US2693413A - Alloy steels - Google Patents

Alloy steels Download PDF

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Publication number
US2693413A
US2693413A US218529A US21852951A US2693413A US 2693413 A US2693413 A US 2693413A US 218529 A US218529 A US 218529A US 21852951 A US21852951 A US 21852951A US 2693413 A US2693413 A US 2693413A
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carbon
alloy
alloys
vanadium
niobium
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US218529A
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Kirkby Henry William
Sykes Charles
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Firth Vickers Stainless Steels Ltd
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Firth Vickers Stainless Steels Ltd
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron

Definitions

  • alloy composition might also include silicon up to 3%, manganese up to 4%, and cobalt up to 10%, and the preferred proportions of the various constituents was said to be as follows:
  • the carbon content of alloys within the broad range of composition referred to above is maintained within the limits of 0.07-0.12%. By this modification a softer final product is obtained.
  • the alloys of the present invention are of the ferritic type, that is to say they are magnetic, can be hardened and tempered and have thermal expansion properties similar to those of carbon and low alloy steels. Alloys within the invention possess high creep resistance at temperatures at least up to 700 C. In addition to high creep resistance, the alloys of this invention possess high tensile and proof properties and good scale resistance. They are suitable for many higher temperature applications, particularly in jet engines. In general, the high temperature properties of the present alloys are only a little inferior to those of alloys having the composition preferred in our prior application. Stress rupture tests on alloys within the present preferred range, after suitable heat treatment, gave the following results:
  • a forgeable ferritie alloy steel possessing high creep resistance at temperatures at least up to 700 C. composed essentially of carbon 0.07-0.12%, chromium 4- 20%, molybdenum interchangeable with tungsten 0.5- 3%, niobium 0.2-2.5 vanadium 0.l2%, nitrogen 0.05-0.l0%, and the remainder iron, with incidental impurities in ordinary amounts, which do not affect the physical properties and high temperature characteristics of the steel.
  • a forgeable ferritic alloy steel possessing high creep resistance at temperatures at least up to 700 C. and having a composition comprising carbon 0.07-0.12%, silicon 0.50-1.0%, manganese 0.50-1.0%, nickel 0.5- 1.5%, chromium 9l1%, molybdenum 0.4-1.0%, vanadium 0.1-0.3%, niobium including any residual tantalum 0.2-0.6%, nitrogen ODS-0.10%, and the remainder substantially all iron.
  • a forgeable ferritic alloy steel comprising carbon about 0.10%, silicon about 0.5%, manganese about 1.0%, nickel about 0.7%, chromium about 10.5%, molybdenum about 0.75%, vanadium about 0.15%, niobium about 0.5%, nitrogen about 0.08%, and the remainder iron, with incidental impurities in ordinary amounts, which do not affect the physical properties and high temperature characteristics of the steel.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Steel (AREA)

Description

nited States Patent Ofifice 2,693,413 Patented Nov. 2, 1954 ALLOY STEELS Henry William Kirlrby and Charles Sykes, Shetlield, England, assignors to Firth-Vickers Stainless Steels Limited, Shefilield, England, a British company No Drawing. Application March 30, 1951, Serial No. 218,529
Claims priority, application Great Britain January 31, 1951 3 Claims. (Cl. 75-128) This invention is concerned with improvements relating to alloy steels.
The specification of our copending United States patent application Serial No. 126,698, filed November 10, 1949, now Patent No. 2,590,835, describes the invention comprising a forgeable ferritic alloy steel possessing high creep resistance at temperatures at least up to 700 C., and having a composition including as essential constituents carbon 0.05 to 0.5%, chromium 4 to 20%, molybdenum up to 3% interchangeable with tungsten up to 3%, niobium up to 2.5%, boron up to 0.5% and vanadium up to 2%.
In the aforesaid specification No. 126,698 it was indicated that the alloy composition might also include silicon up to 3%, manganese up to 4%, and cobalt up to 10%, and the preferred proportions of the various constituents was said to be as follows:
Per cent to .25 to 1.5 to 1.5 to 1.5 to 14.0 to 1.5 to 0.3 to 3.0
Carbon .10 Silicon Manganese Nickel Chromium PP PPP QH Ig I IUI Vanadium Tungsten Niobium Nitrogen Boron 0.025 to 0.10 Cobalt nil to 5 Iron Remainder The present invention comprises improvements in or modifications of the foregoing invention forming the subject matter of our prior application.
According to the principal feature of the present invention the carbon content of alloys within the broad range of composition referred to above, is maintained within the limits of 0.07-0.12%. By this modification a softer final product is obtained.
Further modifications in the limits of proportions of certain of the constituents of the alloy-still within the broad range previously indicatedhave also been found It will be noted that in the above preferred composition no boron is present.
Like the alloys of application Serial No. 126,698 aforesaid, the alloys of the present invention are of the ferritic type, that is to say they are magnetic, can be hardened and tempered and have thermal expansion properties similar to those of carbon and low alloy steels. Alloys within the invention possess high creep resistance at temperatures at least up to 700 C. In addition to high creep resistance, the alloys of this invention possess high tensile and proof properties and good scale resistance. They are suitable for many higher temperature applications, particularly in jet engines. In general, the high temperature properties of the present alloys are only a little inferior to those of alloys having the composition preferred in our prior application. Stress rupture tests on alloys within the present preferred range, after suitable heat treatment, gave the following results:
Test Tem- Rupture Stress perature, Strength,
0. hrs.
15 tons/sq. in 650 -200 The following is an example of a specific alloy within the invention:
The above alloy, after air or oil hardening from 1160 C. followed by a tempering treatment at 675 C. was found to possess the desirable creep resistance properties previously indicated herein.
We claim:
1. A forgeable ferritie alloy steel possessing high creep resistance at temperatures at least up to 700 C. composed essentially of carbon 0.07-0.12%, chromium 4- 20%, molybdenum interchangeable with tungsten 0.5- 3%, niobium 0.2-2.5 vanadium 0.l2%, nitrogen 0.05-0.l0%, and the remainder iron, with incidental impurities in ordinary amounts, which do not affect the physical properties and high temperature characteristics of the steel.
2. A forgeable ferritic alloy steel possessing high creep resistance at temperatures at least up to 700 C. and having a composition comprising carbon 0.07-0.12%, silicon 0.50-1.0%, manganese 0.50-1.0%, nickel 0.5- 1.5%, chromium 9l1%, molybdenum 0.4-1.0%, vanadium 0.1-0.3%, niobium including any residual tantalum 0.2-0.6%, nitrogen ODS-0.10%, and the remainder substantially all iron.
3. A forgeable ferritic alloy steel comprising carbon about 0.10%, silicon about 0.5%, manganese about 1.0%, nickel about 0.7%, chromium about 10.5%, molybdenum about 0.75%, vanadium about 0.15%, niobium about 0.5%, nitrogen about 0.08%, and the remainder iron, with incidental impurities in ordinary amounts, which do not affect the physical properties and high temperature characteristics of the steel.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,120,554 Franks Dec. 20, 1938 2,140,905 Franks Dec. 20, 1938 2,212,496 De Vries Aug. 27, 1940 2,432,614 Franks Dec. 16, 1947 2,513,935 Harris July 4, 1950

Claims (1)

1. A FORGEABLE FERRITIC ALLOY STEEL POSSESSING HIGH CREEP RESISTANCE AT TEMPERATURES AT LEAST UP TO 700* C. COMPOSED ESSENTIALLY OF CARBON 0.07-0.12%, CHROMIUM 420%, MOLYBDENUM INTERCHANGEABLE WITH TUNGSTEN 0.53%, NIOBIUM 0.2-2.5%, VANADIUM 0.1-2%, NITROGEN 0.05-0.10%, AND THE REMAINDER IRON, WITH INCIDENTAL IMPURITIES IN ORDINARY AMOUNTS, WHICH DO NOT EFFECT THE PHYSICAL PROPERTIES AND HIGH TEMPERATURE CHARACTERISTICS OF THE STEEL.
US218529A 1951-01-31 1951-03-30 Alloy steels Expired - Lifetime US2693413A (en)

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2905577A (en) * 1956-01-05 1959-09-22 Birmingham Small Arms Co Ltd Creep resistant chromium steel
US3069257A (en) * 1960-06-02 1962-12-18 Armco Steel Corp Alloy steel and method
US3141801A (en) * 1961-06-27 1964-07-21 Prutton Daniel Howard Method of hardening a case hardened steel
FR2566429A1 (en) * 1984-06-21 1985-12-27 Toshiba Kk Heat resistant martensitic chromium steel
EP0333129A2 (en) * 1988-03-14 1989-09-20 Hitachi, Ltd. Gas turbine, shroud for gas turbine and method of producing the shroud
EP0338133A2 (en) * 1988-04-20 1989-10-25 Kawasaki Steel Corporation Steels for hot working press tools
EP0472305A1 (en) * 1990-07-30 1992-02-26 Nkk Corporation Martensitic stainless steel for oil well
US5310431A (en) * 1992-10-07 1994-05-10 Robert F. Buck Creep resistant, precipitation-dispersion-strengthened, martensitic stainless steel and method thereof
US5674449A (en) * 1995-05-25 1997-10-07 Winsert, Inc. Iron base alloys for internal combustion engine valve seat inserts, and the like
US20040154707A1 (en) * 2003-02-07 2004-08-12 Buck Robert F. Fine-grained martensitic stainless steel and method thereof
US20040154706A1 (en) * 2003-02-07 2004-08-12 Buck Robert F. Fine-grained martensitic stainless steel and method thereof
US20060283526A1 (en) * 2004-07-08 2006-12-21 Xuecheng Liang Wear resistant alloy for valve seat insert used in internal combustion engines

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2120554A (en) * 1935-06-08 1938-06-14 Union Carbide & Carbon Corp Chromium steel
US2140905A (en) * 1936-05-02 1938-12-20 Union Carbide & Carbon Res Lab Turbine blade
US2212496A (en) * 1939-01-10 1940-08-27 Allegheny Ludlum Steel Alloy steel
US2432614A (en) * 1945-06-13 1947-12-16 Haynes Stellite Co Ferrous alloys for high temperature service
US2513935A (en) * 1947-12-13 1950-07-04 Jessop William & Sons Ltd Alloy steels

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2120554A (en) * 1935-06-08 1938-06-14 Union Carbide & Carbon Corp Chromium steel
US2140905A (en) * 1936-05-02 1938-12-20 Union Carbide & Carbon Res Lab Turbine blade
US2212496A (en) * 1939-01-10 1940-08-27 Allegheny Ludlum Steel Alloy steel
US2432614A (en) * 1945-06-13 1947-12-16 Haynes Stellite Co Ferrous alloys for high temperature service
US2513935A (en) * 1947-12-13 1950-07-04 Jessop William & Sons Ltd Alloy steels

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2905577A (en) * 1956-01-05 1959-09-22 Birmingham Small Arms Co Ltd Creep resistant chromium steel
US3069257A (en) * 1960-06-02 1962-12-18 Armco Steel Corp Alloy steel and method
US3141801A (en) * 1961-06-27 1964-07-21 Prutton Daniel Howard Method of hardening a case hardened steel
FR2566429A1 (en) * 1984-06-21 1985-12-27 Toshiba Kk Heat resistant martensitic chromium steel
EP0333129A3 (en) * 1988-03-14 1991-08-28 Hitachi, Ltd. Gas turbine, shroud for gas turbine and method of producing the shroud
EP0333129A2 (en) * 1988-03-14 1989-09-20 Hitachi, Ltd. Gas turbine, shroud for gas turbine and method of producing the shroud
EP0338133A3 (en) * 1988-04-20 1992-03-18 Kawasaki Steel Corporation Steels for hot working press tools
EP0338133A2 (en) * 1988-04-20 1989-10-25 Kawasaki Steel Corporation Steels for hot working press tools
EP0472305A1 (en) * 1990-07-30 1992-02-26 Nkk Corporation Martensitic stainless steel for oil well
US5167731A (en) * 1990-07-30 1992-12-01 Nkk Corporation Martensitic stainless steel for an oil well
US5310431A (en) * 1992-10-07 1994-05-10 Robert F. Buck Creep resistant, precipitation-dispersion-strengthened, martensitic stainless steel and method thereof
US5674449A (en) * 1995-05-25 1997-10-07 Winsert, Inc. Iron base alloys for internal combustion engine valve seat inserts, and the like
US20040154707A1 (en) * 2003-02-07 2004-08-12 Buck Robert F. Fine-grained martensitic stainless steel and method thereof
US20040154706A1 (en) * 2003-02-07 2004-08-12 Buck Robert F. Fine-grained martensitic stainless steel and method thereof
US6890393B2 (en) 2003-02-07 2005-05-10 Advanced Steel Technology, Llc Fine-grained martensitic stainless steel and method thereof
US6899773B2 (en) 2003-02-07 2005-05-31 Advanced Steel Technology, Llc Fine-grained martensitic stainless steel and method thereof
US20060283526A1 (en) * 2004-07-08 2006-12-21 Xuecheng Liang Wear resistant alloy for valve seat insert used in internal combustion engines
US7611590B2 (en) 2004-07-08 2009-11-03 Alloy Technology Solutions, Inc. Wear resistant alloy for valve seat insert used in internal combustion engines

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