Abstract:
A roll of which surface cracks are hardly caused under the condition of repetitive heating and cooling. A roll comprises that the alloy consisting of no more than 0.10 percent by weight of carbon, 10˜14 percent by weight of chromium, 0.1˜1.0 percent by weight of molybdenum, 0.5˜2.0 percent by weight of cobalt and essentially balanced iron is coated on the surface of a roll body consisting of low alloy or carbon steel by build-up welding. 
     Therefore, build-up welding layer of the above-mentioned compositions excel in view of resistance to corrosion, and that fact is related with a long-life of a roll.

Description:
A roll having a built-up weld layer thereon. 
     BACKGROUND OF THE INVENTION 
     The present invention relates to a high order of durable roll. In the cases of a roll which is used at hightemperature ranges such as a hot rolling process or a continuous casting process, its strength, toughness and resistance to corrosion at high temperature ranges are required for the roll. As the material of a roll or the material which is formed as a built-up weld layer on the surface of a roll used at high temperature ranges, an alloy steel containing 10˜14 percent by weight of chromium is generally used. However, the aforesaid alloy steel containing 10˜14 percent by weight of chromium does not have enough resistance to repetitive thermal stress, and there are defects which appear when the surface of a roll such as a continuous casting roll sustains continuously repetitive heating and cooling treatment such as cracks which lead to the breakdown of the roll as a consequence of the thermal stress. 
     SUMMARY OF THE INVENTION 
     It is an object of the present invention to provide a high order of durable roll. Another object of the invention is to provide a high order of durable roll especially at high temperature ranges. These objects of the present invention are achieved with an alloy having excellent toughness, resistance to heat, to corrosion, and to repetitive thermal stress. The aforementioned alloy consisting of no more than 0.10 percent by weight of carbon, 10˜14 percent by weight of chromium, 0.1˜1.0 percent by weight of molybdenum, 0.5˜2.0 percent by weight of cobalt and the balance essentially iron, is deposited on the surface of a steel roll body by build-up welding. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a perspective view in accordance with the present invention partially broken away; 
     FIG. 2 is a front view, presenting the shape and size of a test piece for the high-temperature tension test; 
     FIG. 3 is a perspective view, presenting the shape and size of a test piece for the repetitive thermal impact test; 
     FIG. 4 and FIG. 5 show the method of the repetitive thermal impact test; 
     FIG. 6 to FIG. 10 show graphs, presenting the changes of various mechanical properties which accompany the changes of Cr and Co quantities; and 
     FIG. 11 to FIG. 18 show photomicrostructures of the surface condition of test pieces No. 1 to No. 8 after the repetitive impact test. 
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     The roll of the present invention is comprised of a roll body (1) and a built-up weld layer (2) which is welded on the surface of the roll body as shown in FIG. 1. The roll body (1) consists of a low alloy carbon steel and the built-up weld layer (2) consists of an alloy having a composition of no more than 0.10 percent by weight of carbon, 10˜14 percent by weight of chromium, 0.1˜1.0 percent by weight of molybdenium, 0.5˜2.0 percent by weight of cobalt and the balance essentially iron. The experiments for achieving the present invention and their results are shown in the following. 
     Test Pieces 
     Firstly, a built-up weld layer having various component compositions as shown in Table 1, is formed on a steel plate substrate (JIS G3101 SS41) by the multi-layer welding method, and then test pieces after the post weld heat treatment at 625° C. for 2 hours, are prepared for the tension test, the impact test, the hardness test, the high-temperature tension test and the repetitive thermal impact test. Therefore, as regards the shape and size of the above-mentioned test pieces, JIS Z2202, No. 14 test piece (6 mm in diameter) was used for the tension test, and JIS Z2202, No. 4 test piece (5 mm in width) for the impact test. Also, a test piece of the shape and size of FIG. 2 was used for the hightemperature tension test. A test piece as shown in FIG. 3 was used for the repetitive thermal impact test; the built-up layer (2&#39;) of 10 mm thickness was coated on a steel plate substrate of SS41 (1&#39;). 
     Repetitive Thermal Impact Test 
     As to the repetitive thermal impact test for testing resistance to cracks, one set of two induction coils was placed slightly separated from the surface of a test piece as shown in FIG. 4. Then the test piece was subjected to repeated cycles of heating and cooling 1,000 times as shown in FIG. 5, and after that, the surface condition of the test piece was observed. 
     
                       TABLE 1______________________________________(% by weight)No.  C      Si     Mn   P    S    Ni   Cr   Mo   Co______________________________________1    0.06   0.70   1.55 0.011                        0.009                             0.02 10.59                                       0.03 --2    0.06   0.63   0.73 0.018                        0.010                             0.02 10.22                                       0.67 0.743    0.07   0.67   0.71 0.021                        0.012                             0.02 10.37                                       0.76 1.564    0.05   0.69   1.83 0.012                        0.009                             0.03 12.54                                       0.02 0.015    0.05   0.59   0.71 0.017                        0.012                             0.03 13.01                                       0.59 0.756    0.05   0.62   0.73 0.020                        0.014                             0.06 12.32                                       0.61 1.637    0.08   0.61   0.71 0.020                        0.013                             0.02 10.77                                       0.04  0.0148    0.08   0.69   0.45 --   --   0.16 9.01 --   --______________________________________ 
    
     The Results Of Each Test 
     The mechanical properties of each test piece are shown in the following Table 2. 
     
                                           TABLE 2__________________________________________________________________________room temperature high temperature σB                            high temperature φNo.   σB δ    φ       Hv IV            500° C.                600° C.                    700° C.                        800° C.                            500° C.                                600° C.                                    700° C.                                        800° C.__________________________________________________________________________1  68.2  5.0    55.7       221          2.1            45.1                36.6                    23.6    51.5                                59.9                                    81.22  68.4 11.8    51.0       238          4.2            46.9                39.7                    25.9                        15.9                            44.7                                50.4                                    69.0                                        84.73  73.0 15.3    54.4       239          2.8            50.5                42.5                    28.0                        16.1                            51.9                                58.3                                    72.8                                        74.64  55.3 21.0    43.2       192          1.9            35.7                28.9                    17.6                        11.0                            44.8                                50.8                                    75.5                                        83.75  59.7 17.5    38.8       206          2.9            41.3                33.7                    22.5                        14.1                            41.0                                48.7                                    68.0                                        81.96  59.3 19.3    45.4       210          2.2            40.5                33.5                    22.3                        13.2                            40.4                                44.8                                    64.0                                        79.07  66.0 16.7    49.8  2.7            44.0                36.2                    24.0                        13.7                            45.7                                49.9                                    75.0                                        78.88  81.2 15.4    49.0       252          2.1            50.1                41.7                    26.8    43.1                                45.1                                    64.2__________________________________________________________________________ 
    
     In the above identified Table 2, σB presents the tensile strength (Kgf/mm 2 ), δ presents the elongation (%), ψ presents the reduction of area (%), Hv presents Vickers hardness, and IV presents Charpy impact value (Kfgm/cm 2 ), (hereinafter referred to in the same manner). 
     The results of the above-mentioned Table 2, diagrammatically shown in FIG. 6 to FIG. 10, clearly show the effects of the addition of Cr and Co in particular at room temperature. Referring now to FIG. 6 to FIG. 10, &#34; &#34; indicates the case of 10 percent by weight of Cr, &#34; &#34; indicates the case of more than 12 percent by weight of chromium, &#34;Δ&#34; indicates the case of 9 percent by weight of chromium and small sized numbers in the above identified Figures indicate the numbers of the test pieces which are shown in Table 1. 
     Secondly, photomicrostructures of the surface of test pieces (No. 1˜No. 8) after the repetitive thermal impact test are shown in FIG. 11 to FIG. 18. In the case of the 9 percent by weight of chromium test piece, as shown in FIG. 18, surface cracks and corroded grooves along the boundary of weld beads were caused on the test piece by the repetitive thermal impact test. Therefore, at least 10 percent by weight of chromium is necessary for resistance to thermal impact cracks and to corrosion. However, with large quantities of chromium, the strength and the toughness seen to become law as indicated in FIG. 6 to FIG. 10. Also, the effects on the improvement of the mechanical properties by adding cobalt are not observed. Hereby it is proved that no more than 14 percent by weight of chromium is a desirable chromium quantity. 
     Next, cobalt is used for the improvement of the mechanical properties, especially resistance to the occurrence of surface cracks by repetitive heating and cooling, and resistance to roughness on the surface as shown in Table 2 and FIG. 11 to FIG. 18. That is to say, the roughness on the surface of a roll is observed to be pronounced in test pieces (FIG. 11, 14, 17 and 18) which essentially do not contain cobalt, and in particular in a test piece (FIG. 18) which contains a small quantity of chromium, cracks were caused along weld beads. On the other hand, the occurrence of surface cracks is not observed in the materials containing cobalt which were used for the built-up layer of the present invention (FIGS. 12, 13, 15 and 16), and also it is proved that roughness on the surface is hardly observed. However, as regards more than 2.0 percent by weight for the addition of cobalt, it can hardly be expected that the effects of adding a cobalt quantity as clarified in Table 2  and FIG. 6 to FIG. 10, so that 0.5˜2.0 percent by weight of cobalt is a sufficient cobalt quantity. Also 0.1˜1.0 percent by weight of molybdenum is included for the purpose of improving resistance to temper brittleness. Carbon is the component for improving the strength of steel, but in the case of more than 0.10 percent by weight of carbon, its toughness becomes low and weldability is impaired. Therefore, the quantity of carbon is limited to 0.1 percent by weight as the maximum.