WO2021165532A1 - Verfahren zum induktiven randschichthärten - Google Patents
Verfahren zum induktiven randschichthärten Download PDFInfo
- Publication number
- WO2021165532A1 WO2021165532A1 PCT/EP2021/054327 EP2021054327W WO2021165532A1 WO 2021165532 A1 WO2021165532 A1 WO 2021165532A1 EP 2021054327 W EP2021054327 W EP 2021054327W WO 2021165532 A1 WO2021165532 A1 WO 2021165532A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- inductor
- end zone
- hardened
- zone
- leading
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 39
- 230000001939 inductive effect Effects 0.000 title claims abstract description 9
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 8
- 239000010959 steel Substances 0.000 claims abstract description 8
- 238000010438 heat treatment Methods 0.000 claims description 31
- 238000010791 quenching Methods 0.000 claims description 21
- 230000000171 quenching effect Effects 0.000 claims description 16
- 239000002344 surface layer Substances 0.000 claims description 12
- 230000002093 peripheral effect Effects 0.000 claims description 7
- 230000000712 assembly Effects 0.000 claims description 6
- 238000000429 assembly Methods 0.000 claims description 6
- 239000007921 spray Substances 0.000 abstract 2
- 230000005672 electromagnetic field Effects 0.000 description 9
- 239000010410 layer Substances 0.000 description 7
- 238000005096 rolling process Methods 0.000 description 2
- 208000032544 Cicatrix Diseases 0.000 description 1
- 206010039580 Scar Diseases 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 208000014745 severe cutaneous adverse reaction Diseases 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 230000007704 transition Effects 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
- C21D1/06—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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/62—Quenching devices
- C21D1/667—Quenching devices for spray 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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/34—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for tyres; for rims
-
- 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
- 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
- C21D2221/00—Treating localised areas of an article
- C21D2221/01—End parts (e.g. leading, trailing end)
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Definitions
- the invention relates to a method for inductive surface hardening of a surface which surrounds an annular component made of hardenable steel.
- Process for inductive hardening of a surface layer refers to processes in which the edge layer of the steel material adjoining the surface to be hardened, of which the component supporting the surface is made, is heated to hardening temperature by means of an electromagnetic field induced in the component and in which the section of the edge layer heated in this way is then cooled sufficiently quickly by the application of a suitable quenching agent to produce a hardened structure in the relevant edge section.
- the ring-shaped components on which surfaces can be surface hardened by means of the method according to the invention are typically around bearing rings for large roller bearings or the like.
- Such bearing rings are used, for example, for rolling bearings in which the rotors of large wind power plants are stored, or for rolling bearings in which tower cranes and the like are rotatably mounted about a vertical axis.
- the diameters of such bearings are typically in the range of 40-1000 cm.
- Circumferential surfaces of such large ring-shaped components can be surface hardened particularly effectively through the use of two inductors, which are moved in synchronous, counter-rotating movements along the surface to be hardened.
- the inductors successively heat the surface sections covered by the electromagnetic field they generate to hardening temperature.
- the surface sections heated in this way are then quenched by shower jets, which are applied by a shower that follows the inductors.
- the starting zone of the surface to be hardened, over which the inductors are closely spaced at the start of the hardening process proves to be less problematic than the end zone, since a previously heated surface section does not have to be quenched at the same time as the starting zone is heated This means that there is enough time available to heat migration from the electromagnetic fields of the inductors not to bring directly swept area to hardening temperature.
- a first example of such a method is known from EP 1 848 833 B1.
- at least two inductors are arranged at the beginning of hardening over a common starting zone of the ring-shaped raceway to be hardened and there heat the opposite surface layer to hardening temperature.
- the inductors are moved in the opposite direction along the raceway in order to heat the intermediate zones of the annular raceway of the bearing ring that adjoin the starting zone in each case.
- EP 2 310 543 B1 Another method of the type in question is known from EP 2 310 543 B1. This method is based on the older method described in EP 1 848 833 B1 and provides that the auxiliary inductor used in the method known from EP 1 848 833 B1 for preheating the end zone to equalize the heating in one compared to that already in the older one Method provided movements additional degree of freedom, for example pendulum or circling, is moved.
- a third method for hardening a workpiece describing a closed curve, such as a bearing ring or toothed ring, is known from EP 1 977 020 B1.
- a first work step at least two inductors are attached to the workpiece in a starting area, the inductors being in starting positions which are closely adjacent to one another and which delimit a starting zone between them.
- the starting zone is then heated to hardening temperature by means of at least one of the inductors and then quenched.
- the inductors are then moved, starting from their respective starting position, along the workpiece, the direction of movement of one inductor being directed opposite to the direction of movement of the other inductor, and the direction of movement in each case Sections of the workpiece located in the active area of the inductors are heated to hardening temperature and then quenched.
- the opposite movements of the inductors are continued until the inductors have reached an end position in which they are arranged closely adjacent to the respective other inductor. An end zone is now enclosed between the end positions of the two inductors which are then reached.
- the inductors are moved together in the direction of one of the directions of movement of the inductors and the end zone is heated to hardening temperature by the inductor that has already been moved in this direction of movement. In this way, the end zone is completely passed over by at least one of the inductors and brought evenly to hardening temperature.
- EP 2 542 707 B1 discloses a method and a device for induction hardening of an annular surface of a circular component, in which four inductors are grouped into two inductor pairs and arranged on the annular surface to be hardened, with each inductor pair being assigned and closed Beginning of the heating the showers are arranged closely adjacent to one another. The inductors of the inductor pairs and the associated showers are also arranged directly next to one another. The inductor-shower combinations thus aligned over an initial zone of the track to be hardened are moved in opposite circumferential directions along the respective intermediate section of the track to be hardened, so that the surface sections previously heated to hardening temperature by means of the inductor pairs are quenched immediately afterwards.
- the inductor pairs continue to move in opposite directions until the respective leading inductors of the inductor pairs meet over an end zone of the track. When the end zone is reached, the leading inductors are removed from the tread to make room for the trailing inductors of the Inductor pairs. These trailing inductors are moved further in their respective previous circumferential direction until they too meet over the end zone and also the end zone of the two trailing ones
- Inductors is heated to hardening temperature. After the following inductors have been moved away from the end zone of the surface to be hardened one after the other or at the same time together with the shower assigned to them, the end zone is also quenched by a further shower in order to also achieve a hardening structure there.
- the task has arisen to create a method that is optimized in terms of the time required and that makes it possible to edge-harden a circumferential surface of an annular component in an optimally uniform and uninterrupted manner.
- the invention has achieved this object by a method in which at least the work steps specified in claim 1 are carried out.
- a method according to the invention is used for inductive surface hardening of an annular component made of hardenable steel, in particular a bearing ring for a large roller bearing, which has an initial zone, which is surface hardened at the beginning, and an end zone which is surface hardened at the end.
- a method according to the invention comprises the following work steps: a) surface hardening of the initial zone by bringing the initial zone to the hardening temperature by means of at least one inductor and quenching it by means of at least one shower which directs a jet of a quenching medium onto the heated initial zone; b) subsequent to the surface layer hardening of the initial zone, successive surface layer hardening of the surface of the ring-shaped component that is to be surface hardened
- inductor assemblies each having a leading inductor, which preheats the area of the surface to be hardened by it, a trailing inductor which is offset from the leading inductor in the direction of the starting zone and a finished heating of the area previously covered by the leading inductor causes preheated area to hardening temperature, as well as include a shower that quenches with a jet of a quenching agent around the area of the surface to be hardened before the area of the surface to be hardened by the inductor running after the inductor is running,
- the other inductor arrangement is designed to be movable and is moved for the surface hardening along the surface to be hardened and
- the ring-shaped component rotates about an axis of rotation in order to move the surface to be hardened along the stationary inductor arrangement, the speed at which the movable inductor arrangement is moved along the surface to be hardened is greater than the peripheral speed of the surface to be hardened on the surface of the ring-shaped component; c) Hardening of the end zone by, when the end zone is at a certain distance from the inductor arrangements, the leading inductor of at least one of the inductor arrangements is moved at least temporarily at a higher feed rate than the trailing inductor of this inductor arrangement in the direction of the end zone, so that a increased distance between the relevant leading inductor and the trailing inductor assigned to it occurs and the leading inductor is located earlier at the end zone with an impure time interval, the duration of which is equal to the duration that the trailing inductor needs until the one between it and the leading inductor Distance is overcome, so that the at least one leading inductor that has first arrived at the end zone
- intermediate zones between the starting zone and the end zone of the surface to be hardened of which the first intermediate zone is connected to the starting zone in a first circumferential direction and of which the second intermediate zone is connected to the starting zone in a second circumferential direction opposite to the first circumferential direction, so that the end zone extends between the ends of the intermediate zones facing away from the initial zone.
- These intermediate zones are swept over during the surface layer hardening by the inductor arrangements used according to the invention as a result of the movement carried out by the movable inductor arrangement and the simultaneous rotation of the annular component.
- the end zone of the surface to be hardened is thus preheated by means of at least one of the inductors which are already involved in the surface layer hardening of the intermediate zones of the surface taking place in circulation.
- the leading inductor approaching the end zone reaches the end zone of the surface to be hardened more quickly, so that it can preheat it as long as the trailing inductor of its inductor arrangement is still on its way to the end zone or the end zone is on the way to the respective trailing inductor.
- the leading inductor is moved away from the end zone and the trailing inductor takes its place in order to finish heating the end zone to hardening temperature.
- the trailing inductor can also be removed from the end zone and the end zone can be quenched using the shower provided for this purpose.
- the end zone can also be moved to a shower in order to carry out the deterrent.
- the feed rate at which the moving inductor arrangement is moved along the circumferential surface to be hardened, which is also moved at a circumferential speed, is greater than the circumferential speed of the circumferential surface, so that the moving inductor arrangement leads the circumferential surface.
- the movement of the movable inductor arrangement along the rotating peripheral surface to be hardened at the edge layer and the direction of rotation of the peripheral surface to be hardened at the edge layer are correspondingly aligned.
- the leading inductor of the moving inductor arrangement is arranged in front of the trailing inductor in the feed direction, behind which, in relation to the feed direction, the shower of the inductor arrangement is positioned.
- new, unhardened area of the peripheral surface to be hardened continuously comes into the effective area of the electromagnetic field induced by the leading inductor of the moving inductor arrangement, and is consequently preheated and reaches then without interruption into the effective area of the electromagnetic field induced by the trailing inductor of the moving inductor arrangement.
- the respectively detected zone of the surface to be hardened is completely heated to hardening temperature, in order then to be quenched by the shower of the moving inductor arrangement.
- the leading inductor is offset from the trailing inductor against the direction of rotation of the circumferential surface of the ring-shaped component, so that as a result of the rotational movement of the ring-shaped component, an unhardened area of the surface to be hardened and the end zone existing intermediate zones) into the effective area of the electromagnetic field of the leading inductor ("preheating inductor") and then into the effective area of the electromagnetic field of the following inductor ("finished heat inductor") of the stationary inductor arrangement, in order to then get from the shower assigned to the stationary inductor arrangement to be quenched, which is arranged in relation to the direction of rotation of the annular component behind the trailing inductor of the stationary inductor arrangement.
- a symmetrical hardening of the intermediate zones can be achieved in that the feed speed of the fixed inductor arrangement is kept constant equal to twice the circumferential speed of the circumferential surface to be hardened of the annular component.
- the leading inductor of the moving inductor arrangement can, after reaching the distance to the end zone provided as the starting point for its acceleration, be moved further at an increased speed in the direction of the end zone compared to the feed rate of the moving inductor arrangement maintained up to that point, while the trailing inductor and the shower are moving Inductor assembly can continue to be moved at the feed rate that has already been maintained.
- the leading inductor of the stationary inductor arrangement can also be moved towards the end zone, in this case opposite to the direction of rotation of the circumferential surface to be hardened, as soon as the end zone is at the distance from the leading inductor provided for the start of this movement.
- the speed at which the leading inductors move towards one another is optimally the same. In this way, the leading inductors meet above the end zone in order to then heat them together.
- the direction of movement of the leading inductor of the stationary inductor arrangement is reversed after reaching the end zone and the two leading inductors of the stationary and movable inductor arrangement are advanced together at a speed that is set so that there is no more relative movement between the end zone and the leading inductors, which advancing inductors remain constant over the end zone of the circumferential surface to be hardened and in this way preheat them together evenly.
- the end zone of the surface to be hardened and with it the leading inductors approach the trailing inductor of the stationary inductor arrangement and, at the same time, of the opposite side, the trailing inductor of the moving inductor arrangement of the end zone. If the trailing inductor of the moving inductor arrangement has reached the end zone and the end zone has reached the stationary trailing inductor of the stationary inductor arrangement, the respective leading inductor still located above the end zone can Inductor can be moved away to make room for the lagging inductors.
- the respective leading inductors can be moved away one after the other, so that the leading inductor still lingering over the end zone can continue to heat the end zone until it too has to be moved away to make room for the following one
- the finished heating can also be carried out by the following inductors of the inductor arrangements together or by one of the respective following inductors.
- showers used according to the invention direct a single jet of the quenching rriedium at the respective zone to be quenched, provided that this jet is sufficiently strong and the volume of liquid dispensed is sufficiently large to remove heat from the zone to be hardened at the required speed.
- showers which emit a large number of individual jets at the same time in order to reliably and completely apply a sufficient amount of quenching medium for heat removal to the zone to be quenched have proven effective for this.
- preheating and / or finishing the end zone with only one inductor in each case is that mutual interference in the respective effective electromagnetic field, which can occur when two inductors close together to heat a zone, do not occur. Special measures to avoid these disturbances are therefore not required.
- the use of a single inductor for preheating and / or finishing heating of the end zone allows precise control of the temperature in the end zone introduced heat, so that, for example, a correspondingly precisely designed hardness profile can be achieved in the hardened surface layer.
- Finishing heating of the end zone has only been carried out with one inductor, in cases where, for example, heating to hardening temperature is to be achieved as quickly as possible, it is also possible to carry out the preheating and / or finishing heating by two inductors together.
- the speed difference between the leading inductor, which is moving at an increased feed rate, and the trailing inductor assigned to it or between the circumferential surface of the annular component to be hardened and the respective leading inductor is set, for example, so that the duration required for preheating the end zone is available through the preceding inductor is 1 - 10 s.
- suitable increased feed speeds of the leading inductors are in practice, for example, in the range from 240 mm / min to 1800 mm / min, whereas the feed speeds at which the trailing inductors and temporarily also the leading inductors are moved along the intermediate zones are in the range of 180 mm / min to 1200 mm / min. It goes without saying that within the ranges specified for the increased feed speed of the leading inductors and the feed speed of the trailing inductors, the respective speed is selected so that the increased advance speed of the leading inductors is higher than the speed at which the trailing inductors be moved.
- the distance measured is 40 - 300 mm.
- the respective leading inductor In order to ensure that the respective leading inductor also generates sufficient heat in the areas covered by it during the phase of its rapid movement, it can be useful to increase the electrical power of the inductor leading with increased feed speed compared to the electrical power with which the respective inductor leading inductor is operated as long as it is moved at the same feed speed as the inductor running after its inductor arrangement. It can also be expedient to adjust the power of the respective trailing inductor if the leading inductor assigned to it is moved at an increased feed rate in order to ensure sufficient heat input for heating to the hardening temperature.
- step a) the heating of the initial zone to the hardening temperature can be carried out by an inductor of one of the inductor arrangements. This results in a movement sequence of the inductors involved that is easy to implement in practice if the inductor used to heat the initial zone is a trailing inductor of one of the inductor arrangements provided according to the invention.
- the trailing inductor used to heat the initial zone can, after the initial zone has been heated to the hardening temperature, in particular suddenly, in the direction of the starting area of the intermediate zone assigned to its inductor arrangement are moved so that then the beam is intended for quenching the initial zone shower can be directed towards the starting zone in the space that has become free by moving the inductor away.
- the shower used for quenching the start zone or the end zone can be a shower from one of the inductor arrangements.
- at least the shower used for this purpose can be moved independently of the inductors, so that it can be moved to an operating position in which its shower jet is optimally open to quench the initial zone from its spatial assignment to the inductors in normal shepherd's operation hits the initial zone to be deterred.
- At least one of the showers carried along with the inductor arrangements can be used to quench the end zone.
- the shower can be moved independently of the inductors of the respective inductor arrangement, so that it can be brought into an operating position in which its shower jet is optimal in order to quench the end zone from its spatial association with the inductors of the respective inductor arrangement meets the end zone to be deterred.
- Figures 1-9b each show schematically and not to scale in plan view a device for surface hardening in different phases of the method according to the invention.
- the device shown in FIGS. 1-9b serves to harden the surface layer of a circumferential surface 2a of a bearing ring 2. It comprises an inductor arrangement 1 which is arranged in a stationary manner and which has a preheating inductor 1a, a finished heating inductor 1b and a shower 1c.
- the preheating inductor 1 a is arranged in a circumferential direction U in front of the finished heating inductor 1 b on the circumferential surface 2 a of the bearing ring 2 to be hardened.
- the finished heat inductor 1b which is also arranged closely adjacent to the circumferential surface 2a, is in turn positioned in the circumferential direction U in front of the shower 1c, which is arranged offset outwardly in the radial direction relative to the circumferential surface 2a in relation to the inductors 1a, 1b.
- the device has a movable second inductor arrangement 3, which can be moved in the circumferential direction U along the bearing ring 2.
- the second inductor arrangement 3 comprises a preheating inductor 3a, a finished heat inductor 3b arranged in the circumferential direction U behind the vonhärminduktor 3a and a shower 3c arranged in the circumferential direction U behind the finished heat inductor 3b.
- the shower 3c is positioned offset in the radial direction outwards with respect to the circumferential surface 2a of the bearing ring 2 so that it is in the starting position in which the movable inductor arrangement 3 is in close proximity to the stationary inductor arrangement 1 (see FIG.
- the finished heat inductor 3 b of the movable inductor arrangement 3 is positioned in the circumferential direction U directly next to the finished heat inductor 1 b of the stationary inductor arrangement 1.
- the shower 1 c of the stationary inductor arrangement 1 is located behind the finished heat inductor 3 b, offset in the radial direction outward in relation to the circumferential surface 2a.
- the bearing ring 2 stands still or is operated oscillating in a small angular range in order to even out the heat input when the initial zone A of the circumferential surface 2a to be hardened is heated.
- the inductors 1a, 1b of the stationary inductor arrangement 1 and 3a, 3b of the movable inductor arrangement 3 now jointly heat the starting zone A (FIG. 1).
- the bearing ring 2 is rotated in the circumferential direction U about the axis X so that the circumferential surface 2a revolves around the axis X at a circumferential speed V1.
- the shower 1c of the stationary inductor unit 1 is switched on and scares off the initial zone A moving along it.
- the preheating inductors 1a, 3a of the stationary and movable inductor units 1, 3 are switched on and the movable inductor unit 3 is moved at a speed V2 in the circumferential direction U along the circumferential surface 2a of the bearing ring 2.
- the shower 3c of the movable inductor arrangement 3 is switched on as soon as it has passed the finished heat inductor 1b of the stationary inductor arrangement 1 (FIG. 2).
- the zone of the circumferential surface 2a located in the active area of the inductor unit 3 is successively hardened and quenched.
- the preheating inductor 3a preheats and the finished heat inductor 3b causes the respective zone to be heated to the hardening temperature, while the shower 3c quells the zone heated to hardening temperature in order to create hardened structures in the edge layer adjacent to the peripheral surface 2a.
- the feed speed V2 of the movable inductor arrangement 3 is twice that of the circumferential speed V1
- the relative speed between the inductor arrangement 3 and the circumferential surface 2 is equal to the circumferential speed V1.
- the movable inductor arrangement 3 moves towards the end zone E of the circumferential surface 2a at the same speed as the end zone E towards the stationary inductor arrangement 1 (FIGS. 2-4).
- the successive hardening of the circumferential surface 2a is continued until the end zone E of the circumferential surface 2a has approached the preheating inductor 1a of the stationary inductor arrangement 1 at a certain distance. From this point on, the preheating inductor 3 a of the movable inductor arrangement 3 is advanced in the direction of the end zone E with a feed speed V2 ′ that is additionally increased compared to the feed speed V2. At the same time, the preheating inductor 1 a of the stationary inductor arrangement 1 is used to move the preheating inductor 3 a and to rotate the bearing ring
- both preheating inductors 1a, 3a are moved together in the direction of the stationary finished heating inductor 1b at a feed rate that is set so that there is no more relative movement between the preheating inductors 1a, 3a and the end zone E, while the finished heating inductor 3b and the shower 3c and the bearing ring 2 are moved on unchanged until the inductor 1a is back in its original stationary position.
- the end zone E is jointly preheated by the preheating inductors 1a, 3a (FIG. 6).
- the preheating inductor 3a of the movable inductor arrangement 3 is now switched off and moved into a waiting position remote from the circumferential surface 2a.
- the preheating inductor 3a continues to move at speed V2 'in the direction of the stationary finished heating inductor 1b, while the finished heating inductor 3b and the shower 3c as well as the bearing ring 2 continue to move unchanged until the preheating inductor 3a has approached the finished heating inductor 3b (Fig. 7).
- the preheating inductor 3a is now switched off and moved into a waiting position, while the movable finished heating inductor 3b with the shower 3c continues to move towards the stationary finished heating inductor 1b at the speed V2 in the circumferential direction U, while the position 2 continues to move at the circumferential speed V1, until the moved finished heat inductor 3b is in a position immediately adjacent to the stationary finished heat inductor 1b.
- the movement of the bearing ring 2 is now stopped and the finished heating of the end zone E, which is now located exactly below the finished heat inductors 1b, 3b, is carried out jointly by the finished heat inductors 1b, 3b (FIG. 8).
- the finished heat inductors 1b, 3b are pivoted away from the end zone E and the quenching is carried out by means of an additional shower 5 (Fig. 9a) or according to a second variant the bearing ring 2 at high speed in the circumferential direction U rotates until the end zone E is arranged under the stationary shower 1c, which then carries out the deterrent (FIG. 9b).
- the invention thus provides a method for inductive surface layer hardening of a surface 2a which runs around an annular component made of hardenable steel and which achieves uniform and uninterrupted hardening.
- an initial zone A of the surface 2a is hardened on the surface by bringing it to hardening temperature by means of an inductor 1a, 1b, 3a, 3b and quenching it with a shower 1c, 3c.
- the surface 2a is hardened by means of a stationary inductor arrangement 1 and a movably arranged inductor arrangement 1, 3, each of which has a leading inductor 1a, 3a for preheating the area of the surface 2a it swept over, one offset in the direction of the starting zone A, trailing behind Inductor 1b, 3b for the final heating of the preheated area to hardening temperature and a shower 1c, 3c for quenching the heated area, the movable inductor arrangement 3 is moved along the surface 2a and at the same time the annular component 2 rotates about an axis of rotation X ⁇ around to move the surface 2a to be hardened along the stationary inductor arrangement 1, the speed V2 of the movable inductor arrangement 3 along the surface 2a being greater than its peripheral speed V1.
- an end zone E of the surface 2a is hardened by, when the end zone E is in a certain distance to the inductor assemblies 1, 3 is located, the leading inductor 1a, 3a of one of the inductor assemblies 1, 3 is temporarily moved at a higher feed rate V1 ', V2' than its trailing inductor 1b, 3b in the direction of the end zone E, so that a increased distance between the leading inductor 1a, 3a and the trailing inductor 1b, 3b and the leading inductor 1a, 3a is a time interval earlier at the end zone E, which is equal to the duration that the trailing inductor 1b, 3b needs , until the distance created between it and the leading inductor has been overcome, so that the at least one leading inductor 1a, 3a that first arrived at the end zone E preheats the end zone E until the trailing inductor 1b, 3b is located at the end zone E and the End zone E heated to the hardening temperature.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Articles (AREA)
- General Induction Heating (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2022549476A JP2023508238A (ja) | 2020-02-20 | 2021-02-22 | 表面層誘導硬化の方法 |
MX2022010285A MX2022010285A (es) | 2020-02-20 | 2021-02-22 | Metodo para el endurecimiento inductivo de capa superficial. |
EP21707672.8A EP4107296A1 (de) | 2020-02-20 | 2021-02-22 | Verfahren zum induktiven randschichthärten |
US17/801,119 US20230082585A1 (en) | 2020-02-20 | 2021-02-22 | Method for Inductive Surface Layer Hardening |
CN202180015791.3A CN115151662A (zh) | 2020-02-20 | 2021-02-22 | 用于感应式表层硬化的方法 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102020104476.3 | 2020-02-20 | ||
DE102020104476 | 2020-02-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2021165532A1 true WO2021165532A1 (de) | 2021-08-26 |
Family
ID=74701498
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2021/054327 WO2021165532A1 (de) | 2020-02-20 | 2021-02-22 | Verfahren zum induktiven randschichthärten |
Country Status (6)
Country | Link |
---|---|
US (1) | US20230082585A1 (de) |
EP (1) | EP4107296A1 (de) |
JP (1) | JP2023508238A (de) |
CN (1) | CN115151662A (de) |
MX (1) | MX2022010285A (de) |
WO (1) | WO2021165532A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102021125307A1 (de) | 2021-09-29 | 2023-03-30 | Sms Elotherm Gmbh | Vorrichtung und Verfahren zur Aufnahme und zum Antrieb mindestens eines im Wesentlichen ringförmigen Werkstücks in einer Bearbeitungsanlage sowie entsprechendes System |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010007635A1 (en) * | 2008-07-15 | 2010-01-21 | Saet S.P.A. | Method and device for localized induction hardening treatment of mechanical components, specifically thrust blocks for large-sized rolling bearings |
US20110248023A1 (en) * | 2010-04-13 | 2011-10-13 | Doyon Gary A | Induction heat treatment of an annular workpiece |
EP1848833B1 (de) | 2005-02-15 | 2012-07-04 | Rothe Erde GmbH | Verfahren zum herstellen eines lagerringes für grosswälzlager mittels induktionshärten |
ITTO20120051A1 (it) * | 2012-01-23 | 2013-07-24 | Saet Spa | Metodo e dispositivo per tempra ad induzione localizzata di componenti meccanici circolari di grandi dimensioni, in particolare ralle per cuscinetti di rotolamento |
EP1977020B1 (de) | 2006-01-23 | 2013-12-25 | SMS Elotherm GmbH | Verfahren zum härten eines einen geschlossenen kurvenzug beschreibenden werkstücks |
EP2542707B1 (de) | 2010-03-05 | 2016-05-11 | Saet S.p.A. | Verfahren und vorrichtung für lokalisierte induktionshärtung von grossen kreisförmigen mechanischen komponenten , im besonderen ringe für wälzlager |
EP2310543B1 (de) | 2008-07-18 | 2019-08-07 | thyssenkrupp Rothe Erde GmbH | Verfahren zum härten wenigstens einer laufbahn eines lagerrings für ein grosswälzlager |
US20190352729A1 (en) * | 2018-05-18 | 2019-11-21 | Aktiebolaget Skf | Induction-hardening system for induction hardening of a large rolling-element bearing ring |
-
2021
- 2021-02-22 WO PCT/EP2021/054327 patent/WO2021165532A1/de active Application Filing
- 2021-02-22 CN CN202180015791.3A patent/CN115151662A/zh not_active Withdrawn
- 2021-02-22 MX MX2022010285A patent/MX2022010285A/es unknown
- 2021-02-22 US US17/801,119 patent/US20230082585A1/en not_active Abandoned
- 2021-02-22 EP EP21707672.8A patent/EP4107296A1/de not_active Withdrawn
- 2021-02-22 JP JP2022549476A patent/JP2023508238A/ja not_active Withdrawn
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1848833B1 (de) | 2005-02-15 | 2012-07-04 | Rothe Erde GmbH | Verfahren zum herstellen eines lagerringes für grosswälzlager mittels induktionshärten |
EP1977020B1 (de) | 2006-01-23 | 2013-12-25 | SMS Elotherm GmbH | Verfahren zum härten eines einen geschlossenen kurvenzug beschreibenden werkstücks |
WO2010007635A1 (en) * | 2008-07-15 | 2010-01-21 | Saet S.P.A. | Method and device for localized induction hardening treatment of mechanical components, specifically thrust blocks for large-sized rolling bearings |
EP2310543B1 (de) | 2008-07-18 | 2019-08-07 | thyssenkrupp Rothe Erde GmbH | Verfahren zum härten wenigstens einer laufbahn eines lagerrings für ein grosswälzlager |
EP2542707B1 (de) | 2010-03-05 | 2016-05-11 | Saet S.p.A. | Verfahren und vorrichtung für lokalisierte induktionshärtung von grossen kreisförmigen mechanischen komponenten , im besonderen ringe für wälzlager |
US20110248023A1 (en) * | 2010-04-13 | 2011-10-13 | Doyon Gary A | Induction heat treatment of an annular workpiece |
ITTO20120051A1 (it) * | 2012-01-23 | 2013-07-24 | Saet Spa | Metodo e dispositivo per tempra ad induzione localizzata di componenti meccanici circolari di grandi dimensioni, in particolare ralle per cuscinetti di rotolamento |
US20190352729A1 (en) * | 2018-05-18 | 2019-11-21 | Aktiebolaget Skf | Induction-hardening system for induction hardening of a large rolling-element bearing ring |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102021125307A1 (de) | 2021-09-29 | 2023-03-30 | Sms Elotherm Gmbh | Vorrichtung und Verfahren zur Aufnahme und zum Antrieb mindestens eines im Wesentlichen ringförmigen Werkstücks in einer Bearbeitungsanlage sowie entsprechendes System |
Also Published As
Publication number | Publication date |
---|---|
EP4107296A1 (de) | 2022-12-28 |
MX2022010285A (es) | 2022-09-19 |
JP2023508238A (ja) | 2023-03-01 |
US20230082585A1 (en) | 2023-03-16 |
CN115151662A (zh) | 2022-10-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1848833B1 (de) | Verfahren zum herstellen eines lagerringes für grosswälzlager mittels induktionshärten | |
EP2310543B1 (de) | Verfahren zum härten wenigstens einer laufbahn eines lagerrings für ein grosswälzlager | |
EP1977020B1 (de) | Verfahren zum härten eines einen geschlossenen kurvenzug beschreibenden werkstücks | |
EP1375684B2 (de) | Verfahren zum Herstellen von Lagerringen für Grosswälzlager | |
EP0384964B1 (de) | Verfahren und Vorrichtung zum induktiven Härten der gewellten Oberfläche eines Werkstücks | |
EP4107296A1 (de) | Verfahren zum induktiven randschichthärten | |
EP2801628B1 (de) | Verfahren zum Randschichthärten eines metallischen Bauteils | |
WO2011054540A2 (de) | Verfahren und vorrichtung zum induktiven härten grosser ringförmiger werkstücke | |
EP2814990B1 (de) | Verfahren zum induktiven randschichthärten einer ringfläche | |
EP1208243B1 (de) | Verfahren zum härten mindestens einer fläche einer wand eines bauteils und vorrichtung zu seiner durchführung | |
WO2022049150A1 (de) | Verfahren und vorrichtung zur induktiven härtung einer randschicht | |
WO2016177733A1 (de) | Verfahren und vorrichtung zum induktiven vorschubhärten mit steuerbarem vorwärmen und einem zum vorwärmen und härten ausgebildeten induktor | |
WO2021160655A1 (de) | Verfahren zum induktiven randschichthärten | |
DE102018207904A1 (de) | Induktionshärteanlage zum induktiven Härten eines Großwälzlagerrings | |
DE19757485A1 (de) | Vorrichtung zum kontrollierten Abkühlen von warmgewalzten Profilen, insbesondere Trägern, direkt aus der Walzhitze | |
DE102005021856A1 (de) | Induktionserwärmungsanlage | |
EP3631024B1 (de) | Härtungsverfahren und härtungsvorrichtung zum oberflächenhärten eines rotationssymmetrischen werkstücks | |
EP3108018A1 (de) | System, fertigungsanlage und verfahren | |
DE102022200322A1 (de) | Induktionshärteanlage | |
EP0520220A1 (de) | Verfahren und Einrichtung zum induktiven Randschichthärten von Haupt- oder Hublagerzapfen an Kurbelwellen | |
CH712700A2 (de) | Verfahren zur Herstellung von Führungsschienen für ein Linearwälzlager. | |
DE102022200324A1 (de) | Induktionshärteanlage und Induktionshärteverfahren | |
DE19955670B4 (de) | Verfahren und Vorrichtung zum Härten von Flächen einer Kurbel- oder Nockenwelle | |
EP1057920A1 (de) | Vorrichtung und Verfahren zum Behandeln einer Warenbahn und Trommel mit einer Oberfläche mit einem veränderlichen Radius |
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: 21707672 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2022549476 Country of ref document: JP Kind code of ref document: A |
|
WWE | Wipo information: entry into national phase |
Ref document number: 202237046667 Country of ref document: IN |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
ENP | Entry into the national phase |
Ref document number: 2021707672 Country of ref document: EP Effective date: 20220920 |