EP0601451B1 - Process for hardness increasing and possibly for smoothing of work pieces and work pieces made by this process - Google Patents
Process for hardness increasing and possibly for smoothing of work pieces and work pieces made by this process Download PDFInfo
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- EP0601451B1 EP0601451B1 EP93119338A EP93119338A EP0601451B1 EP 0601451 B1 EP0601451 B1 EP 0601451B1 EP 93119338 A EP93119338 A EP 93119338A EP 93119338 A EP93119338 A EP 93119338A EP 0601451 B1 EP0601451 B1 EP 0601451B1
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- accordance
- treatment
- laser
- cementite
- layer
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- 238000000034 method Methods 0.000 title claims description 39
- 238000009499 grossing Methods 0.000 title claims description 12
- 230000008569 process Effects 0.000 title description 11
- 229910001567 cementite Inorganic materials 0.000 claims description 37
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims description 37
- 238000011282 treatment Methods 0.000 claims description 33
- 239000010410 layer Substances 0.000 claims description 26
- 239000002344 surface layer Substances 0.000 claims description 19
- 238000010894 electron beam technology Methods 0.000 claims description 14
- 229910000831 Steel Inorganic materials 0.000 claims description 13
- 239000010959 steel Substances 0.000 claims description 13
- 238000002844 melting Methods 0.000 claims description 12
- 230000008018 melting Effects 0.000 claims description 12
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 10
- 229910001018 Cast iron Inorganic materials 0.000 claims description 10
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- 239000000758 substrate Substances 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 6
- 239000010451 perlite Substances 0.000 claims description 6
- 235000019362 perlite Nutrition 0.000 claims description 6
- 238000010791 quenching Methods 0.000 claims description 6
- 239000011159 matrix material Substances 0.000 claims description 5
- 241000446313 Lamella Species 0.000 claims description 4
- 229910001566 austenite Inorganic materials 0.000 claims description 4
- 238000009792 diffusion process Methods 0.000 claims description 4
- 238000004090 dissolution Methods 0.000 claims description 3
- 239000007789 gas Substances 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 235000011837 pasties Nutrition 0.000 claims description 3
- 238000001556 precipitation Methods 0.000 claims description 3
- 230000000171 quenching effect Effects 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 3
- 238000000859 sublimation Methods 0.000 claims description 3
- 230000008022 sublimation Effects 0.000 claims description 3
- 230000007423 decrease Effects 0.000 claims description 2
- 229910001349 ledeburite Inorganic materials 0.000 claims description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims 2
- 229910001035 Soft ferrite Inorganic materials 0.000 claims 1
- 230000004927 fusion Effects 0.000 claims 1
- 229910052757 nitrogen Inorganic materials 0.000 claims 1
- 230000002093 peripheral effect Effects 0.000 claims 1
- 238000009834 vaporization Methods 0.000 claims 1
- 229910000734 martensite Inorganic materials 0.000 description 9
- 229910001562 pearlite Inorganic materials 0.000 description 8
- 230000015572 biosynthetic process Effects 0.000 description 5
- 239000013078 crystal Substances 0.000 description 5
- 230000008020 evaporation Effects 0.000 description 5
- 238000001704 evaporation Methods 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 238000002156 mixing Methods 0.000 description 5
- 239000010439 graphite Substances 0.000 description 4
- 229910002804 graphite Inorganic materials 0.000 description 4
- 230000009466 transformation Effects 0.000 description 4
- 229910000859 α-Fe Inorganic materials 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000013532 laser treatment Methods 0.000 description 3
- 230000005855 radiation Effects 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 244000052616 bacterial pathogen Species 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 238000012805 post-processing Methods 0.000 description 2
- 238000010792 warming Methods 0.000 description 2
- 206010013486 Distractibility Diseases 0.000 description 1
- 238000005255 carburizing Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
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- 230000029142 excretion Effects 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- QMQXDJATSGGYDR-UHFFFAOYSA-N methylidyneiron Chemical compound [C].[Fe] QMQXDJATSGGYDR-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
Images
Classifications
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- 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
-
- 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
- C21D5/00—Heat treatments of cast-iron
-
- 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
- C21D2211/007—Ledeburite
-
- 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
- C21D2211/009—Pearlite
-
- 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
- C21D9/30—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for crankshafts; for camshafts
Definitions
- the present invention relates to a method for hardening and possibly smoothing machine components using a cause surface heating of the respective component Beam, e.g. a laser beam, an electron beam or the beam of an arc lamp.
- Beam e.g. a laser beam, an electron beam or the beam of an arc lamp.
- a laser is basically considered to be high energy Heat source used for martensite hardening without thereby melting the surface of the treated components.
- induction hardening Operation performed examples of such processes are U.S. Patent Nos. 4,304,978, 4,093,842 and 4,686,349, and U.S. Pat German patent 33 43 783 and the Metal Science Heat Treatment 20, No. 7/8, 1978, Pages 544-546.
- martensite hardening leads to a martensitic Structure that is very hard, but a needle-like one Has structure so that it is not necessarily the ideal hard Surface with regard to abrasive and adhesive wear represents.
- the martensitic structure is therefore for Components such as camshafts and rocker arms are not the ideal Structure.
- DD-A-204 106 does not expressly say that the method mentioned there is martensite hardness.
- the specified hardness values (HV 0.05 ) are between 1500 and 1650.
- the surface to be hardened is sanded beforehand.
- the laser treatment converts both the steel (examples 1 and 2) and the cast iron (example 3) to the previously existing pearlite / ferrite structure without melting the surface. Graphite deposits in cast iron are not changed by laser treatment.
- Another category of processes includes laser layer melting.
- one on one The graphite layer applied to the substrate is melted into the layer Solidify or cool the substrate themselves carbides.
- the graphite carbon introduced into the layer molten state dissolves, a mixed crystal forms and when cooling with atoms of the substrate Cr, W, V, Mn, Fe forms carbides in the form of granular or dendritic
- excretions for example TiC (if the substrate is a Ti material) from the dissolved Graphite.
- An example of this procedure is the DE-OS 35 45 128.
- a high-power laser often a CO 2 laser, is used.
- DE-OS 39 32 328 is a method for the rest Machining of surfaces subjected to friction in Internal combustion engines, especially the cylinder surfaces known from piston engines, the area honed and additional is subjected to a laser beam treatment.
- This Laser beam treatment after honing is preferred by a pulsed excimer laser carried out, this treatment a surface evaporation of micro grooves while maintaining the macro grooves (oil-producing honing grooves) without unwanted remelting caused.
- DE-OS 39 32 398 does not mention one targeted "skin" in the nanometer range ( ⁇ 1 ⁇ m), i.e. in the order of 0.001 ⁇ m. Due to the extreme quenching rates it is usually oversaturated or already already amorphous and therefore possibly hard.
- the present one Invention based on the object, a method of provide the kind mentioned that the hardening and preferably also the simultaneous micro-smoothing of machine components, enables which either in the form of a Chilled cast part with ledeburitic structure or in the form of a Steel part with pearlitic structure are present, the Process is carried out so that a new structure is reached on the surface of the component, not only a hard and preferably also micro-smooth Surface offers, but also no post-processing requires, but a possible postprocessing for Special purposes is not excluded.
- the structural component By treatment with the respective working beam (laser, electron beam or arc lamp) is a structural component locally dough or it melts while the other structural components remain in the solid state.
- the structural component is which locally becomes dough or melts around the Areas between the large cementite slats and the Perlite. This is where the iron-carbon state diagram plays taking into account the imbalance ratios a crucial role.
- the treatment should be carried out in this way, i.e. in front everything so short that there are none in the boundary layer Homogeneous, e.g. form austenitic mixed crystals can, always enough cementite germs in the surface layer and must be present in the substrate so that when quenching (self-deterrence or possibly with With the help of a cold jet) always cementite and not Austenite is formed.
- Homogeneous e.g. form austenitic mixed crystals can, always enough cementite germs in the surface layer and must be present in the substrate so that when quenching (self-deterrence or possibly with With the help of a cold jet) always cementite and not Austenite is formed.
- the treatment can be carried out in this way, for example with a pulsed radiation source of high energy density, such as. with an excimer laser that a pronounced Evaporation (sublimation) and melting a thin one Surface skin occurs, resulting in a pronounced Micro-smoothing the surface leads.
- a pulsed radiation source of high energy density such as. with an excimer laser that a pronounced Evaporation (sublimation) and melting a thin one Surface skin occurs, resulting in a pronounced Micro-smoothing the surface leads.
- the respective component to grind at least on the surface to be treated, but also hard shell cast surfaces can be treated with the method according to the invention can.
- Typical application examples for the present Processes are the generation of hard and possibly micro-smooth surfaces on camshafts or cam followers of internal combustion engines.
- Typical values for the energy density used are in the range from 2 x 10 3 to 5 x 10 5 W / cm 2 .
- the invention deals with machine components that either in the form of a hard casting with ledeburitic Structure or in the form of a steel part with pearlitic Structures are present, with the special characteristic, that an almost closed cementite surface is present, the component having a surface hardness above 900 HV, preferably about 1100 HV and the cementite precipitation density in the interlamellar Areas from the surface towards Matrix is continuously decreasing.
- the component can for example a camshaft or a rocker arm be, but there are of course many other conceivable Machine components which are treated according to the invention can be.
- the treatment can basically be carried out in the air, at least with a laser beam or with an arc lamp, since there is little or no fear of oxidation processes. It may be useful to carry out the treatment with the selected jet type in a selected gas atmosphere in order to achieve special effects.
- the treatment could be carried out in a nitrogen-containing or CO 2 -containing atmosphere if nitriding or carburizing the surface of the workpiece is additionally desired.
- the invention is concerned with the surface treatment of machine components with heterogeneous (over-, under- or -eutectic) Casting structure, as shown in Fig. 1, or with over-, under- or -eutectoidal steel structure, such as shown in Fig. 3.
- FIG. 1 shows a TIG remelted tread of a Cast iron camshaft with an hypoeutectic structure made of cementite flakes and fine pearlite.
- the TIG remelting process represents a possible, but not mandatory pretreatment.
- the cementite lamellas are the large islands, while the pearlite areas the filigree structure exhibit.
- a qualitatively similar structure also delivers Chilled cast iron.
- a surface structure according to FIG. 2 is formed. From the structural components as in FIG. 1, ie from the cementite lamellae and fine Perlite has formed an almost closed layer of non-stoichiometric cementite in the surface layer. It is characteristic of this treatment that the surface layer is briefly heated up to the vicinity of the melting temperature (continuously or by repeated pulses) so that the carbon diffuses in the boundary layer from the cementite lamellae of the ledeburite into the soft, interlamellar ferrite areas.
- the holding time at this temperature is chosen so that there is no complete dissolution of existing phase components and formation of a homogeneous mixed crystal.
- a regression to the original phase state cannot take place or can only take place incompletely.
- the cementite substance "blends", as can clearly be seen in FIG. 2, at the expense of the stoichiometric structure, combined with the effect of hardening the surface layer up to 1100 HV.
- FIG. 3 shows a scanning electron microscope Inclusion of a steel eutectoid structure about 0.8% C.
- ferrite dark parts of the Matrix
- cementite as light parts of the matrix in lamellar Arrangement.
- Fig. 4 After treatment with the excimer laser, As for the cast iron sample of Fig. 1, a structure is created in the surface layer, as shown in Fig. 4.
- the surface layer has briefly warmed up up to near the melting temperature (continuously or by repeated pulses of the laser) a diffusion of carbon in an edge layer from the cementite flakes of pearlite into the soft interlamellar ferrite areas.
- the temperature reached near the melting temperature must be chosen so that it is not a complete Dissolution of existing phase components and A homogeneous mixed crystal is formed. Here too prevents self-quenching following heat treatment a regression in the surface layer the original phase state. Likewise, in this example an imbalance with a cementite higher volume than the original.
- the ground ledeburitic cam surface of a camshaft is cut with a CO 2 laser in CW mode (continuous, non-pulsed laser beam) with a rectangular beam cross-section of size 2 x 10 or 1 x 20 mm 2 by rotating the camshaft under the laser beam treated.
- the width of approx. 10 or 20 mm corresponds to the cam width of an NW with 4 or 2 valve technology.
- the surface temperature in the area of liquidus solidus from 1150 to 1250 ° C (pasty state of the surface layer) is monitored with known "on line" temperature measuring systems.
- the power density is 5 x 10 3 to 10 5 W / cm 2 .
- a laser power of 5 to 8 kW is required.
- the speed of rotation of the camshaft is determined from the dwell time of the laser beam on the cam surface.
- a dwell time (exposure time) of 0.3 to 10 s is required for a carbide layer thickness of 3 to 10 ⁇ m. If the treatment in pulse mode is carried out with a CO 2 or Nd: YAG laser, at least 20% lower average power densities are required.
- the ledeburitic cam tread of a hard cast or surface layer remelted (TIG; laser, electron beam) Rocker arm is used for training purposes thin, but almost dense carbide Wear layer treated with the electron beam.
- the e-beam with 0.1 to 0.5 mm beam diameter grids the entire cam tread in a known manner one or more times. Repeated scanning of the Surface also becomes an almost constant, medium one Temperature of the surface above the liquidus does not rise, remain intact. For example becomes a deflection frequency of the e-beam from 100 to 500 Hz in the Y axis and a feed rate the rocker arm applied in the X-axis from 5 to 60 mm / s, depending on whether preheating the rocker arm has previously taken place or not.
- the in Example required power of the electron beam gun was 3 kW (60 V, 50 A).
- the advantage of the electron beam is in this case in the high level of guidance and distractibility as well as in the local repeatability of the treatment. This allows you to do so without any special effort as required different carbide layers on one surface Thickness can be generated (customized layer thicknesses).
- a CO 2 laser in CW operation works with a laser power density in the range of 2 x 10 4 to 5 x 10 5 W / cm 2 and in pulse mode with an average power density that is at least 20% lower.
- Characteristic of the carbide layer of the present Invention is that these are wear-resistant on existing Ledeburit or perlite is produced, the wear resistance is improved and that the cementite precipitation density in the interlamellar areas always from the surface towards the matrix decreases.
- the exposure times of 0.017 to 0.026 S mentioned in the US patent are also not comparable with the values of 0.1 to 10 s mentioned in the present application.
- the average power density for example in the case of an Nd: YAG laser, with a beam cross section of 0.5 x 0.5 cm 2 and an average power of 500 W is of the order of 20,000 W / cm 2 and therefore in a completely different range as indicated in U.S. Patent No. 4,304,978.
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- 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)
- Laser Beam Processing (AREA)
Description
Die vorliegende Erfindung betrifft ein Verfahren zum Aufhärten und ggf. Glätten von Maschinenbauteilen mittels eines eine Oberflächenaufwärmung des jeweiligen Bauteils bewirkenden Strahls, wie z.B. eines Laserstrahls, eines Elektronenstrahls oder des Strahles einer Lichtbogenlampe.The present invention relates to a method for hardening and possibly smoothing machine components using a cause surface heating of the respective component Beam, e.g. a laser beam, an electron beam or the beam of an arc lamp.
Es sind im Stand der Technik verschiedene Verfahren mit Maschinenbauteilen, die mit Laserstrahlen oder Elektronenstrahlen behandelt werden, bekannt, um bestimmte Eigenschaften an den Oberflächen der Bauteile zu erreichen.In the prior art, there are various processes with machine components, those with laser beams or electron beams are known to have certain properties to achieve on the surfaces of the components.
Beispielsweise ist das sogenannte Laserumwandlungshärten bekannt. Hier wird im Grunde genommen ein Laser als energiereiche Wärmequelle zum Martensithärten verwendet, ohne dabei die Oberfläche der behandelten Bauteile zu schmelzen. Mit anderen Worten wird ein dem Induktionshärten ähnlicher Vorgang durchgeführt. Beispiele für solche Verfahren sind den US-PS'en 4 304 978, 4 093 842 und 4 686 349 sowie der deutschen Patentschrift 33 43 783 und der Zeitschrift Metal Science Heat Treatment 20, No. 7/8, 1978, Seiten 544-546 zu entnehmen.For example, the so-called laser transformation hardening known. Here a laser is basically considered to be high energy Heat source used for martensite hardening without thereby melting the surface of the treated components. In other words, it becomes more similar to induction hardening Operation performed. Examples of such processes are U.S. Patent Nos. 4,304,978, 4,093,842 and 4,686,349, and U.S. Pat German patent 33 43 783 and the Metal Science Heat Treatment 20, No. 7/8, 1978, Pages 544-546.
Das Martensithärten führt bekanntlich zu einem martensitischen Gefüge, das zwar sehr hart ist, jedoch ein nadeliges Gefüge aufweist, so daß es nicht unbedingt die ideale harte Oberfläche im Hinblick auf abrasiven und adhäsiven Verschleiß darstellt. Das martensitische Gefüge ist daher für Bauteile wie Nockenwellen und Schlepphebel nicht das ideale Gefüge. As is well known, martensite hardening leads to a martensitic Structure that is very hard, but a needle-like one Has structure so that it is not necessarily the ideal hard Surface with regard to abrasive and adhesive wear represents. The martensitic structure is therefore for Components such as camshafts and rocker arms are not the ideal Structure.
In der DD-A-204 106 wird nicht ausdrücklich gesagt, daß es sich bei dem dort angesprochenem Verfahren um Martensithärten handelt. Die angegebenen Härtewerte (HV0.05) liegen zwischen 1500 und 1650. Die zu härtende Oberfläche wird vorher geschliffen. Durch die Laserbehandlung wird sowohl bei Stahl (Beispiele 1 und 2) als auch bei Gußeisen (Beispiel 3) das zuvor existierende Perlit/Ferrit-Gefüge umgewandelt, ohne daß dabei die Oberfläche geschmolzen wird. Graphitausscheidungen im Gußeisen werden durch die Laserbehandlung nicht verändert.DD-A-204 106 does not expressly say that the method mentioned there is martensite hardness. The specified hardness values (HV 0.05 ) are between 1500 and 1650. The surface to be hardened is sanded beforehand. The laser treatment converts both the steel (examples 1 and 2) and the cast iron (example 3) to the previously existing pearlite / ferrite structure without melting the surface. Graphite deposits in cast iron are not changed by laser treatment.
Bei der zweiten Schrift "Metal Science and Heat Treatment Nr. 20" wird der Einfluß von Elektronenstrahlung auf Eigenschaften von verschiedenen Gußeisensorten untersucht. Die erzeugten Oberflächentemperaturen werden ausdrücklich so gesteuert, daß es zu einem Umwandlungshärten durch Martensitbildung kommt, wie aus dem dritten und zweiten Absatz von unten auf Seite 545 der entsprechenden Zeitschrift zum Ausdruck kommt. Auf Seite 544 ist allerdings erwähnt, daß durch Bestrahlung mit Elektronen Zementit einer Härte von HV1100 in Zementit einer Härte von HV1250 umgewandelt wurde.In the second writing "Metal Science and Heat Treatment No. 20 "is the influence of electron radiation on properties of different types of cast iron. The generated surface temperatures are expressly so controlled to undergo transformation hardening by martensite formation comes from the third and second paragraph from below on page 545 of the corresponding magazine on Expression comes. On page 544, however, it is mentioned that through Irradiation with electron cementite with a hardness of HV1100 in cementite a hardness of HV1250 was converted.
Werkstatt und Betrieb 123 (1990) November, Nr.11, S.875-877, bezieht sich auf das Martensithärten mit Laserstrahlen unter Anwendung einer Kohlepulver-Beschichtung; bei zu hohen Schichtdicken wurden Kohlenstoff-Diffusion und eine Umschmelz-Umwandlung in Ledeburit beobachtet. Werkstatt und Betrieb 123 (1990) November, No. 11, p.875-877 on martensite hardening using laser beams Carbon powder coating; if the layer thicknesses were too high, carbon diffusion and a remelting conversion to ledeburit was observed.
Weiterhin gibt es das Verfahren des sogenannten Laserumschmelzhärtens. Hier wird mittels des Laserstrahls eine geschmolzene Schicht an der Oberfläche des Bauteils erzeugt, welche durch rasche Erstarrung zu einem harten ledeburitischen Gefüge führt. Beispiele für diese Verfahrensweise sind aus den deutschen Patentschriften 34 18 555 und 36 26 799 bekannt.There is also the process of laser remelt hardening. Here is a melted by means of the laser beam Creates a layer on the surface of the component, which through rapid solidification into a hard ledeburitic Structure leads. Examples of this procedure are from German patents 34 18 555 and 36 26 799 known.
Eine weitere Verfahrenskategorie umfaßt das Laserschichteinschmelzen. Bei diesem Verfahren wird eine auf einem Substrat aufgetragene Graphitschicht in die Schicht eingeschmolzen.Beim Erstarren bzw. Abkühlen des Substrats bilden sich Karbide. Mit anderen Worten wird durch Einschmelzen des Graphits Kohlenstoff in die Schicht eingebracht, der im schmelzflüssigen Zustand sich auflöst, ein Mischkristall bildet und beim Abkühlen mit Atomen des Substrats Cr, W, V, Mn, Fe Karbide bildet, die in Form von körniger bzw. dendritischer Ausscheidungen vorliegen, beispielsweise TiC (wenn das Substrat ein Ti-Werkstoff ist) aus dem gelösten Graphit. Ein Beispiel für diese Verfahrensweise ist der DE-OS 35 45 128 zu entnehmen.Another category of processes includes laser layer melting. In this process, one on one The graphite layer applied to the substrate is melted into the layer Solidify or cool the substrate themselves carbides. In other words, by melting of the graphite carbon introduced into the layer molten state dissolves, a mixed crystal forms and when cooling with atoms of the substrate Cr, W, V, Mn, Fe forms carbides in the form of granular or dendritic There are excretions, for example TiC (if the substrate is a Ti material) from the dissolved Graphite. An example of this procedure is the DE-OS 35 45 128.
In allen diesen Fällen wird ein Hochleistungslaser, häufig ein CO2-Laser benutzt.In all of these cases, a high-power laser, often a CO 2 laser, is used.
Aus der DE-OS 39 32 328 ist im übrigen ein Verfahren zur Bearbeitung von durch Reibung beanspruchten Flächen in Brennkraftmaschinen, insbesondere der Zylinderlaufflächen von Kolbenmotoren bekannt, wobei die Fläche gehont und zusätzlich einer Laserstrahlbehandlung unterzogen wird. Diese Laserstrahlbehandlung nach vorherigem Honen wird vorzugsweise durch einen gepulsten sogenannten Excimer-Laser durchgeführt, wobei diese Behandlung eine Oberflächenabdampfung von Mikroriefen bei Erhaltung der Makroriefen (ölfördernde Honriefen) ohne ungewollte Umschmelzerscheinungen verursacht. Die DE-OS 39 32 398 erwähnt eine nicht gezielt erzeugte "Haut" im Nanometerbereich (< 1µm), d.h. in der Größenordnung von 0,001µm. Durch die extremen Abschreckraten ist sie meist übersättigt oder bereits schon amorph und deshalb eventuell hart.DE-OS 39 32 328 is a method for the rest Machining of surfaces subjected to friction in Internal combustion engines, especially the cylinder surfaces known from piston engines, the area honed and additional is subjected to a laser beam treatment. This Laser beam treatment after honing is preferred by a pulsed excimer laser carried out, this treatment a surface evaporation of micro grooves while maintaining the macro grooves (oil-producing honing grooves) without unwanted remelting caused. DE-OS 39 32 398 does not mention one targeted "skin" in the nanometer range (<1 µm), i.e. in the order of 0.001 µm. Due to the extreme quenching rates it is usually oversaturated or already already amorphous and therefore possibly hard.
Im Vergleich zu den bekannten Verfahren liegt der vorliegenden Erfindung die Aufgabe zugrunde, ein Verfahren der eingangs genannten Art vorzusehen, das das Aufhärten und vorzugsweise auch das gleichzeitige Mikroglätten von Maschinenbauteilen, ermöglicht, welche entweder in Form eines Hartgußteils mit ledeburitischem Gefüge oder in Form eines Stahlteils mit perlitischem Gefüge vorliegen, wobei das Verfahren so durchgeführt wird, daß eine neuartige Gefügestruktur an der Oberfläche des Bauteiles erreicht wird, das nicht nur eine harte und vorzugsweise auch mikroglatte Oberfläche bietet, sondern auch keinerlei Nachbearbeitung erfordert, wobei aber eine eventuelle Nachbearbeitung für Sonderzwecke nicht ausgeschlossen ist.In comparison to the known methods, the present one Invention based on the object, a method of provide the kind mentioned that the hardening and preferably also the simultaneous micro-smoothing of machine components, enables which either in the form of a Chilled cast part with ledeburitic structure or in the form of a Steel part with pearlitic structure are present, the Process is carried out so that a new structure is reached on the surface of the component, not only a hard and preferably also micro-smooth Surface offers, but also no post-processing requires, but a possible postprocessing for Special purposes is not excluded.
Zur Lösung dieser Aufgabe werden erfindungsgemäß die Merkmale von Anspruch 1 vorgesehen. Bevorzugte Ausführungsformen der Erfindung sind in den Ansprüchen 2-16 definiert. According to the invention, the features are used to achieve this object provided by claim 1. Preferred embodiments of the invention are in the claims 2-16 defined.
Im Gegensatz zu den bekannten Laserumwandlungshärten, das eine martensitische Struktur an der Oberfläche des Maschinenbauteils erzeugt, wird durch die Erfindung durch gezielte Wahl der Leistungsdichte sowie der Zeitdauer der lokalen Aufwärmung eine nahezu geschlossene Zementitoberfläche anstelle des Perlits in Stahl und Perlitbereiche im Hartguß erzeugt. Die Wahl der Leistungsdichte und Zeitdauer der Behandlung wird weiterhin so getroffen, daß nach der lokalen Aufwärmung der Oberfläche eine Selbstabschreckung der Oberflächenschicht durch die Umgebungstemperatur und die innerhalb des Bauteils herrschenden Temperaturen eintritt, wobei eine Rückbildung in den ursprünglichen Phasenzustand nicht oder nur unvollständig erfolgt. Dies bedeutet, daß es bei einem perlitischen oder ledeburitischem Gefüge an der Oberfläche bzw. an der Oberflächenschicht zu einem Vermengen der Zementitsubstanz auf Kosten des stöchiometrischen Gefügeaufbaus kommt. Durch die Behandlung mit dem jeweiligen Arbeitsstrahl (Laser, Elektronenstrahl bzw. Lichtbogenlampe) wird das eine Gefügebestandteil lokal teigig bzw. es schmilzt, während die anderen Gefügebestandteile im festen Zustand verbleiben. Üblicherweise handelt es sich bei dem Gefügebestandteil, der lokal teigig wird bzw. schmilzt, um die Bereiche zwischen den großen Zementitlamellen und dem Perlit. Hier spielt das Eisen-Kohlenstoffzustandsdiagramm unter Berücksichtigung der Ungleichgewichtsverhältnisse eine entscheidende Rolle.In contrast to the known laser transformation hardness, which has a martensitic structure on the surface of the Machine component is produced by the invention through a targeted choice of power density and duration the local warming up is almost closed Cementite surface instead of pearlite in steel and Pearlite areas created in chilled cast iron. The choice of Power density and duration of treatment will continue to be made so that after local warming up the surface a self-quenching of the surface layer by the ambient temperature and the inside prevailing temperatures of the component, wherein a regression to the original phase state not or only incompletely. This means, that it is in a pearlitic or ledeburitic Microstructure on the surface or on the surface layer to mix the cementite substance at the expense of stoichiometric structure comes. By treatment with the respective working beam (laser, electron beam or arc lamp) is a structural component locally dough or it melts while the other structural components remain in the solid state. Usually the structural component is which locally becomes dough or melts around the Areas between the large cementite slats and the Perlite. This is where the iron-carbon state diagram plays taking into account the imbalance ratios a crucial role.
Die Behandlung soll so durchgeführt werden, d.h. vor allem so kurz dauern, daß sich in der Randschicht keine Homogene, z.B. austenitische Mischkristalle ausbilden können, wobei stets genügend Zementitkeime in der Randschicht und im Substrat vorhanden sein müssen, so daß beim Abschrecken (Selbstabschreckung oder evtl. mit Hilfe eines Kältestrahls) stets Zementit und nicht Restaustenit gebildet wird. The treatment should be carried out in this way, i.e. in front everything so short that there are none in the boundary layer Homogeneous, e.g. form austenitic mixed crystals can, always enough cementite germs in the surface layer and must be present in the substrate so that when quenching (self-deterrence or possibly with With the help of a cold jet) always cementite and not Austenite is formed.
Die Behandlung läßt sich so durchführen, beispielsweise mit einer gepulsten Strahlenquelle hoher Energiedichte, wie z.B. mit einem Excimer-Laser, daß ein ausgeprägtes Abdampfen (Sublimation) und Schmelzen einer dünnen Oberflächenhaut erfolgt, was zu einem ausgeprägten Mikroglätten der Oberfläche führt.The treatment can be carried out in this way, for example with a pulsed radiation source of high energy density, such as. with an excimer laser that a pronounced Evaporation (sublimation) and melting a thin one Surface skin occurs, resulting in a pronounced Micro-smoothing the surface leads.
Im allgemeinen ist es sinnvoll, vor der Behandlung mit dem Strahl hoher Energiedichte, das jeweilige Bauteil wenigstens an der zu behandelnden Oberfläche zu schleifen, wobei aber auch schalenhart gegossene Oberflächen mit dem erfindungsgemäßen Verfahren behandelt werden können. Typische Anwendungsbeispiele für das vorliegende Verfahren sind die Erzeugung von harten und ggf. mikroglatten Oberflächen an Nockenwellen oder Schlepphebel von Verbrennungsmotoren.In general, it makes sense to start with before treatment the beam of high energy density, the respective component to grind at least on the surface to be treated, but also hard shell cast surfaces can be treated with the method according to the invention can. Typical application examples for the present Processes are the generation of hard and possibly micro-smooth surfaces on camshafts or cam followers of internal combustion engines.
Typische Werte für die verwendete Energiedichte liegen im Bereich von 2 x 103 bis 5 x 105 W/cm2.Typical values for the energy density used are in the range from 2 x 10 3 to 5 x 10 5 W / cm 2 .
Angaben zu typischen Belichtungszeiten bzw. Behandlungszeiten für die einzelnen Stellen der Oberfläche sind den weiteren Unteransprüchen bzw. den Beispielen zu entnehmen. Die Erfindung schafft daher eine berührungslose, sehr schnelle Methode zum gleichzeitigen Glätten und Aufhärten von heterogenen Verschleißoberflächen metallischer Werkstoffe. Weiterhin ermöglicht es die Erfindung das Mikroglätten geschliffener Verschleißoberflächen mit dem Aufhärten durch Zementitvermengung an gegossenen Hartgußteilen mit ledeburitischem bzw. Stahl mit perlitischem Gefüge in einer Operation zu vereinigen. Durch die Bildung von nahezu kompakten geschlossenen Zementitoberflächen anstelle des Perlits im Stahl und Perlitbereichen im Hartguß, wird besonders die adhäsive Verschleißbeständigkeit stark verbessert. Die Erfindung weist auch folgende Vorteile auf:
- sie ersetzt das mechanische Mikroglätten (Mikrofinishen) von Verschleißoberflächen auf Nockenwellen und Schlepphebeln,
- sie verringert den Einlaufverschleiß,
- die Behandlung dauert sehr kurz, typischerweise bis zu einer halben Minute pro Nockenwelle,
- die Methode läßt sich sehr gut in die Produktionslinie einfügen.
- it replaces mechanical micro-smoothing (microfinishing) of wear surfaces on camshafts and rocker arms,
- it reduces run-in wear,
- the treatment takes a very short time, typically up to half a minute per camshaft,
- the method can be inserted very well into the production line.
Durch die Erfindung werden Maschinenbauteile behandelt, die entweder in Form eines Hartgußteils mit ledeburitischem Gefüge oder in Form eines Stahlteils mit perlitischem Gefüge vorliegen, mit dem besonderen Kennzeichen, daß eine nahezu geschlossene Zementitoberfläche vorliegt, wobei das Bauteil eine Oberflächenhärte oberhalb von 900 HV, vorzugsweise etwa 1100 HV aufweist und die Zementitausscheidungsdichte in den zwischenlamellaren Bereichen von der Oberfläche in Richtung Matrix kontinuierlich abnimmt. Das Bauteil kann beispielsweise eine Nockenwelle oder ein Schlepphebel sein, es sind aber natürlich auch viele andere denkbare Maschinenbauteile, welche erfindungsgemäß behandelt werden können.The invention deals with machine components that either in the form of a hard casting with ledeburitic Structure or in the form of a steel part with pearlitic Structures are present, with the special characteristic, that an almost closed cementite surface is present, the component having a surface hardness above 900 HV, preferably about 1100 HV and the cementite precipitation density in the interlamellar Areas from the surface towards Matrix is continuously decreasing. The component can for example a camshaft or a rocker arm be, but there are of course many other conceivable Machine components which are treated according to the invention can be.
Schließlich soll zum Ausdruck gebracht werden, daß die Behandlung grundsätzlich in der Luft durchführbar ist, wenigstens mit einem Laserstrahl oder mit einer Lichtbogenlampe, da Oxidationsvorgänge nicht oder nicht im ausgeprägten Maße zu befürchten sind. Es kann unter Umständen nützlich sein, die Behandlung mit der gewählten Strahlart in einer ausgewählten Gasatmosphäre durchzuführen, um spezielle Effekte zu erreichen. Beispielsweise könnte die Behandlung in einer stickstoffhaltigen oder CO2-haltigen Atmosphäre durchgeführt werden, wenn ein Nitrieren oder Aufkohlen der Oberfläche des Werkstücks zusätzlich erwünscht ist.Finally, it should be expressed that the treatment can basically be carried out in the air, at least with a laser beam or with an arc lamp, since there is little or no fear of oxidation processes. It may be useful to carry out the treatment with the selected jet type in a selected gas atmosphere in order to achieve special effects. For example, the treatment could be carried out in a nitrogen-containing or CO 2 -containing atmosphere if nitriding or carburizing the surface of the workpiece is additionally desired.
Die Erfindung wird nachfolgend näher erläutert, anhand von vier elektronenmikroskopischen Abbildungen und drei Ausführungsbeispielen.The invention is explained in more detail below with reference to of four electron microscopic images and three Embodiments.
Die rasterelektronenmikroskopischen Abbildungen zeigen:
- Fig. 1
- eine Draufsicht auf eine umgeschmolzene Lauffläche einer Gußeisennockenwelle vor Anwendung der erfindungsgemäßen Behandlung (2580 mal vergrößert),
- Fig. 2
- die Oberfläche nach Fig. 1, jedoch nach zusätzlicher erfindungsgemäßer Behandlung mit einem Excimer-Laser (2040 mal vergrößert),
- Fig. 3
- eine Draufsicht auf ein eutektoidales Gefüge eines unbehandelten Stahls mit 0,8%C (1010 mal vergrößert und geätzt),
- Fig. 4
- das Gefüge aus Fig. 3 nach erfindungsgemäßer Laserbehandlung mit Schliff senkrecht zur behandelten Oberfläche bei 40000-facher Vergrößerung und geätzt.
- Fig. 1
- a plan view of a remelted tread of a cast iron camshaft before applying the treatment according to the invention (enlarged 2580 times),
- Fig. 2
- 1, but after additional treatment according to the invention with an excimer laser (magnified 2040 times),
- Fig. 3
- a plan view of a eutectoidal structure of an untreated steel with 0.8% C (1010 times enlarged and etched),
- Fig. 4
- the structure of Fig. 3 after laser treatment according to the invention with grinding perpendicular to the treated surface at 40,000 times magnification and etched.
Wie bereits oben erläutert, befaßt sich die Erfindung mit der Oberflächenbehandlung von Maschinenbauteilen mit heterogenem (über-, unter- oder -eutektischem) Gußgefüge, so wie in Fig. 1 dargestellt, bzw. mit über-, unter- oder -eutektoidalem Stahlgefüge, so wie in Fig. 3 dargestellt. As already explained above, the invention is concerned with the surface treatment of machine components with heterogeneous (over-, under- or -eutectic) Casting structure, as shown in Fig. 1, or with over-, under- or -eutectoidal steel structure, such as shown in Fig. 3.
Die rasterelektronenmikroskopische Draufsicht der Fig. 1 zeigt eine WIG-umgeschmolzene Lauffläche einer Gußeisennockenwelle mit einem untereutektischem Gefüge aus Zementitlamellen und feinem Perlit. Das WIG-Umschmelzverfahren stellt eine mögliche, jedoch nicht zwingend erforderliche Vorbehandlung dar. In Fig. 1 sind die Zementitlamellen die großflächigen Inseln, während die Perlitbereiche die filigrane Struktur aufweisen. Ein qualitativ ähnliches Gefüge liefert auch Schalenhartguß.The scanning electron microscopic top view of FIG. 1 shows a TIG remelted tread of a Cast iron camshaft with an hypoeutectic structure made of cementite flakes and fine pearlite. The TIG remelting process represents a possible, but not mandatory pretreatment. In Fig. 1 the cementite lamellas are the large islands, while the pearlite areas the filigree structure exhibit. A qualitatively similar structure also delivers Chilled cast iron.
Nach zusätzlicher Behandlung der Oberfläche mit einem Excimer-Laser mit einer Pulsleistungsdichte von beispielsweise 40 mJ/mm2, 2 Pulse, Pulsdauer 40 ns entsteht eine Oberflächenstruktur nach Fig. 2. Aus den Gefügebestandteilen wie im Fig. 1, d.h. aus den Zementitlamellen und feinem Perlit hat sich eine nahezu geschlossene Schicht eines nichtstöchiometrischen Zementits in der Randschicht gebildet. Charakteristisch für diese Behandlung ist, daß die Oberflächenschicht bis in die Nähe der Schmelztemperatur kurzzeitig (kontinuierlich oder durch mehrmalige Pulse) erwärmt wird, so daß in der Randschicht eine Diffusion des Kohlenstoffs aus den Zementitlamellen des Ledeburits in die weichen zwischenlamellaren Ferritbereiche stattfindet. Die Haltezeit auf dieser Temperatur wird so gewählt, daß es nicht zu einer vollständigen Auflösung vorhandener Phasenbestandteile und Bildung eines homogenen Mischkristalls kommt. Durch die darauffolgende Selbstabschreckung der Oberflächenschicht kann eine Rückbildung in den ursprünglichen Phasenzustand nicht oder nur unvollständig erfolgen. Es entsteht daher ein Ungleichgewichtzementit mit einem höheren Volumen als das ursprüngliche. Bei einem perlitischen Gefüge kommt es zu einem "Vermengen" der Zementitsubstanz, wie aus Fig. 2 klar ersichtlich, auf Kosten des stöchiometrischen Gefügeaufbaus, verbunden mit dem Effekt einer Aufhärtung der Oberflächenschicht bis auf 1100 HV.After additional treatment of the surface with an excimer laser with a pulse power density of, for example, 40 mJ / mm 2 , 2 pulses, pulse duration 40 ns, a surface structure according to FIG. 2 is formed. From the structural components as in FIG. 1, ie from the cementite lamellae and fine Perlite has formed an almost closed layer of non-stoichiometric cementite in the surface layer. It is characteristic of this treatment that the surface layer is briefly heated up to the vicinity of the melting temperature (continuously or by repeated pulses) so that the carbon diffuses in the boundary layer from the cementite lamellae of the ledeburite into the soft, interlamellar ferrite areas. The holding time at this temperature is chosen so that there is no complete dissolution of existing phase components and formation of a homogeneous mixed crystal. As a result of the subsequent self-quenching of the surface layer, a regression to the original phase state cannot take place or can only take place incompletely. This creates an imbalance cementite with a higher volume than the original one. In the case of a pearlitic structure, the cementite substance "blends", as can clearly be seen in FIG. 2, at the expense of the stoichiometric structure, combined with the effect of hardening the surface layer up to 1100 HV.
Die Fig. 3 zeigt eine rasterelektronenmikroskopische Aufnahme eines eutektoidalen Gefüges eines Stahls mit ungefähr 0,8%C. Man sieht Ferrit als dunkle Teile der Matrix und Zementit als helle Teile der Matrix in lamellarer Anordnung. Nach Behandlung mit dem Excimer-Laser, wie für die Gußeisenprobe der Fig. 1, entsteht ein Gefügeaufbau in der Randschicht, wie in Fig. 4 dargestellt. Die ursprünglichen Zementitlamellen, welche als hellere Kerne weiterhin sichtbar sind, haben sich in einer Randschicht von ungefähr 2 µm Tiefe "vermengt". Nahezu die ganze Randschicht besteht aus einem vermutlich nicht gleichgewichtigen, teils körnig ausgeschiedenem Zementit. Auch hier hat die kurzzeitige Erwärmung der Oberflächenschicht bis in die Nähe der Schmelztemperatur (kontinuierlich oder durch mehrmalige Pulse des Lasers) in einer Randschicht eine Diffusion des Kohlenstoffs aus den Zementitlamellen des Perlits in die weichen zwischenlamellaren Ferritbereiche bewirkt.3 shows a scanning electron microscope Inclusion of a steel eutectoid structure about 0.8% C. One sees ferrite as dark parts of the Matrix and cementite as light parts of the matrix in lamellar Arrangement. After treatment with the excimer laser, As for the cast iron sample of Fig. 1, a structure is created in the surface layer, as shown in Fig. 4. The original cementite slats, which are considered lighter Cores are still visible, have been in an edge layer of about 2 µm depth. Almost that whole edge layer probably does not consist of one balanced, partly granular excreted cementite. Here too, the surface layer has briefly warmed up up to near the melting temperature (continuously or by repeated pulses of the laser) a diffusion of carbon in an edge layer from the cementite flakes of pearlite into the soft interlamellar ferrite areas.
Die erreichte Temperatur in der Nähe der Schmelztemperatur muß so gewählt werden, daß es nicht zu einer vollständigen Auflösung vorhandener Phasenbestandteile und Bildung eines homogenen Mischkristalls kommt. Auch hier verhindert die der Wärmebehandlung folgende Selbstabschreckung der Oberflächenschicht eine Rückbildung in den ursprünglichen Phasenzustand. Ebenso entsteht in diesem Beispiel ein Ungleichgewicht Zementit mit einem höheren Volumen als das ursprüngliche.The temperature reached near the melting temperature must be chosen so that it is not a complete Dissolution of existing phase components and A homogeneous mixed crystal is formed. Here too prevents self-quenching following heat treatment a regression in the surface layer the original phase state. Likewise, in this example an imbalance with a cementite higher volume than the original.
Sowohl bei dem perlitischen als auch bei dem ledeburitischem Gefüge kommt es daher zu einem "Vermengen" der Zementitsubstanz auf Kosten des stöchiometrischen Gefügeaufbaus, verbunden mit dem Effekt einer Aufhärtung der Oberflächenschicht bis auf 1100 HV. Im günstigsten Fall wird es bei beiden Metallsorten auf der behandelten Oberfläche zur Ausbildung einer sogar geschlossenen nichtstöchiometrischen Zementitschicht kommen, die eine erhebliche Verbesserung der abrasiven und besonders der adhäsiven Verschleißbeständigkeit in der Einlaufphase und im weiteren Betrieb zur Folge hat.Both the pearlitic and the ledeburitic Therefore there is a "blending" of the microstructures Cementite substance at the expense of the stoichiometric structure, combined with the effect of hardening the surface layer down to 1100 HV. In the cheapest Case it is treated with both types of metal on the Surface to form an even closed one non-stoichiometric layer of cementite come one significant improvement in abrasive and especially the adhesive wear resistance in the running-in phase and results in further operation.
Von Bedeutung bei beiden Metallsorten ist auch, daß das lokale Teigigwerden bzw. Schmelzen der einen, bei gleichzeitigem Verbleiben der anderen Gefügebestandteile im festen Zustand möglich ist, so daß die primären Werkstückoberflächen auch nach der Behandlung formtreu erhalten bleiben, wenn von geringer Oberflächenglättung infolge Abdampfen einer Oberflächenschicht abgesehen wird. Da die Behandlung nur so kurz dauert, daß sich in der Randschicht kein homogener, z.B. austenitischer Mischkristall ausbilden kann, sind stets genügend Zementitkeime in der Randschicht und im Substrat vorhanden, das beim Abschrecken abermals stets Zementit und nicht Restaustenit gebildet wird. Wird die Randschicht mit einer gepulsten Strahlenquelle, vorzugsweise mit einem Excimer-Laser behandelt, so wird zusätzlich ein starkes Abdampfen (Sublimation) und Schmelzen einer dünnen Oberflächenhaut stattfinden. Infolge des Verdampfens sowie der Oberflächenspannung der geschmolzenen Oberflächenhaut wird in diesem Fall ein zusätzliches Mikroglätten (Entfernen der Schleifriefen, Verschuppungen und des Blechmantels) stattfinden. Bei entsprechender Einstellung der Laserparameter wird ein gleichzeitiges Glätten der Oberfläche und "Vermengen" des Zementits bis zur Ausbildung einer geschlossenen Schicht stattfinden.It is also important for both types of metal that the local dough or melting of some, at the other structural components remain at the same time is possible in the solid state, so that the primary Workpiece surfaces are true to shape even after treatment are retained if the surface smoothness is low due to evaporation of a surface layer is disregarded. Because the treatment is so short, that no homogeneous, e.g. austenitic Mixed crystal can always be sufficient Cementite germs in the surface layer and in the substrate is present, which is always cementite when quenched and no residual austenite is formed. Will the boundary layer with a pulsed radiation source, preferably treated with an excimer laser, so is additional a strong evaporation (sublimation) and melting a thin surface skin. As a result of Evaporation and the surface tension of the melted Surface skin becomes an additional one in this case Micro smoothing (removal of the sanding marks, scaling and the sheet metal jacket) take place. With appropriate Setting the laser parameters will be a simultaneous smoothing of the surface and "blending" of cementite until the formation of a closed one Shift take place.
Die Erfindung beschreibt daher eine Methode der berührungslosen Erzeugung von dünnen Verschleißschichten, hauptsächlich durch "Vermengung" der Zementitoberfläche. Dabei wird auch eine Verbesserung der Pitting- und Ermündungsbeständigkeit erreicht. Die Erfindung beinhaltet gleichzeitig eine Glättung der Oberfläche. Diese Behandlung kann das mechanische Mikrofinishen erfolgreich ersetzen. Der Einlaufverschleiß wird durch das Glätten stark reduziert. Das Verfahren hat auch den besonderen Vorteil, daß es sich ohne weiteres in bestehenden Produktionslinien ohne großen Aufwand integrieren läßt.The invention therefore describes a method of non-contact Generation of thin wear layers, mainly by "mixing" the cementite surface. It will also improve pitting and Maturation resistance achieved. The invention includes at the same time smoothing the surface. This Mechanical microfinishing can be successful replace. The inlet wear is caused by the Smoothing greatly reduced. The procedure also has the special advantage that it is easily in existing production lines without much effort integrates.
Um die praktische Ausübung der Erfindung näher darzustellen, werden nun einige konkrete Ausführungsbeispiele beschrieben:In order to illustrate the practice of the invention in more detail, are now some concrete examples described:
Die geschliffene ledeburitische Nockenoberfläche einer Nockenwelle (NW) wird mit einem CO2-Laser im CW-Betrieb (Kontinuierlicher, nicht gepulster Laserstrahl) mit einem rechteckigen Strahlquerschnitt der Größe 2 x 10 bzw. 1 x 20 mm2 durch Rotation der Nockenwelle unter dem Laserstrahl behandelt. Die Breite von ca. 10 bzw. 20 mm entspricht der Nockenbreite einer NW mit 4- bzw. 2-Ventiltechnik. Die Oberflächentemperatur im Bereich Liquidus-Solidus von 1150 bis 1250°C (teigiger Zustand der Oberflächenschicht) wird mit bekannten "on line" Temperaturmeßsystemen überwacht.The ground ledeburitic cam surface of a camshaft (NW) is cut with a CO 2 laser in CW mode (continuous, non-pulsed laser beam) with a rectangular beam cross-section of size 2 x 10 or 1 x 20 mm 2 by rotating the camshaft under the laser beam treated. The width of approx. 10 or 20 mm corresponds to the cam width of an NW with 4 or 2 valve technology. The surface temperature in the area of liquidus solidus from 1150 to 1250 ° C (pasty state of the surface layer) is monitored with known "on line" temperature measuring systems.
Die Leistungsdichte beträgt 5 x 103 bis 105 W/cm2. Bei genannter Strahlquerschnittgröße wird eine Laserleistung von 5 bis 8 kW benötigt. Die Rotationsgeschwindigkeit der Nockenwelle wird aus der Verweilzeit des Laserstrahls auf der Nockenoberfläche bestimmt. Für eine Karbidschichtdicke von 3 bis 10 µm wird eine Verweilzeit (Belichtungszeit) von 0,3 bis 10 s benötigt. Wird die Behandlung im Pulsbetrieb mit einem CO2- bzw. Nd: YAG-Laser durchgeführt, so werden mindestens um 20% geringere mittlere Leistungsdichten benötigt. The power density is 5 x 10 3 to 10 5 W / cm 2 . With the beam cross-section size mentioned, a laser power of 5 to 8 kW is required. The speed of rotation of the camshaft is determined from the dwell time of the laser beam on the cam surface. A dwell time (exposure time) of 0.3 to 10 s is required for a carbide layer thickness of 3 to 10 µm. If the treatment in pulse mode is carried out with a CO 2 or Nd: YAG laser, at least 20% lower average power densities are required.
Die ledeburitische Nockenlauffläche eines schalenhartguß- bzw. randschichtumschmolzenen (WIG; Laser, Elektronenstrahl) Schlepphebels wird zwecks Ausbildung einer dünnen, jedoch nahezu dichten karbidischen Verschleißschicht mit dem Elektronenstrahl behandelt. Der E-Strahl mit 0,1 bis 0,5 mm Strahldurchmesser rastert die gesamte Nockenlauffläche auf bekannter Weise ein oder mehrmals ab. Bei mehrmaligen Abrastern der Oberfläche wird ebenfalls eine nahezu konstante, mittlere Temperatur der Oberfläche, die über den Liquidus nicht hinaussteigt, erhalten bleiben. Beispielsweise wird eine Ablenkungsfrequenz des E-Strahles von 100 bis 500 Hz in der Y-Achse und eine Vorschubgeschwindigkeit des Schlepphebels in X-Achse von 5 bis 60 mm/s angewandt, abhängig davon, ob eine Vorwärmung des Schlepphebels vorher stattgefunden hat oder nicht. Die im Beispiel benötigte Leistung der Elektronenstrahlkanone betrug 3 kW (60 V, 50 A).The ledeburitic cam tread of a hard cast or surface layer remelted (TIG; laser, electron beam) Rocker arm is used for training purposes thin, but almost dense carbide Wear layer treated with the electron beam. The e-beam with 0.1 to 0.5 mm beam diameter grids the entire cam tread in a known manner one or more times. Repeated scanning of the Surface also becomes an almost constant, medium one Temperature of the surface above the liquidus does not rise, remain intact. For example becomes a deflection frequency of the e-beam from 100 to 500 Hz in the Y axis and a feed rate the rocker arm applied in the X-axis from 5 to 60 mm / s, depending on whether preheating the rocker arm has previously taken place or not. The in Example required power of the electron beam gun was 3 kW (60 V, 50 A).
Der Vorteil des Elektronenstrahls liegt in diesem Fall in der hohen Führungsgenauigkeit und Ablenkbarkeit sowie in der lokalen Wiederholbarkeit der Behandlung. Dadurch können ohne speziellen Aufwand je nach Bedarf auf einer Oberfläche Karbidschichten unterschiedlicher Dicke erzeugt werden (maßgeschneiderte Schichtdicken).The advantage of the electron beam is in this case in the high level of guidance and distractibility as well as in the local repeatability of the treatment. This allows you to do so without any special effort as required different carbide layers on one surface Thickness can be generated (customized layer thicknesses).
Zur Erzeugung einer dünnen Karbidschicht auf Stahloberflächen mit perlitisch bzw. perlitisch-ferritischem Gefüge werden Oberflächentemperaturen von 1250 bis 1450°C benötigt. Bei einem CO2-Laser im CW-Betrieb (Kontinuierlicher Strahl) wird mit einer Laserleistungsdichte im Bereich 2 x 104 bis 5 x 105 W/cm2 und im Pulsbetrieb mit einer mittleren Leistungsdichte die mindestens 20% geringer ist, gearbeitet.Surface temperatures of 1250 to 1450 ° C are required to produce a thin carbide layer on steel surfaces with pearlitic or pearlitic-ferritic structure. A CO 2 laser in CW operation (continuous beam) works with a laser power density in the range of 2 x 10 4 to 5 x 10 5 W / cm 2 and in pulse mode with an average power density that is at least 20% lower.
Die Strahleinwirkungszeit ist vergleichbar mit der, die für ein ledeburitisches Gefüge benötigt wird (Beispiel 1). Zwar liegt hier die Liquidus-Solidus-Temperatur höher, jedoch ist auch die Diffusionsgeschwindigkeit entsprechend der Temperatur höher.The radiation exposure time is comparable to that is required for a ledeburitic structure (example 1). The liquidus solidus temperature is here higher, but the diffusion rate is also higher according to the temperature higher.
Charakteristisch für die Karbidschicht der vorliegenden Erfindung ist, daß diese auf vorhandenen verschleißfesten Ledeburit bzw. Perlit erzeugt wird, die Verschleißbeständigkeit verbessert wird und daß die Zementitausscheidungsdichte in den zwischenlamellaren Bereichen stets von der Oberfläche in Richtung Matrix abnimmt.Characteristic of the carbide layer of the present Invention is that these are wear-resistant on existing Ledeburit or perlite is produced, the wear resistance is improved and that the cementite precipitation density in the interlamellar areas always from the surface towards the matrix decreases.
Durch die oben gemachten Beispiele und die dort genannten Parameterwerte werden die Unterschiede zu den in der US-PS 4 304 978 verwendeten Parameterwerten klar, d.h. es liegt nicht nur ein unterschiedliches Bestreben vor (wie eingangs genannt, befaßt sich die US-PS mit Umwandlungshärten, das durch Martensitbildung erreicht werden), sondern führen auch die in der US-PS 4 304 978 genannten Parameterwerte nicht zufällig zu der in der vorliegenden Anmeldung angestrebten Zementitvermengung.Through the examples made above and those mentioned there Parameter values are the differences from those in U.S. Patent No. 4,304,978 used parameter values clearly, i.e. it is not just a different endeavor before (as mentioned at the beginning, the US PS deals with Transformation hardness achieved through martensite formation ), but also perform those in U.S. Patent No. 4,304,978 parameter values mentioned are not random to the one in the present application aimed cementite mixing.
Die in der US-PS 4 304 978 beschriebene Leistungsdichte von 1550 bis 2480 W/cm2 steht dem Wert von 5000 bis 500 000 W/cm2 nach der vorliegenden Erfindung gegenüber. Auch die in der US-PS genannten Belichtungszeiten von 0,017 bis 0,026 S sind mit den in der vorliegenden Anmeldung genannten Werten von 0,1 bis 10 s nicht vergleichbar.The power density of 1550 to 2480 W / cm 2 described in U.S. Patent No. 4,304,978 contrasts with the value of 5,000 to 500,000 W / cm 2 according to the present invention. The exposure times of 0.017 to 0.026 S mentioned in the US patent are also not comparable with the values of 0.1 to 10 s mentioned in the present application.
Werden die Parameter des gepulsten Excimer-Lasers in
Betracht gezogen, liegen bei der vorliegenden Erfindung
wesentlich kürzere Belichtungszeiten von
Claims (16)
- Method of hardening and optionally smoothing machine components by means of a beam which brings about a surface heating of the respective component, such as for example a laser beam, an electron beam or an arc, wherein the respective component, which is present either in the form of a chill cast part with ledeburitic structure or in the form of a steel part with perlitic structure, is treated with a high energy density and the surface layer is heated up to and into the region of the melting temperature, i.e. into the region of the liquidus-solidus, for a short period of time, either continuously or by multiple pulses, so that in a marginal layer a diffusion of the carbon takes place from the cementite lamella of the ledeburite and/or of the perlite into the soft ferrite regions between the lamella, with the power density and time duration of the treatment being so selected that with perlitic and ledeburitic structures an increase of the cementite volume occurs at the surface or in the layer close to the surface with a non-stochiometric structure, with the one structure component becoming locally pasty or fusing during the treatment while the other structure components remain in the solid state, with the holding time at the temperature in the vicinity of the melting temperature being so selected that a non-complete dissolution of existing phase components arises and no austenite is formed and sufficient cementite nuclei are present in the marginal layer and in the substrate so that during quenching cementite is once more always formed and not rest austenite, with the power density and also the time duration of the local heating being so selected that a cementite surface arises instead of the perlite in steel and instead of the perlite regions in chill cast iron.
- Method in accordance with claim 1, characterised in that the treatment takes place with a pulsed beam source of high energy density such as for example with an excimer laser in order to additionally cause pronounced vaporisation (sublimation) and fusion of a thin surface layer.
- Method in accordance with one of the preceding claims, characterised in that prior to the treatment with the beam of high power density the respective component is ground, at least at the surface to be treated, or cast skin hard.
- Method in accordance with one of the preceding claims, characterised in that it is carried out on cam shafts or rocker arms.
- Method in accordance with one of the preceding claims, characterised in that the power density preferably lies in the range of 5 x 103 to 5 x 105 W/cm2.
- Method in accordance with one of the preceding claims for the treatment of a cam shaft with a ledeburitic cam surface, characterised in that the treatment is carried out with a CO2 laser in constant wave operation (continuous, non-pulsed laser beam) with a rectangular beam cross-section with a size in the range 3 mm x 5 mm to 25 mm x 10 mm, preferably 2 mm x 10 mm to 1 mm x 20 mm, with the cam shaft being turned during the treatment with the dwell time (exposure time) at each point of the treated surface lying in the range between 0.3 to 10 seconds in order to achieve a carbide layer thickness of 3 to 10 µm.
- Method in accordance with claim 6, characterised in that the laser power lies in the range from 4 to 12 kW.
- Method in accordance with one of the preceding claims, in particular in accordance with claim 6, characterised in that the surface temperature is kept in the region of the liquidus-solidus from 1150 to 1250°C (parily pasty state of the surface structure) and is preferably monitored by means of a temperature measuring system.
- Method in accordance with claim 7 or claim 8, characterised in that the treatment is carried out in pulse operation instead of in constant wave operation, with either a CO2 laser or an Nd:YAG laser being used, with the mean power density being at least 20 % lower than in constant wave operation.
- Method in accordance with one of the preceding claims 1 to 5 for the treatment of a ledeburitic cam running surface of a chill cast or surface layer remelted rocker arm by means of an electron beam, with the electron beam having a circular cross-section with a diameter of 0.1 to 0.8 mm which scans the entire cam running surface in grid-like manner once or several times and produces an almost constant average temperature of the surface which does not go above the liquidus.
- Method in accordance with one of the claims 1 to 5 for the treatment of a ledeburitic cam running surface of a chill cast or surface layer remelted rocker arm by means of an electron beam, with the electron beam having an almost rectangular cross-section which covers the entire cam running surface width or sliding bearing surface width and continuously or multiply swingingly treats the surface in the peripheral direction and thus produces an almost constant mean temperature of the surface which does not go above the liquidus or only increases above it in locally restricted part regions or insubstantially.
- Method in accordance with claim 10 or 11, characterised in that the electron beam gun has a power of about 3 kW, for example 50 A at 60 V.
- Method in accordance with claim 10, 11 or 12, characterised in that with alignment of the electron beam gun in the Z-axis the beam is deflected in a direction substantially perpendicular thereto, for example in the direction of the Y- or X-axis with a deflection frequency of 100 to 500 Hz over the width or length of the cam running surface of the rocker arm, with the cam running direction being advanced in the respective other X- or Y-axial direction obliquely to it at a speed of advance of 5 to 60 mm/sec depending on whether a preheating of the rocker arm has previously taken place.
- Method in accordance with one of the claims 1 to 5, characterised in that, for production of thin carbide layers on steel surfaces with a perlitic or perlitic-ferritic structure, the surface is heated to a temperature in the range of 1250° to 1450°C which is produced with a CO2 laser in constant wave operation (continuous beam) with a power density in the range of 5 x 103 to 5 x 105 W/cm2 and in pulsed operation with an average power density which is about 20 % lower, with the time of action of the beam, i.e. the dwell time at each point of the treated surface amounting to 0.1 to 10 s.
- Method in accordance with one of the preceding claims, characterised in that the cementite precipitation density in the regions between the lamella continuously decreases from the surface in the direction of the matrix.
- Method in accordance with one of the preceding claims, characterised in that the treatment with the beam is carried out in a gas atmosphere, for example in a gas atmosphere which contains nitrogen or CO2.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE4241527 | 1992-12-10 | ||
| DE4241527A DE4241527A1 (en) | 1992-12-10 | 1992-12-10 | Process for hardening and possibly smoothing machine components as well as machine components manufactured according to this process |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0601451A1 EP0601451A1 (en) | 1994-06-15 |
| EP0601451B1 true EP0601451B1 (en) | 2000-08-23 |
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ID=6474825
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP93119338A Expired - Lifetime EP0601451B1 (en) | 1992-12-10 | 1993-12-01 | Process for hardness increasing and possibly for smoothing of work pieces and work pieces made by this process |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0601451B1 (en) |
| DE (2) | DE4241527A1 (en) |
| ES (1) | ES2151496T3 (en) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09216075A (en) * | 1996-02-06 | 1997-08-19 | Aisin Aw Co Ltd | Surface finishing method of metallic member and metallic member obtained thereby |
| JPH1060619A (en) * | 1996-08-13 | 1998-03-03 | Tochigi Fuji Ind Co Ltd | Member made of structural steel |
| DE19637464C1 (en) | 1996-09-13 | 1997-10-09 | Fraunhofer Ges Forschung | Wear resistant camshaft |
| US6288876B1 (en) * | 1999-04-16 | 2001-09-11 | International Business Machines Corporation | Melting and refreezing method for smothing and load/unloading lift tab for disk drive smoothed lift tab and gimbal assembly and data storage device incorporating smoothed lift tab |
| DE19959608B4 (en) * | 1999-12-10 | 2008-07-03 | Volkswagen Ag | Device for the laser treatment of cylindrical inner surfaces, preferably of cylinder running surfaces for internal combustion engines |
| DE10228743B4 (en) * | 2002-06-27 | 2005-05-04 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Method for smoothing and polishing surfaces by machining with laser radiation |
| DE10257165B4 (en) * | 2002-12-02 | 2004-09-23 | Cis Solartechnik Gmbh | Process for the production of thin-film solar cells with a CuInSe2 layer on a metallic, band-shaped substrate |
| EP2289687A1 (en) | 2007-05-16 | 2011-03-02 | Entex Rust & Mitschke GmbH | Method for machining products to be degassed |
| DE102009009775B4 (en) | 2008-02-22 | 2019-05-09 | Entex Rust & Mitschke Gmbh | Planetary roller extruder with fragmented planetary roller spindles |
| DE102009013839A1 (en) | 2009-02-20 | 2010-09-23 | Entex Rust & Mitschke Gmbh | Planetary-gear extruder for producing mixtures of e.g. plastics utilized for pipe, has planetary gear spindle extending over extruder section housing, where length of piece of spindle is five times of pitch diameter of tooth system of piece |
| DE102009059912B4 (en) | 2009-12-20 | 2023-08-03 | Entex Rust & Mitschke Gmbh | planetary roller extruder |
| DE102012107827A1 (en) * | 2012-08-24 | 2014-02-27 | Sandvik Surface Solutions Division Of Sandvik Materials Technology Deutschland Gmbh | Method for producing gloss effects on pressing tools |
| AT519996B1 (en) * | 2017-06-01 | 2020-03-15 | Andritz Ag Maschf | Steel surface treatment method |
| DE102018108145A1 (en) | 2018-04-06 | 2019-10-10 | Volkswagen Ag | Method for processing surfaces of components produced by means of 3D printing, and such a machined component |
| WO2025032245A1 (en) * | 2023-08-10 | 2025-02-13 | Caterpillar Motoren Gmbh & Co. Kg | Method for treating cylindrical tracks of cylinders or cylindrical sleeves by laser application |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4093842A (en) * | 1976-01-19 | 1978-06-06 | General Motors Corporation | Ported engine cylinder with selectively hardened bore |
| US4304978A (en) * | 1978-10-05 | 1981-12-08 | Coherent, Inc. | Heat treating using a laser |
| DD204106B1 (en) * | 1982-03-31 | 1988-02-03 | Adw Ddr | PROCESS FOR SURFACE HARDENING IRON-CARBON ALLOYS |
| DE3343783C1 (en) * | 1983-12-03 | 1984-07-05 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8900 Augsburg | Process for the production of wear-resistant cylinder running surfaces of internal combustion engines |
| DE3418555C1 (en) * | 1984-05-18 | 1985-07-25 | Audi AG, 8070 Ingolstadt | Process for remelting the surface of cylinders made of carbon-containing cast iron |
| JPS619517A (en) * | 1984-06-22 | 1986-01-17 | Mitsubishi Electric Corp | Surface reforming apparatus of mechanical parts for rotator |
| GB2169318A (en) * | 1985-01-04 | 1986-07-09 | Rolls Royce | Metal surface hardening by carbide formation |
| JPS6233720A (en) * | 1985-08-08 | 1987-02-13 | Toyota Motor Corp | Production of chilled cam shaft by remelting |
| JPS6293314A (en) * | 1985-10-21 | 1987-04-28 | Honda Motor Co Ltd | Wear-resistant sliding parts |
| DE3932328A1 (en) * | 1989-09-28 | 1991-04-11 | Opel Adam Ag | METHOD FOR MACHINING SURFACES HIGHLY STRESSED BY FRICTION IN INTERNAL COMBUSTION ENGINES, AND DEVICE FOR CARRYING OUT THE METHOD |
| ES2083164T3 (en) * | 1991-04-12 | 1996-04-01 | Mordike Barry Leslie | PROCEDURE FOR THE LASER REFUNDITION OF METALLIC SURFACES. |
-
1992
- 1992-12-10 DE DE4241527A patent/DE4241527A1/en not_active Withdrawn
-
1993
- 1993-12-01 DE DE59310090T patent/DE59310090D1/en not_active Expired - Fee Related
- 1993-12-01 EP EP93119338A patent/EP0601451B1/en not_active Expired - Lifetime
- 1993-12-01 ES ES93119338T patent/ES2151496T3/en not_active Expired - Lifetime
Non-Patent Citations (1)
| Title |
|---|
| Werkstatt und Betrieb, 123(1990)11, 875-877 * |
Also Published As
| Publication number | Publication date |
|---|---|
| DE59310090D1 (en) | 2000-09-28 |
| ES2151496T3 (en) | 2001-01-01 |
| DE4241527A1 (en) | 1994-06-16 |
| EP0601451A1 (en) | 1994-06-15 |
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