NZ196063A - Producing aluminium plated steel sheet - Google Patents
Producing aluminium plated steel sheetInfo
- Publication number
- NZ196063A NZ196063A NZ196063A NZ19606381A NZ196063A NZ 196063 A NZ196063 A NZ 196063A NZ 196063 A NZ196063 A NZ 196063A NZ 19606381 A NZ19606381 A NZ 19606381A NZ 196063 A NZ196063 A NZ 196063A
- Authority
- NZ
- New Zealand
- Prior art keywords
- content
- steel
- temperature
- plated steel
- plating
- Prior art date
Links
- 229910000831 Steel Inorganic materials 0.000 title claims description 67
- 239000010959 steel Substances 0.000 title claims description 67
- 229910052782 aluminium Inorganic materials 0.000 title claims description 11
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 9
- 239000004411 aluminium Substances 0.000 title 1
- 230000003647 oxidation Effects 0.000 claims description 28
- 238000007254 oxidation reaction Methods 0.000 claims description 28
- 238000007747 plating Methods 0.000 claims description 21
- 239000000203 mixture Substances 0.000 claims description 16
- 238000000034 method Methods 0.000 claims description 12
- 238000000137 annealing Methods 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 9
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 7
- 238000005098 hot rolling Methods 0.000 claims description 7
- 238000009849 vacuum degassing Methods 0.000 claims description 7
- 230000001590 oxidative effect Effects 0.000 claims description 6
- 239000000126 substance Substances 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 238000005554 pickling Methods 0.000 claims description 4
- 238000005097 cold rolling Methods 0.000 claims description 3
- 238000009749 continuous casting Methods 0.000 claims description 3
- 238000007670 refining Methods 0.000 claims description 3
- 238000005266 casting Methods 0.000 claims description 2
- 241001125671 Eretmochelys imbricata Species 0.000 claims 1
- 239000000463 material Substances 0.000 description 18
- 230000000052 comparative effect Effects 0.000 description 13
- 239000000758 substrate Substances 0.000 description 11
- 208000021017 Weight Gain Diseases 0.000 description 10
- 230000004584 weight gain Effects 0.000 description 10
- 235000019786 weight gain Nutrition 0.000 description 10
- 230000000694 effects Effects 0.000 description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 7
- 239000010410 layer Substances 0.000 description 7
- 230000032683 aging Effects 0.000 description 6
- 238000010791 quenching Methods 0.000 description 6
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 238000009628 steelmaking Methods 0.000 description 4
- 238000005054 agglomeration Methods 0.000 description 3
- 230000002776 aggregation Effects 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 230000015556 catabolic process Effects 0.000 description 3
- 238000006731 degradation reaction Methods 0.000 description 3
- 238000009792 diffusion process Methods 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910001021 Ferroalloy Inorganic materials 0.000 description 1
- 229910000604 Ferrochrome Inorganic materials 0.000 description 1
- 229910000616 Ferromanganese Inorganic materials 0.000 description 1
- 229910001200 Ferrotitanium Inorganic materials 0.000 description 1
- 229910001327 Rimmed steel Inorganic materials 0.000 description 1
- 238000003723 Smelting Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- DALUDRGQOYMVLD-UHFFFAOYSA-N iron manganese Chemical compound [Mn].[Fe] DALUDRGQOYMVLD-UHFFFAOYSA-N 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
Classifications
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0278—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular surface treatment
-
- 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
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/024—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by cleaning or etching
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0273—Final recrystallisation annealing
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Coating With Molten Metal (AREA)
- Heat Treatment Of Steel (AREA)
Description
New Zealand Paient Spedficaiion for Paient Number 1 96063
1960 6 3
Patents Form No. 5
NEW ZEALAND PATENTS ACT 195 3 COMPLETE SPECIFICATION
"A PROCESS FOR PREPARING ALUMINUM-PLATED STEEL SHEETS HAVING LOW YIELD STRENGTH AND HIGH OXIDATION RESISTANCE"
i/WE NISSHIN STEEL COMPANY, LTD., a joint stock company of Japan, located at 4-1 Marunouchi 3-Chome, Chiyoda-ku, Tokyo Japan hereby declare the invention, for which -I-/we pray that a patent may be granted to me/us, and the method by which it is to be performed, to be particularly described in and by the following statement
(fotlowtxi by pzgt | A >
- 1A-
19606
Title of the Invention
A process for preparing aluminum-plated steel sheei having low yield strength and high oxidation resistance Technical Field of the Invention 5 This invention relates to a process for preparing molten-aluminum-plated steel sheets which have low yield strength and exhibit low oxidation weight gain when subjected to oxidation at high temperatures.
Background of the Invention 10 Heretofore, molten-aluminum-plated steel sheets
(hereinafter simply referred to as "aluminum-plated steel sheets") for use wherein heat resistance and corrosion resistance are required have been mainly made of cold-rolled sheets of low carbon rimmed steels. However, it 15 is well known that aluminum-plated steel sheets made of rimmed steel substrate sheets incur degradation in quality due to quench aging caused by rapid cooling at the time of plating, which hardens the material.
The main measures that can be employed to prevent 20 the above mentioned degradation are:
(1) To use substrate sheets made of a steel from which C and N, which cause quench aging, have been removed as completely as possible;
(2) To add a carbide-forming element such as Ti to fix 2 5 C and N in the substrate material, which cause quench aging;
)
(3) To effect over-aging of the aluminum-plated sheets in which quench aging has occurred;
1960:3
and so forth.
However, the measure (1) is not economical in the case when steel sheets are plated by the in-line annealing type hot dip plating apparatus with a non oxidizing furnace, although it can be realized in the ordinary steel-making process by employment of decarburizing annealing.
The measure (2) is economical per se, but when it is applied to low carbon steels which are to be obtained by the ordinary converter process only, a considerable amount of Ti must be used and highly oxidizable Ti produces not a small amount of oxide inclusion which results in degradation of the surface quality of the product. Therefore, this measure is not, in the final analysis, either economically or technically desirable.
The measure (3) is economical. But this treatment may increase the Fe-Al alloy layer, which has poor formability, even if the aluminum plating has been carried out under the conditions that control formation of the Fe-Al alloy layer. Therefore, by this treatment, although the property of the substrate material is improved, the formability of the aluminum-plated layer is impaired.
There has previously been disclosed a process for preparing aluminum-plated steel sheets comprising: hot-rolling a steel essentially consisting of C: 0.001 -0.020 %, Si: £0.05^, Mn« 0.05 - O.kO %, Cr: 0.10 - 0.30 effective Ti (total Ti less Ti in the oxide form): 0.03 -0.^0 fc and that not less than 4 times (C + N) N: ^ 0.006 $,
. • '060CZ
0: 1 0.020 %, and the balance of Fe and inevitable incidental impurities at a temperature not lower than 800°C; cold-rolling the hot coil at a reduction rate of 40 % or more; annealing the rolled sheet at 800-950 C, and immersing the sheet in an Al-Si alloy bath (Si:£ 10%) maintained at 640 — 700°C for not more than 10 minutes.
The aluminium-plated steel sheet obtained by
2
this process has a yield point strength of 13-17 kg/mm and an elongation of 44-47% in the state of a cold-rolled sheet of 0.8 mm thickness. Today, however, demand for more easily formable materials is rising.
Disclosure of the Invention
We have, studied ways for meeting this demand and have arrived at the idea of employing the following three measures to obtain improved aluminium-plated steel sheets which have good formability with low yield strength and are very low in the high temperature oxidation weight gain.
(1) To lower the content of C and 0 in the substrate steel sheet by employing vacuum degassing treatment and preliminary deoxidizing with A1 in the stage of steel-making and thus reducing the Ti content which is necessary to fix C and N and controlling formation of oxides.
(.2) To reduce the content of Mn which raises yield strength and to add Cr which lowers yield strength.
(3) To promote agglomeration and growth of the
N.Z. PATENT OFFICE
2 t OCT 1983
RECEIVED
precipitated Ti carbide by coiling the finished hot coil at a'temperature as high as 700°C and thus to preventing hardening by formation of carbide of the Ti added to the substrate material. And to further promotion of agglomeration of the Ti carbide by heating the cold-rolled sheet at a temperature of 850° C or more when it is passed through an in-line annealing type hot dip plating apparatus with a non-oxidizing furnace (which is commonly called NOF type plating apparatus in Japan).
Additionally, the invention of this application is characterized in that high temperature oxidation resistance of the material is improved by combined addition of Ti and Cr. That is, oxidation weight ^in at high temperatures is remarkably reduced by decarburizing the substrate material, and it is further improved by addition of Ti. The reasons are: (1) By decarburizing or addition of Ti, cleanliness of the iron material is improved, and Al of the aluminum layer easily diffuses into the Fe substrate and an Al diffusion layer, having excellent high temperature oxidation resistance is formed; and (2) The Ti in the material diffuses toward the surface and forms a Ti-concentrated layer under the Al diffusion layer when the material is subjected to high temperature, and thus prevents the further diffusion of Al into the interior, thereby retarding decrease in the Al concentration in the surface layer, and also fixes oxygen which has penetrated into the iron.
Thus according to this invention a process for preparing molten-aluminum-plated steel sheets having
I 96063
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Vi" j improved yield strength and resistance to high-temperature oxidation comprising: producing a steel the chemical composition of which essentially consisting of C: 0.001 -0.020 %, Mn: 0.05 - 0.30 %, Cr: 0.05 - 0.^0%, Al: 0.01 -0.10 %, Ti: 0.10 - 0.50 % and that not less than 10 times the precentage of C, the balance consisting of Fe and inevitable incidental impurities, by the ordinary converter-refining and vacuum degassing; making it into a slab by the ordinary casting and slabbing or the ordinary continuous casting; continuously hot-rolling said slab coiling it at a temperature not lower than 70°°C; cold-rolling the resulting hot coil after the ordinary pickling treatment; heating the cold-rolled sheet at a temperature not lower than 850°C; and plating it with molten aluminum by means of an in-lining annealing type hot dip plating apparatus with a non-oxidizing furnace is provided.
In the preferred embodiment, the C content is 0c001 - 0.010 %, the Mn content is 0.05 - 0.20 %, the Cr content is 0.07 - 0.4-5 %t the Al content is 0.02 -0.05 %, and the Ti content is 0.15 - 0.40 % and not less than 20 times the C content.
In the more preferred embodiment, the C content is 0.001 - 0.007 %* the Mn content is 0.10 - 0.I7 %, the Cr content is 0.07 - 0.42 %, the Al content is 0.03 - 0.041 %, and the Ti content is 0.19 - 0.23 % and not less than 30 times the C content, the hot coil coiling temperature is
I
720 - 730°C and the heating temperature at plating is 860 - 900°C.
J 960^3
The reasons for the numerical limitations defined in the main claim are as follows.
The lower the carbon content is, the more the effect of quench aging is reduced. Therefore, it is 5 desirable to reduce the C content as much as possible. But it is not easy to reduce the C content to less than 0.001 % even by the modern steel-making process in which vacuum degassing is employed. Even if it can be achieved, it is not an economical operation. Therefore, the lower 10 limit of the C content is defined as 0.001 %. The reason why its upper limit is defined as 0.020 % is that if the C content is over this limit, the amount of Ti to be added for prevention of the undesirable effect of C inducing quench aging must be uneconomically increased. 15 The reason for defining the Mn content as 0.05 -
O.30 % is that it is difficult to obtain a steel the Mn content of which is less than 0.05 % by the ordinary steel-making process and when the Mn content exceeds 0.30 %, the steel becomes hard and, as a consequence, has high yield 20 strength.
The reason for defining the Cr content as 0.05 -0.50 % is that Cr in the amount of less than 0.05 % does not give sufficient effect in reducing yield ratio, and on the other hand, more than 0.50 % of Cr also reduces 25 said effect.
Al is used for deoxidation of the molten steel and, especially in this invention, it plays an important role as the preliminary deoxidation material which prevents
1960 6 3
wasteful use of Ti. From this point of view, the lower limit of the Al content is defined as 0.01 %. However,
if Al is added in an amount over 0.10 %, the surface properties and formability of the resulting steel sheet are impa ired.
The reason why the Ti content is defined as 0.10 - 0.50 % and 10 times the C content is as follows.
If the Ti content is less than 0.10 %, the effect of improving high temperature oxidation resistance as represented by oxidation weight gain is not sufficient, although the yield strength is rather low. On the other hand, if the Ti content is in excess of 0.50 %, the material becomes hard and loses its low yield strength characteristic,
although the oxidation weight gain becomes smaller. If the Ti content is less than 10 times the C content, the fixation of C with Ti is not sufficient, resulting in a rise in the yield strength and an increase in the oxidation weight gain, which eliminate the characteristics of this invention^
In the process of this invention, Si, P and S as the inevitable impurities can be present to the extent that is ordinary and common in steels of this kind. Nitrogen and 0 can, without any inconveniences, be present at the levels usually attained by the vacuum degassing process.
The reason why the coiling temperature is defined as not lower than 700°C is that at temperature lower than this, softening of the material owing to agglomeration and growth of the Ti precipitate, which has been formed by fixation of C with Ti, is not sufficient, and thus one of the features
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Ltl cc of this invention is lost. Further it is required that in the aluminum plating line the cold-rolled sheet must be heated at not lower than 850°C before entering the plating bath in order to give the cold-rolled sheet an annealing effect so that the Ti precipitate further agglomerates to larger particles and thus softens the material.
In the process of this invention, the composition . of the substrate steel is different from that of the substrates steel of the method of the aforementioned process described at page 2 line 21 to page 3 line 6 only in that the steel of this invention contains Al added intentionally. But the procedure is completely different from that of said invention.
Description of Embodiments of the Invention
Now the invention is explained in detail specifically on the basis of the results of experiments.
Steel samples, the compositions of which are indicated in Table 1, were prepared by converter refining and vacuum degassing. The ingots were subjected to slabbing and continuous hot-rolling and the rolled products were coiled at varied temperatures as indicated therein and hot coils of 2.5 mm thickness were obtained. After ordinary pickling, the hot coils were made into cold-rolled sheets of 0.8 mm thickness. The thus prepared cold-rolled sheets were heated at varied temperatures and plated with aluminum (6Og/m )
by means of an in-line annealing type hot dip plating apparatus
\
with a non-oxidizing furnace (practically, a modified Sendzimir apparatus), under the ordinary conditions. The aluminum-plated
I >' 6 06 3
sheets were subjected to the material test and oxidation test. The results (mechanical properties and oxidation weight gains) are shown in the same table. The material tests were carried out with specimens prepared according to JIS (Japanese Industrial Standards) Z-22 01 No. 5 (available on the Patent Office file) cut in the direction of rolling, and the oxidation test with five repeated runs of a cycle of holding the samples at 830°C in the atmosphere for 48 hours and cooling to room temperature.
In Table 1, samples D, E and F are within the composition range defined in this invention and F is within the scope of the invention in the heating temperature before the plating. This table shows that materials excellent both in formability and oxidation resistance are obtained only when all three factors of the composition of the substrate steel, the coiling temperature and the plating temperature satisfy the conditions defined in this invention.
When sample A and B are compared, it is learned that decrease in the Mn content contributes to lowering of the yield strength. Comparison of B and C shows that addition of Ti contributes to lowering of the yield strength, too. Comparison of C and F shows that combined addition of Ti and Cr also contributes to lowering of the yield strength.
Table 2 shows mechanical properties of the aluminium-plated steel sheet samples which were prepared by obtaining the steels with the compositions indicated therein and treating them in the same way as above.
196063
According to this table, it is learned that Cr is effective for lowering the yield strength when contained in the amount of about 0.05 - 0.50 %.
Table 3 shows mechanical properties and oxidation 5 weight gains of the aluminum-plated steel sheet samples which were prepared by obtaining the steels the compositions of which are indicated therein and treating them in the same way as above. According to this table, it is learned that when the amount of the added Ti is 0.1 % or more and that 10 more than 10 times the amount of C, the effects of lowering the yield strength and oxidation weight gain are achieved. But as seen in sample G, when the Ti content exceeds 0.5 $» the yield strength again rises.
Table 4-2 shows the results of the same tests as 15 above carried out with respect to the samples prepared in the same way as above from steels with the compositions indicated in Table 4-1. According to this table, it is learned that when the coiling temperature is lower than 700°C, the softening of the material is not sufficient, and when the 20 heating temperature before plating is 850°C or higher, the softening is remarkable.
Preferred embodiments of this invention are described below.
Example 1
Ingots, the compositions of which are indicated in Table 5 as sample No. 1 and No. 2, were obtained by vacuum-degassing molten steel prepared by an LD converter so as to reduce the contents of C and 0, and thereafter
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19606 3
adjusting the composition by addition of ferro alloys such as ferrochromium, ferrotitanium, ferromanganese, etc. The ingots were made into slabs and the slabs were hot-rolled into 2.5 mm thick hot coils under the conditions indicated in 5 Table 6. After pickling, the hot coils were cold-rolled into 0.8 mm thick sheets. The cold-rolled sheets were plated with aluminum by means of an in-line annealing type hot dip plating apparatus with a non-oxidizing furnace (a modified Sendzimir apparatus) under the conditions indicated -10 Table 6. The mechanical properties and oxidation weight gain of the thus obtained aluminum plated steel sheets as tested in the same manner as above are shown in Table 6.
Both sheets exhibit excellent properties low yield strength and high oxidation resistance at high temperatures. 15 Example 2
Slabs, the compositions of which are indicated in Table 5 as sample No. 3 and No. 4, were obtained by continuous casting after smelting in the same way as in Example 1. The slabs were made into aluminum-plated steel 20 sheets in the same way as described in Example 1. Mechanical properties and the test results of the thus obtained steel sheets as tested in the same way as in Example 1 are shown in Table 6. These sheets have excellent characteristics comparable to those of the sheets of Example 1.
Industrial Applicability
The products of this invention are suitable for manufacturing parts with complicated shapes used at high temperatures such as exhaust gas treating apparatuses for internal combustion engines.
• • • •
Table 1
Samples
Chemical Composition
(*)
Coiling Temp. in hot rolling
Temp. of cold-
rolled sheets
Mechanical Properties
Oxidation weight gain
Remarks
C
Mn
Ti
Cr
Al
(°C)
at plating (°C)
TS Kg/mm2
YP Kg/mm2
El *
(g/m2)
A
0.007
0.27
-
-
0.03
570
870
34
22
49
182
Comparative steel
B
0.006
0.15
-
-
o.o4
560
880
33
19
49
138
Comparative steel
C
0.007
0.13
0.21
-
0.04
710
890
31
51
78
Comparative steel
D
0.006
0.13
0.23
0.11
0.04
550
890
32
16
48
49
Comparative steel
E -
0.004
0.11
0.20
0.14
0.03
730
810
31
51
47
Comparative steel
F
0.005
0.12
0.23
0.13
0 .04
720
890
31
13
53
43
Invent ion steel
TS : Tensile strength, YP : Yield point strength, El : Elongation
O
o o o
Ul
Table 2
Chemical Composition {%)
Mechanical Properties
Samples
TS
YP
El
Remarks
C
Mn
Ti
Cr
Al
Kg/mm2
Kg/mm2
*
A
0.007
0.14
0.19
-
0.03
32
16
47
Comparative steel
B
0.006
0.15
0.22
0.03
0.05
31
48
Comparative steel
C
0.004
0.17
0.20
0.07
0.04
31
13
51
Invention steel
D
0.005
0.15
0.18
o„16
o.o4
32
13
52
Invent ion steel
E
0.004
0.13
0.19
0.30
0.05
31
14
51
Invention steel
"F
0.007
0.14
0.22
0.42
0.03
32
14
49
Invention steel
G
0.004
0.11
0.19
0.58
0.05
32
17
46
C omparat ive steel
TS : Tensile strength, YP : Yield point strength, El : Elongation sO
O O
o
Table 3
Chemical Composition
(*)
Mechanical Properties
Oxidation we ight ga in
I
Samples
TS
YP
El
Remarks
C
Ti
Cr
Ti/C
Kg/mm2
Kg/mm2
%
g/m2
A
0.016
0.13
0.11
8
34
19
45
118
Comparative: steel
B
0.011
0.12
0 .14
11
32
16
49
61
Invention steel
C
0.007
0.08
CM
t-H
0
11
33
17
48
92
Comparative ! steel !
1
D
0.006
0.18
0.11
13
52
48
Invention steel
E
0.007
0.23
0.15
33
32
14
50
39
Invention steel
F
0.006
0.3^
0.12
57
33
17
49
57
Invention steel
G
0.017
0.56
0.10
33
38
24
41
69
Comparative steel
TS : Tensile strength, YP : Yield point strength, El : Elongation
>0 O
o o i\ 'I
Table 4-1
c
Si
Mn
P
S
Cr
Al
Ti
Ti/C
0.006
0.02
0 .12
0.008
0.006
0.10
0.02?
0.21
Table 4-2
Hot rolling conditions
Temp, of cold-rolled sheets
Mechanical Properties
Oxidation we ight
Finish temp. (°C)
C oiling temp. (°C)
at plating
(°c)
TS Kg/mm2
YP Kg/mm2
El *
gain g/m2
Remarks
850
680
905
33
18
44
89
Comparative steel
830
650
890
33
17
45
101
Comparative steel
840
730
810
32
49
76
Comparative steel
850
720
860
31
13
52
47
Invention steel
860
730
880
13
53
39
Invention steel
TS : Tensile strength, YP : Yield point strength, El : Elongation
Claims (6)
1 0.007 0.02 0 .12 0.009 0.009 0.11 0.028 ON *—i;0;27;2;0.006;0.03;0;.11;0.008;0.007;0.10;0.034;0.21;35;3;0.008;0.04;0;.13;0.009;0.006;o.i4;0.038;0.20;25;4;0.007;0.05;0;.12;0.008;o .007;0.09;0.04l;0.22;31;Table 6;Sample;Hot rolling conditions;1;Temp, of cold-rolled sheets at plating;(°C);Mechanical Properties;Oxidation weight gam g/m2;Finish temp. (°C);Coiling temp.;(°c);TS Kg/mm2;YP Kg/mm2;El fo;1;850;730;900;31;13;50;46;2;830;730;880;30;12;51;48;3;840;720;890;30;13;52;39;4;860;730;880;31;13;51;54;TS : Tensile strength, YP : Yield point strength, El : Elongation;- 17 -;WBAJJ/WE CLAIM Glaime;1. A process for preparing molten-aluminum-plated steel sheets having improved yield strength and resistance to high-temperature oxidation comprising: producing a;5 steel the chemical composition of which essentially consisting of C: 0.001 - 0.020 %, Mn: 0.05 - 0.30 %, Cr: 0.05 - 0.50 %, Al: 0.01 - 0.10 %, Ti: 0.10 - 0.50 % and that not less than 10 times the percentage of C, the balance consisting of Fe and inevitable incidental impurities, 10 by the ordinary converter-refining and vacuum degassing;;making it into a slab by the ordinary casting and slabbing or the ordinary continuous casting; continuously hot-rolling said slab coiling it at a temperature not lower than 700°C; cold-rolling the resulting hot coil after the ordinary 15 pickling treatment; heating the cold-rolled sheet at a temperature not lower than 850°C; and plating it with molten aluminum by means of an in-line annealing type hot dip plating apparatus with a non-oxidizing furnace.;
2. The process as claimed in Claim 1, wherein the;20 C content is 0.001 - 0.010 %, the Mn content is 0.05 - 0.20 %, the Cr content is 0.07 - 0.4-5 the Al content is 0.02 -0.05 %, and the Ti content is 0.15 - 0.40 % and not less than 20 times the C content.;
3. The process as claimed in Claim 2, wherein the C content is 0.001 - 0.007 %, the Mn content*is 0.10 - 0.17 $, the Cr content is 0.07 - 0.42 %, the Al content is 0.03 -0.041 %, and the Ti content is 0.19 - 0.23 % and not less than 30 times the C content, the hot coil coiling temperature 1 9606 - 18 - is 720 - 730°C and the heating temperature at the plating is 860 - 900°C.
4. Molten-Aluminium-plated steel sheets having improved yield strength and resistance to high-temperature oxidation produced by the process as described in any of the preceding claims.
5. A process for preparing molten-aluminium-plated steel sheets having improved yield strength and resistance to high temperature oxidation substantially as hereinbefore described with reference to the Examples.
6. Molten-aluminium-plated steel sheets substantially as hereinbefore described with reference to the Examples. BALDWIN, SON & CAREY, ^ornevs'for'the applicants
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP533380A JPS56102523A (en) | 1980-01-22 | 1980-01-22 | Manufacture of aluminum-plated steel sheet having resistance to oxidation at high temperature |
Publications (1)
Publication Number | Publication Date |
---|---|
NZ196063A true NZ196063A (en) | 1984-02-03 |
Family
ID=11608303
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NZ196063A NZ196063A (en) | 1980-01-22 | 1981-01-21 | Producing aluminium plated steel sheet |
Country Status (15)
Country | Link |
---|---|
JP (1) | JPS56102523A (en) |
AU (1) | AU538073B2 (en) |
BE (1) | BE887191A (en) |
BR (1) | BR8100316A (en) |
CA (1) | CA1178182A (en) |
DE (1) | DE3101850C2 (en) |
DK (1) | DK157690C (en) |
ES (1) | ES498742A0 (en) |
FR (1) | FR2474060A1 (en) |
GB (1) | GB2069001B (en) |
IT (1) | IT1143260B (en) |
NL (1) | NL182414C (en) |
NZ (1) | NZ196063A (en) |
SE (1) | SE449758B (en) |
ZA (1) | ZA8167B (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6013053A (en) * | 1983-07-04 | 1985-01-23 | Nisshin Steel Co Ltd | Aluminized steel sheet with superior strength at high temperature and superior heat resistance |
JPS6043476A (en) * | 1983-08-17 | 1985-03-08 | Nippon Steel Corp | Continuous melt aluminization method |
JPS61177378A (en) * | 1985-02-01 | 1986-08-09 | Nippon Steel Corp | Chromate-treated coated Cr-containing steel sheet with excellent painting performance |
WO2009131233A1 (en) * | 2008-04-22 | 2009-10-29 | 新日本製鐵株式会社 | Plated steel sheet and method of hot-pressing plated steel sheet |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1015231A (en) * | 1971-12-07 | 1977-08-09 | David W. Gomersall | Aluminum coated steel |
US3881880A (en) * | 1971-12-07 | 1975-05-06 | Inland Steel Co | Aluminum coated steel |
DE2264519A1 (en) * | 1972-11-13 | 1974-05-22 | Toyo Kogyo Co | Aluminising treatment for automobile mufflers - improve high temp. corro-sion resistance as well as giving oxidn. resistance |
US3881882A (en) * | 1973-04-19 | 1975-05-06 | Inland Steel Co | Aluminum coated steel |
US3905780A (en) * | 1973-06-25 | 1975-09-16 | Armco Steel Corp | Oxidation-resistant low alloy steel with Al coating |
JPS5135532A (en) * | 1974-09-20 | 1976-03-26 | Sumitomo Shipbuild Machinery | KAATSUSENKANSHI KISAIDEIHO |
JPS582248B2 (en) * | 1976-09-16 | 1983-01-14 | 日新製鋼株式会社 | Manufacturing method for hot-dip galvanized steel sheet with excellent workability |
US4144379A (en) * | 1977-09-02 | 1979-03-13 | Inland Steel Company | Drawing quality hot-dip coated steel strip |
-
1980
- 1980-01-22 JP JP533380A patent/JPS56102523A/en active Granted
-
1981
- 1981-01-06 ZA ZA00810067A patent/ZA8167B/en unknown
- 1981-01-07 NL NLAANVRAGE8100030,A patent/NL182414C/en not_active IP Right Cessation
- 1981-01-09 IT IT67019/81A patent/IT1143260B/en active
- 1981-01-16 AU AU66291/81A patent/AU538073B2/en not_active Ceased
- 1981-01-19 DK DK022381A patent/DK157690C/en active
- 1981-01-20 FR FR8100958A patent/FR2474060A1/en active Granted
- 1981-01-20 SE SE8100310A patent/SE449758B/en not_active IP Right Cessation
- 1981-01-20 CA CA000368870A patent/CA1178182A/en not_active Expired
- 1981-01-21 NZ NZ196063A patent/NZ196063A/en unknown
- 1981-01-21 DE DE3101850A patent/DE3101850C2/en not_active Expired
- 1981-01-21 GB GB8101817A patent/GB2069001B/en not_active Expired
- 1981-01-21 BR BR8100316A patent/BR8100316A/en unknown
- 1981-01-22 ES ES498742A patent/ES498742A0/en active Granted
- 1981-01-22 BE BE0/203568A patent/BE887191A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
ES8204477A1 (en) | 1982-05-01 |
SE449758B (en) | 1987-05-18 |
FR2474060B1 (en) | 1984-06-01 |
IT1143260B (en) | 1986-10-22 |
GB2069001A (en) | 1981-08-19 |
FR2474060A1 (en) | 1981-07-24 |
DK22381A (en) | 1981-07-23 |
BE887191A (en) | 1981-07-22 |
NL8100030A (en) | 1981-08-17 |
NL182414C (en) | 1988-03-01 |
GB2069001B (en) | 1983-06-02 |
NL182414B (en) | 1987-10-01 |
AU538073B2 (en) | 1984-07-26 |
IT8167019A0 (en) | 1981-01-09 |
BR8100316A (en) | 1981-08-11 |
JPS633929B2 (en) | 1988-01-26 |
SE8100310L (en) | 1981-07-23 |
JPS56102523A (en) | 1981-08-17 |
DE3101850A1 (en) | 1981-11-19 |
DK157690C (en) | 1990-07-02 |
ZA8167B (en) | 1982-03-31 |
DK157690B (en) | 1990-02-05 |
AU6629181A (en) | 1981-07-30 |
CA1178182A (en) | 1984-11-20 |
DE3101850C2 (en) | 1983-12-22 |
ES498742A0 (en) | 1982-05-01 |
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