DE1608097C3 - Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy - Google Patents

Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy

Info

Publication number
DE1608097C3
DE1608097C3 DE1608097A DE1608097A DE1608097C3 DE 1608097 C3 DE1608097 C3 DE 1608097C3 DE 1608097 A DE1608097 A DE 1608097A DE 1608097 A DE1608097 A DE 1608097A DE 1608097 C3 DE1608097 C3 DE 1608097C3
Authority
DE
Germany
Prior art keywords
steel alloy
nickel
tough
rustproof
aluminum
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
Application number
DE1608097A
Other languages
German (de)
Other versions
DE1608097A1 (en
DE1608097B2 (en
Inventor
D. Cameron Middletown Ohio Perry
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Armco Steel Co LP
Original Assignee
Armco Steel Co LP
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=27404660&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE1608097(C3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Armco Steel Co LP filed Critical Armco Steel Co LP
Publication of DE1608097A1 publication Critical patent/DE1608097A1/en
Publication of DE1608097B2 publication Critical patent/DE1608097B2/en
Application granted granted Critical
Publication of DE1608097C3 publication Critical patent/DE1608097C3/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/12Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium

Landscapes

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

Description

Die Erfindung betrifft die Verwendung einer zähen, ausscheidungshärtbaren, rostfreien, chrom-, nickel- und aluminiumhaltigen Stahllegierung als Werkstoff für bestimmte Gegenstände, wie zusammengesetzte maschinenverarbeitete, geschweißte oder gelötete Teile von Druckkesseln oder Flugkörpern.The invention relates to the use of a tough, precipitation hardenable, stainless, chrome, nickel and aluminum-containing steel alloy as a material for certain items, such as composite machine-processed, welded or soldered parts of pressure vessels or missiles.

In der US-Patentschrift 31 31 055 ist eine Stahllegierung beschrieben, die aus 5 bis 16,5% Chrom, 10 bis 18,5% Nickel, 1 bis 6% Aluminium, bis zu 0,15% Kohlenstoff, bis zu 4% Mangan, bis zu 2% Silicium und zum Rest aus Eisen besteht, wobei das Aluminium teilweise durch Titan und/oder Molybdän ersetzt sein kann und der Aluminiumgehalt nicht unter 0,5% fällt. Dabei handelt es sich um einen ausscheidungshärtbaren rostfreien Stahl, der keinen freien cf-Ferrit enthält und eine leichte Strukturhärtung unter Erzielung einer guten Reproduzierbarkeit seiner mechanischen Eigenschaften erlaubt. Über die Zähigkeits- und Festigkeitseigenschaften dieses bekannten Stahls und über spezielle Anwendungsgebiete enthält diese Patentschrift keinerlei Angaben. Aus Küntscher-Kilger-Biegler, »Technische Baustähle«, 3. Auflage, Halle (Saale) 1958, Seiten 374/375 und 404, ist es ferner bekannt, daß rostfreien Stählen Niob zugesetzt werden kann. Daraus sind jedoch ebenfalls keine spezifischen Angaben in bezug auf Zähigkeits- und Festigkeitseigenschaften sowie spezielle Anwendungsgebiete der darin beschriebenen Stähle zu entnehmen.In US Pat. No. 31 31 055, a steel alloy is described, which consists of 5 to 16.5% chromium, 10 to 18.5% nickel, 1 to 6% aluminum, up to 0.15% carbon, up to 4% manganese, up to 2% silicon and the The remainder consists of iron, with the aluminum being partially replaced by titanium and / or molybdenum and the aluminum content does not fall below 0.5%. It is a precipitation hardenable stainless steel Steel that does not contain free cf ferrite and is a light one Structural hardening is allowed while achieving good reproducibility of its mechanical properties. About the toughness and strength properties of this well-known steel and about special areas of application this patent specification does not contain any information. From Küntscher-Kilger-Biegler, »Technical Structural Steel«, 3rd edition, Halle (Saale) 1958, pages 374/375 and 404 is it is also known that niobium can be added to stainless steels. However, none of these are either specific information regarding toughness and strength properties as well as special areas of application of the steels described therein.

In dem Patent 14 58 330 ist die Verwendung einer zähen, ausscheidungshärtbaren, rostfreien, chrom-, nikkel- und aluminiumhaltigen Stahllegierung, die aus 11,5 bis 13,5% Chrom, 7,0 bis 10,0% Nickel, 0,5 bis 1,5% Aluminium, 1,75 bis 2,50% Molybdän, bis zu 0,05% Kohlenstoff, bis zu 0,50% Mangan, bis zu 0,60% Silicium, bis zu 0,020% Schwefel, bis zu 0,05% Stickstoff, Rest Eisen einschließlich erschmelzungsbedingter Verunreinigungen besteht, als Werkstoff für Gegenstände, die bei Raumtemperatur in ausgehärtetem Zustand eine Mindestzugfestigkeit von 149,0 kg/mm2 in der Längs- und Querrichtung, eine Dehnung innerhalb 50,8 mm Meßlänge von mindestens 8% und eine Einschnürung von mindestens 29,3% aufweisen, wie zusammengesetzte maschinenverarbeitete, geschweißte oder gelötete Teile von Druckkesseln oder Flugkörpern, beschrieben.In the patent 14 58 330 is the use of a tough, precipitation hardenable, stainless, chromium, nickel and aluminum-containing steel alloy consisting of 11.5 to 13.5% chromium, 7.0 to 10.0% nickel, 0.5 up to 1.5% aluminum, 1.75 to 2.50% molybdenum, up to 0.05% carbon, up to 0.50% manganese, up to 0.60% silicon, up to 0.020% sulfur, up to 0 .05% nitrogen, the remainder iron, including impurities caused by the melting, as a material for objects that have a minimum tensile strength of 149.0 kg / mm 2 in the longitudinal and transverse direction at room temperature in the hardened state, an elongation within 50.8 mm measuring length of at least 8% and a necking of at least 29.3%, as described as assembled, machine-processed, welded or soldered parts of pressure vessels or missiles.

Die hier beschriebene Erfindung stellt nun eine weitere Ausgestaltung des Gegenstandes des oben genannten Patents dar und betrifft die Verwendung einer zähen, ausscheidungshärtbaren, rostfreien, chrom-, nickel- und aluminiumhaltigen Stahllegierung der vorstehend angegebenen Zusammensetzung für den in dem Patent genannten Zweck, die zusätzlich noch mehr als 0,10 und bis zu 0,50% Titan und/oder bis zu 0,75% Niob enthält.The invention described here represents a further embodiment of the subject matter of the above Patent and relates to the use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminous steel alloy of the above composition for the one in the patent mentioned purpose, which also contains more than 0.10 and up to 0.50% titanium and / or up to 0.75% niobium.

Beste Ergebnisse werden erzielt, wenn die Stahllegierung der vorstehend angegebenen Zusammensetzung 0,10 bis 0,50% Niob und weniger als 0,015% Schwefel enthält.Best results are obtained when the steel alloy has the composition given above Contains 0.10 to 0.50% niobium and less than 0.015% sulfur.

Die erfindungsgemäß verwendeten titanhaltigen und/ oder niobhaltigen Stähle sind frei von jeder interkristallinen oder intergranulären Korrosion im frisch geschweißten Zustand sowie im geschweißten und ausscheidungsgehärteten Zustand und sie sind im gehärteten Zustand nach dem Schweißen oder Hartlöten besonders korrosionsbeständig.The titanium-containing and / or niobium-containing steels used according to the invention are free of any intergranularity or intergranular corrosion in the freshly welded state as well as in the welded and precipitation hardened Condition and they are special in the hardened condition after welding or brazing corrosion resistant.

Die erfindungsgemäß verwendete Stahllegierung eignet sich insbesondere für die Herstellung von Teilen, bei denen Spannungen längs aller drei Hauptachsen auftreten. Der erfindungsgemäß zu verwendende Stahl weist eine ausgezeichnete Spannungsrißkorrosionsbeständigkeit auf selbst in einer stark salzhaltigen Atmosphäre.The steel alloy used according to the invention is particularly suitable for the manufacture of parts where stresses occur along all three main axes. The steel to be used according to the invention has excellent stress corrosion cracking resistance even in a highly saline atmosphere.

Claims (2)

Patentansprüche:Patent claims: 1. Verwendung einer zähen, ausscheidungshärtbaren, rostfreien, chrom-, nickel- und aluminiumhaltigen Stahllegierung, bestehend aus 11,5 bis 13,5% Chrom, 7,0 bis 10,0% Nickel, 0,5 bis 1,5% Aluminium, 1,75 bis 2,50% Molybdän, bis zu 0,05% Kohlenstoff, bis zu 0,50 % Mangan, bis zu 0,60% Silicium, bis zu 0,020% Schwefel, bis 0,05% Stickstoff, Rest Eisen einschließlich erschmelzungsbedingter Verunreinigungen, als Werkstoff für Gegenstände, die bei Raumtemperatur in ausgehärtetem Zustand eine Mindestzugfestigkeit von 149,0 kg/mm2 in der Längs- und Querrichtung, eine Dehnung innerhalb 50,8 mm Meßlänge von mindestens 8% und eine Einschnürung von mindestens 29,3% aufweisen, wie zusammengesetzte maschinenverarbeitete, geschweißte oder gelötete Teile von Druckkesseln oder Flugkörpern mit der Maßgabe, daß die Stahllegierung zusätzlich mehr als 0,10 und bis zu 0,50% Titan und/ oder bis zu 0,75% Niob enthält.1. Use of a tough, precipitation-hardenable, rustproof, chromium, nickel and aluminum-containing steel alloy, consisting of 11.5 to 13.5% chromium, 7.0 to 10.0% nickel, 0.5 to 1.5% aluminum , 1.75 to 2.50% molybdenum, up to 0.05% carbon, up to 0.50% manganese, up to 0.60% silicon, up to 0.020% sulfur, up to 0.05% nitrogen, the remainder iron including impurities caused by melting, as a material for objects that have a minimum tensile strength of 149.0 kg / mm 2 in the longitudinal and transverse direction at room temperature in the hardened state, an elongation within 50.8 mm measuring length of at least 8% and a constriction of at least 29 , 3%, such as assembled, machine-processed, welded or soldered parts of pressure vessels or missiles with the proviso that the steel alloy additionally contains more than 0.10 and up to 0.50% titanium and / or up to 0.75% niobium. 2. Verwendung einer Stahllegierung nach Anspruch 1, die 0,10 bis 0,50% Niob und weniger als 0,015% Schwefel enthält, für den Zweck nach Anspruch 1.2. Use of a steel alloy according to claim 1, which is 0.10 to 0.50% niobium and less than Contains 0.015% sulfur for the purpose of claim 1.
DE1608097A 1963-08-02 1967-07-21 Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy Expired DE1608097C3 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US29948463A 1963-08-02 1963-08-02
US37657064A 1964-06-19 1964-06-19
US58529866A 1966-10-10 1966-10-10

Publications (3)

Publication Number Publication Date
DE1608097A1 DE1608097A1 (en) 1973-05-24
DE1608097B2 DE1608097B2 (en) 1977-06-02
DE1608097C3 true DE1608097C3 (en) 1985-04-25

Family

ID=27404660

Family Applications (2)

Application Number Title Priority Date Filing Date
DE1458330A Expired DE1458330C3 (en) 1963-08-02 1964-08-03 Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy
DE1608097A Expired DE1608097C3 (en) 1963-08-02 1967-07-21 Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE1458330A Expired DE1458330C3 (en) 1963-08-02 1964-08-03 Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy

Country Status (5)

Country Link
US (1) US3556776A (en)
BE (2) BE651249A (en)
DE (2) DE1458330C3 (en)
GB (2) GB1077979A (en)
SE (1) SE316023B (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE651249A (en) * 1963-08-02 1964-11-16
US3769003A (en) * 1971-04-05 1973-10-30 Int Nickel Co Alloy steel particularly adaptable for use as a filler metal
US4125260A (en) * 1976-05-17 1978-11-14 True Temper Corporation Tubular golf shaft of stainless steel
US4049430A (en) * 1976-08-18 1977-09-20 Carpenter Technology Corporation Precipitation hardenable stainless steel
FR2419472A1 (en) * 1978-03-08 1979-10-05 Ciat Sa Heating system for swimming pool - has air treated by heat pump with some flow by=passed around evaporator with total flow passing over condenser
US4754950A (en) * 1984-10-30 1988-07-05 Kabushiki Kaisha Toshiba Valve
US5855844A (en) * 1995-09-25 1999-01-05 Crs Holdings, Inc. High-strength, notch-ductile precipitation-hardening stainless steel alloy and method of making
US5681528A (en) * 1995-09-25 1997-10-28 Crs Holdings, Inc. High-strength, notch-ductile precipitation-hardening stainless steel alloy
US5888449A (en) * 1997-05-30 1999-03-30 Teledyne Industries, Inc. Stainless steel
US7901519B2 (en) * 2003-12-10 2011-03-08 Ati Properties, Inc. High strength martensitic stainless steel alloys, methods of forming the same, and articles formed therefrom
FR2887558B1 (en) * 2005-06-28 2007-08-17 Aubert & Duval Soc Par Actions MARTENSITIC STAINLESS STEEL COMPOSITION, PROCESS FOR MANUFACTURING A MECHANICAL PART THEREFROM, AND PIECE THUS OBTAINED
US7931758B2 (en) * 2008-07-28 2011-04-26 Ati Properties, Inc. Thermal mechanical treatment of ferrous alloys, and related alloys and articles
JP5502575B2 (en) * 2010-04-16 2014-05-28 株式会社日立製作所 Precipitation hardening martensitic stainless steel and steam turbine blades
JP5528986B2 (en) * 2010-11-09 2014-06-25 株式会社日立製作所 Precipitation hardening type martensitic stainless steel and steam turbine member using the same
JP5764503B2 (en) * 2012-01-19 2015-08-19 三菱日立パワーシステムズ株式会社 Precipitation hardening type martensitic stainless steel, steam turbine long blade, turbine rotor and steam turbine using the same
JP6317542B2 (en) 2012-02-27 2018-04-25 三菱日立パワーシステムズ株式会社 Steam turbine rotor
JP6259579B2 (en) * 2012-03-29 2018-01-10 新日鐵住金ステンレス株式会社 High-strength stainless steel wire, high-strength spring, and method of manufacturing the same
JP6113456B2 (en) * 2012-10-17 2017-04-12 三菱日立パワーシステムズ株式会社 Precipitation hardened martensitic stainless steel and steam turbine long blades using it
US10655195B2 (en) * 2015-04-21 2020-05-19 Jfe Steel Corporation Martensitic stainless steel
ES2862309T3 (en) * 2016-04-12 2021-10-07 Jfe Steel Corp Martensitic stainless steel sheet
SE539763C2 (en) * 2016-06-16 2017-11-21 Uddeholms Ab Steel suitable for plastic moulding tools

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR743179A (en) * 1933-03-25
AT146720B (en) * 1931-06-23 1936-08-10 Krupp Ag Manufacture of objects that must have special strength properties, in particular high vibration resistance and / or should have high resistance to becoming brittle due to intergranular corrosion.
US2505763A (en) * 1946-09-06 1950-05-02 Armco Steel Corp Stainless steel and method
US2505764A (en) * 1946-09-06 1950-05-02 Armco Steel Corp Stainless steel and method
US2505762A (en) * 1946-09-06 1950-05-02 Armco Steel Corp Stainless steel and method
US2799602A (en) * 1956-10-04 1957-07-16 Allegheny Ludlum Steel Process for producing stainless steel
US2958618A (en) * 1957-07-31 1960-11-01 Armco Steel Corp Method for hardening chromiumnickel stainless steel
US2958617A (en) * 1957-07-31 1960-11-01 Armco Steel Corp Method for hardening chromiumnickel stainless steel
US3117860A (en) * 1958-04-11 1964-01-14 Ferrolegeringar Trollhetteverk Methods of removing copper and related metals from sulfidic molybdenum ores and molybdenum-containing materials
US2999039A (en) * 1959-09-14 1961-09-05 Allegheny Ludlum Steel Martensitic steel
US3131055A (en) * 1960-03-11 1964-04-28 Soc Metallurgique Imphy Alloy based on iron, containing nickel, chromium and aluminium, and process for obtaining same
BE651249A (en) * 1963-08-02 1964-11-16

Also Published As

Publication number Publication date
GB1138098A (en) 1968-12-27
DE1608097A1 (en) 1973-05-24
DE1458330B2 (en) 1977-02-24
BE651249A (en) 1964-11-16
DE1608097B2 (en) 1977-06-02
BE697441A (en) 1967-10-02
DE1458330A1 (en) 1972-03-23
US3556776A (en) 1971-01-19
GB1077979A (en) 1967-08-02
SE316023B (en) 1969-10-13
DE1458330C3 (en) 1984-09-20

Similar Documents

Publication Publication Date Title
DE1608097C3 (en) Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy
DE1483331B2 (en) USE OF A HARDENABLE STEEL ALLOY
DE3024380C2 (en) Use of a steel alloy
DE1558683B1 (en) Use of a cobalt-chromium-tungsten-nickel-Kent alloy
DE1483177A1 (en) Semi-austenitic, precipitation hardenable, rustproof chrome-nickel-aluminum steel
DE3604789C1 (en) Quenched and tempered steel
DE1232759B (en) Martensite-hardenable chrome-nickel steel
DE1239109B (en) Use of a martensite-hardenable steel alloy as a material for pressure and impact-resistant objects
DE681719C (en) Material for welding rods for the production of non-hardenable, fine-grained and stretchable welding on objects made of ferritic chrome steels
DE1558676C3 (en)
DE1533298A1 (en) Martensite-hardenable nickel-molybdenum steel alloy
DE1178609B (en) Low-alloy, easily weldable steel suitable for pressure vessels and components used in the same way
DE1950004B2 (en) Use of steel for components with high vibration resistance
DE2209085A1 (en) Age hardened martensitic nickel steel
DE1239857B (en) Use of an austenitic steel alloy for forgeable components
DE630744C (en) Steel for seamless pipes, which have high resistance to scaling and good strength properties
DE1903712B2 (en) USE OF A COPPER-ALUMINUMBERYLLUM ALLOY FOR THE PRODUCTION OF HIGHLY CAVITATION-RESISTANT OBJECTS
DE1279337B (en) Use of a carbide hard alloy for parts subject to wear and tear for writing implements, in particular writing tubes for tube pens and balls for ballpoint pens
DE1533228B1 (en) Use of a nickel-chromium-iron alloy for the production of tough, hot and cold formable objects which are exposed to the attack of combustion products of vanadium and / or sulfur-containing fuels at temperatures above 500 ° C
DE2117030B2 (en) Use of a nickel-chromium steel of a certain composition as a high-temperature material
DE1483466B1 (en) COVERED WELDING ELECTRODE
DE2106506C3 (en) Use of a chrome-nickel steel for the manufacture of components
DE659831C (en) Structural steel with high strength and yield strength and at the same time high elongation
DE3808451A1 (en) ALLOYS WITH EXCELLENT EROSION RESISTANCE
CH275201A (en) Alloy sintered steel.

Legal Events

Date Code Title Description
AF Is addition to no.

Ref country code: DE

Ref document number: 1458330

Format of ref document f/p: P

8281 Inventor (new situation)

Free format text: CLARKE JUN., WILLIAM C., DUNDALK, MD., US PERRY, D. CAMERON, MIDDLETOWN, OHIO, US

AF Is addition to no.

Ref country code: DE

Ref document number: 1458330

Format of ref document f/p: P

C3 Grant after two publication steps (3rd publication)