EP1297192A1 - Stahlzusammensetzungen, verfahren zu ihrer herstellung und daraus hergestellte formteile - Google Patents

Stahlzusammensetzungen, verfahren zu ihrer herstellung und daraus hergestellte formteile

Info

Publication number
EP1297192A1
EP1297192A1 EP01949617A EP01949617A EP1297192A1 EP 1297192 A1 EP1297192 A1 EP 1297192A1 EP 01949617 A EP01949617 A EP 01949617A EP 01949617 A EP01949617 A EP 01949617A EP 1297192 A1 EP1297192 A1 EP 1297192A1
Authority
EP
European Patent Office
Prior art keywords
weight
composition according
steel
mechanical
parts
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
EP01949617A
Other languages
English (en)
French (fr)
Other versions
EP1297192B1 (de
Inventor
Jacques Frey
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.)
Aubert and Duval SA
Original Assignee
Industrielle De Metallurgie Avancee (sima) Ste
Aubert and Duval SA
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
Application filed by Industrielle De Metallurgie Avancee (sima) Ste, Aubert and Duval SA filed Critical Industrielle De Metallurgie Avancee (sima) Ste
Publication of EP1297192A1 publication Critical patent/EP1297192A1/de
Application granted granted Critical
Publication of EP1297192B1 publication Critical patent/EP1297192B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
    • 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
    • C22C38/34Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
    • 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
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/52Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
    • 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
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/004Dispersions; Precipitations

Definitions

  • the invention relates to a steel more particularly intended for the production of mechanical parts which can be used under severe conditions of use, in nuclear installations but also in industries such as the food industry, energy or mechanical engineering. .
  • cobalt-based alloys pose both economic and technical problems.
  • cobalt is an expensive raw material with few sources of supply.
  • this element is highly undesirable in the nuclear environment because it forms isotopes with long lifespan which are released by the wear of the parts and are one of the main sources of exposure to radiations of the people working in these installations.
  • the cobalt content must therefore be limited as much as possible in the steels or alloys which are used in particular in this industry for the production of valve seats.
  • US Patent 3,912,503 describes compositions of stainless steels resistant to wear and corrosion. They include 0.12% by weight of carbon at most, 7 to 13% by weight of manganese, 3 to 5% by weight of silicon, 12 to 19% by weight of chromium, 4 to 12% by weight of nickel, 0 , 03 to 0.3% by weight of nitrogen, the balance consisting of iron. These compositions have a coefficient of friction close to that of cobalt-based alloys but have a hardness at room temperature of only 200 Vickers, hardness which drops to 150 Vickers from 200 ° C. In addition, their ductility is much too great to allow use for the production of mechanical parts subjected to high stresses.
  • US Patent 4,814,140 describes the same type of steel as US Patent 3,912,503 and makes it possible to improve the resistance to seizing.
  • the claimed compositions comprise 0.25% by weight of carbon at most, 2 to 7% by weight of manganese, 1 to 5% by weight of silicon, 12 to 20% by weight of chromium, 2 to 7.75% by weight of nickel, 0.35% by weight of nitrogen at most, the remainder consisting of iron.
  • the mechanical properties which include ductility, hardness at room temperature and when hot, are similar to that of the compositions of US Pat. No. 3,912,503 and are therefore also insufficient for the applications envisaged.
  • the main object of the present invention is therefore to provide such a material.
  • a first object of the invention consists of a steel composition comprising, expressed in percentages by weight:
  • the steel composition comprises, expressed in percentages by weight:
  • unavoidable impurities mention will be made in particular of sulfur and phosphorus which should be kept at the lowest level compatible with the manufacturing process or the raw materials used.
  • the hardnesses obtained with the steels according to the invention are between 350 and 550 Vickers.
  • the carbon content of the steels according to the invention is between 0.40 and 0.50% by weight, when the parts to be produced do not require hardness and resistance to l 'very high wear. In another preferred embodiment of the invention, the carbon content of the steels according to the invention is between 0.50 and 0.60% by weight, when the parts to be produced require hardness and resistance to slightly higher wear. In another mode preferred embodiment of the invention, the carbon content is between 0.70 and 0.80% by weight for applications in which the hardness and the resistance to wear must be high. It can therefore be seen that these two characteristics of steel can be adjusted by varying this carbon content, within certain predefined limits.
  • the silicon is present at a content of 3.00 to 4.50% by weight, preferably 3.50 to 4.00% by weight. It plays a role in improving friction and seizure resistance due to the formation of adherent oxide film on the surface of the parts. It also has a favorable role in corrosion resistance.
  • Nickel is a gamma element which participates in balancing the composition. It is present in a content of 3.50 to 4.50% by weight and provides the steel compositions with good corrosion resistance.
  • Manganese is present at a content of 7.00 to 10.00% by weight. Its role is similar to that of nickel.
  • the chromium is present in an amount of 20.00 to 27.00% by weight, preferably 24 to 26% by weight. It also plays an important role in the good resistance against corrosion of the steels according to the invention. It may be possible to replace part of the chromium present in the composition with molybdenum on the basis of 1% molybdenum for 3% chromium.
  • the tungsten is present in an amount of 0.50 to 4.50% by weight, preferably 0.50 to 1.50% by weight. It makes it possible in particular to obtain good heat resistance of the compositions according to the invention.
  • the niobium is present in an amount of 0 to 2.5% by weight. It is a carburetor element which contributes to the hardness of the shade while having a favorable action on the heat resistance of steel compositions.
  • the nitrogen is present in an amount of 0.20 to 0.50% by weight in the compositions according to the invention. It contributes to the balance of the composition by its gamma influence, and to the hardness by its participation in the formation of niobium carbonitrides in particular.
  • Cobalt is an undesirable element the content of which is limited to a maximum of 1% by weight, preferably 0.5% by weight. Its content will be limited technically as much as possible and will be more particularly reduced to a trace state.
  • a second object of the invention consists of a process for the preparation of mechanical parts, characterized in that it comprises the following steps: a - constitution of a charge intended to obtain a chemical composition according to any of the variants previously exposed , b - preparation of said load, c - shaping of a blank of said mechanical part by molding, d- machining of said mechanical part from the blank, e - optional, heat treatment for use of said mechanical piece.
  • a process for the preparation of mechanical parts comprises the following stages: a - constitution of a charge intended to obtain a chemical composition according to any of the variants previously exposed, b - melting of said charge in a crucible, c - "molding" by centrifugation of a blank of said mechanical part, and machining of said mechanical part from the blank, e - as an option, heat treatment using said mechanical part.
  • This centrifugal molding process is traditionally used to form cobalt-based alloys, since it has great advantages, it consists in gradually introducing the mass of molten metal into a jacket heated in rotation, so that that a very thin layer of metal, on the order of a tenth of a millimeter, is deposited on the inside of the liner each turn. ie therefore independently of the previously deposited layers, which makes it possible to obtain a blank with a fine and isotropic structure, without micro-porosities.
  • the finished parts obtained after machining the blank are free from shrinkage, very resistant and have a very good surface condition.
  • the present inventors have therefore found, quite surprisingly, that it is perfectly possible to centrifuge mold the mechanical parts to be produced in the compositions according to the invention.
  • the melting of the steel compositions it can be carried out by any known process, in particular in an arc furnace.
  • the steel compositions according to the invention can in particular be in three different forms depending on their thermal state. These are the so-called “raw pouring” state, the state dissolved in temperatures from 1050 to 1150 ° C. and the stabilized state obtained by practicing one or more stabilization treatments of 700 at 900 ° C on a part in the raw casting state or in the dissolved state.
  • the thermal state essentially depends on the conditions under which the part will be used.
  • a stabilization treatment by aging comprising dissolving followed by slow cooling in a fluid such as air. This treatment allows the formation of precipitates in the steel matrix which will then no longer vary in hardness or dimensions.
  • a third object of the invention consists of the mechanical parts produced in the compositions and / or using the methods described above. Examples include valve seats, valve seats, friction rings and discs, gas turbine components, punches and cutting tools for hot work, knives and shear blades working at high temperature.
  • R p o, 2 conventional elastic limit at 0.2% deformation
  • A elongation
  • Z necking
  • HV Vickers hardness
  • HRC Rockwell hardness
  • grade ES the composition of which is as follows:
  • the tests were carried out on steel samples in the three previously defined thermal states, namely the raw casting state, the dissolved state and the stabilized state.
  • the reference material of the prior art chosen for comparison is a cobalt base alloy CoCr29W5, the composition of which is as follows: C 1, 10%
  • - 8 corresponds to a material having a few spots around the bites.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Heat Treatment Of Articles (AREA)
EP01949617A 2000-07-04 2001-07-03 Stahlzusammensetzungen, verfahren zu ihrer herstellung und daraus hergestellte formteile Expired - Lifetime EP1297192B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0008698 2000-07-04
FR0008698A FR2811336B1 (fr) 2000-07-04 2000-07-04 Compositions d'acier, procede pour son obtention et pieces fabriquees a partir de ces compositions
PCT/FR2001/002121 WO2002002830A1 (fr) 2000-07-04 2001-07-03 Compositions d'acier, procede pour son obtention et pieces fabriquees a partir de ces compositions

Publications (2)

Publication Number Publication Date
EP1297192A1 true EP1297192A1 (de) 2003-04-02
EP1297192B1 EP1297192B1 (de) 2010-09-01

Family

ID=8852104

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01949617A Expired - Lifetime EP1297192B1 (de) 2000-07-04 2001-07-03 Stahlzusammensetzungen, verfahren zu ihrer herstellung und daraus hergestellte formteile

Country Status (6)

Country Link
EP (1) EP1297192B1 (de)
AU (1) AU2001270741A1 (de)
DE (1) DE60142968D1 (de)
ES (1) ES2349399T3 (de)
FR (1) FR2811336B1 (de)
WO (1) WO2002002830A1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201716640D0 (en) * 2017-10-11 2017-11-22 Rolls Royce Plc Cobalt-free alloys
CN111850428B (zh) * 2019-04-28 2022-01-25 重庆三爱海陵实业有限责任公司 气门合金材料及气门

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2686116A (en) * 1952-06-18 1954-08-10 Crucible Steel Company Age hardening austenitic steel
FR1314540A (fr) * 1961-11-30 1963-01-11 Universal Cyclops Steel Corp Alliage d'acier inoxydable
DE3247568A1 (de) * 1981-12-23 1983-06-30 Kubota Ltd., Osaka Reaktorrohr fuer das thermische cracken oder reformieren von kohlenwasserstoffen
US4803045A (en) * 1986-10-24 1989-02-07 Electric Power Research Institute, Inc. Cobalt-free, iron-base hardfacing alloys
JP3721637B2 (ja) * 1996-04-22 2005-11-30 大同特殊鋼株式会社 含Caオーステナイト系耐熱鋼の製造方法
JPH10280907A (ja) * 1997-04-07 1998-10-20 Mitsubishi Heavy Ind Ltd 蒸気タービン動翼

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO0202830A1 *

Also Published As

Publication number Publication date
WO2002002830A1 (fr) 2002-01-10
AU2001270741A1 (en) 2002-01-14
FR2811336B1 (fr) 2002-08-30
FR2811336A1 (fr) 2002-01-11
DE60142968D1 (de) 2010-10-14
EP1297192B1 (de) 2010-09-01
ES2349399T3 (es) 2011-01-03

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