidation resistance such as stainless steel. Subsequently, the bag is vacuum pumped, and then filled with an inert gas such as nitrogen gas, and then heated from the outside of the bag to allow laminated metal plates to be diffusion bonded. After diffusion bonded, hot rolling may be performed to obtain a desired plate thickness, and then annealing and cold rolling may be further repeated to obtain a flat three-layer clad steel plate. It is noted that the last step before the embossing process described below is preferably an annealing step.
(13) There is no particular limitation for the type of the base material of the three-layer clad steel plate. Steel plates such as those made of low carbon steel, medium carbon steel, high carbon steel, alloy steel, and the like can be used as the base material. When good press-formability is required, deep drawing steel plates such as those made of low carbon steel alloyed with Ti, low carbon steel alloyed with Nb, and the like are preferred as an underlying steel plate. Further, high-strength steel plates alloyed with P, Si, Mn, and the like may be used.
(14) When low carbon steel is used as the base material, for example, SPCC as defined in JIS G 3141 is preferred. Specifically, those may be used having a carbon concentration of 0.15% by mass or less, a manganese concentration of 0.60% by mass or less, a phosphorus concentration of 0.10% by mass or less, and a sulfur concentration of 0.05% by mass or less.
(15) There is no particular limitation for the type of stainless steel used for the mating materials of the three-layer clad steel plate. Ferrite-based, austenite-based, or biphasic stainless steel plates may be used as the mating materials, depending on usage environments of a clad steel plate. When the usage environments of the clad steel plate are relatively mild with regard to corrosion, a ferrite-based stainless steel plate, which is less expensive, can be used. In usage environments where acid resistance and workability are important, an austenite-based stainless steel plate may be preferably used as the mating materials. Alternatively, when high strength and pitting resistance are required, a biphasic stainless steel plate may be used as the mating materials.
(16) Further, there is no particular limitation for the surface finishing process of stainless steel plates as the mating materials of the three-layer clad steel plate, and any known means may be used. The thicknesses of two mating materials each disposed on either surface of the base material may be the same or different. When the clad steel plate is to be subjected to plastic working such as bending, stainless steel plates with different thickness may also be used as the mating materials depending on the method of working for plastic working and the shape after working.
(17) (Embossing Process)
(18) The clad steel plate according to an embodiment of the present invention has a plurality of protruded portions and depressed portions on at least one surface thereof. Formation of a depression-protrusion pattern including protruded portions and depressed portions on a surface of the clad steel plate can further improve thermal conductivity from one side, e.g., a heated side, of the clad steel plate to the other side, e.g., a non-heated side. As a means of providing such a depression-protrusion pattern, for example, embossing process may be used. Specifically, the rolling method, the press working, and the like may be used.
(19) With regard to a method of embossing, the rolling method using a emboss roll has superior productivity. Even when an emboss roll used for rolling is worn or damaged, the profile of the emboss roll can be reworked by performing cutting or etching process. Therefore, the rolling method is also preferred in view of cost reduction.
(20) When the rolling method as described above is used, a four-stage rolling machine, for example, as shown in
(21) (Protrusion Area Percentage)
(22) The percentage of the area of protruded portions on the clad steel plate relative to the surface area of the clad steel plate on which the protruded portions are formed (hereinafter may also be referred to as the protrusion area percentage) is preferably 20 to 80%.
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(24) The protrusion area percentage can be calculated as follows. First, a two-dimensional profile where the vertical axis corresponds to the plate thickness direction as shown in
(25) Here, the data of the two-dimensional profile is linearly approximated for protruded portions and depressed portions of a clad steel plate, and the slope of the resulting straight line is further corrected horizontally to identify a reference line M. Portions located above the reference line M on the surface are considered as protruded portions to be measured.
(26) A protrusion area percentage of less than 20% increases a proportion of portions where depressed portions are formed with large-diameter portions of a stepped roll upon forming a depression-protrusion pattern by the rolling method, resulting in an increased burden to the roll due to increased rolling load. This will reduce the life time of the roll, and result in increased manufacturing cost. On the other hand, when the protrusion area percentage is more than 80%, an effect for improving thermal conductivity is small.
(27) Depression-Protrusion Difference
(28) The depression-protrusion difference is preferably 0.02 to 0.2 mm in the plate thickness direction of a depression-protrusion clad steel plate. The depression-protrusion difference corresponds to the protrusion height H as shown in
(29) A clad steel plate can retain good thermal conductivity, and can be used for a prolonged time when it has a protrusion area percentage of 20 to 80% and a depression-protrusion difference of 0.02 to 0.2 mm as described above.
(30) (Depression-Protrusion Pattern)
(31) As described above, a clad steel plate can be used in which a depression-protrusion pattern including protruded portions and depressed portions are formed by embossing process. A pattern of the depression-protrusion pattern may be regular, or may be partially or entirely random. For example, a random depression-protrusion pattern may be formed as shown in
(32) The cross section of two-dimensional profiles of a clad steel plate having a depression-protrusion pattern on a surface thereof are shown in
(33) The depression-protrusion patterns in
(34) (Plate Thickness Ratio L)
(35) The plate thickness ratio L of a clad steel plate is defined by the following Equation (1) using the thickness of a base material and the total thickness of mating materials:
the plate thickness ratio L=the thickness of the base material/the total thickness of the mating materialsEquation (1).
The mating materials are each disposed on either surface of the base material, and thus the total thickness of the mating materials each disposed on either surface is used in Equation (1). The thickness of the base material and the thicknesses of the mating materials are those at protruded portions.
(36) A plate thickness ratio L of less than 1.0 means that the proportion of mating materials in a clad steel plate is large. When mating materials are made of a material (stainless steel) having a relatively lower heat conductivity than a base material (carbon steel), the heat conductivity of the resulting clad steel plate may be decreased. Moreover, mating materials may be detached from a base material at a working site due to different ductility between the base material and the mating materials when comprehension stress is exerted on a clad steel plate during work. On the other hand, a plate thickness ratio of more than 5.0 means that the proportion of mating materials is excessively small. This may result in breakage of the mating materials (stainless steel plates) when a clad steel plate is subjected to plastic working such as bending. Therefore, the plate thickness ratio L preferably falls within the range of 1.0 to 5.0. The lower limit thereof is more preferably 1.5, even more preferably 2.0. The upper limit thereof is more preferably 4.0, even more preferably 3.5.
EXAMPLES
(37) Below, Examples of the present invention will be described. The present invention shall not be limited to the following Examples.
(38) First, the following four types of three-layer clad steel plates were manufactured. It is noted that the four types of three-layer clad steel plates manufactured each have a plate thickness of 0.8 mm. Hereinafter, the plate thickness ratio L may also be referred to as the plate thickness ratio.
(39) (1) A three-layer clad steel plate including a base material made of a cold rolled steel plate of 0.64-mm thick SPCC (JIS G 3141) (hereinafter referred to SPCC) and mating materials made of 0.08-mm SUS304 each disposed on either surface thereof; and having a plate thickness ratio of 4.0.
(2) A three-layer clad steel plate including a base material made of 0.56-mm thick SPCC and mating materials made of 0.12-mm SUS304 each disposed on either surface thereof; and having a plate thickness ratio of 2.3.
(3) A three-layer clad steel plate including a base material made of 0.48-mm thick SPCC and mating materials made of 0.16-mm SUS304 each disposed on either surface thereof, and having a plate thickness ratio of 1.5.
(4) A three-layer clad steel plate including a base material made of 0.72-mm thick SPCC and mating materials made of 0.04-mm SUS304 each disposed on either surface thereof; and having a plate thickness ratio of 9.
(40) Next, among these, the three-layer clad steel plates having a plate thickness ratio of 4.0, 2.3, and 1.5 were subjected to embossing process to form protruded portions and depressed portions on a surface of the respective three-layer clad steel plate using a four-stage rolling machine as shown in
(41) Comparative Examples 1 and 2 are three-layer clad steel plates without embossing process.
(42) It is noted that the plate thickness ratio at protruded portions of the depression-protrusion clad steel plates did not differ from that of the three-layer clad steel plates before forming a depression-protrusion pattern.
(43) The protrusion area percentage and depression-protrusion difference of the depression-protrusion pattern formed on a surface of the depression-protrusion clad steel plate manufactured were measured from a profile obtained by expanding a region with an area of 100 mm.sup.2 arbitrarily selected from the clad steel plate using a profile measuring machine (contracer). Examples of the two-dimensional profile, the two-dimensional profiles of the clad steel plates from Examples 1 and 4 in which the vertical axis corresponds to the plate thickness are shown in
(44) TABLE-US-00001 TABLE 1 Plate Depression-protrusion Protrusion area thickness ratio L difference (mm) percentage (%) Example 1 4.0 0.06 80 Example 2 2.3 0.06 80 Example 3 1.5 0.06 80 Example 4 4.0 0.20 55 Example 5 2.3 0.20 55 Example 6 1.5 0.20 55 Comparative 1.5 Example 1 Comparative 9.0 Example 2
(Tests for Evaluating Heat Transfer Properties)
(45) Tests for evaluating a heat transfer rate were performed according to the following procedure. A test piece having a standardized and predetermined surface area (A) and thickness (B) was produced, and thermocouples were each attached to either surface thereof, i.e., either a front or back surface thereof. Then, the test piece was heated on an electromagnetic cooker at a constant power (E) to measure temperature at the both surfaces, i.e., the front and back surfaces of the test piece. A temperature difference (D) was obtained from the measured temperature values, and a heat transfer rate (C) was computed by the following equation (2). The larger is the heat transfer rate (C), the larger is the amount of heat transferred from a heated side to a non-heated side through a test piece. Therefore, a larger heat transfer rate indicates that heat transfer is facilitated.
C=(EB)/(AD)Equation (2)
(46) In the heating test, a square test piece with a side length of 50 mm was cut out from a depression-protrusion clad steel plate having a depression-protrusion pattern, and this was placed on an electromagnetic cooker set at a power of 500 W, and then heated until a heated surface of the test piece reached a target temperature. The target temperature was set at 100 C., 300 C., and 500 C. because a heat transfer rate changes depending on heating temperature.
(47) Heat transfer properties were evaluated based on the computed heat transfer rate (W/m.Math.K). The evaluation results are shown in Table 2. Evaluation criteria were as follows: those having a heat transfer rate improved by 50% or more relative to Comparative Example 1 were designated as very good; those improved by 25% or more but less than 50% were designated as good; those improved by 5% or more but less than 25% were designated as fair; and those improved by less than 5% were designated as poor.
(48) (Tests for Evaluating Workability)
(49) Workability was evaluated according to the following procedure. A rectangular test piece with a longer side length of 50 mm and a shorter side length of 20 mm was cut out from a depression-protrusion clad steel plate having a depression-protrusion pattern. The above rectangular test piece was subjected to contact bending at the center portion of the longer side thereof, and then the presence or absence of a crack at the working site around the center portion was visually observed for evaluation. The evaluation results are shown in Table 2. A test piece having no observable crack was designated as good; those having an observable crack was designated as poor.
(50) TABLE-US-00002 TABLE 2 Evaluation of thermally conductivity 100 C. 300 C. 500 C. Heat Heat Heat transfer transfer transfer rate rate rate Evaluation (W/m .Math. (W/m .Math. (W/m .Math. of K) Evaluation K) Evaluation K) Evaluation workability Example 1 53.7 very 50.5 good 44.2 good good good Example 2 43.2 fair 41.6 fair 37.9 fair good Example 3 37.6 fair 36.6 fair 33.7 fair good Example 4 56.7 very 53.3 very 46.6 good good good good Example 5 45.6 good 43.9 good 40.0 good good Example 6 39.7 fair 38.7 fair 35.6 fair good Comparative 35.7 34.8 32.0 good Example 1 Comparative 61.0 very 60.0 very 42.0 good poor Example 2 good good
(Evaluation Results of Thermal Conductivity)
(51) As shown in Table 1, Examples 1 to 6 are depression-protrusion clad steel plates each having a depression-protrusion pattern formed on a surface of a steel plate and having a plate thickness ratio L of 1.0 to 5.0. As shown in Table 2, the depression-protrusion clad steel plates from Examples 1 to 6 were found to have better thermal conductivity as compared with the clad steel plate having no depression-protrusion pattern from Comparative Example 1.
(52) A depression-protrusion clad steel plate, which is a composite material, has a heat transfer property in which a thermal gradient varies across the plate thickness direction. When the heat transfer rate of the base material (SPCC) is compared with that of the mating materials (SUS304), the heat transfer rate of SUS304 is smaller than that of SPCC. This means that the thermal gradient 1 of the mating materials (stainless steel)>the thermal gradient 2 of the base material (carbon steel).
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(55) As described above, a depression-protrusion clad steel plate having better thermal conductivity can be obtained when a depression-protrusion pattern having a large depression-protrusion difference and a small protrusion area percentage is formed on a surface of the clad steel plate, and further a base material having a large heat transfer rate such as carbon steel is used so as to have a high plate thickness ratio.
(56) (Evaluation Results of Workability)
(57) Results from workability evaluation by contact bending are shown in Table 2 for the depression-protrusion clad steel plates from Examples and the clad steel plates from Comparative Examples. Examples 1 to 6 and Comparative Example 1 did not show a crack in stainless steel plates as the mating materials. In contrast, Comparative Example 2 showed a crack in stainless steel at the outer side of the test piece which was bent. Comparative Example 2 has a plate thickness ratio (carbon steel/stainless steel) of 9.0 and a relatively small thickness of the mating materials (stainless steel). When contact bending is performed on a test piece, the tensile stress exerted on the surface of a test piece will concentrate on a mating material. Therefore, the concentrated stress exerted on the test piece of Comparative Example 2 presumably exceeded the mechanical strength of the mating material (stainless steel), resulting in a crack. Further, contact bending was found to be possible when the plate thickness ratio (carbon steel/stainless steel) was 7.0 or less.
(58) As described above, the product value was able to be increased, for example, good thermal conductivity was obtained, and crack development upon working was prevented, when the conditions of the present invention were satisfied.
EXPLANATION OF REFERENCE NUMERALS
(59) 1, 3 Three-layer clad steel plate having no depression-protrusion pattern 2 Depression-protrusion clad steel plate 11, 21, 31 Carbon steel 12, 13, 22, 23, 32, 33 Stainless steel 24 Depressed portion 25, 26 Protruded portion B Plate thickness of clad steel plate SP, SP Thickness of carbon steel SU, SU Thickness of stainless steel SP Thickness of carbon steel at depressed portion SU Thickness of stainless steel at depressed portion t1, t1, t1 Temperature at heated surface t0, t0, t0 Temperature at surface opposite to heated surface D, D, D Difference between temperatures of heated surface and surface opposite to heated surface X Heated surface Z Heating direction 1 Thermal gradient in stainless steel 2 Thermal gradient in carbon steel 40 Upper work roll (stepped roll) 41 Lower work roll (flat roll) 42 back-up roll 43 back-up roll 44 Pay-off reel 45 take-up roll 46 Three-layer clad steel plate having no depression-protrusion pattern 47 Depression-protrusion clad steel plate having depression-protrusion pattern