EP1888278B9 - Verfahren zum verdichten einer verzahnung mit unterschiedlichen verfahren - Google Patents

Verfahren zum verdichten einer verzahnung mit unterschiedlichen verfahren Download PDF

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Publication number
EP1888278B9
EP1888278B9 EP06761986A EP06761986A EP1888278B9 EP 1888278 B9 EP1888278 B9 EP 1888278B9 EP 06761986 A EP06761986 A EP 06761986A EP 06761986 A EP06761986 A EP 06761986A EP 1888278 B9 EP1888278 B9 EP 1888278B9
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EP
European Patent Office
Prior art keywords
toothing
tooth
preform
rolling
tool
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
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EP06761986A
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German (de)
English (en)
French (fr)
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EP1888278B1 (de
EP1888278A2 (de
Inventor
Gerhard Kotthoff
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GKN Sinter Metals Holding GmbH
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GKN Sinter Metals Holding GmbH
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Publication date
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Publication of EP1888278A2 publication Critical patent/EP1888278A2/de
Application granted granted Critical
Publication of EP1888278B1 publication Critical patent/EP1888278B1/de
Publication of EP1888278B9 publication Critical patent/EP1888278B9/de
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Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/08Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of toothed articles, e.g. gear wheels; of cam discs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21HMAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
    • B21H5/00Making gear wheels, racks, spline shafts or worms
    • B21H5/02Making gear wheels, racks, spline shafts or worms with cylindrical outline, e.g. by means of die rolls
    • B21H5/022Finishing gear teeth with cylindrical outline, e.g. burnishing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/16Both compacting and sintering in successive or repeated steps
    • B22F3/164Partial deformation or calibration
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D7/00Modifying the physical properties of iron or steel by deformation
    • C21D7/02Modifying the physical properties of iron or steel by deformation by cold working
    • C21D7/04Modifying the physical properties of iron or steel by deformation by cold working of the surface
    • C21D7/08Modifying the physical properties of iron or steel by deformation by cold working of the surface by burnishing or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F2003/248Thermal after-treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10Processes characterised by the sequence of their steps
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49462Gear making
    • Y10T29/49467Gear shaping
    • Y10T29/4948Gear shaping with specific gear material
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/19Gearing
    • Y10T74/1987Rotary bodies

Definitions

  • the invention relates to a surface compression of a workpiece with at least one toothing made of sintered material.
  • Sintered gear elements such as powder wheels produced by powder metallurgy are used in a wide range. Sintered materials generally have a lower density compared to conventionally forged materials of, for example, steel. From the US2004 / 0177719A1 shows that a gear-shaped green compact is sintered, the sintered workpiece is shot peened in a tooth root and then the gear is calibrated.
  • Object of the present invention is to achieve an improvement of a strength profile of a metal toothed element comprising a sintered material.
  • a surface compression of a workpiece with at least one gearing of sintered material which is surface-compacted by means of a rolling process is proposed, wherein a first surface of the workpiece, an internal gearing is compacted with a different method than a second surface of the workpiece, an external toothing.
  • a first toothing of the workpiece has a different compression than a second toothing of the workpiece.
  • an outer toothing is surface-compacted by means of a rolling process, while a second surface is a bore, which is surface-compacted with another method.
  • a bore in the workpiece receives a hardened surface after surface compacting and is then brought to a final shape.
  • This allows the use of the bore for a shaft or an axle.
  • An improvement in accuracy can be achieved by surface hardening after hardening of the toothing.
  • a preform of the toothed element is produced with a locally selective oversize relative to a final dimension of the toothed element and rolled to the final dimension by means of at least one rolling tool, wherein the Gear element is compressed locally varies at least in the region of at least one flank and / or a foot of a tooth of the toothed element to produce a compacted edge layer on a surface locally.
  • a toothed element is, for example, a toothed wheel, a rack, a cam, a P-rotor, a ring gear, a sprocket or the like.
  • the compacted sintered material is produced in particular by powder metallurgy methods.
  • a metal powder is sintered under pressure in conjunction with a heat treatment.
  • metal powder is injection-molded in conjunction with plastic and in particular sintered under a pressure, preferably with a heat treatment.
  • a sintered mold is used which has at least almost the final dimension of the toothed element to be produced.
  • the preform used is preferably the workpiece resulting directly from the sintering process.
  • at least one further surface treatment step can also be connected downstream.
  • the preform has an allowance, which is to be understood as a difference to a final dimension, wherein the difference is preferably defined pointwise perpendicular to the surface.
  • a rolling tool for example, a roller is used, which is provided with a toothing, which is engageable with the toothing of the toothing element.
  • a rolling tool is in particular rolled under pressure on a surface of the toothed element.
  • two or more such rolling tools are preferably used simultaneously.
  • a gear to be produced can be arranged centrally between two rolling tools.
  • a surface compression of the sintered material of the toothing can be effected.
  • such a manufacturing method starts, for example Takeya et al, "Surface Rolling of Sintered Gears", SAE 1982 World Congress, Technical Paper 820234 or. Also from DE 33 250 37 , out U.S.
  • a first rolling tool can be used under a first pressure substantially for rough contour rolling and then a second rolling tool under a second pressure to achieve the targeted surface densification.
  • the locally-selective allowance is in particular dimensioned so that the toothed element is compacted locally at least in the region of at least one flank and / or one foot of a tooth of the toothed element in a peripheral layer on a surface.
  • a full density is achieved within the compacted edge layer, the full density preferably being understood based on a density of a comparable powder-forged tooth.
  • a preform made of a sintered material in a core has a density of at least 6.8 d / cm 3 , preferably at least 7.1 g / cm 3, and more preferably at least 7.3 g / cm 3 .
  • the preform has, for example, a density of at least 7.7 g / cm 3 , preferably of at least 7.8 g / cm 3 , which corresponds to the density of a powder-forged preform of the same material.
  • a load-bearing strength characteristic is achieved particularly advantageously.
  • a highly stressable sintered toothing is preferably provided with a locally variable and load-adapted density profile.
  • the density profile can have a greater degree of density over a larger area, in particular in the areas subject to higher stress, in comparison to areas of lesser load which are directly adjacent to one another.
  • the respective differently densified edge layer is co-produced via a different allowance along a flank and / or tooth bottom of the preform.
  • a depth of the compacted edge layer in each case viewed perpendicular to the surface, has a maximum of the density approximately at the location of maximum stress. This can, for example, halfway up the Be tooth and steadily decrease to the tooth head and the tooth root to zero.
  • a particularly high compression in the sintering material is set.
  • other courses can be provided.
  • a force profile on a tooth flank of the toothed element in its intended use is taken into account.
  • the forces acting on teeth of a gear in a transmission are used and the resulting comparison voltage profiles are used below the surface. This procedure is also possible with other gears.
  • an allowance on a first flank of the tooth is selected differently than on a second flank of the tooth.
  • a force transmission direction is considered in a purpose of use of a toothing element according to the use. In the case of a gear wheel, this takes into account, for example, that, depending on a direction of rotation in the direction of rotation, other forces occur on the tooth flanks than counter to the direction of rotation.
  • a different compression due to a direction of rotation of a rolling tool can be compensated.
  • the oversizes are selected such that after a compression process, an identical compression profile results along the first and second tooth flanks.
  • a locally compressed surface layer is also sought in these areas. It is particularly useful if an asymmetric allowance is selected in a tooth base. For example, a left tooth root area has a different compression depth than a right tooth root. In particular, between two teeth in each case a preferably continuous variation of a depth of a boundary layer can be provided by a corresponding variation of the oversize.
  • a different, in particular asymmetrical, measure is preferably provided not only with respect to one flank, but preferably with respect to two mutually opposite flanks.
  • a different measure in the tooth root is provided, which is preferably asymmetrical.
  • tooth flanks and tooth roots of a toothing can each be asymmetric.
  • an undersize By this is meant that less sintered material is provided in a Beeich than would have to be provided with respect to a final contour after a processing step.
  • the determined undersize ensures, for example, that when displacing sintered material no undesirable elevations arise.
  • the undersize therefore represents a region of a preform with a toothing that is to be replenished by, in particular, displacement of sintered material.
  • the pressure angle of one flank of the tooth may differ by at least 15% from the pressure angle of the other flank of the tooth.
  • At least 20 .mu.m below a surface of a first flank of the tooth is generated by 2%, to at least 15% higher density than on a second flank of the tooth at the same height.
  • a density is achieved on the first flank of the tooth, which corresponds at least approximately to the density which is achieved for a powder-forged toothed element, whereas the second flank has a lower density.
  • a density in a range between 7.2 g / cm / set 3 and 7.7 g cm 3 on one side, while in the corresponding region of the second flank has a density between 7.5 g / cm 3 and 7.82 g / cm 3 is set.
  • rotational direction-dependent different loads of the two tooth flanks are taken into account.
  • a requirement-based elasticity and hardness profile is achieved. More preferably, this reduces a noise development, for example in a transmission.
  • a local allowance on a first flank of the tooth is selected larger by at least 10% than an allowance on a second flank of the tooth at the same height.
  • this achieves, for example, that an identical compression course is achieved on the first and the second tooth flank due to different pressurization during compression as a function of the direction of rotation.
  • a different compression course is achieved on the first and the second tooth flank.
  • different maximum densities, their depths as well as their location in relation to the height of the toothing can be set specifically.
  • an amount of a maximum local allowance is at least 15 ⁇ m, preferably at least 100 ⁇ m and particularly preferably at least 400 ⁇ m. If the density of the preform in a range between 7.2 g / cm 3 and 7.5 g / cm 3 , preferably a maximum allowance between 20 and 150 microns is provided. If the density of the preform between 6.7 g / cm 3 and 7.2 g / cm 3 , preferably a maximum allowance between 50 microns and 500 microns is used.
  • An oversize may also be negative locally, taking into account, for example, a lateral redistribution of material. A lateral redistribution can be done by flowing material as a result of a rolling process.
  • an at least locally negative oversize can be provided, which lies locally below the final dimension.
  • the negative allowance is preferably at most 100 ⁇ m.
  • the negative measurement is at most less than 50 ⁇ m and in particular less than 20 ⁇ m.
  • the maximum negative allowance is in a range between 100 ⁇ m and 20 ⁇ m.
  • a compression is achieved which reaches a depth between 1 mm and 1.5 mm, at least in a region of a tooth flank of the toothing.
  • the compaction in the tooth root may be lower.
  • the maximum depth of compaction of a tooth flank is greater by at least a factor of 6 than a maximum depth of compaction in a region of the associated tooth root. This allows the toothing on the one hand has sufficient strength, but on the other hand also retains a certain deformability. A tooth breakage is thereby avoided.
  • the preform and the rolling tool are rolled on each other until a final shaping movement between the toothed element produced thereby and the rolling tool is generated.
  • This is used for example for the production of intermeshing gears.
  • a distance between the rolling tool and preform is reduced during the rolling process with the rolling tool.
  • a rolling pressure is adjusted or adjusted.
  • a combination of force and path control in the manufacture of the teeth. In this case, in one section of the production, a pure travel control can take place and in another section of the production a pure force control. These can also alternate several times.
  • a cam is produced as a toothed element.
  • a cam can be produced, as used for example for the mechanical actuation of an adjusting device, for example for adjusting a valve or the like.
  • an improved strength profile with a lower susceptibility to wear is provided.
  • a further improvement in surface hardening can be achieved, in particular, by virtue of the fact that the method for producing a metal-toothed element which is at least partially surface-sealed comprises a thermal and / or chemical surface hardening process.
  • case hardening is used as the thermal and / or chemical hardening process. Preference is given here in addition to an increase in hardness, a reduction of tension.
  • a carbonitriding process is used.
  • a nitration or nitrocaboration process as well as a boriding process can be used.
  • a reduction in stress is also achieved in conjunction with a heat treatment.
  • a vacuum can be set, especially if case hardening is performed. It is also possible to perform an induction hardening.
  • the curing is performed only partially according to an embodiment, for example, made only in the field of teeth.
  • a method for producing an at least partially surface-hardened metal toothed element which has a compacted sintered material comprises the steps "cold or hot pressing, sintering, dimensional and surface compacting rolls and case hardening". For example, first a cold pressing of a metal powder in a mold, which has at least approximately the final dimension of the toothed element to be produced. In a second step, for example, the sintering process takes place under the action of heat with or without pressure. Preferably thereafter, the dimensional and surface compression takes place by means of rollers. As already mentioned above, dimensional and surface compacting rolls preferably take place simultaneously by means of at least two rolling tools. After this, finally, the curing, in particular case hardening can take place, which allows a further hardening of the surface.
  • Starting materials for the preform are sintered metallic powders, in particular pre-alloyed materials, partially alloyed materials or hybrid alloys.
  • Cold-pressing, sintering in a temperature range between 1100 ° C. and 1150 ° C., surface compacting, case hardening and subsequent grinding are performed on a prealloyed material to achieve a final shape of a toothed workpiece.
  • a manufacturing process can proceed as follows: choice of the powder material, cold pressing of the powder material, sintering preferably at a temperature of about 1120 ° C, connect forging, preferably at a temperature around 1000 ° C, eventually removing an oxidation layer, surface compacting in particular by rolling, Surface hardening, in particular case hardening, and possibly subsequent partial grinding to a final contour.
  • the process can take place completely or partially in a production line.
  • a further embodiment envisages hot pressing a partially alloyed sintered material, in particular in a temperature range between 50 ° C. and 90 ° C., carrying out a high temperature sintering, in particular in a temperature range between 1240 ° C. and 1290 ° C., performing a surface compression, a vacuum Use hardening and possibly then to honing.
  • a further embodiment of the invention provides that a surface thinning can be carried out using a wide variety of methods.
  • One embodiment provides, in particular, that in a first region the surface compression is carried out using a different method than in a second, different region.
  • beam hardening, shot peening, compacting by means of a ball, by means of a roller or by means of another rotatable body, by means of tooth-shaped tools, in particular rolling tools and the like can be used. These methods are also suitable in each case separately from each other to allow a necessary surface compaction.
  • the tooth root is not or only slightly compressed with a tool with which the tooth flank is compressed. It is possible to compact the surface in a section so far that only the pores on the surface are closed. Subsequently, the tooth root can be processed with another tool or remplinverdichtungshabilit. In particular, it is possible to achieve a different surface compression along the tooth flank in comparison with the tooth root. For example, it is possible to set different surface qualities, for example with regard to roughness. Also, the maximum surface depth may be different due to the different techniques. Furthermore, there is the possibility that the entire workpiece with the toothing receives a surface compression, such as surface blasting. In this way, in particular aluminum-containing sintered materials or other oxide-forming sintered materials can be processed, since with the surface densification in addition also removal of an oxide layer can be made possible.
  • a surface compression such as surface blasting.
  • the invention further relates to a preform for a method for producing an at least partially surface-hardened metal toothed element, which has a compacted sintered material, wherein a first and a second flank of a tooth each have different asymmetric dimensions. Furthermore, it is also provided that a first and a second foot region of a tooth have divergent, in particular asymmetrical, measurements.
  • the invention relates to a toothed element with a metallic sintered material, wherein the toothed element at least in the region of at least one edge of a Tooth of the toothed element has a locally varied compression.
  • This is preferably a suitable for many applications elasticity of the powder metallurgical material in conjunction with a surface hardening possible.
  • a noise reduction in the power transmission allows and at the same time provided a good wear resistance.
  • the toothed element is a toothed gear.
  • the toothed element is a helical gear.
  • a bevel gear can be provided. According to the above description, it is expedient if opposing flanks of teeth of a toothed element have an asymmetric compression.
  • an asymmetrical compaction is present in a foot area.
  • This compression is adapted in particular to forces occurring during a use according to the application.
  • provision is made in particular for the depth of the locally densified edge layer to be only so high that sufficient elasticity or rigidity of the tooth is still ensured.
  • the depth of the compacted edge layer is less in the foot region than on a tooth flank.
  • the toothed element is a cam.
  • the above statements are to apply accordingly, for example, flanks of the cam occur in place of the edges of teeth.
  • a ferrous material is selected as the main constituent of the sintered material and at least one alloying constituent from the group consisting of carbon, molybdenum, nickel, copper, manganese, chromium and vanadium.
  • An iron alloy is, for example, Fe -1.0 Cr -0.3 V +0.2 relative to a reference 15CrNiMo6.
  • Another iron alloy is for example Fe -1.5 Mo + 0.2C based on 20MnCr5.
  • the iron-containing alloy Fe -3.5 Mo based on 16MnCr5 is provided.
  • the alloy C 0.2% Cr 0.5% Mn 0.5% Mo 0.5% with the remainder containing iron and impurity.
  • other compositions may be provided.
  • a surface-compressed toothing made of sintered material has at least 80% aluminum and at least copper and magnesium as further sintering materials.
  • a first embodiment provides that additionally silicon is used as sintered material.
  • silicon may range from about 0.45% to about 0.8%, preferably between 0.6% and 0.75%. However, silicon may also be present in a higher range, for example between 13% and 17%, in particular between 14.5% and 15.5%. If the silicon content is higher, the copper content of the sintered material is reduced.
  • a first mixture may comprise copper at 4% to 5%, silicon at 0.45% to about 0.8%, magnesium at about 0.35% to 0.7%, and the balance at least primarily aluminum.
  • a pressing aid is preferably added. This can have a proportion between 0.8 and 1.8%.
  • a wax, in particular Amldwachs be used for this purpose.
  • a second blend may comprise copper at 2.2% to 3%, silicon at 13% to about 17%, magnesium at about 0.4% to 0.9%, and the balance at least primarily aluminum.
  • a pressing aid can be used as exemplified above. After a surface compaction, at least one region of the toothing has a density of, for example, more than 2.5 g / cm 3, preferably up to the maximum density.
  • such a manufactured workpiece with a toothing has a tensile strength of at least 240 N / mm 2 and a hardness of at least 90HB. If the silicon is higher, the density may in particular also be more than 2.6 g / cm 3 .
  • a second embodiment provides that in addition at least zinc is used as the sintering material in addition to copper and magnesium as additives and aluminum.
  • copper has a content in a range between 1.2% and 2.1%, in particular between 1.5% and 1.65%, magnesium between 1.9% and 3.1%, preferably between 2.45% and 2.65%, zinc between 4.7% and 6.1%, in particular between 2.3% and 5.55%.
  • the rest is at least mainly aluminum.
  • a pressing aid as described above can also be used here.
  • a workpiece made from this mixture with a toothing preferably has, after the surface compaction, at least one region of the toothing in which a density of at least 2.58 g / cm 3 extends up to the maximum density.
  • such a manufactured workpiece with a toothing a tensile strength of at least 280 N / mm 2 and a hardness of at least 120HB on.
  • a toothed element with a further functional component in particular a shaft or another gear, is sintered.
  • compliance with a precise working distance between a plurality of toothed elements, for example in a transmission, is thereby facilitated.
  • the toothed element is part of a pump.
  • it is an involute gear, which is brought into engagement with another involute gear.
  • the invention relates to a device for producing an at least partially surface-compressed toothing element, in particular for carrying out a method described above with a tool control adapted to a different allowance.
  • the device comprises in particular at least one rolling tool, which can preferably act on the preform with the aid of the adapted tool control, preferably under an adapted pressure and / or controlled path, in a matched engagement.
  • the device comprises a rolling tool with a toothed surface, which is engageable with the toothing of the toothed element and can be rolled over thereon.
  • the invention further provides an apparatus for producing an at least partially surface-hardened toothing element from a preform consisting of a sintered material at least in a surface region, wherein the device comprises a tool which compensates for different oversizes at a first and a second flank of a rolling movement to be compacted Tooth of the preform has.
  • the rolling tool can have a contour necessary for the shaping, for example an involute toothing, only on one flank or on both flanks of a tooth.
  • the invention relates to a method for designing an allowance for achieving a surface compression of a sintered-metal toothed element in a Rolling process, wherein the allowance is determined iteratively.
  • a geometry and in particular a torque and / or a pressure distribution is specified.
  • a design of a rolling tool is defined.
  • a preform with a locally defined allowance is determined.
  • a selection can be made using data libraries.
  • Such a data library contains, for example, experimental density profiles determined using various parameters.
  • a simulation of the compression or rolling process can take place.
  • the kinematics of the rolling process in conjunction with a simulation of elastic and plastic properties of the preform and optionally of the rolling tool is simulated.
  • the simulation of the elastic or plastic properties of the preform reference is made, for example, to models of continuum mechanics in conjunction with a discrete solution using, for example, finite element or finite volume methods.
  • a geometry of a rolling tool is determined iteratively taking into account the oversize. For example, an allowance of an involute toothing of the hobbing tool can be determined. Accordingly, an allowance for other than involute gearing can be determined.
  • a first step at least in a region of a flank of a tooth locally varied, at least pointwise definable allowance of a preform of the toothing element is automatically generated based on at least one design specification
  • a geometry of a rolling tool automatically is generated
  • a rolling process and thereby generated local course of compression of at least one edge layer of the toothed element is simulated
  • an automatic evaluation of the generated course of compaction is compared with a default, and optionally the method from the first step is repeated using at least one variation for optimization until an abort criterion is met.
  • the variation takes place, for example, with the aid of an optimization method.
  • An abort criterion is, for example, a tolerance between the desired density profile and the density profile achieved in the simulation. Furthermore, an abort criterion can also be an exceeding of a predefinable number of iterations.
  • the torque is to be understood here as the torque occurring in the intended use of a toothed element.
  • a material tension is simulated, at least in the area of compaction, and used in particular for evaluation. It is preferably avoided that a surface is indeed sufficiently cured, but is brittle due to stresses and tends to stress cracks.
  • data stored for variation in a database library is used.
  • methods for optimization and data analysis can be used, for example, by means of neural networks.
  • features stored in the database are used, for example, for optimization by means of a genetic algorithm.
  • At least one of the steps can be replaced by a default.
  • a rolling tool geometry is fixed. This is taken into account, for example, the fact that a rolling tool is much more expensive to modify, for example, as a preform.
  • Another embodiment provides a reverse approach. Preferably, starting from a final shape, a preform or the rolling tool for producing the final shape as well as the press tool for producing the preform are calculated.
  • the subject matter of the invention is a computer program product with program code means which are stored on a computer-readable medium in order to carry out at least one of the methods described above when the program is executed on a computer.
  • a computer-readable medium is for example a magnetic, a magneto-optical or an optical storage medium.
  • a memory chip is used.
  • a computer-readable medium can also be realized by means of a remote memory, for example by means of a computer network.
  • the computer program can be stored, for example, in a machine for surface compaction. Also, a calculation can be made separately from the machine for surface compaction.
  • the machine has a controller, in particular a path and / or force-guided control in which the coordinates and movements can be entered to compact the preform.
  • a die mold with which a preform can be pressed from sintered material, which is subsequently surface-compacted to a final shape.
  • This press tool shape is calculated iteratively.
  • a rolling test stand which offers the possibility of being able to carry out test rolling for a wide variety of surface densifications.
  • the rolling test bench can also have an automated measurement of surface-compacted workpieces which have a toothing.
  • f H ⁇ are the deviation with respect to the toothing
  • F ⁇ is the total deviation
  • f f ⁇ is the profile shape deviation of the flanks.
  • the specified values correspond to the DIN classes with respect to the deviation.
  • an iteration takes into account parameters which relate to a material behavior in a surface compression of the tooth form.
  • An embodiment provides that an iteration for determining a preform of input data emanates, which are taken from a specification of the final shape.
  • Preferably, at least one rolling tool is used, which has the same quality as the final shape created later.
  • the iterative determination and thereby extremely Precise machining during surface compaction allows the quality of the tool to be transferred to the preform.
  • the extremely accurate surface compaction makes it possible for the toothing to have this quality of the final shape after the surface compacting without any further material-removing post-processing step.
  • a workpiece with the gearing is made to have a core density of at least 7.4 g / cm 3 with a surface density that is at most in a region of a tooth flank, with the maximum surface density extending at least 0.02 ⁇ m in depth in the region ,
  • a method for producing a toothing of compacted sintered material wherein a pre-compacted tooth preform is compacted to its final shape at least in one area by means of iteratively determined data, and a roughness in the area opposite the preform is improved by at least 400%, with a surface hardness of at least 130 HB being set.
  • a core density of the final shape is set which has at least a density of 7.3 g / cm 3 and imprinted with a surface hardness having a convex course from the surface toward a center of the final shape.
  • the toothing of precompressed material has a roughness in a first surface-compacted area that is at least 400% smaller than a roughness in a second area that is less or not surface-compacted.
  • the roughness R z is, for example, less than 1 ⁇ m in the first region.
  • a further embodiment provides that a surface hardness of at least 700 HV [0.3] is present at the surface of the final shape, while at a depth of 0.4 mm from the surface at least a hardness of 500 HV [0.3] is present .
  • Another embodiment has a surface hardness of at least 700 HV [0.3] on the surface of a tooth flank and in a tooth root, wherein a hardness of at least 500 HV [0.3] at a depth of 0.6 mm from the surface in the Tooth base and a hardness of at least 500 HV [0.3] is present at a depth of 0.8 mm from the surface on the tooth flank.
  • the production of surface compaction makes it possible to set exact compaction as well as hardening according to desired specifications.
  • a calculation method for designing a preform of a toothing made of sintered material is proposed, wherein data enter into the calculation method, which consists of a predetermined final form of Gearing are determined, depending on at least one condition of use of the final shape one or more load parameters of the gearing are determined, a local allowance of the preform is calculated, which correlates with an expected densification of the preform at the surface, wherein a load of the sintered material below the surface in the calculation is received.
  • the calculation is additionally based on penetration of the tool into the workpiece to be produced in the calculation, wherein in particular the behavior of the sintered material during penetration and after penetration can be taken into account.
  • the calculation method provides that an elastic deformation of the sintering material to be compacted is taken into account.
  • the calculation method can provide that an elastic-plastic deformation of the sintering material to be compacted at the surface is taken into account.
  • a depth of a maximum load below the surface for example, when using the workpiece as a force-transmitting gear in the calculation method.
  • the calculation method may further include shrinking the sintered material during sintering in the calculation. Also empirically determined data can also be included in the calculation.
  • a calculation method for designing a tool for surface compacting a preform of a toothing made of, in particular, compacted sintered material to produce a predetermined tooth geometry is proposed predetermined tooth geometry to be produced for calculating machine tool kinematics taking into account associated machine parts of a workpiece, from which the tool to be produced is formed, and at least one tool former whose coupled system coordinates and their movement to one another, iteratively included.
  • contact conditions between the workpiece to be produced and the tool former between a tip and a foot of the toothing enter into the calculation method.
  • a maximum stress on the surface is also included in the calculation in the region of one foot of the toothing.
  • a maximum stress below the surface is included in the calculation.
  • a press mold with a press geometry for producing a preform of a toothing made of sintered material is proposed, wherein the press geometry adapted to a surface compression of the toothing course with at least has a survey that generates a recess at least in the region of the toothing of the preform, which can be filled with sintered material during surface compaction.
  • the survey on a front side of the preform causes a depression in the region of a head of a tooth of the toothing.
  • the height of the elevation or depth of the depression as well as other dimensions thereof can be determined.
  • a further embodiment provides, instead of a one-sided survey, that a bilateral elevation is provided in order to effect a depression on both end faces of the tooth.
  • the bump is arranged according to a further development in a region of the geometry which causes a depression on a tooth head of the preform, wherein the bump has a dimension such that the shaped well at least partially grows the tooth head due to the processing of the preform into the final shape by the surface compacting at least diminished.
  • a preform with at least one depression on an end face of a toothing to compensate for a material Aufsches in a surface compression of a tread of the toothing calculate and in particular finished.
  • a preform with at least one depression on a tooth head of a toothing for at least reducing a growth of the tooth head in the amount in a surface compaction at least calculate the flanks of the teeth and in particular finished.
  • the calculation method for determining a geometry of a preform or a press mold preferably provides that the geometry is determined based on data of a final shape of the preform and at least a calculation or elevation is calculated, which at least partially compensates for a material displacement during surface compacting.
  • a method for surface densification of a gear wherein a number of repetitive compacting motion of a mold for surface compacting a surface on the preform is calculated iteratively. Preferably, rollover is iteratively calculated until a predetermined surface density is reached.
  • an advance of the molding tool is calculated iteratively.
  • the preform is overrolled less than 20 times to achieve the predetermined geometry of a final shape of the surface compacting. Rolling over is preferably less than 10 times. In particular, overrolling of the preform is performed less than 6 times until a given geometry of a final shape of the surface compacting is achieved.
  • a method is proposed in which a reversing rolling on a toothing made of sintered material is carried out to densify the preform to the final shape of a surface compacting.
  • a short unloading of the preform is carried out by the mold before a reversal of direction. It has been found that by reversing, that is, by reversing the movement, a uniform compaction can be achieved.
  • manufacturing problems were further minimized by reducing the tool's pressure on the workpiece before the motion reversal began. The tool can remain in contact with the workpiece. It can also be detached from the surface for a short time.
  • a shaft with at least a first and a second toothing wherein the first toothing of sintered material is rolled and surface-compressed.
  • first toothing of sintered material is rolled and surface-compressed.
  • the shaft has a second toothing, which is produced by a different method than the first toothing.
  • the second toothing forms according to a further embodiment with the first toothing a workpiece.
  • both teeth may have been produced together in a press machine.
  • the first and second teeth have been calculated iteratively and prepared accordingly.
  • the production can take place successively, but also simultaneously according to another embodiment. In particular, this also applies to further processing steps such as a surface compaction.
  • the second toothing has a hardened surface without surface compaction.
  • the density inherent in sintering or the inherent strength of the material used is sufficient. This applies, for example, for pump applications.
  • At least the first toothing has at least one tooth each different edge slopes at the same height of the tooth. This is advantageous in applications in which a Schomosrlchtung and in particular only one direction of rotation of the shaft is specified.
  • the different edge slopes can thus be designed wear and noise-minimized.
  • the second toothing is forged. It can additionally be surface-compacted. For example, this toothing can absorb a greater force transmission than the first toothing.
  • the second toothing is made of a different material than the first toothing.
  • the second toothing is made of steel.
  • the second toothing can also consist of a different sintered material than the first toothing.
  • the shaft may also be made of sintered material. It may, for example, have the same material as the first toothing.
  • the shaft can be formed at least together with the first toothing, ie be pressed from powder material, preferably in a common mold.
  • An exemplary method for producing the shaft described above may also provide that at least the first gearing receives a surface compaction and a bore for receiving the shaft is surface-compacted, hardened and then honed before the shaft and the first gearing are joined together. For this purpose, preferably, starting from an end shape of the shaft with the first toothing, an iterative calculation of a preform of the first toothing takes place.
  • a preform for producing a toothing made of sintered material is used, wherein the preform has a negative allowance.
  • the negative allowance is arranged at least on an edge of a tooth of the toothing.
  • the negative allowance can run asymmetrically along the flank.
  • a further development provides that on each flank of a tooth, a negative measure is proceed.
  • a tooth at the same height has a first negative allowance on a first flank and a second negative allowance on a second flank, wherein the first flank and the second flank extend asymmetrically relative to one another.
  • the negative allowance is located between a head portion of the tooth and a measure on a flank of the tooth. Additionally or alternatively, the negative allowance can be arranged in a corner region of the tooth root. Furthermore, there is the possibility that a flank slope of the flanks of a tooth are different.
  • a development provides a method for producing a toothing of a sintered material, wherein a preform is assigned at least one determined by iterative calculation negative allowance, the case of a surface compression of the toothing is at least partially filled by displacement of the sintered material. Preferably, an oversize material adjacent to the negative allowance is displaced into the negative allowance.
  • the preform may be surface-compacted into the desired final shape, optionally with curing and / or surface finishing. This can be done before or after surface compacting. As a fine machining honing as well as a grinding is considered.
  • the design of the negative amount takes place via an iterative calculation, in which a simulation of the surface compaction on the preform determines whether the adjacent allowance of its shape is designed so that the negative allowance can be smoothed towards the desired final contour.
  • a machine for calculating and / or performing a surface compaction of a toothing is provided, wherein a calculated kinematics is einar, by means of the surface densification a negative allowance on a flank of the toothing can be smoothed to a desired final contour.
  • a method for producing a surface compaction on a toothing is proposed, wherein at least two preforms simultaneously receive surface compaction in a device.
  • the preforms are arranged on parallel shafts and at the same time engage with at least one tool for surface compaction.
  • At least two preforms are arranged on a common shaft and jointly brought into engagement with at least one tool for surface compaction.
  • a device for producing a surface compaction on a tooth system wherein at least two preforms for surface compaction in the device are durable and can be processed at the same time.
  • a movement of at least one shaft is provided, in which both preforms come into engagement with a tool for surface compaction.
  • at least three shafts for at least two preforms and at least one tool are arranged parallel to one another and a Form triangle, at least one of the waves is zubewegbar on the two other waves.
  • at least two preforms can be attached to a common shaft, wherein the tool has a greater length than an added length of at least both preforms.
  • the preforms can lie with their end faces together.
  • a distance is arranged between the preforms, the tool protruding along the shaft over both outer end faces of the preforms.
  • a component with a surface-compressed toothing made of sintered material is proposed, wherein the component, viewed over a cross-section, has a gradient with respect to the sintering materials used.
  • the component has a gradient that has a jump function.
  • the sintered materials are provided with a transition boundary at least in this area. According to one embodiment, this transition boundary is present along the entire surface between the first and second sintered material. Another embodiment provides that there is no fixed boundary in a region but a gradual transition. In particular, it can be provided that the component has different sintered materials which extend into one another without exhibiting a pronounced mixing zone with increasing or decreasing gradient.
  • a first development of the component includes that the sintered material of the toothing has a lower core density than the sintered material of a region of the component adjoining the toothing.
  • a second development of the component provides that the sintered material of the toothing has a higher core density than the sintered material of a region of the component adjoining the toothing.
  • a further embodiment has a component which has a first toothing with a first sintered material and has a second toothing with a second sintered material.
  • a toothing has different flank angles on a tooth at the same height.
  • a first sintered material can be arranged in an outer region of the component and form the toothing, and a second sintered material is arranged in an inner region of the component and forms a bore.
  • a method for producing a surface-compressed toothing on a component wherein a first sintered material is introduced into a mold before a second sintered material is added, followed by pressing and sintering and densified by means of a surface compression of the toothing only one of the two sintered materials, while the other sinter material undergoes no change.
  • a further embodiment provides that a second surface compaction is carried out, which relates only to the not yet surface-compressed sintered material. It is preferably provided that the first sintered material forms at least one surface of the toothed edges and the second material forms a relining of the toothing.
  • Another proposed method for producing a surface-compressed toothing on a component is to admit a first sintered material in a mold before a second sintered material is added, then perform a pressing and sintering and compacting the first and the second sintered material by means of a surface compression of the toothing ,
  • a movement sequence for surface compaction is determined iteratively taking into account a material behavior of at least one of the two sintered materials.
  • a further development for both methods provides that a relative rotation acts between the mold, in particular a press mold, and a sintered material to be filled, so that the sintered material accumulates in an outer region of the mold as a function of a speed of the relative rotation.
  • first and at least the second sintered material are added to the mold overlapping at least over a period of time.
  • the manufacturing process also provides grinding or honing of the compacted tooth flanks and / or tooth roots in addition to the surface compacting step of the toothing.
  • the forging achieves a density of at least 7.6 g / cm 3 as the core density.
  • the surface compacting can therefore cause a full compression and / or a precision of the shape of the toothing.
  • an oversize for this step in a range of 4 ⁇ m to 8 ⁇ m material is above the final dimension for a material-removing machining step after surface compacting.
  • honing is preferably 30 .mu.m to 50 .mu.m and grinding is 50 .mu.m to 0.3 mm, preferably 0.1 mm to 0.2 mm Surface compacting provided.
  • the iterative calculation makes it possible to determine the areas and dimensions beforehand and to be able to implement them later in the procedure.
  • sprocket or ring gear is preferably also provided a surface compaction, followed by curing and then preferably honing.
  • the bore may also have an oversize between 30 ⁇ m and 50 ⁇ m after surface compacting.
  • lubrication occurs during surface compacting.
  • emulsions can be lubricated in particular with oils. This is preferred for hot rolling, for example at temperatures above 220 ° C.
  • Fig. 1 shows an exemplary Wälzan eleven in a schematic view.
  • a first rolling tool 101 with a first toothing 102 is rotatably mounted about a first axis 103 in a rotatlon direction 104.
  • the first toothing 102 is engaged with a second toothing 105 of a preform 106.
  • the preform 106 is rotatably mounted about a second axis 107. Accordingly, a second rotational direction 108 results.
  • the second toothing 105 is engaged with a third toothing 109 of a second rolling tool 110.
  • This second rolling tool 110 is rotatably mounted about a third axis 111 in a third rotational direction 112.
  • the first axis 103 or the second axis 107 may be fixed axes while the two other axes can execute a feed movement.
  • the third axis 111 is displaceable in a displacement direction 113 along a connecting line 114 of the first 103, the second 107 and the third axis 111.
  • a doctorwalzvorgang be made.
  • tooth flanks are only slightly compacted and, in particular, the tooth roots are not compacted. This results in a surface compaction in a desired area.
  • the tooth base can also be surface-compacted only or additionally. For example, during a rolling process, a progressive displacement in the direction of the displacement direction 113 takes place.
  • a region of the tooth roots of the preform 106 is also compacted.
  • an adjusting device is preferably provided with a gear. In particular, very high pressures can be applied.
  • Fig. 2 shows a first tooth 201 of an associated toothed element, not shown.
  • This toothed element is a toothed wheel.
  • a geometry of the toothed element or of the first tooth 201 is characterized by a first root circle 202, a first root circle 203, a first rolling crown 204 and a first head circle 205.
  • the first tooth 201 On a first flank 206, the first tooth 201 has a first flow path 207 before a rolling process. After a completed rolling operation results in a first End configuredverlauf 208, whereby a first compacted edge layer 209 results accordingly. Schematically, this is limited by a first compression boundary line 210. This line limits the area of the first tooth 201 within which full density is achieved. The full density is preferably based on a density of a comparable powder-forged tooth.
  • Fig. 3 shows a second tooth 301 of a toothed element, not shown.
  • This toothed element is also a gear wheel.
  • Second tooth 301 and gear are characterized by a second tip circle 302, a second pitch circle 303, a second root circuit 304 and a second root circle 305.
  • a second oversize course 308 and a third oversize course 309 are provided.
  • a second final dimension 310 results on the second flank 306 and a third final dimension 311 on the third flank 307.
  • a second compression limit line 312 and a third compression limit line result 313.
  • the second oversize course 308 and the third oversize course 309 are configured differently.
  • the different action of forces on the tooth flanks 306, 307 during a rolling process is illustrated by the illustrated sliding speed directions.
  • a first 314 and a second sliding speed direction 315 result. These are directed from the second pitch circle 303 in the direction of the second tip circle 302 and in the direction of the second root circle 305, respectively.
  • On the third flank 307 results in a third sliding speed direction 316 and a fourth sliding speed direction 317, which are directed against each other.
  • Fig. 4 shows a third tooth 401 of a toothed element, not shown.
  • This toothed element is also a gear wheel.
  • Gear and third tooth 401 are in turn characterized by a third tip circle 402, a Kopfnutz Vietnamese 403, a third pitch circle 404, a third penalnutz Vietnamese 405 and by a third vis Vietnamese 406.
  • third tooth 401 is a toothing with a tip retraction, preferably in the form of a head rounding.
  • a tooth profile is withdrawn in a tooth head region 401.1 between the third head circle 402 and the head cycle 403. As a result, the tooth does not engage in involute counter-toothing in this area.
  • an active tooth area lies only in the area between the head use circle 403 and the foot circle 405 or between the head circle 403 and the third foot circle 406.
  • a fourth ramp 407 results after a rolling process in a fourth compression boundary line 408 Flank 409 achieved a fourth End configuredverlauf 410.
  • Fig. 5 shows a Aufbornverlauf between two adjacent teeth of a toothed element, not shown.
  • This toothed element is again a toothed wheel.
  • the gear and the teeth are characterized by a fourth root circle 502, a fourth nose shank 503 of the preform, a fifth helical gear 504 of the preform after a grinding operation, a fourth head circle 505 after a milling operation, and a fifth head circle 506 after a finishing operation.
  • After a rolling operation results in a fifth Endemblverlauf 507.
  • a lateral dimension in millimeters is plotted.
  • On the ordinate axis, the correspondingly perpendicular lateral dimension is also plotted in millimeters.
  • the teeth run completely in the plane of the drawing.
  • Fig. 6 shows a compilation of further measurement progressions.
  • the nominal ground length along a flank line of a toothed element is shown.
  • this curved line relates to a progression from a tooth tip of a first tooth to a tooth tip of an adjacent tooth.
  • the absolute arc length of the corresponding flank line in millimeters is correspondingly shown on the upper abscissa axis.
  • the left ordinate axis indicates an allowance in millimeters.
  • the right ordinate axis describes the corresponding radius of the associated toothing. Shown are a sixth Aufbornverlauf 601, a seventh Aufbornverlauf 602 and an eighth constitutivverlauf 603.
  • the sixth oversize profile 601 and the eighth oversize profile 603 are in this case implemented symmetrically to a basic tooth symmetry line 605.
  • the seventh oversize profile 607 is designed asymmetrically. In the vicinity of the tooth symmetry baseline 605, that is to say in the tooth base region, the oversizes each have a local minimum. This promotes a reduction of a risk of stress cracking.
  • Fig. 7 shows a further oversize course. Shown is a ninth oversize progression, which runs asymmetrically from a left tooth head 702 to a right tooth head 703. As already in Fig. 6 An oversize in the area of a tooth root 704 is also shown here to be smaller than in the area of the fifth 705 and the sixth flank 706. This serves, in particular, to avoid stress cracks.
  • Fig. 8 shows a first process scheme.
  • a geometry of a rolling tool is generated with a first geometry generation module 802.
  • a geometry of a preform is generated in a second geometry generation module 803.
  • a rolling process is simulated. In this case, both a kinematics of the rolling process and the compression process, which is caused during rolling, simulated.
  • a redistribution of material such as in Fig. 3 outlined, considered.
  • the simulation of a plastic deformation takes place here for example by means of a finite element method. This can be coupled with a CAD program.
  • a second simulation module 805 for simulating a stress can be considered. Both the target 801 and the preform geometry are included in this module.
  • that allows Second simulation module 805 further includes a correction of the detected geometry of the preform.
  • the first geometry generation module 802, the second geometry generation module 803, the first simulation module 804, and optionally the second simulation module 805 may be repeatedly executed in an optimization loop.
  • Fig. 9 shows a second process scheme.
  • a ninth oversize profile 902 of a tooth profile 903 is generated.
  • a second tooth profile 905 of a third rolling tool 906 is generated.
  • a rolling process is simulated.
  • the rolling process of the first tooth profile 903 on the second tooth profile of the rolling tool 905 and the resulting compression is simulated.
  • the first, second and third steps 901, 904, 907 are optionally repeated in a variation 908.
  • Fig. 10 shows an oversize course of a toothed element of a rolling tool. Shown is a tenth Aufbornverlauf 1001 of a fifth tooth 1002 of a rolling tool, not shown. At a seventh flank 1003 and an eighth flank 1004 of the fifth tooth 1002, a different allowance is provided. At the seventh flank 1003, a material addition is provided, which is indicated by a first arrow 1005. In contrast, a tooth return is provided on the eighth edge 1004, which is indicated by the second arrow 1008.
  • the allowance in this example is based on a regular profile of involute toothing.
  • Fig. 11 shows a schematic view of a calculated depression on an end face of a toothing.
  • the depression serves to at least minimize, if not even compensate, growth of the sintering material displacement achieved by the surface compaction and concomitant growth of the tooth in height and / or width.
  • the shape of the depression depends on the allowance and on the dimensions of the tooth. The shape can be optimized iteratively using the calculation method. A simulation allows an estimation of the actual behavior of the preform later on.
  • FIG. 12 Figure 11 is a schematic view of calculated extreme cases of surface compaction tools that are calculable.
  • the starting point of the calculation is the left-hand end geometry of the toothing.
  • Fig. 13 a schematic view of an approach in the iterative calculation and links in a simulation.
  • the machine kinematics can be modeled. This is assumed, for example, by the associated machine axes.
  • an optimization of the tool to be designed can then be carried out by means of the available degrees of freedom. This will be on again Fig. 12 directed.
  • the examples presented there have corresponding disadvantages, for example too weak foot region in the middle representation or too pointed head design in the right representation.
  • an iteration can then be carried out in the material to a contour of the tool which is suitable for the respective requirement profile.
  • the determined final geometry with the calculated measurements is taken as a starting point.
  • Fig. 14 shows a view of density gradients as a function of different initial densities of the preforms used. If the density of the preform is changed outwardly in its core as well as in the course, influences on the surface compaction process result. This goes from the right picture of the Fig. 14 out. By changing the respective preform, the density profile after a surface compression can also be strongly influenced. Therefore, the output core density as well as the shape of the preform are important parameters in the iteration and computation.
  • Fig. 15 gives an exemplary overview of the detected errors that occur at different surface densification steps and characterize the material behavior.
  • the error is specified in error classes according to DIN 3972 or DIN 3970.
  • An important point in determining a suitable surface compaction by rolling is the profile change of the rolling tool.
  • cm 3 of a preform having a core density of 7.3 g / which was in engagement with an unmodified set of rolling tools and has been surface compressed.
  • the geometry of the gear changes. The goal is to achieve the desired final contour, as it is prescribed. From the pictures of Fig.
  • a new tool can then be determined, again perform the tests and iteratively determine an optimized geometry for the tool in this way.
  • the calculation makes it possible to determine a final contour for the tool with, for example, two or even one iteration.
  • Fig. 16 shows a hardness curve in HV on a flank of a toothing applied over the distance from the surface on the x-axis in [mm].
  • the profile profile of the hardness can be influenced by suitable dimensioning as well as by feed movement.
  • the course may be at least partially convex or concave.
  • the preform designated AVA7-1 has a larger oversize than the preform designated AVA4-2. Both have an opposite course of hardness: while in the first part until reaching 550 HVAVA7-1 has a more convex shape, AVA4-2 has a more concave course. After falling below 550HV this changes.
  • Fig. 17 a hardness curve in HV in a foot region of a toothing at different heatverdichtungsuzeen. Due to the smaller oversize there compared to the flank allowance and due to the geometry results in a different hardness profile. The hardness drops steeply at first, but then almost goes over into a straight course with only a slight inclination.
  • Fig. 18 shows a schematic view of various calculated Aufiqueverierin for different densities based on a final tooth thickness.
  • the diameter is plotted on the y-axis.
  • the oversize is indicated on the x-axis.
  • D_a or d_a indicates the head circle diameter or the tip circle diameter
  • 0 is a specification of an amount, for example, by a value on the pitch circle
  • d_b is the base circle diameter.
  • A indicates the range of preferred values for the pitch circle area.
  • B indicates a critical area, since material failure during rolling can already occur there.
  • Fig. 19 shows a schematic representation of parameters that can be included in the iterative calculation.
  • these locations may be the maximum load.
  • a comparison voltage curve is preferably used in which the following applies: A maximum voltage occurs below the surface, in particular in the region of a negative slip, therefore preferably below the specified pitch circle diameter d_w1.
  • the right photo indicates a tooth fracture due to excessive bending load. It follows for the calculation model that a location of the maximum Zahnfußbe pipeung is determined and taken into account. This can be determined, for example, via the 30 ° tangent according to DIN or via the Lewis parabola according to AGMA.
  • For the comparison voltage it is preferably assumed that a maximum stress occurs on the surface.
  • Fig. 20 shows a schematic view of another way, such as simultaneously at least two preforms can be compacted.
  • a movement of the preforms in the direction of the tool can take place.
  • the invention can be used, for example, in camshaft sprockets, in planetary gears, in sun gears, in drive gears, in differential gears, in gear wheels, in clutch gears, in pump gears, in spur gears, in helical gears, in electric motors, in internal combustion engines, in variable speed drives, in external gears. or internal gears, for straight or helical or external helical gear units, for bevel gear units with straight, helical or curved teeth, helical gear units or worm gear units, as well as for helical and helical hub connections.
  • a gear made of sintered metal The other may be made of plastic or another material, for example.
  • At least one of the two gear wheels has a coating which in particular has a noise minimizing effect.
  • a Kegeischraubradcru can be created to thereby form a Hypoldgetriebe.
  • the workpieces me gearing in automotive technology, in engine technology, in transmission technology, in adjusting devices, in power transmitting devices, in toys, in precision mechanical devices, household appliances, especially mobile home appliances, and others are used.

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  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Gears, Cams (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
EP06761986A 2005-06-10 2006-06-08 Verfahren zum verdichten einer verzahnung mit unterschiedlichen verfahren Not-in-force EP1888278B9 (de)

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DE102005027054A DE102005027054A1 (de) 2005-06-10 2005-06-10 Werkstück mit unterschiedlicher Beschaffenheit
PCT/EP2006/005476 WO2006131356A2 (de) 2005-06-10 2006-06-08 Werkstück mit unterschiedlicher beschaffenheit

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US (2) US20080201951A1 (zh)
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Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT505118B1 (de) 2007-03-28 2013-03-15 Miba Sinter Austria Gmbh Verfahren zur bearbeitung einer verzahnung an einem sinterteil
DE102010039491A1 (de) 2010-08-18 2012-02-23 Deckel Maho Pfronten Gmbh Verfahren und Vorrichtung zum Erzeugen von Steuerdaten zur Ausbildung einer Zahnflanke durch fräsende Bearbeitung eines Werkstücks an einer Werkzeugmaschine
DE102010039490A1 (de) * 2010-08-18 2012-02-23 Deckel Maho Pfronten Gmbh Verfahren und Vorrichtung zum Erzeugen von Steuerdaten zur Ausbildung eines Zahns einer Stirnradverzahnung durch fräsende Bearbeitung eines Werkstücks an einer Werkzeugmaschine
DE102012214870A1 (de) * 2012-08-22 2014-02-27 Schaeffler Technologies AG & Co. KG Antriebsrad und Verfahren zu seiner Herstellung
CN104438993B (zh) * 2014-10-22 2016-04-06 山东大学 一种改善齿形突耳缺陷的齿轮滚轧成形方法
CN105234496A (zh) * 2015-10-27 2016-01-13 江苏科技大学 一种共轭齿轮或转子的加工方法
RU2710827C1 (ru) * 2015-12-31 2020-01-14 Кхван Хи ЛИ Способ изготовления зубчатых колес и зубчатое колесо, изготовленное с его помощью
CN108720097B (zh) * 2016-02-01 2020-04-07 叶正瑜 吸水层完整的简易乳垫的制造方法
US20170266726A1 (en) * 2016-03-17 2017-09-21 GM Global Technology Operations LLC Method and system for surface densification
DE102019126669A1 (de) * 2019-10-02 2021-04-08 Profilator Gmbh & Co. Kg Verfahren und Vorrichtung zum Glätten der Zahnflanken der Zähne verzahnter Werkstücke
US11707786B2 (en) 2020-04-17 2023-07-25 PMG Indiana LLC Apparatus and method for internal surface densification of powder metal articles
US11707792B2 (en) 2020-09-28 2023-07-25 GM Global Technology Operations LLC Scattered topography rolling of powered metal gears

Family Cites Families (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461734A (en) * 1945-06-19 1949-02-15 R K Leblond Machine Tool Co Flame hardening apparatus
US2542912A (en) * 1945-12-08 1951-02-20 Ford Motor Co Process and apparatus for coining sintered articles
US2561579A (en) * 1947-10-02 1951-07-24 Gen Motors Corp Impregnated ferrous gear
US3037400A (en) * 1959-01-14 1962-06-05 Edward V Sundt Differential gear reducer
US3043164A (en) * 1959-05-11 1962-07-10 Edward V Sundt Differential gear reducer
US3851512A (en) * 1973-03-08 1974-12-03 G Zhuravlev Method of and device for gear teeth hardening
US4059879A (en) 1975-11-17 1977-11-29 Textron Inc. Method for the controlled mechanical working of sintered porous powder metal shapes to effect surface and subsurface densification
DE3325037C1 (de) 1983-07-11 1984-07-12 Sintermetallwerk Krebsöge GmbH, 5608 Radevormwald Mit wenigstens einer Verzahnung versehener Sintermetallkoerper
US4708912A (en) * 1984-07-18 1987-11-24 Sintermetallwerk Krebsoege Gmgh Sintered metal body with at least one toothing
US4666665A (en) * 1986-01-30 1987-05-19 Federal-Mogul Corporation Hot-forging small inner diameter powdered metal parts
GB2197605B (en) * 1986-12-30 1990-06-20 Honda Motor Co Ltd Forming cup-shaped products having internal gears
US5711187A (en) 1990-10-08 1998-01-27 Formflo Ltd. Gear wheels rolled from powder metal blanks and method of manufacture
GB2250227B (en) 1990-10-08 1994-06-08 Formflo Ltd Gear wheels rolled from powder metal blanks
JPH05117703A (ja) * 1991-09-05 1993-05-14 Kawasaki Steel Corp 粉末冶金用鉄基粉末組成物およびその製造方法ならびに鉄系焼結材料の製造方法
US5903815A (en) 1992-02-12 1999-05-11 Icm/Krebsoge Composite powdered metal component
DE4211319C2 (de) * 1992-04-04 1995-06-08 Plansee Metallwerk Verfahren zur Herstellung von Sintereisen-Formteilen mit porenfreier Zone
WO1994005822A1 (en) * 1992-09-09 1994-03-17 Stackpole Limited Powder metal alloy process
DE69314438T2 (de) 1992-11-30 1998-05-14 Sumitomo Electric Industries Niedrig legierter Sinterstahl und Verfahren zu dessen Herstellung
JPH07505679A (ja) * 1992-12-21 1995-06-22 スタックポール リミテッド ベアリングの製造方法
US5286323A (en) * 1993-02-23 1994-02-15 Corning Incorporated Dome shaped extrusion dies
US5308556A (en) * 1993-02-23 1994-05-03 Corning Incorporated Method of making extrusion dies from powders
US5659955A (en) * 1994-01-21 1997-08-26 Plamper; Gerhard Method of making powder metal helical gears
US5613180A (en) * 1994-09-30 1997-03-18 Keystone Investment Corporation High density ferrous power metal alloy
US5754937A (en) 1996-05-15 1998-05-19 Stackpole Limited Hi-density forming process
US5729822A (en) 1996-05-24 1998-03-17 Stackpole Limited Gears
CA2268649C (en) * 1996-10-15 2002-10-01 Zenith Sintered Products, Inc. Surface densification of machine components made by powder metallurgy
AT406836B (de) * 1997-10-30 2000-09-25 Miba Sintermetall Ag Verfahren und vorrichtung zum herstellen eines zahnrades
US6110419A (en) * 1997-12-02 2000-08-29 Stackpole Limited Point contact densification
US5972132A (en) * 1998-02-11 1999-10-26 Zenith Sintered Products, Inc. Progressive densification of powder metallurgy circular surfaces
EP1018387B1 (en) * 1998-04-01 2004-08-25 Mitsubishi Heavy Industries, Ltd. Gear shaping method and device and spiral bevel gear cutter
US6044555A (en) * 1998-05-04 2000-04-04 Keystone Powered Metal Company Method for producing fully dense powdered metal helical gear
US6151941A (en) * 1999-01-25 2000-11-28 Federal-Mogul World Wide, Inc. Apparatus and method for roll forming gears
US6168754B1 (en) * 1999-02-17 2001-01-02 Federal-Mogul World Wide, Inc. Method and apparatus for densifying powder metal preforms
US6017489A (en) * 1999-02-17 2000-01-25 Federal-Mogul World Wide, Inc. Method of densifying powder metal preforms
US6170156B1 (en) * 1999-03-24 2001-01-09 General Motors Corporation Gear tooth smoothing and shaping process
EP1045410B1 (en) * 1999-04-16 2007-01-24 Matsushita Electric Industrial Co., Ltd. Anodic electrode for electrolytic capacitor and process of producing the same
US6779270B2 (en) * 1999-07-13 2004-08-24 The Penn States Research Foundation Full form roll finishing technique
GB2360825B (en) * 2000-03-30 2004-11-17 Formflo Ltd Gear wheels roll formed from powder metal blanks
US6514307B2 (en) * 2000-08-31 2003-02-04 Kawasaki Steel Corporation Iron-based sintered powder metal body, manufacturing method thereof and manufacturing method of iron-based sintered component with high strength and high density
AT409466B (de) * 2000-11-30 2002-08-26 Miba Sintermetall Ag Verfahren und vorrichtung zum herstellen eines zahnrades
US6630101B2 (en) * 2001-08-16 2003-10-07 Keystone Investment Corporation Method for producing powder metal gears
US6517772B1 (en) * 2001-09-26 2003-02-11 Federal-Mogul World Wide, Inc. Apparatus and method for forming powder metal gears
AT5886U1 (de) * 2002-03-27 2003-01-27 Plansee Ag Gesinterte schalt- oder schiebemuffe
US7574947B2 (en) * 2002-05-29 2009-08-18 Massachusetts Institute Of Technology Rotary fast tool servo system and methods
FR2840552B1 (fr) * 2002-06-06 2005-02-18 Escofier Tech Sa Formage a froid par roulage de pieces en materiau presse-fritte
GB2420791B (en) * 2002-09-18 2006-12-13 Smith International Method of manufacturing a cutting element from a partially densified substrate
US7160351B2 (en) * 2002-10-01 2007-01-09 Pmg Ohio Corp. Powder metal clutch races for one-way clutches and method of manufacture
JP2005344126A (ja) * 2002-10-04 2005-12-15 Hitachi Powdered Metals Co Ltd 焼結歯車
DE10247330B4 (de) * 2002-10-10 2013-02-28 PMG Füssen GmbH Pulvermetallurgisch hergestellte Schaltmuffe
JP4376503B2 (ja) * 2002-10-25 2009-12-02 ボルグワーナー・モールステック・ジャパン株式会社 サイレントチェーン用スプロケットおよびその製造方法
US6899846B2 (en) * 2003-01-14 2005-05-31 Sinterstahl Corp.-Powertrain Method of producing surface densified metal articles
JP2006523775A (ja) * 2003-03-18 2006-10-19 ザ ペン ステート リサーチ ファウンデーション オースフォーミングによって粉末金属製歯車を強靭にする方法および装置
JP4570066B2 (ja) * 2003-07-22 2010-10-27 日産自動車株式会社 サイレントチェーン用焼結スプロケットの製造方法
US7025928B2 (en) * 2003-07-24 2006-04-11 The Gates Corporation Method of flow forming a metal part
DE10342495B4 (de) * 2003-09-12 2017-02-02 Reishauer Ag Verfahren und Vorrichtung zum Einzentrieren von vorverzahnten Werkstücken auf Verzahnungsfeinbearbeitungsmaschinen
US7416696B2 (en) * 2003-10-03 2008-08-26 Keystone Investment Corporation Powder metal materials and parts and methods of making the same
US7025929B2 (en) * 2004-04-08 2006-04-11 Pmg Ohio Corp. Method and apparatus for densifying powder metal gears
US7393498B2 (en) * 2004-04-21 2008-07-01 Hoganas Ab Sintered metal parts and method for the manufacturing thereof

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CA2611669A1 (en) 2006-12-14
WO2006131356A2 (de) 2006-12-14
ES2379640T3 (es) 2012-04-30
US20080201951A1 (en) 2008-08-28
EP1888278B1 (de) 2012-01-18
WO2006131356A3 (de) 2009-02-05
US20120227530A1 (en) 2012-09-13
ATE541659T1 (de) 2012-02-15
CN101466489B (zh) 2014-06-18
EP1888278A2 (de) 2008-02-20
CN101466489A (zh) 2009-06-24

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