DE1608097B2 - USING A TOUGH, PRECIPITABLE, STAINLESS, CHROME, NICKEL AND ALUMINUM STEEL ALLOY - Google Patents

USING A TOUGH, PRECIPITABLE, STAINLESS, CHROME, NICKEL AND ALUMINUM STEEL ALLOY

Info

Publication number
DE1608097B2
DE1608097B2 DE19671608097 DE1608097A DE1608097B2 DE 1608097 B2 DE1608097 B2 DE 1608097B2 DE 19671608097 DE19671608097 DE 19671608097 DE 1608097 A DE1608097 A DE 1608097A DE 1608097 B2 DE1608097 B2 DE 1608097B2
Authority
DE
Germany
Prior art keywords
steel alloy
nickel
tough
aluminum
stainless
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.)
Granted
Application number
DE19671608097
Other languages
German (de)
Other versions
DE1608097C3 (en
DE1608097A1 (en
Inventor
William C Dundalk Md.; Perry D. Cameron Middletown Ohio; Clarke jun. (V.StA.)
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(B2) "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 <5- 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) 195g 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 remainder consists of iron, 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 one stainless steel that does not contain any free <5 ferrite and a slight structural hardening with good Reproducibility of its mechanical properties allowed. About the toughness and strength properties This patent does not contain any of this known steel and special fields of application Declarations. From Küntscher-Kilger-Biegler »Technical Structural Steel«, 3rd edition, Halle (Saale) 195g Pages 374/375 and 404, it is also known that niobium can be added to stainless steels. From it however, they are also not specific information with regard to toughness and strength properties as well as special fields of application of the steels described therein.

In der Patentanmeldung P 14 58 330 ist die Verwendung einer zähen, aushärtungshärtbaren, rostfreien, chrom-, nickel- 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-In the patent application P 14 58 330 is the use of a tough, age hardenable, rustproof, chromium, nickel and aluminum-containing steel alloy made 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 direction at room temperature in the hardened state

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.and transverse direction, an elongation within 50.8 mm gauge length of at least 8% and a constriction of at least 29.3%, such as compound machined, welded or soldered Parts of pressure vessels or missiles described.

Die in der vorliegenden Zusatzanmeldung beschriebene Erfindung stellt nun eine weitere Ausgestaltung des Gegenstandes der oben genannten Hauptpatentanmeldung dar und betrifft die Verwendung einer zähen, ausscheidungshärtbaren, rostfreien, chrom-, nickel- und aluminiumhaltigen Stahllegierung der vorstehend angegebenen Zusammensetzung für den in dem Hauptpatent genannten Zweck, die zusätzlich noch mehr als 0,10 und bis zu 0,50% Titan und/oder bis zu 0,75% Niob enthält. Beste Ergebnisse werden erzielt, wenn die Stahllegierung der vorstehend angegebenen Zusammensetzung 0,10 bis 0,50% Niob und weniger als 0,015% Schwefel enthält.The invention described in the present additional application represents a further embodiment the subject of the above-mentioned main patent application and relates to the use of a tough, precipitation hardenable stainless, chromium, nickel and aluminum containing steel alloys of the above Composition for the purpose mentioned in the main patent, which are additionally more than 0.10 and contains up to 0.50% titanium and / or up to 0.75% niobium. Best results are obtained when the steel alloy of the composition given above, 0.10 to 0.50% niobium and less than 0.015% sulfur contains.

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 intergranular or intergranular corrosion in the freshly welded as well as in the welded state and precipitation hardened state, and they are in the hardened state after welding or brazing particularly 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 production of parts, in which 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 one The atmosphere.

Claims (2)

Patentansprüche:Patent claims: 1. Verwendung einer zähen, aushärtungshärtbaren, 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 verschmelzungsbedingter 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 nach Patentanmeldung P 14 58 330 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, age-hardening, rust-free, 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 the merger, 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 according to patent application P 14 58 330 with the proviso that the steel alloy additionally contains more than 0.10 and up to 0.50% titanium and / or up to 0 , Contains 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 true DE1608097B2 (en) 1977-06-02
DE1608097C3 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
US5681528A (en) * 1995-09-25 1997-10-28 Crs Holdings, Inc. High-strength, notch-ductile precipitation-hardening stainless steel alloy
US5855844A (en) * 1995-09-25 1999-01-05 Crs Holdings, Inc. High-strength, notch-ductile precipitation-hardening stainless steel alloy and method of making
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
ES2811140T3 (en) * 2015-04-21 2021-03-10 Jfe Steel Corp Martensitic stainless steel
KR102169859B1 (en) * 2016-04-12 2020-10-26 제이에프이 스틸 가부시키가이샤 Martensite stainless steel plate
SE1650850A1 (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.
US2505762A (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
US2505763A (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
US2958617A (en) * 1957-07-31 1960-11-01 Armco Steel Corp Method for hardening chromiumnickel stainless steel
US2958618A (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
BE697441A (en) 1967-10-02
DE1458330B2 (en) 1977-02-24
DE1608097C3 (en) 1985-04-25
US3556776A (en) 1971-01-19
DE1458330A1 (en) 1972-03-23
BE651249A (en) 1964-11-16
DE1608097A1 (en) 1973-05-24
DE1458330C3 (en) 1984-09-20
SE316023B (en) 1969-10-13
GB1077979A (en) 1967-08-02
GB1138098A (en) 1968-12-27

Similar Documents

Publication Publication Date Title
DE1608097C3 (en) Use of a tough, precipitation hardenable, rustproof, chrome, nickel and aluminum containing steel alloy
DE3685795T2 (en) STAINLESS DUPLEX STEEL WITH HIGH NITROGEN CONTENT AND CHARACTERIZED BY HIGH CORROSION RESISTANCE AND GOOD STRUCTURAL STABILITY.
DE69317971T2 (en) Super alloy with a set coefficient of thermal expansion
DE3117539C2 (en)
DE8703670U1 (en) Valve for normally aspirated and turbocharged petrol and diesel engines as well as turbine units
DE2505212A1 (en) STAINLESS FERRITIC STEEL
DE69112007T2 (en) Ferritic, heat-resistant cast steel and process for its manufacture.
DE1558683C2 (en) Use of a cobalt-chromium-tungsten-nickel wrought alloy
DE1483331B2 (en) USE OF A HARDENABLE STEEL ALLOY
DE3024380C2 (en) Use of a steel alloy
DE2161954A1 (en) FERRITIC HEAT RESISTANT STEEL
DE1483177B2 (en) USE OF A PRECIPITABLE, STAINLESS, CHROME-NICKEL-ALUMINUM STEEL ALLOY
DE1918176A1 (en) Low-alloy, homogeneous iron powder for the production of hardenable sintered steels
DE68916235T2 (en) Zirconium-based alloy with increased resistance to corrosion by nitric acid and with good creep resistance.
DE1232759B (en) Martensite-hardenable chrome-nickel steel
DE2331134A1 (en) ROLL-CLAD MATERIALS MADE FROM A BASE MATERIAL MADE FROM STEEL AND FROM CLADDING MATERIALS MADE FROM CORROSION-RESISTANT AUSTENITIC STEELS AND ALLOYS
DE1239109B (en) Use of a martensite-hardenable steel alloy as a material for pressure and impact-resistant objects
DE1178609B (en) Low-alloy, easily weldable steel suitable for pressure vessels and components used in the same way
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)
DE3627668C1 (en) Well weldable structural steel with high resistance to stress corrosion cracking
DE1950004B2 (en) Use of steel for components with high vibration resistance
DE3720605A1 (en) AUSTENITIC STEEL FOR GAS EXCHANGE VALVES OF COMBUSTION ENGINES
DE1239857B (en) Use of an austenitic steel alloy for forgeable components
DE2209085A1 (en) Age hardened martensitic nickel 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)