US2082783A - Method of making alloy steels - Google Patents
Method of making alloy steels Download PDFInfo
- Publication number
- US2082783A US2082783A US42861A US4286135A US2082783A US 2082783 A US2082783 A US 2082783A US 42861 A US42861 A US 42861A US 4286135 A US4286135 A US 4286135A US 2082783 A US2082783 A US 2082783A
- Authority
- US
- United States
- Prior art keywords
- titanium
- lime
- aluminum
- chromium
- carbon
- 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.)
- Expired - Lifetime
Links
- 229910000831 Steel Inorganic materials 0.000 title description 7
- 239000010959 steel Substances 0.000 title description 7
- 229910045601 alloy Inorganic materials 0.000 title description 6
- 239000000956 alloy Substances 0.000 title description 6
- 238000004519 manufacturing process Methods 0.000 title description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 26
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 23
- 239000004571 lime Substances 0.000 description 20
- 235000008733 Citrus aurantifolia Nutrition 0.000 description 19
- 235000011941 Tilia x europaea Nutrition 0.000 description 19
- 229910052782 aluminium Inorganic materials 0.000 description 19
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 19
- 239000002893 slag Substances 0.000 description 19
- 229910052804 chromium Inorganic materials 0.000 description 17
- 239000011651 chromium Substances 0.000 description 17
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 16
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 16
- 229910052719 titanium Inorganic materials 0.000 description 16
- 239000010936 titanium Substances 0.000 description 16
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 15
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 13
- 229910052799 carbon Inorganic materials 0.000 description 13
- 229910052759 nickel Inorganic materials 0.000 description 13
- 229910052751 metal Inorganic materials 0.000 description 12
- 239000002184 metal Substances 0.000 description 12
- 238000007792 addition Methods 0.000 description 9
- 239000000203 mixture Substances 0.000 description 9
- 230000001590 oxidative effect Effects 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 239000000155 melt Substances 0.000 description 6
- 150000002739 metals Chemical class 0.000 description 6
- 239000012530 fluid Substances 0.000 description 5
- ODINCKMPIJJUCX-UHFFFAOYSA-N Calcium oxide Chemical compound [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 4
- 229910000640 Fe alloy Inorganic materials 0.000 description 4
- 229910001021 Ferroalloy Inorganic materials 0.000 description 4
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- HMDDXIMCDZRSNE-UHFFFAOYSA-N [C].[Si] Chemical compound [C].[Si] HMDDXIMCDZRSNE-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 235000012255 calcium oxide Nutrition 0.000 description 2
- 239000000292 calcium oxide Substances 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 239000005997 Calcium carbide Substances 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- XFWJKVMFIVXPKK-UHFFFAOYSA-N calcium;oxido(oxo)alumane Chemical compound [Ca+2].[O-][Al]=O.[O-][Al]=O XFWJKVMFIVXPKK-UHFFFAOYSA-N 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 1
- -1 chromium carbides Chemical class 0.000 description 1
- 239000010436 fluorite Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000010079 rubber tapping Methods 0.000 description 1
- CLZWAWBPWVRRGI-UHFFFAOYSA-N tert-butyl 2-[2-[2-[2-[bis[2-[(2-methylpropan-2-yl)oxy]-2-oxoethyl]amino]-5-bromophenoxy]ethoxy]-4-methyl-n-[2-[(2-methylpropan-2-yl)oxy]-2-oxoethyl]anilino]acetate Chemical compound CC1=CC=C(N(CC(=O)OC(C)(C)C)CC(=O)OC(C)(C)C)C(OCCOC=2C(=CC=C(Br)C=2)N(CC(=O)OC(C)(C)C)CC(=O)OC(C)(C)C)=C1 CLZWAWBPWVRRGI-UHFFFAOYSA-N 0.000 description 1
- 229910003470 tongbaite Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
- C21C7/00—Treating molten ferrous alloys, e.g. steel, not covered by groups C21C1/00 - C21C5/00
Definitions
- This invention relates to the. manufacture of corrosion resisting ferro-alloys, particularly of the austenitic stainless steel type, and has for its object to prevent the formation of undesirable carbides and in general toimprove the quality lime and fluorspar.
- the melt is practically free of carbon the oxidizing slag is removed and the bath is covered with a mixture of burnt lime and either titanium oxide or rutile. As soon as this mixture becomes fluid there is charged into of the product.
- alloys of the type menture of lime, aluminum in the form of shot or tioned usually containing approximately 18 per turnin and rutile- T e quantity of titanium cent chromium and 8 per cent nickel, be free from desire which p ds upon t e car t.
- titanium is usually the metal added to the alloys of the type to prevent formation of be had by increasing the aluminum content but 35 as the latter is more costly than titanium oxide chroimum carbide, and for this purpose the titath e aluminum ratio is kept low.
- a ro of making ferrous alloys contain- 55 ing substantially 18 per cent chromium and 8 per cent nickel, the remainder being predominantly iron, which comprises refining molten steel under an oxidizing slag, removing the slag and covering the bath with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-silicon-containing material, then after said covering has become fluid adding titanic oxide, burnt lime, and aluminum in proportions having the ratio 2 :1:1, respectively, then adding chromium and nickel at intervals to supply the desired percentages of these two metals, with further additions of small quantities of-lime and aluminum after each addition of chromium and nickel, and titanic oxide if necessary to maintain the said ratio, the quantity of titanic oxide supplied being such that the percentage of titanium ranges from the quantity thereof necessary to form carbide with the carbon in the metal in excess of the carbon held in solution up to 4 per cent of the total metal.
- a process of making ferrous alloys containing substantially 18 per cent chromium, 8 per cent nickel and up to 4 per cent titanium, the remainder being predominantly iron which comprises covering a bath of molten steel, that has been treated under an oxidizing slag, with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-silicon-containing material, then after said covering has become fluid adding titanic oxide, lime and aluminum in proportions having the ratio 2 :1:1, respectively, then adding chromium and nickel in the form of ferro alloys at intervals to supply the desired percentages of these two metals, with further additions of small quantities of lime and aluminum, and also titanic oxide if necessary to maintain the said ratio after each addition of chromium and nickel, the quantity of titanic oxide supplied being more than that necessary to form a carbide with the carbon present in excess of 0.02 per cent and less than will leave in the alloy titanium substantially in excess of 4 per cent.
- a process of making ferrous alloys containing nickel and chromium which comprises covering a bath of molten steel, that has been treated under an oxidizing slag, with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-siliconcontaining material, then after said covering has become fluid adding titanium oxide, lime and aluminum in proportions having the ratio 2 :1: 1, respectively, then adding chromium and nickel in the form of ferro alloys at intervals to supply the desired percentages of these two metals, with further small quantitiesof lime and aluminum, and also titanium oxide if necessary to maintain the said ratio, after each addition of chromium and nickel.
- a process of making ferrous alloys containing nickel and chromium which comprises covering a bath of molten steel, that has been treated under an oxidizing slag, with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-siliconcontaining material, then after said covering has become fluid adding titanium oxide, lime and aluminum in proportions having the ratio 2 :1: 1, respectively, then adding chromium and nickel in the form of ferro alloys at intervals to supply the desired percentages- 0f these two metals, with further small quantities of lime and aluminum, also titanium oxide if necessary to maintain thesaid ratio, after each addition of chromium and nickel, adding small quantities of aluminum and titanium oxide until the melt is in satisfactory condition, adding more lime approximately five minutes after the last addition of aluminum and titanium oxide, and then tapping the melt.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Treatment Of Steel In Its Molten State (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
Patented June 8, 1937 METHOD OF MAKING ALLOY STEELS Thomas N. Armstrong, Jr., and Fred B. Anderson, Portsmouth, Va.
No Drawing. Application September 30, 1935, Serial No. 42,861
4 Claims. (Cl. 75-127) (Granted under the act of March 3, 1883, as
amended April 30, 1928; 370 0. G. 757) This invention relates to the. manufacture of corrosion resisting ferro-alloys, particularly of the austenitic stainless steel type, and has for its object to prevent the formation of undesirable carbides and in general toimprove the quality lime and fluorspar. When the melt is practically free of carbon the oxidizing slag is removed and the bath is covered with a mixture of burnt lime and either titanium oxide or rutile. As soon as this mixture becomes fluid there is charged into of the product. the furnace, preferably in small portions, a mix- 5 It is important that alloys of the type menture of lime, aluminum in the form of shot or tioned, usually containing approximately 18 per turnin and rutile- T e quantity of titanium cent chromium and 8 per cent nickel, be free from desire which p ds upon t e car t.
10 oxides and from dissolved gases. The oxides are will determinethe qua i Of titanium de a d ordinarily removed by drawing ofi the oxidizing lime added to the slag. Lime is added in small 10 slag under which the charge has been melted quantiti s as n d d o prevent the Slag from down and refined and replacing it with a basic thinning down too greatly. slag which is, in the final operation, brought to Theoretically, one pound of aluminum will rea reducing condition with carbon, silicon, ferroduce 2.22 pounds of titanium oxide to yield 1.34
silicon, or aluminum. When lime slags are empounds .of titanium. In practice, because of the 15 ployed these agents form calcium carbide, caloxidized condition of the bath after being subcium silicate, and calcium aluminate respectively. je te t0 the oxidizing sla d because Qf the Austenitic steels of the 18-8 type usually concomplexity of the slag formed, it requires more tain more than 0.02 per cent carbon. It is genthan the theoretical quantity of aluminum, and 0 erally accepted that this quantity is the maxialso more than the theoretical quantity of tita- 20 mum that is retained in solution, and all carbon nium oxide to obtain the desired recovery of titain excess thereof unites with chromium to form illm and to keep the slag in a redu d t o chromium carbide. The formation of the chro- Part of the titaniumremains in the slag. It remium carbide impoverishes the iron of chromium quires approximately four times the titanium 5 and makes the metal susceptible to intergranuoxide theoretically necessary. The following ralar corrosion. It has been shown that the formatio, by weight, should be maintained: tion of chromium carbides can be prevented by 7 Part adding to the alloy a suflicient quantity of some Titanium oxide 2% metal having greater affinity for carbon than has Aluminum 1 chromium. Titanium, vanadium, molybdenum Lime 1 ai g gi gfi fi gg fi fig i f g 325 8 223 The slag is calculated on the quantity of titanium th oxide required by the carbon in the melt. A
e most powerful carbide former. For this reaigher percentage of recovery of titanium can son titanium is usually the metal added to the alloys of the type to prevent formation of be had by increasing the aluminum content but 35 as the latter is more costly than titanium oxide chroimum carbide, and for this purpose the titath e aluminum ratio is kept low. mum is added in suificient quantity to insure the A110 1 t l h h d k l f 6 times as much titanium as the cary ng a sue 1 romlmp an me e g g z of 0 02 er cent in the ano The are added in small quantities at a time after the 40 is iisually aided in the form o ferm- Slag is a reducing I} smal-l additim of a mixture of lime and aluminum is usually tttamum or low carbon lmn'chronuum'tlta' madeafter each addition of the alloying metals. mum a These costly as a After the alloying metals have been added small contain some carbon which necessitates adding quantities of the mixture of aluminum and additional titanium to compensate therefor. titanium Oxidev are charged at intervals until 45 Under the present method a reducmg Slag 15 the melt has the desired composition. Approxiformed without carbon or silicon and this slag mately five minutes after t t; addition of reduces titanium from the inexpensive titanium aluminum and t t oxide some lime is oxide, or rutile, which is a titanium oxide ore. charged 't metal is tapped 5 Any desired q y of titanium, p to pe The invention described herein may be manuc t (P a y higher) can be added by this factured for use by or for the Government of the method- United States, without the payment of any royal- We subject the melt to any of the usual oxidizti th reon, ing slags, or if the charge is low in, or practically What i claim d is; I
free from carbon, the charge is melted down with 1, A ro of making ferrous alloys contain- 55 ing substantially 18 per cent chromium and 8 per cent nickel, the remainder being predominantly iron, which comprises refining molten steel under an oxidizing slag, removing the slag and covering the bath with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-silicon-containing material, then after said covering has become fluid adding titanic oxide, burnt lime, and aluminum in proportions having the ratio 2 :1:1, respectively, then adding chromium and nickel at intervals to supply the desired percentages of these two metals, with further additions of small quantities of-lime and aluminum after each addition of chromium and nickel, and titanic oxide if necessary to maintain the said ratio, the quantity of titanic oxide supplied being such that the percentage of titanium ranges from the quantity thereof necessary to form carbide with the carbon in the metal in excess of the carbon held in solution up to 4 per cent of the total metal.
2. A process of making ferrous alloys containing substantially 18 per cent chromium, 8 per cent nickel and up to 4 per cent titanium, the remainder being predominantly iron, which comprises covering a bath of molten steel, that has been treated under an oxidizing slag, with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-silicon-containing material, then after said covering has become fluid adding titanic oxide, lime and aluminum in proportions having the ratio 2 :1:1, respectively, then adding chromium and nickel in the form of ferro alloys at intervals to supply the desired percentages of these two metals, with further additions of small quantities of lime and aluminum, and also titanic oxide if necessary to maintain the said ratio after each addition of chromium and nickel, the quantity of titanic oxide supplied being more than that necessary to form a carbide with the carbon present in excess of 0.02 per cent and less than will leave in the alloy titanium substantially in excess of 4 per cent.
3. A process of making ferrous alloys containing nickel and chromium, which comprises covering a bath of molten steel, that has been treated under an oxidizing slag, with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-siliconcontaining material, then after said covering has become fluid adding titanium oxide, lime and aluminum in proportions having the ratio 2 :1: 1, respectively, then adding chromium and nickel in the form of ferro alloys at intervals to supply the desired percentages of these two metals, with further small quantitiesof lime and aluminum, and also titanium oxide if necessary to maintain the said ratio, after each addition of chromium and nickel.
4. A process of making ferrous alloys containing nickel and chromium, which comprises covering a bath of molten steel, that has been treated under an oxidizing slag, with a mixture consisting substantially of lime and titanium oxide which is substantially devoid of carbon-siliconcontaining material, then after said covering has become fluid adding titanium oxide, lime and aluminum in proportions having the ratio 2 :1: 1, respectively, then adding chromium and nickel in the form of ferro alloys at intervals to supply the desired percentages- 0f these two metals, with further small quantities of lime and aluminum, also titanium oxide if necessary to maintain thesaid ratio, after each addition of chromium and nickel, adding small quantities of aluminum and titanium oxide until the melt is in satisfactory condition, adding more lime approximately five minutes after the last addition of aluminum and titanium oxide, and then tapping the melt.
THOMAS N. ARMSTRONG, JR. FRED B. ANDERSON.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US42861A US2082783A (en) | 1935-09-30 | 1935-09-30 | Method of making alloy steels |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US42861A US2082783A (en) | 1935-09-30 | 1935-09-30 | Method of making alloy steels |
Publications (1)
Publication Number | Publication Date |
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US2082783A true US2082783A (en) | 1937-06-08 |
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ID=21924127
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US42861A Expired - Lifetime US2082783A (en) | 1935-09-30 | 1935-09-30 | Method of making alloy steels |
Country Status (1)
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2430671A (en) * | 1943-12-02 | 1947-11-11 | American Rolling Mill Co | Alloy process |
US2844458A (en) * | 1954-01-28 | 1958-07-22 | Iii John H Hillman | Method of introducing titanium into molten metals and composition for such process |
-
1935
- 1935-09-30 US US42861A patent/US2082783A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2430671A (en) * | 1943-12-02 | 1947-11-11 | American Rolling Mill Co | Alloy process |
US2844458A (en) * | 1954-01-28 | 1958-07-22 | Iii John H Hillman | Method of introducing titanium into molten metals and composition for such process |
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