WO2022154807A1 - Dual step quenched martensite for bearing applications, and bearing produced according to this method - Google Patents
Dual step quenched martensite for bearing applications, and bearing produced according to this method Download PDFInfo
- Publication number
- WO2022154807A1 WO2022154807A1 PCT/US2021/013797 US2021013797W WO2022154807A1 WO 2022154807 A1 WO2022154807 A1 WO 2022154807A1 US 2021013797 W US2021013797 W US 2021013797W WO 2022154807 A1 WO2022154807 A1 WO 2022154807A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- steel component
- component
- temperature
- quenching
- steel
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 61
- 229910000734 martensite Inorganic materials 0.000 title claims abstract description 36
- 230000009977 dual effect Effects 0.000 title description 10
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 111
- 239000010959 steel Substances 0.000 claims abstract description 111
- 238000010791 quenching Methods 0.000 claims abstract description 77
- 238000010438 heat treatment Methods 0.000 claims abstract description 39
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 32
- 230000000171 quenching effect Effects 0.000 claims abstract description 27
- 230000000717 retained effect Effects 0.000 claims abstract description 23
- 229910001563 bainite Inorganic materials 0.000 claims abstract description 18
- 150000001247 metal acetylides Chemical class 0.000 claims abstract description 11
- 239000000463 material Substances 0.000 claims description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 13
- 229910052799 carbon Inorganic materials 0.000 claims description 13
- 238000005496 tempering Methods 0.000 claims description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 10
- 230000006698 induction Effects 0.000 claims description 6
- 229910052757 nitrogen Inorganic materials 0.000 claims description 5
- 230000008569 process Effects 0.000 abstract description 27
- 238000005096 rolling process Methods 0.000 abstract description 8
- 239000007789 gas Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 230000009466 transformation Effects 0.000 description 4
- 238000005279 austempering Methods 0.000 description 3
- 238000005255 carburizing Methods 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 2
- 239000002480 mineral oil Substances 0.000 description 2
- 235000010446 mineral oil Nutrition 0.000 description 2
- 229910001562 pearlite Inorganic materials 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000010561 standard procedure Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 210000001331 nose Anatomy 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/19—Hardening; Quenching with or without subsequent tempering by interrupted quenching
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/19—Hardening; Quenching with or without subsequent tempering by interrupted quenching
- C21D1/20—Isothermal quenching, e.g. bainitic hardening
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/25—Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/26—Methods of annealing
- C21D1/32—Soft annealing, e.g. spheroidising
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D6/00—Heat treatment of ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/40—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for rings; for bearing races
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/28—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases more than one element being applied in one step
- C23C8/30—Carbo-nitriding
- C23C8/32—Carbo-nitriding of ferrous surfaces
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/40—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using liquids, e.g. salt baths, liquid suspensions
- C23C8/52—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using liquids, e.g. salt baths, liquid suspensions more than one element being applied in one step
- C23C8/54—Carbo-nitriding
- C23C8/56—Carbo-nitriding of ferrous surfaces
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/80—After-treatment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/58—Raceways; Race rings
- F16C33/64—Special methods of manufacture
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/06—Surface hardening
- C21D1/09—Surface hardening by direct application of electrical or wave energy; by particle radiation
- C21D1/10—Surface hardening by direct application of electrical or wave energy; by particle radiation by electric induction
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2202/00—Solid materials defined by their properties
- F16C2202/02—Mechanical properties
- F16C2202/04—Hardness
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2202/00—Solid materials defined by their properties
- F16C2202/02—Mechanical properties
- F16C2202/06—Strength or rigidity
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/60—Ferrous alloys, e.g. steel alloys
- F16C2204/66—High carbon steel, i.e. carbon content above 0.8 wt%, e.g. through-hardenable steel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/10—Hardening, e.g. carburizing, carbo-nitriding
Definitions
- the present invention relates to through hardening and case hardening steel components, and more particularly to methods to achieve improved rolling contact fatigue (RCF) resistance characteristics in through hardened and case hardened steel components, and the components that are through hardened and case hardened using such methods.
- RCF rolling contact fatigue
- a heat treatment process that includes heating a steel component to a high temperature as an austenitizing step to change the microstructure of the steel to a pure austenite microstructure.
- the austenitizing process may include one or more heating cycles or one or more austenitization cycles.
- the component is then rapidly quenched to increase a hardness throughout a steel component, which increases the strength of the component.
- Different quench mediums include forced air or gas, still air or gas, quench oil, water and a liquid salt.
- the component may be quenched to a temperature, such as near or below a martensite start temperature (TMS), which enables further transformation of the microstructure of the component.
- TMS martensite start temperature
- the microstructure can be transformed from austenite to martensite, bainite, pearlite, or a combination of these microstructures.
- the component may be tempered after the component is quenched by re-heating the component to decrease a brittleness of the component.
- Case hardening is another known heat treatment process in which a hardened, “case region” is created only at the surface of the component and to a depth extending at most to two centimeters below the surface of the component.
- the case hardening can be done in two different manners. A first is by preferentially enriching the steel surface with carbon and/or nitrogen followed by a quenching step. A second is by preferentially austenitizing the near surface material (case region) by induction heating followed by a quench step.
- the improved heat treating process provides improved rolling contact fatigue (RCF) resistance, which has been found to improve the life of bearings used in high-debris applications, such as earth-moving and drilling equipment.
- debris e.g., sand, grit, etc.
- bearing steel heat treated with the process described below increases the life expectancy of these bearings that see significant debris denting.
- the process does not necessarily prevent or reduce the denting, but rather improves the rolling contact fatigue (RCF) resistance such that even when heavily dented by debris, the bearings still last longer.
- the present disclosure provides, in one aspect, a method for through hardening steel, and particularly bearing steel components.
- the method includes austenitizing a steel component, quenching the steel component to a first quench temperature below the martensite start temperature (Ms) and within a range of 0.8Ms to 0.98Ms, holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours, and quenching the steel component to a second quench temperature below 100 degrees C.
- Ms martensite start temperature
- the resulting component has a through hardness of at least 50 HRC, a retained austenite content of at least 10% to a depth of at least 1 mm from a surface of the steel component, residual tensile stresses to a depth of at least 1 mm from the surface of the steel component, and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite throughout a cross-section of the steel component.
- the present disclosure provides, in another aspect, a method for case hardening steel, and particularly bearing steel components.
- the method includes preferentially austenitizing a near surface material of the steel component by induction heating and quenching the steel component to a first quench temperature to create a case region. Because of preferential austenitizing and quenching, the case region has a higher hardness than the material in the core, and in this context, the case has hardness of at least 50HRC.
- the case region has a depth from a surface of the steel component ranging from 100 microns to 1 cm, and the first quench temperature is below a martensite start temperature (Ms) of material in the case region and within a range of 0.8Ms to 0.98Ms.
- Ms martensite start temperature
- the method further includes holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours, and quenching the steel component to a second quench temperature below 100 degrees C.
- the resulting steel component has a hardness of at least 50 HRC in the case region of the steel component, a retained austenite content of at least 10% to a depth of at least 100 microns from the surface of the steel component, residual compressive stresses to a depth of at least 100 microns to 2 cm from the surface of the steel component, and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite in the case region of the steel component.
- the present disclosure provides, in another aspect, a method for case hardening steel, and particularly bearing steel components.
- the method includes diffusing carbon and/or nitrogen into a surface of the steel component while austenitizing the steel component and quenching the steel component to a first quench temperature to create a case region.
- the case region has higher hardness than the material in the core, and in this context, the case has a hardness of at least 50HRC.
- the case region has a depth from a surface of the steel component ranging from 100 microns to 1 cm, and the first quench temperature is below a martensite start temperature (Ms) of material in the case region and within a range of 0.8Ms to 0.98Ms.
- Ms martensite start temperature
- the method further includes holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours, and quenching the steel component to a second quench temperature below 100 degrees C.
- the resulting steel component has a hardness of at least 50 HRC to a depth of at least 100 microns from the surface of the steel component, a retained austenite content of at least 10% to a depth of at least 100 microns from the surface of the steel component, residual compressive stresses to a depth of at least 100 microns to 2 cm from the surface of the steel component, and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite in the case region of the steel component.
- Fig. 1 is a time-temperature-transformation chart of the austenite to martensite+bainite+retained austenite conversion in various stages.
- Figs. 2 illustrates the microstructure of an example component that has been heat treated using the method described herein.
- Fig. 3 is an alternative time-temperature-transformation chart of the austenite to martensite+bainite+retained austenite conversion in various stages.
- Fig. 4 illustrates a graph of bearing life for bearings produced by the heat treating processes of Figs. 1 and 3 as compared to other conventional heat treating processes.
- the present disclosure is related to a heat treatment process explained using an example of austempering of bearing steel grades, such as 100CrMo7-3 or!00CrMnSi6-4, or any other steel grade having a carbon composition of at least 0.7 weight% (wt%).
- the typical chemical composition of 100CrMo7-3 steel includes 0.9 wt% carbon, 0.3 wt% silicon, 0.7 wt% manganese, 1.8 wt% chromium, 0.3 wt% molybdenum.
- the typical chemical composition of 100CrMnSi6-4 steel includes 0.9 wt% carbon, 0.6 wt% silicon, 1.1 wt% manganese, 1.5 wt% chromium.
- Typical through hardening bearing steels with carbon content of more than 0.7% can be found in the ISO standard ISO 683-17:2014(en).
- the through hardening process described herein is a dual step quenched martensite process for a bearing steel component (e.g., a bearing race or roller, such as a bearing steel component 20 represented in the microstructure view of Fig. 2).
- the steel component may first be austenitized throughout its cross section by heating the component to an initial temperature Ti, which in the illustrated embodiment is a temperature from 700 degrees Celsius to 1000 degrees Celsius. To fully austenitize, the component is held at the temperature Ti for a duration of time 5 minutes to 240 minutes. One or more heating cycles may be used to austenitize the component or one or more austenitizing cycles may be used.
- Fig. 1 depicts a time-temperature-transformation (TTT) chart 4 showing a transformation curve 8 of the heat treatment process described herein. Beginning at a time ti, the component is quenched from the initial temperature Ti to a temperature T2 by a time t2. In some instances, the quench rate from Ti to T2 also touches and/or crosses the noses of the C-shaped curves. If that were the case, the microstructure could contain small amounts of pearlite and/or upper bainite.
- TTTT time-temperature-transformation
- the temperature T2 is below the martensite start temperature TMS of the material, such as from 0.8*TMS to 0.98*TMS, and in some instances from 0.8*TMS to 0.9*TMS.
- TMS is about 200 degrees Celsius, and the temperature T2 ranges from 160 degrees C to 195 degrees C. For other steels having higher a higher TMS temperature, the T2 range would also be correspondingly higher.
- the initial amount of martensite formed upon reaching the quench temperature T2 is typically about 5% to about 40%.
- the component is then held at the temperature T2 for a time interval Ati from time t2 to time b.
- the quench and holding medium includes a liquid salt bath or a quench oil bath.
- the time interval Ati may be any length of time from 0.5 hours to 8 hours, and alternatively may be from 0.5 hours to 4 hours.
- the component is held at temperature T2, and during this time, isothermal tempering of the formed martensite occurs.
- isothermal tempering of the formed martensite occurs.
- some formation of bainite e.g., 5-30%) has been observed during this isothermal tempering.
- the component is quenched to a temperature at or below a room temperature, 100 degrees Celsius, or an ambient temperature.
- the quench medium includes water, oil, still air or gas, forced air or gas.
- the resulting microstructure has been found to contain 5-30% bainite (lower bainite), 10-35% retained austenite, less than 7% carbides, and the remainder being martensite.
- Fig. 2 illustrates the microstructure, with areas labeled “B” for bainite, “RA” for retained austenite, and “M” for martensite. Carbides are also indicated.
- the component has a through hardness of at least 50 HRC and retained austenite content of at least 10% to a depth of at least 1 mm from the surface of the steel component.
- the component also exhibits residual tensile stresses to a depth of at least 1mm from the surface of the steel component. Those residual stresses range from 10 to 150 MPa.
- the component may be tempered after the second quench or may be used without tempering.
- the steel component may be heated to a fourth temperature that is from 100 degrees Celsius to 350 degrees Celsius and quenched to an ambient or room temperature.
- the through hardness of the steel part remains at least 50 Rockwell C (HRC) throughout the cross-section of the component after the quench tempering heat treatment (i.e., after t4).
- the quench tempering heat treatment 12 after t4 can be done to reduce the amount of retained austenite to less than 15%.
- the quench tempering heat treatment 12 begins at time t4 and includes heating the component to a temperature T4 for a short period of time At2, after which the component is again quenched to a temperature at or below a room temperature, 100 degrees Celsius, or an ambient temperature.
- the quench tempering heat treatment 12 is optional.
- the resulting microstructure increase the rolling contact fatigue life of the component, thus enabling the components to last longer.
- the increased rolling contact fatigue life is evident from the bearing life testing as shown in Fig. 4.
- Rolling contact surfaces were dented by debris as per standard procedures and then life tested in viscosity grade 10 mineral oil.
- Fig. 4 shows the life of bearings made using conventional heat treats that are used in the field as compared to the inventive dual quench martensite heat treatment described above.
- the improved fatigue resistance properties are attributed to martensite forming at the second quench step and the bainite formed during the isothermal tempering.
- Fig. 3 is an alternative time-temperature-transformation chart 30 of the austenite to martensite+bainite+retained austenite conversion in various stages.
- the steel used in the illustrated example is bearing steel grades, such as 100CrMo7-3 orl00CrMnSi6-4, or any other steel having a carbon composition of at least 0.7 wt%.
- the heat treatment process shown in the alternative time-temperature-transformation chart 30 of Fig. 3 includes an additional heating and quenching cycle 34 that may be added to the heat treatment process 4 described above.
- the component is first heated to a high temperature of T-2, which is a carbide dissolution temperature of approximately 900 to 1100 degrees Celsius. This heating stage has a duration Ats of at least 30 minutes.
- the duration Ats is from 30 minutes to 300 minutes.
- the duration Ats is inclusive of the heating time, holding time, and cooling time of the heating stage.
- the temperature T-2 is above the Ai and the ACM temperatures for the steel component.
- the Ai transformation temperature is the temperature at which the ferritic phase of the steel starts to transform into austenite.
- the ACM temperature is the temperature at which the ferritic phase of the steel is completely transformed into austenite.
- T-i is less than 500 degrees Celsius, but in one embodiment may be less than 300 degrees Celsius.
- the component is then reheated to a temperature above the Ai temperature, and may also be above the ACM temperature.
- the ACM transformation temperature is the temperature at which the ferrite phase of the steel completely transforms into austenite. In the illustrated example, this temperature is the same as the temperature Ti of the heat treatment cycle described in Fig. 1.
- the temperature of the second heating stage may be within the range of 750 to 900 degrees Celsius.
- the heat treatment cycle of Fig. 3 is identical to the heat treatment cycle of Fig. 1. However, the additional heating stage results in components with improved fatigue resistance and refined microstructures. Thus, the heat treatment cycle of Fig. 3 may be better for some applications than the heat treatment cycle of Fig. 1.
- Fig. 4 illustrates the results of bearing life testing conducted for bearings heat- treated using the Dual Quench Martensite processes of Fig. 1, as compared to bearings that underwent different heat treat processes.
- Rolling contact surfaces of all the bearings were debris dented first as per a standard procedure, and then life tested in a viscosity grade 10 mineral oil. In contrast to smoother bearing surfaces, the dented bearing surfaces decrease the bearing lives drastically. This testing is done typically to evaluate the durability of bearings used in high-debris applications, such as earth-moving and drilling equipment.
- the illustrated Heat Treat 2 results depict results from an austempering process.
- the illustrated Heat Treat 3 results depict results from a dual step austempering process.
- the illustrated Heat Treat 4 results depict a case carburized bearing with martensitic microstructure. Also shown for comparison purposes is the estimated bearing life without debris denting of the bearing races.
- a case hardening process can also be performed in conjunction with, or after, a case hardening process is performed on the bearing component.
- a case carburizing process only the near surface material can be hardened by diffusing carbon and/or nitrogen into the steel surface during the austenitization step followed by quenching.
- the case region can be created in a separate process prior to the Dual Quench Martensite process 4 described above with respect to Fig. 1, or simultaneously during the austenitizing step of the Dual Quench Martensite processes described above with respect to Fig. 1.
- the Ms temperature is based on the material in the case region.
- the near surface material can be hardened to create the case region by selectively heating the near surface material via induction heating followed by quenching.
- the induction heating of the near surface region functions as the austenitizing step(s) of the Dual Quench Martensite processes 4 or 30 described above with respect to Figs. 1 and 3.
- the Ms temperature is based on the material in the case region.
- the case-hardened region typically has a depth of 100 microns to 1 cm, a hardness of at least 50 HRC in that case-hardened region, and the microstructure has at least 10% retained austenite in that case hardened region.
- the overall resulting microstructure in the case region has been found to contain 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and the remainder being martensite.
- residual compressive stresses at the surface region to a depth of at least 100 microns to 2 cm have been observed.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Heat Treatment Of Articles (AREA)
Abstract
A heat treatment process for through hardening results in improved rolling contact fatigue (RCF) resistance. The method includes austenitizing a steel component, quenching the steel component to a first quench temperature below the martensite start temperature (Ms), holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours, and quenching the steel component to a second quench temperature below 100 degrees C. The resulting component has a through hardness of at least 50 HRC, a retained austenite content of at least 10% to a depth of at least 1 mm from a surface of the steel component, residual tensile stresses to a depth of at least 1 mm from the surface of the steel component, and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite throughout a cross-section of the steel component.
Description
DUAL STEP QUENCHED MARTENSITE FOR BEARING APPLICATIONS, AND BEARING PRODUCED ACCORDING TO THIS METHOD
[0001] The present invention relates to through hardening and case hardening steel components, and more particularly to methods to achieve improved rolling contact fatigue (RCF) resistance characteristics in through hardened and case hardened steel components, and the components that are through hardened and case hardened using such methods.
BACKGROUND
[0002] Through hardening is a heat treatment process that includes heating a steel component to a high temperature as an austenitizing step to change the microstructure of the steel to a pure austenite microstructure. The austenitizing process may include one or more heating cycles or one or more austenitization cycles. The component is then rapidly quenched to increase a hardness throughout a steel component, which increases the strength of the component. Different quench mediums include forced air or gas, still air or gas, quench oil, water and a liquid salt. The component may be quenched to a temperature, such as near or below a martensite start temperature (TMS), which enables further transformation of the microstructure of the component. For example, the microstructure can be transformed from austenite to martensite, bainite, pearlite, or a combination of these microstructures. Additionally, the component may be tempered after the component is quenched by re-heating the component to decrease a brittleness of the component.
[0003] Case hardening is another known heat treatment process in which a hardened, “case region” is created only at the surface of the component and to a depth extending at most to two centimeters below the surface of the component. The case hardening can be done in two different manners. A first is by preferentially enriching the steel surface with carbon and/or nitrogen followed by a quenching step. A second is by preferentially austenitizing the near surface material (case region) by induction heating followed by a quench step.
SUMMARY
[0004] In one aspect, the improved heat treating process provides improved rolling contact fatigue (RCF) resistance, which has been found to improve the life of bearings used in high-debris applications, such as earth-moving and drilling equipment. In those applications, debris (e.g., sand, grit, etc.) gets into the bearing and dents the races and/or rollers. It has been found that bearing steel heat treated with the process described below
increases the life expectancy of these bearings that see significant debris denting. To be clear, the process does not necessarily prevent or reduce the denting, but rather improves the rolling contact fatigue (RCF) resistance such that even when heavily dented by debris, the bearings still last longer.
[0005] The present disclosure provides, in one aspect, a method for through hardening steel, and particularly bearing steel components. The method includes austenitizing a steel component, quenching the steel component to a first quench temperature below the martensite start temperature (Ms) and within a range of 0.8Ms to 0.98Ms, holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours, and quenching the steel component to a second quench temperature below 100 degrees C. The resulting component has a through hardness of at least 50 HRC, a retained austenite content of at least 10% to a depth of at least 1 mm from a surface of the steel component, residual tensile stresses to a depth of at least 1 mm from the surface of the steel component, and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite throughout a cross-section of the steel component.
[0006] The present disclosure provides, in another aspect, a method for case hardening steel, and particularly bearing steel components. The method includes preferentially austenitizing a near surface material of the steel component by induction heating and quenching the steel component to a first quench temperature to create a case region. Because of preferential austenitizing and quenching, the case region has a higher hardness than the material in the core, and in this context, the case has hardness of at least 50HRC. The case region has a depth from a surface of the steel component ranging from 100 microns to 1 cm, and the first quench temperature is below a martensite start temperature (Ms) of material in the case region and within a range of 0.8Ms to 0.98Ms. The method further includes holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours, and quenching the steel component to a second quench temperature below 100 degrees C. The resulting steel component has a hardness of at least 50 HRC in the case region of the steel component, a retained austenite content of at least 10% to a depth of at least 100 microns from the surface of the steel component, residual compressive stresses to a depth of at least 100 microns to 2 cm from the surface of the steel component, and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite in the case region of the steel component.
[0007] The present disclosure provides, in another aspect, a method for case hardening steel, and particularly bearing steel components. The method includes diffusing carbon and/or nitrogen into a surface of the steel component while austenitizing the steel component and quenching the steel component to a first quench temperature to create a case region. Because of enriched carbon and/or nitrogen in the near surface material, the case region has higher hardness than the material in the core, and in this context, the case has a hardness of at least 50HRC. The case region has a depth from a surface of the steel component ranging from 100 microns to 1 cm, and the first quench temperature is below a martensite start temperature (Ms) of material in the case region and within a range of 0.8Ms to 0.98Ms. The method further includes holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours, and quenching the steel component to a second quench temperature below 100 degrees C. The resulting steel component has a hardness of at least 50 HRC to a depth of at least 100 microns from the surface of the steel component, a retained austenite content of at least 10% to a depth of at least 100 microns from the surface of the steel component, residual compressive stresses to a depth of at least 100 microns to 2 cm from the surface of the steel component, and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite in the case region of the steel component.
[0008] Other features and aspects of the invention will become apparent by consideration of the following detailed description and accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0009] Fig. 1 is a time-temperature-transformation chart of the austenite to martensite+bainite+retained austenite conversion in various stages.
[0010] Figs. 2 illustrates the microstructure of an example component that has been heat treated using the method described herein.
[0011] Fig. 3 is an alternative time-temperature-transformation chart of the austenite to martensite+bainite+retained austenite conversion in various stages.
[0012] Fig. 4 illustrates a graph of bearing life for bearings produced by the heat treating processes of Figs. 1 and 3 as compared to other conventional heat treating processes.
[0013] Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting.
DETAILED DESCRIPTION
[0014] The present disclosure is related to a heat treatment process explained using an example of austempering of bearing steel grades, such as 100CrMo7-3 or!00CrMnSi6-4, or any other steel grade having a carbon composition of at least 0.7 weight% (wt%). However, those of ordinary skill in the art would understand that the inventive heat treatment process could be applied to other steels as well. The typical chemical composition of 100CrMo7-3 steel includes 0.9 wt% carbon, 0.3 wt% silicon, 0.7 wt% manganese, 1.8 wt% chromium, 0.3 wt% molybdenum. The typical chemical composition of 100CrMnSi6-4 steel includes 0.9 wt% carbon, 0.6 wt% silicon, 1.1 wt% manganese, 1.5 wt% chromium. Typical through hardening bearing steels with carbon content of more than 0.7% can be found in the ISO standard ISO 683-17:2014(en).
[0015] The through hardening process described herein is a dual step quenched martensite process for a bearing steel component (e.g., a bearing race or roller, such as a bearing steel component 20 represented in the microstructure view of Fig. 2). As shown in Fig. 1, the steel component may first be austenitized throughout its cross section by heating the component to an initial temperature Ti, which in the illustrated embodiment is a temperature from 700 degrees Celsius to 1000 degrees Celsius. To fully austenitize, the component is held at the temperature Ti for a duration of time 5 minutes to 240 minutes. One or more heating cycles may be used to austenitize the component or one or more austenitizing cycles may be used. After the austenitization is complete and the component has a microstructure of austenite and some carbide particles, the component is then heat treated using the dual step quenched martensite process described herein beginning at an initial time to, which is shown in Fig. 1.
[0016] Fig. 1 depicts a time-temperature-transformation (TTT) chart 4 showing a transformation curve 8 of the heat treatment process described herein. Beginning at a time ti, the component is quenched from the initial temperature Ti to a temperature T2 by a time t2. In some instances, the quench rate from Ti to T2 also touches and/or crosses the noses of the C-shaped curves. If that were the case, the microstructure could contain small amounts of pearlite and/or upper bainite. The temperature T2 is below the martensite start temperature TMS of the material, such as from 0.8*TMS to 0.98*TMS, and in some instances from 0.8*TMS to 0.9*TMS. For the example type of bearing steel described herein, TMS is about 200 degrees Celsius, and the temperature T2 ranges from 160 degrees C to 195 degrees C. For other steels having higher a higher TMS temperature, the T2 range would also be correspondingly higher. The initial amount of martensite formed upon reaching the quench temperature T2 is typically about 5% to about 40%. The component is then held at the temperature T2 for a time interval Ati from time t2 to time b. The quench and holding medium includes a liquid salt bath or a quench oil bath. The time interval Ati may be any length of time from 0.5 hours to 8 hours, and alternatively may be from 0.5 hours to 4 hours. During the time interval Ati, the component is held at temperature T2, and during this time, isothermal tempering of the formed martensite occurs. In addition, some formation of bainite (e.g., 5-30%) has been observed during this isothermal tempering.
[0017] At time t3, the component is quenched to a temperature at or below a room temperature, 100 degrees Celsius, or an ambient temperature. The quench medium includes water, oil, still air or gas, forced air or gas. After quenching, the resulting microstructure has been found to contain 5-30% bainite (lower bainite), 10-35% retained austenite, less than 7% carbides, and the remainder being martensite. Fig. 2 illustrates the microstructure, with areas labeled “B” for bainite, “RA” for retained austenite, and “M” for martensite. Carbides are also indicated. The component has a through hardness of at least 50 HRC and retained austenite content of at least 10% to a depth of at least 1 mm from the surface of the steel component. The component also exhibits residual tensile stresses to a depth of at least 1mm from the surface of the steel component. Those residual stresses range from 10 to 150 MPa.
[0018] The component may be tempered after the second quench or may be used without tempering. To temper the steel component, the steel component may be heated to a fourth temperature that is from 100 degrees Celsius to 350 degrees Celsius and quenched to an ambient or room temperature. The through hardness of the steel part remains at least 50
Rockwell C (HRC) throughout the cross-section of the component after the quench tempering heat treatment (i.e., after t4). The quench tempering heat treatment 12 after t4 can be done to reduce the amount of retained austenite to less than 15%. The quench tempering heat treatment 12 begins at time t4 and includes heating the component to a temperature T4 for a short period of time At2, after which the component is again quenched to a temperature at or below a room temperature, 100 degrees Celsius, or an ambient temperature. The quench tempering heat treatment 12 is optional.
[0019] The resulting microstructure increase the rolling contact fatigue life of the component, thus enabling the components to last longer. The increased rolling contact fatigue life is evident from the bearing life testing as shown in Fig. 4. Rolling contact surfaces were dented by debris as per standard procedures and then life tested in viscosity grade 10 mineral oil. Fig. 4 shows the life of bearings made using conventional heat treats that are used in the field as compared to the inventive dual quench martensite heat treatment described above. The improved fatigue resistance properties are attributed to martensite forming at the second quench step and the bainite formed during the isothermal tempering.
[0020] Fig. 3 is an alternative time-temperature-transformation chart 30 of the austenite to martensite+bainite+retained austenite conversion in various stages. The steel used in the illustrated example is bearing steel grades, such as 100CrMo7-3 orl00CrMnSi6-4, or any other steel having a carbon composition of at least 0.7 wt%. The heat treatment process shown in the alternative time-temperature-transformation chart 30 of Fig. 3 includes an additional heating and quenching cycle 34 that may be added to the heat treatment process 4 described above. In the illustrated example, the component is first heated to a high temperature of T-2, which is a carbide dissolution temperature of approximately 900 to 1100 degrees Celsius. This heating stage has a duration Ats of at least 30 minutes. In one example, the duration Ats is from 30 minutes to 300 minutes. The duration Ats is inclusive of the heating time, holding time, and cooling time of the heating stage. The temperature T-2 is above the Ai and the ACM temperatures for the steel component. The Ai transformation temperature is the temperature at which the ferritic phase of the steel starts to transform into austenite. The ACM temperature is the temperature at which the ferritic phase of the steel is completely transformed into austenite. During this heat treatment stage 34 at least some of the carbides in the component are dissolved. After the heating stage 34, the component is
quenched to a temperature T-i. The temperature T-i is less than 500 degrees Celsius, but in one embodiment may be less than 300 degrees Celsius.
[0021] Next, the component is then reheated to a temperature above the Ai temperature, and may also be above the ACM temperature. The ACM transformation temperature is the temperature at which the ferrite phase of the steel completely transforms into austenite. In the illustrated example, this temperature is the same as the temperature Ti of the heat treatment cycle described in Fig. 1. Alternatively, the temperature of the second heating stage may be within the range of 750 to 900 degrees Celsius. Following the second heating stage, the heat treatment cycle of Fig. 3 is identical to the heat treatment cycle of Fig. 1. However, the additional heating stage results in components with improved fatigue resistance and refined microstructures. Thus, the heat treatment cycle of Fig. 3 may be better for some applications than the heat treatment cycle of Fig. 1.
[0022] Fig. 4 illustrates the results of bearing life testing conducted for bearings heat- treated using the Dual Quench Martensite processes of Fig. 1, as compared to bearings that underwent different heat treat processes. Rolling contact surfaces of all the bearings were debris dented first as per a standard procedure, and then life tested in a viscosity grade 10 mineral oil. In contrast to smoother bearing surfaces, the dented bearing surfaces decrease the bearing lives drastically. This testing is done typically to evaluate the durability of bearings used in high-debris applications, such as earth-moving and drilling equipment. In Fig. 4, the illustrated Heat Treat 2 results depict results from an austempering process. The illustrated Heat Treat 3 results depict results from a dual step austempering process. The illustrated Heat Treat 4 results depict a case carburized bearing with martensitic microstructure. Also shown for comparison purposes is the estimated bearing life without debris denting of the bearing races.
[0023] The above-described processes described with respect to Fig. 1 can also be performed in conjunction with, or after, a case hardening process is performed on the bearing component. For example, in a case carburizing process, only the near surface material can be hardened by diffusing carbon and/or nitrogen into the steel surface during the austenitization step followed by quenching. With case carburizing, the case region can be created in a separate process prior to the Dual Quench Martensite process 4 described above with respect to Fig. 1, or simultaneously during the austenitizing step of the Dual Quench Martensite processes described above with respect to Fig. 1. When quenching below the Ms
temperature, the Ms temperature is based on the material in the case region. It should also be noted that a lower carbon steel (i.e., lower than 0.7 wt. %) may be used as the base material for this case carburized bearing component, but that the additional diffused carbon in the case region will lead to similar results observed in the case region.
[0024] Alternatively to case carburizing, only the near surface material can be hardened to create the case region by selectively heating the near surface material via induction heating followed by quenching. In this case, the induction heating of the near surface region functions as the austenitizing step(s) of the Dual Quench Martensite processes 4 or 30 described above with respect to Figs. 1 and 3. With this induction hardening process, when quenching below the Ms temperature, the Ms temperature is based on the material in the case region.
[0025] In either method of case hardening, the case-hardened region typically has a depth of 100 microns to 1 cm, a hardness of at least 50 HRC in that case-hardened region, and the microstructure has at least 10% retained austenite in that case hardened region. The overall resulting microstructure in the case region has been found to contain 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and the remainder being martensite. In these case- hardened components, residual compressive stresses at the surface region to a depth of at least 100 microns to 2 cm have been observed.
[0026] Although the invention has been described in detail with reference to certain preferred embodiments, variations and modifications exist within the scope and spirit of one or more independent aspects of the invention as described.
Claims
1. A method of through hardening a bearing steel component with at least 0.7% weight of carbon, the method comprising: austenitizing the steel component to an austenitizing temperature; quenching the steel component to a first quench temperature below a martensite start temperature (Ms) and within a range of 0.8Ms to 0.98Ms; holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours; and quenching the steel component to a second quench temperature below 100 degrees C; wherein the resulting steel component has a through hardness of at least 50 HRC; a retained austenite content of at least 10% to a depth of at least 1 mm from a surface of the steel component; residual tensile stresses to a depth of at least 1 mm from the surface of the steel component; and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite throughout a cross-section of the steel component.
2. The method of claim 1, wherein the austenitizing temperature is from 700 to 1000 degrees Celsius.
3. The method of claim 1, wherein the first quench temperature ranges from 160 degrees Celsius to 195 degrees Celsius.
4. The method of claim 1, wherein the residual tensile stresses range from 10 to 150 MPa.
5. The method of claim 1, further comprising tempering the steel component after quenching the steel component to the second quench temperature.
6. A bearing component through-hardened according to the method of claim 1.
9
7. A method of case hardening a bearing steel component, the method comprising: preferentially austenitizing a near surface material of the steel component by induction heating; quenching the steel component to a first quench temperature to create a case region, the case region having a depth from a surface of the steel component ranging from 100 microns to 1 cm, the first quench temperature being below a martensite start temperature (Ms) of material in the case region and within a range of 0.8Ms to 0.98Ms; holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours; and quenching the steel component to a second quench temperature below 100 degrees C; wherein the resulting steel component has a hardness of at least 50 HRC in the case region; a retained austenite content of at least 10% to a depth of at least 100 microns from the surface of the steel component; residual compressive stresses to a depth of at least 100 microns to 2 cm from the surface of the steel component; and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite in the case region of the steel component.
8. The method of claim 7, wherein the first quench temperature ranges from 160 degrees Celsius to 195 degrees Celsius.
9. The method of claim 7, further comprising tempering the steel component after quenching the steel component to the second quench temperature.
10. A bearing component case-hardened according to the method of claim 7.
11. A method of case hardening a bearing steel component, the method comprising: diffusing carbon and/or nitrogen into a surface of the steel component while austenitizing the steel component; quenching the steel component to a first quench temperature to create a case region, the case region having a depth from a surface of the steel component ranging from 100 microns to 1 cm, the first quench temperature being below a martensite start temperature (Ms) of material in the case region and within a range of 0.8Ms to 0.98Ms; holding the steel component at the first quench temperature for a duration of 0.5 hours to 8 hours; and quenching the steel component to a second quench temperature below 100 degrees C; wherein the resulting steel component has a hardness of at least 50 HRC in the case region; a retained austenite content of at least 10% to a depth of at least 100 microns from the surface of the steel component; residual compressive stresses to a depth of at least 100 microns to 2 cm from the surface of the steel component; and a microstructure of 5-30% bainite, 10-35% retained austenite, less than 7% carbides, and a remainder of martensite in the case region of the steel component.
12. The method of claim 11, further comprising tempering the steel component after quenching the steel component to the second quench temperature.
13. The method of claim 11, wherein the method further provides quenching the steel component after diffusing carbon into the surface of the steel component, and austentizing the steel component again prior to quenching the steel component to the first quench temperature.
14. A bearing component case-hardened according to the method of claim 11.
15. A bearing component case-hardened according to the method of claim 13.
11
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2021/013797 WO2022154807A1 (en) | 2021-01-18 | 2021-01-18 | Dual step quenched martensite for bearing applications, and bearing produced according to this method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2021/013797 WO2022154807A1 (en) | 2021-01-18 | 2021-01-18 | Dual step quenched martensite for bearing applications, and bearing produced according to this method |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2022154807A1 true WO2022154807A1 (en) | 2022-07-21 |
Family
ID=74557267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2021/013797 WO2022154807A1 (en) | 2021-01-18 | 2021-01-18 | Dual step quenched martensite for bearing applications, and bearing produced according to this method |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2022154807A1 (en) |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19849681C1 (en) * | 1998-10-28 | 2000-01-05 | Skf Gmbh | Heat treating components of steel or cast iron |
CN108285965A (en) * | 2018-01-15 | 2018-07-17 | 中国科学院理化技术研究所 | Quenching-partitioning-deep cooling-tempering treatment process for steel material |
-
2021
- 2021-01-18 WO PCT/US2021/013797 patent/WO2022154807A1/en active Application Filing
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19849681C1 (en) * | 1998-10-28 | 2000-01-05 | Skf Gmbh | Heat treating components of steel or cast iron |
CN108285965A (en) * | 2018-01-15 | 2018-07-17 | 中国科学院理化技术研究所 | Quenching-partitioning-deep cooling-tempering treatment process for steel material |
Non-Patent Citations (1)
Title |
---|
PLATL JAN ET AL: "Determination of Martensite Start Temperature of High-Speed Steels Based on Thermodynamic Calculations", STEEL RESEARCH INTERNATIONAL., vol. 91, no. 8, 3 June 2020 (2020-06-03), DE, pages 2000063, XP055837930, ISSN: 1611-3683, Retrieved from the Internet <URL:https://onlinelibrary.wiley.com/doi/full-xml/10.1002/srin.202000063> [retrieved on 20210909], DOI: 10.1002/srin.202000063 * |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8562767B2 (en) | Method of heat treating a steel bearing component | |
US5338377A (en) | Ball-and-roller bearing | |
JP4800444B2 (en) | Steel for machine structure for surface hardening and parts for machine structure | |
JP5700322B2 (en) | Workpiece made of steel hardened to the core zone formed for rolling loads and method for heat treatment | |
US20110073222A1 (en) | Heat-Treatment Process for a Steel | |
KR910003515B1 (en) | Case hardening method for steel parts | |
CN100532887C (en) | Gear part and method of producing thereof | |
JP4408698B2 (en) | Parts formed from steel | |
US20190300977A1 (en) | Method of steel processing combining thermal and mechanical surface treatment to control metallurgical phase and mechanical response | |
CN114574668A (en) | Method for hardening surface of metal member | |
US20220010395A1 (en) | High surface compressive stress for through hardening | |
CN104540970A (en) | Method for heat treating a steel component and a steel component | |
WO2019223491A1 (en) | Method for manufacturing high-strength crankshaft | |
JPH06173967A (en) | Outer race for constant velocity joint | |
JP2015531029A (en) | Method for heat treating steel components and steel components | |
WO2022154807A1 (en) | Dual step quenched martensite for bearing applications, and bearing produced according to this method | |
Dossett | Introduction to cast iron heat treatment | |
WO2019223078A1 (en) | Medium-temperature gas nitrocarburizing quenching process | |
Senatorski et al. | Wear resistance characteristics of thermo-chemically treated structural steels | |
JPH02149616A (en) | Manufacture of nitrided steel member | |
Bhagyalaxmi et al. | Effect of heat treatment and mechanical characterization of AISI 4140 steel | |
Fortini et al. | Heat treatment of bearing steels: An industrial investigation | |
JP2008248282A (en) | Induction hardened component and manufacturing method thereof | |
Smoljan et al. | An analysis of induction hardening of ferritic ductile iron | |
GB2328953A (en) | A process for hardening high alloy steels |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 21703800 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 21703800 Country of ref document: EP Kind code of ref document: A1 |