EP1263540B1 - Verfahren zur herstellung von dünnwandigen bauteilen aus stahl und danach hergestellte bauteile - Google Patents
Verfahren zur herstellung von dünnwandigen bauteilen aus stahl und danach hergestellte bauteile Download PDFInfo
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- EP1263540B1 EP1263540B1 EP01900129A EP01900129A EP1263540B1 EP 1263540 B1 EP1263540 B1 EP 1263540B1 EP 01900129 A EP01900129 A EP 01900129A EP 01900129 A EP01900129 A EP 01900129A EP 1263540 B1 EP1263540 B1 EP 1263540B1
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- hardened
- steel
- composite material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/008—Continuous casting of metals, i.e. casting in indefinite lengths of clad ingots, i.e. the molten metal being cast against a continuous strip forming part of the cast product
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
- Y10S428/924—Composite
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
- Y10S428/924—Composite
- Y10S428/925—Relative dimension specified
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
- Y10S428/924—Composite
- Y10S428/926—Thickness of individual layer specified
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/94—Pressure bonding, e.g. explosive
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12458—All metal or with adjacent metals having composition, density, or hardness gradient
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12472—Microscopic interfacial wave or roughness
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12958—Next to Fe-base component
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12958—Next to Fe-base component
- Y10T428/12965—Both containing 0.01-1.7% carbon [i.e., steel]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12986—Adjacent functionally defined components
Definitions
- the present invention relates to a method for producing thin-walled Steel components, the layers of which different steel alloys exist according to The preamble of claim 1.
- the invention further comprises thin-walled components made of steel with a core layer and edge layers.
- thermal treatment namely martensitic or bainitic.
- Made from hardening steel a component with a uniform, high hardness, which however has a low toughness.
- a cheaper combination wear-resistant surfaces with high toughness in the core zone achieved the use of case-hardened steels.
- Through a carburizing treatment in a thermochemical hardening process produces hardened, hard surface layers, while the core layer continues to maintain high toughness.
- use properties are a relatively complex manufacturing process across from.
- roll-clad is still a substitute for case hardening Steel known, two or more, differently alloyed strips or sheets, preferably from cold rolled strip.
- the core and outer layers are made of different alloys Steels intimately connected to one another in the roll gap on the surfaces.
- annealing results from the diffusion processes of the metallic composite.
- Such a roll cladding process is specified, for example, in DE 41 37 118 A1.
- this creates an abrupt, abrupt transition between the different layers of material.
- the hardship transition between paid and unrefined layers is therefore also correspondingly steep, so that due to the load-induced stress gradient produces relatively thick boundary layers Need to become.
- DE-A-198 15 007 and DE-A-198 50 213 describe methods and procedures manufactured thin metal tapes known, in which a core material an inexpensive material through a casting process with thin metal strips be cast in layers to form a composite material, the thin Metal strips for the production of corrosion-resistant and / or particularly smooth outer layers be used. A subsequent treatment is also in progress here on the influence of other properties of the composite material.
- the task for the present invention is a rational process for the production of thin-walled components made of steel with different Strength and / or hardness properties. Furthermore, a Component with layers of different strength and / or hardness properties be specified, which is particularly cheaper due to the reduced effort than can be produced so far.
- the method according to the invention for the production of thin-walled components Steel that has an inner core layer and outer peripheral layers sees here before that the core and outer layers of different steel alloys exist and in a casting process to a composite material with flat Alloy gradients are connected at the interfaces and the composite deformed to the dimensions of the thin-walled components and heat-treated and the heat treatment becomes a martensitic or bainitic Not all harden, but at least one of the layers leads.
- the method according to the invention is characterized by core and edge layers made of steel materials with different strength and / or hardness properties, namely in particular different martensitic hardenability properties, to combine with each other so that thin-walled components are available be made, which the respective advantages of case hardening and Combine roll cladding.
- the individual layers are preferably made of steel alloys with different martensitic hardenability properties, i.e. different grades formed on carbon, chromium and manganese, the subsequent influencing the strength and / or hardness properties due to martensitic or bainitic Heat treatment takes place, i.e. a heat treatment with the steps of heating-quenching-tempering.
- they consist of their strength and / or Hardness properties of layers of higher alloy, i.e. carbon-rich steel than that not in their strength and / or hardness properties influenceable layers.
- In the area of the flat alloy gradient becomes a correspondingly flat carbon gradient in this case realized.
- This transition zone between higher and lower carbon Layers extends with a wall thickness of the components of less than 4 mm over less than 20%, preferably less than 15% of the wall thickness.
- the range of the flat alloy or carbon gradient is wider than 0.1 mm, i.e. more than an order of magnitude wider than the known one Walzplattiermaschine.
- the strength and / or hardness properties can be influenced Layers the edge layers of the components, which are hard as a surface are and get a hardness curve, which is roughly the case hardening equals.
- the disadvantage of case hardening is that due to the long residence time A relatively coarse grain structure occurs in the marginal zones, which leads to an increased Micro-crack sensitivity is caused by the layer arrangement according to the invention however avoided.
- the Edge layers also have a wear-resistant fine grain structure with high toughness the edge zone, which leads to a particularly low sensitivity to microcracks.
- components with a wall thickness can be made using the method according to the invention less than 4 mm.
- the strength of the wall thickness and / or hardness properties of influenceable layers i.e. the martensitic hardened layers, a cross-sectional proportion of about 10% to 50%.
- the core layer of the components in their strength and / or hardness properties be influenced, for example hardened, while the outer layers Steel alloys which cannot be influenced in their strength and / or hardness properties or stainless steels.
- the layers which can be influenced in their strength and / or hardness properties Materials such as C 55, C 67 or other steels from EN, 100 Cr 6 or X 20 Cr13, X 35 CrMo 17 advantageously form the boundary layers, while the core layers cannot be influenced in their strength and / or hardness properties Materials such as DC 01 or C 10 exist.
- layers also form the core layers, for example one Spring steel core made of C 60, C 67 or C 75, while the outer layers made of easily deformable Steels such as C 10 or DC 01, or also made of rust-resistant Steels like X 5 CrNi 1810.
- the alloy gradient according to the invention between the surface and core layers can be produced in that for the production of the composite material for the Edge layers Boards made of martensitic hardenable steel parallel and spaced apart be arranged and the core layer between them with molten, low-carbon steel is cast.
- the Surface layers become, for example, cold or surface treated hot strip used with predetermined chemical analysis, especially high carbon content. Due to the molten core material cast in between, the has a lower carbon content, local melting occurs of the boards at the material interfaces, which is due to diffusion processes a flat alloy or carbon gradient, with a depth of about 0.1 - 0.3 mm. These properties are due to the invention Connection by means of a casting process close to the final dimensions.
- the boards are preferably at the casting wheels or the casting mold Pouring the molten core material cooled from the outside. This can even with thin blanks, the width of the alloy gradient can be controlled that it is in the range of 0.1 mm and thereby up to 10% of the total cross section is.
- the blanks as strip steel at the edge of the casting gap be fed to a continuously operating casting plant.
- the casting plant can be a continuous casting plant with a fixed continuous mold or for Carrying out a continuous casting and rolling process with the casting gap delimiting rotating rollers (casting wheels).
- the Tapes are bare, scale and oxide free due to the appropriate surface treatment as well as roughened if necessary.
- a protective glass bell is generated by supplying inert gases or inert gas mixtures.
- the aforementioned casting is preferably followed by a hot rolling process. Due to the prevailing temperatures of above 950 ° C due to the high surface pressure and deformation ensures that complete welding of the layers safely achieved in the manner desired according to the invention will, even if the metallic joining when the Melt with the belt surface should not have been sufficient. It forms then at the latest a flat material transition gradient between the layers which is in the 0.1 mm range.
- the surface of the rolling stock receives one Condition poor in rolling scars and scales without flaming or finishing operations.
- the composite material is then rolled by hot and / or cold rolling Rolling degree of regularly more than 30% rolled to a thickness of 1 to 5 mm.
- the final, preferably cold rolling true-to-shape design to the wall thickness of the components, which range up to 4.0 mm, with the surface having the smallest depths of defects and high freedom from pores has what the prerequisite for later use for highly stressed Components, for example machine components. If necessary, the final Shaping multiple cold rolling and intermediate annealing may be required.
- the is on Dimensionally rolled composite material preferably a recrystallization or soft annealing subjected to about 730 ° C. In this soft annealed condition is suitable the composite material is good for cold forming, for example of machine components.
- the composite molded material is used to influence its Strength and / or hardness properties subjected to a heat treatment at which results in a martensitic hardening of the hardenable layers.
- a heat treatment at which results in a martensitic hardening of the hardenable layers.
- partial heat treatment for example by means of laser or electron radiation, can have a locally limited influence on the strength and / or Hardness properties, that is, hardening take place.
- an influencing the strength and / or hardness properties take place in the short-term continuous process, preferably in a protective gas oven. This enables a particularly rational Production of functionally optimized strip material and components.
- a particularly advantageous application has one according to the aforementioned Process-manufactured, thin-walled steel component with a soft core layer and martensitic hardened surface layers, which consists of a cold-formed, hardened multi-layer composite material, which is carbon-rich, martensitic hardened surface layers and a relatively lower-carbon core layer The carbon gradient between the layers is flat.
- This component according to the invention is characterized in that it is The hardness curve and distribution of strength come close to a case-hardened steel component.
- martensitic curable layers can have material properties which cannot be achieved with other hardening processes are.
- the component also boundary layers which cannot be influenced in their strength and / or hardness properties, for example made of stainless steel alloys, and a tempered core layer have, for example made of spring steel.
- the wall thickness of the component according to the invention is preferably up to 4.0 mm.
- the carbon gradient in the transition area extends over approximately 10 up to 30% of the wall thickness, in any case over 0.1 mm.
- the materials for the outer and core layers are preferably one on the other matched that the hardness of the core layer at least 30% to 50% of the hardness corresponds to the boundary layers.
- the component can consist of two different materials, for example from a low-alloy core layer and high-alloy outer layers.
- the chemical composition of the outer layers can, however, if necessary also be different, so that a total of at least three layers with different Material properties are present. This allows one more achieve improved functional optimization of the components, such as corrosion protection or fusion weldability.
- asymmetrical components can be made in components manufactured according to the invention Realize spring travel or self-adjusting spring travel or forces.
- Fig. 1 shows a section through a cold-formed, martensitic surface layer hardened Component 1. This is preferably made of strip material with a total thickness of 5 formed, which is in the range of 0.3 to 4.0 mm.
- the component shown consists of steel layer material with several layers. These include in particular a core area B made of low carbon alloy and outer layers A made of carbon-rich, martensitic hardened steel.
- the Core layer B consists for example of Ck10, DC01, C 10, C 35 or C 53.
- Die outer edge layers consist, for example, of Ck67, C 55, C 67, or also 102 Cr6, x5 Cr Ni 1810 or the like.
- the boundary layers A can in turn also consist of steel alloys with different analyzes.
- the peculiarity of the component 1 shown is that the layers A, B, A even before cold forming to the final dimension 5 according to the invention Processes have been interconnected so that wide at the layer boundaries Transition zones G have been formed, which are indicated by hatching and in which a flat surface is formed by carbon diffusion between the layer materials Has formed a carbon gradient that is in the range of several 1/10 mm.
- the entire component 1 (FIG. 1) is, after which it becomes, for example, a machine component has been cold formed, subjected to a martensitic hardening process Service.
- the outer layers A are hardened, while the core B is a relative one maintains great toughness.
- the flat carbon gradient according to the invention G there is a flat voltage curve at the layer boundaries, so that there is no danger chipping of the outer layers A from the core layer B is like this for example in the case of the roll-clad strip according to the prior art is.
- the component 1 according to the invention as shown in FIG Core layer B which is hardened in particular martensitic or bainitic, and relative have not or less tempered outer layers, whereby it consists of a cold-formed, in its strength and / or hardness properties influenceable multilayer composite consists of a carbon-rich, in their strength and / or Core layer B which can be influenced by hardness properties and relatively low-carbon in relation thereto
- Has boundary layers A the zone of the carbon gradient G, such as explained above, runs flat between the layers A, B.
- a spring steel that can be influenced in its strength and / or hardness properties in the core and low corrosion for example stainless alloys in the Edge layers A conceivable. This allows, for example, an asymmetrical suspension travel or specify a self-adjusting spring force.
- Fig. 2 shows schematically a continuously operating two-roll casting and rolling system. This has two rotating, water-cooled copper rollers 2, which have a casting gap Limit from 1 - 5 mm wide. From above, the melt sump 3 is over Dip tube 4 charged with molten material B. Along the edges of the Casting nip is fed from strip material A from supply coils. With the one in the casting gap encapsulated core material B is there the connection between the as a steel hot band supplied material A and the molten material B instead. Due to the high surface pressure at temperatures above 950 ° C in hot rolling there is definitely an optimal metallic joining.
- the heat dissipation via the copper rollers 2 ensures that Steel warmer A through that the carbon gradient G is the steel warmer A does not penetrate too far. In any case, it remains sufficiently thick Boundary layer of the carbon-rich, martensitic hardenable boundary material A is present, around components in the subsequent heat treatment and hardening processes with the hardness curve shown or the strength distribution.
- steel layer materials can be with extremely different properties in terms of strength and / or hardness properties of the individual layers.
- the cold-formable composite can be processed particularly well and efficiently to final dimensions. in the Contrary to the known methods, neither occurs during the subsequent hardening to a disadvantageous delay in hardness, there is still the risk of flaking off Surface layers. This is because they have a fine, tough structure, which not to break the component even under high loads or short-term overload leads.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Heat Treatment Of Articles (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Continuous Casting (AREA)
- Heat Treatment Of Steel (AREA)
- Powder Metallurgy (AREA)
- Forging (AREA)
Description
- Fig. 1 -
- einen Querschnitt durch ein erfindungsgemäßes Bauteil;
- Fig. 2 -
- eine schematische Darstellung einer Gießanlage zur Herstellung von erfindungsgemäßem Bandmaterial.
Claims (29)
- Verfahren zur Herstellung von dünnwandigen Bauteilen aus Stahl, die eine innere Kernschicht und äußere Randschichten aufweisen, wobei die Kern- und Randschichten aus unterschiedlichen Stahllegierungen bestehen und in einem Gießverfahren zu einem Verbundwerkstoff mit flach verlaufendem Legierungsgradienten an den Grenzflächen verbunden werden und der Verbundwerkstoff auf das Maß der dünnwandigen Bauteile verformt und wärmebehandelt wird und wobei die Wärmebehandlung zu einem martensitischen oder bainitischen Härten nicht aller, jedoch mindestens einer der Schichten führt.
- Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß die gehärtete(n) Schicht(en) aus höher legiertem Stahl bestehen als die nicht in ihren Festigkeits- und/oder Härteeigenschaften veränderte(n) Schicht(en).
- Verfahren nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, daß die Kern- und/oder Randschichten gehärtete und korrosionsfreie Schichten umfassen.
- Verfahren nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß die gehärteten Schichten die Randschichten bilden.
- Verfahren nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß die gehärteten Schichten ein verschleißfestes Feinkorngefüge mit hoher Zähigkeit und geringer Mikrorißempfindlichkeit haben.
- Verfahren nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß die gehärteten Schichten die Kernschichten bilden.
- Verfahren nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß die Bauteile eine Wanddicke von weniger als 4 mm haben.
- Verfahren nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, daß die gehärteten Schichten einen Querschnittsanteil von 10 bis 50% der Wanddicke haben.
- Verfahren nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, daß der Bereich des Legierungsgradienten breiter ist als 0,1 mm.
- Verfahren nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, daß sich der Legierungsgradient auf etwa 10-25% der Wanddicke erstreckt.
- Verfahren nach einem der Ansprüche 1 bis 10, dadurch gekennzeichnet, daß zur Herstellung des Verbundwerkstoffes für die Randschichten Platinen aus martensitisch oder bainitisch härtbarem Stahl parallel mit Abstand zueinander angeordnet werden und die dazwischen befindliche Kernschicht mit schmelzflüssigem, kohlenstoffärmeren Stahl vergossen wird.
- Verfahren nach Anspruch 11, dadurch gekennzeichnet, daß die Platinen von außen gekühlt werden.
- Verfahren nach Anspruch 11 oder 12, dadurch gekennzeichnet, daß die Platinen als Bandstahl am Rand des Gießspaltes einer kontinuierlich arbeitenden Gießanlage zugeführt werden.
- Verfahren nach Anspruch 13, dadurch gekennzeichnet, daß die Stranggießanlage eine feste Durchlaufkokille hat.
- Verfahren nach Anspruch 13, dadurch gekennzeichnet, daß die Gießanlage rotierende, gekühlte Rollen hat, die den Gießspalt begrenzen.
- Verfahren nach Anspruch 1 bis 15, dadurch gekennzeichnet, daß das Verformen des Verbundwerkstoffs durch Warmwalzen erfolgt.
- Verfahren nach einem der Ansprüche 1 bis 15, dadurch gekennzeichnet, daß das Verformen des Verbundwerkstoffs durch Kaltwalzen erfolgt.
- Verfahren nach einem der Ansprüche 1 bis 17, dadurch gekennzeichnet, daß der auf das Maß der Bauteile verformte Verbundwerkstoff weichgeglüht und anschließend zu Bauteilen verformt wird.
- Verfahren nach einem der Ansprüche 1 bis 18, dadurch gekennzeichnet, daß das Härten durch eine Kurzzeitwärmebehandlung erfolgt.
- Verfahren nach einem der Ansprüche 1 bis 19, dadurch gekennzeichnet, daß der auf Endmaß geformte Verbundwerkstoff einer Wärmebehandlung unterzogen wird zur martensitischen oder bainitischen Härtung der gehärteten Schichten.
- Verfahren nach einem der Ansprüche 1 bis 20, dadurch gekennzeichnet, daß eine lokal begrenzte Härtung der gehärteten Schichten erfolgt.
- Verfahren nach einem der Ansprüche 1 bis 21, dadurch gekennzeichnet, daß die martensitische oder bainitische Härtung der Schichten im Durchlaufverfahren erfolgt.
- Dünnwandiges Bauteil aus Stahl, hergestellt nach dem Verfahren gemäß einem oder mehreren der Ansprüche 1 bis 22, dadurch gekennzeichnet, daß es aus einem kaltgeformten Mehrschicht-Verbundwerkstoff besteht, der gehärtete Randschichten und eine nicht gehärtete Kernschicht hat.
- Dünnwandiges Bauteil nach Anspruch 23, dadurch gekennzeichnet, daß die martensitisch oder bainitisch gehärteten Randschichten kohlenstoffreich sind und die Kernschicht relativ dazu kohlenstoffärmer ist, wobei der Kohlenstoffgradient zwischen den Schichten flach verläuft.
- Dünnwandiges Bauteil aus Stahl, hergestellt nach dem Verfahren gemäß einem oder mehreren der Ansprüche 1 bis 22, dadurch gekennzeichnet, daß es aus einem kaltgeformten Mehrschicht-Verbundwerkstoff besteht, der nicht gehärtete Randschichten und eine gehärtete Kernschicht hat.
- Bauteil nach einem der Ansprüche 23 bis 25, dadurch gekennzeichnet, daß die Wanddicke des Bauteils weniger als 4 mm beträgt.
- Bauteil nach Anspruch 23 bis 26, dadurch gekennzeichnet, daß sich der Kohlenstoffgradient über bis zu 10% bis 30% der Wandungsdicke des Bauteils erstreckt.
- Bauteil nach einem der Ansprüche 23 bis 27, dadurch gekennzeichnet, daß sich der Kohlenstoffgradient über mehr als 0,1 mm erstreckt.
- Bauteil nach einem der Ansprüche 23 bis 28, dadurch gekennzeichnet, daß es in der Randzone ein verschleißfestes Feinkorngefüge mit hoher Zähigkeit und geringer Mikrorißempfindlichkeit hat.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10011758 | 2000-03-13 | ||
| DE10011758A DE10011758C2 (de) | 2000-03-13 | 2000-03-13 | Verfahren zur Herstellung von dünnwandigen Bauteilen aus Stahl und danach hergestellte Bauteile |
| PCT/EP2001/000088 WO2001068293A1 (de) | 2000-03-13 | 2001-01-05 | Verfahren zur herstellung von dünnwandigen bauteilen aus stahl und danach hergestellte bauteile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1263540A1 EP1263540A1 (de) | 2002-12-11 |
| EP1263540B1 true EP1263540B1 (de) | 2004-06-30 |
Family
ID=7634263
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP01900129A Expired - Lifetime EP1263540B1 (de) | 2000-03-13 | 2001-01-05 | Verfahren zur herstellung von dünnwandigen bauteilen aus stahl und danach hergestellte bauteile |
Country Status (13)
| Country | Link |
|---|---|
| US (1) | US6953627B2 (de) |
| EP (1) | EP1263540B1 (de) |
| AT (1) | ATE270163T1 (de) |
| AU (1) | AU2372701A (de) |
| BR (1) | BR0109190B1 (de) |
| CA (1) | CA2404361C (de) |
| CZ (1) | CZ303019B6 (de) |
| DE (2) | DE10011758C2 (de) |
| ES (1) | ES2223770T3 (de) |
| HU (1) | HU225711B1 (de) |
| MX (1) | MXPA02008871A (de) |
| SK (1) | SK286356B6 (de) |
| WO (1) | WO2001068293A1 (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12031613B2 (en) | 2019-05-28 | 2024-07-09 | Schaeffler Technologies AG & Co. KG | Profiled nut of a screw drive, in particular a ball screw nut of a ball screw drive, and method for the production thereof |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10202212B4 (de) * | 2002-01-18 | 2004-02-26 | Thyssenkrupp Stahl Ag | Verfahren zum Erzeugen von aus metallischem Verbundwerkstoff bestehendem Band oder Blech |
| DE102005006606B3 (de) * | 2005-02-11 | 2006-03-16 | Thyssenkrupp Steel Ag | Verfahren zum Herstellen von walzplattiertem Warmband zur Weiterverarbeitung zu Kaltband und gewickeltes Coil aus solchem Warmband |
| DE102006019567B3 (de) * | 2006-04-27 | 2007-11-08 | Daimlerchrysler Ag | Verfahren zum Herstellen umgeformter Stahlbauteile |
| DE102007022453B4 (de) * | 2007-05-10 | 2020-02-06 | Thyssenkrupp Steel Europe Ag | Mehrschichtiges Verbundteil und aus diesem hergestelltes Bauteil |
| DE102008018204A1 (de) | 2008-02-04 | 2009-08-06 | Wickeder Westfalenstahl Gmbh | Verbundwerkstoff und Verfahren zur Herstellung eines Verbundwerkstoffs |
| DE102008008113A1 (de) * | 2008-02-08 | 2009-08-13 | Schaeffler Kg | Nichtmagnetisierbares Wälzlagerbauteil aus einem austenitischen Werkstoff und Verfahren zur Herstellung eines derartigen Wälzlagerbauteils |
| PL2123447T3 (pl) * | 2008-05-07 | 2019-05-31 | Thyssenkrupp Steel Europe Ag | Tworzywo kompozytowe z efektem ochrony balistycznej |
| DE102008022709A1 (de) | 2008-05-07 | 2009-11-19 | Thyssenkrupp Steel Ag | Verwendung eines metallischen Verbundwerkstoffs in einer Fahrzeugstruktur |
| US20100330389A1 (en) * | 2009-06-25 | 2010-12-30 | Ford Motor Company | Skin pass for cladding thin metal sheets |
| DE102011106222A1 (de) * | 2011-06-07 | 2012-12-13 | Rwe Power Ag | Dampferzeugerbauteil sowie Verfahren zur Herstellung eines Dampferzeugerbauteil |
| DE102013106570A1 (de) * | 2013-06-24 | 2014-12-24 | Thyssenkrupp Resource Technologies Gmbh | Siebstange, Stangensieb und Verfahren zur Herstellung einer Siebstange |
| DE102013017798A1 (de) * | 2013-10-25 | 2015-04-30 | GM Global Technology Operations LLC (n. d. Ges. d. Staates Delaware) | Verbundstahlblech |
| DE102014116949A1 (de) * | 2014-11-19 | 2016-05-19 | Thyssenkrupp Ag | Verfahren zur Herstellung eines Verbundwerkstoffes |
| DE102017220416A1 (de) | 2016-11-18 | 2018-05-24 | Sms Group Gmbh | Verfahren und Vorrichtung zur Herstellung eines kontinuierlichen bandförmigen Verbundmaterials |
| WO2020154464A1 (en) * | 2019-01-23 | 2020-07-30 | Verd Steel, Inc. | Internal gradient materials, implements and methods |
| KR20230036983A (ko) * | 2021-09-08 | 2023-03-15 | 고오슈우하네쓰렌 가부시기가이샤 | 강재접합체 및 그 제조 방법 |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1435936A (fr) * | 1965-03-08 | 1966-04-22 | Siderurgie Fse Inst Rech | Procédé et dispositif de coulée continue de produits liquides |
| FR1495365A (de) * | 1965-10-01 | 1967-12-20 | ||
| DE3346391C2 (de) * | 1983-12-22 | 1985-11-21 | Mannesmann AG, 4000 Düsseldorf | Stranggießverfahren und Vorrichtung zum Herstellen von Mehrschichtwerkstoffen |
| DE4137118A1 (de) * | 1991-11-12 | 1993-05-13 | Schaeffler Waelzlager Kg | Kaltband zur herstellung praezisions-tiefgezogener, einsatzgehaerteter bauteile, insbesondere waelzlager- und motorenteile |
| DE19631999A1 (de) * | 1996-08-08 | 1998-02-12 | Schloemann Siemag Ag | Stranggießverfahren zur Herstellung von Verbundblechen sowie Stranggießanlage |
| DE19731124C1 (de) | 1997-07-19 | 1999-01-21 | Schloemann Siemag Ag | Verfahren und Vorrichtung zur Erzeugung von beschichtetem Warm- und Kaltband |
| DE19850213C2 (de) * | 1998-01-23 | 2001-08-30 | Sms Demag Ag | Gießverfahren für ein dünnes Metallband und zugehörige Gießvorrichtung |
| DE19815007C2 (de) * | 1998-01-23 | 2000-07-06 | Sms Demag Ag | Gießverfahren für einen Metallstrang |
-
2000
- 2000-03-13 DE DE10011758A patent/DE10011758C2/de not_active Expired - Lifetime
-
2001
- 2001-01-05 BR BRPI0109190-5A patent/BR0109190B1/pt not_active IP Right Cessation
- 2001-01-05 AU AU23727/01A patent/AU2372701A/en not_active Abandoned
- 2001-01-05 CZ CZ20023038A patent/CZ303019B6/cs not_active IP Right Cessation
- 2001-01-05 CA CA002404361A patent/CA2404361C/en not_active Expired - Fee Related
- 2001-01-05 ES ES01900129T patent/ES2223770T3/es not_active Expired - Lifetime
- 2001-01-05 DE DE50102738T patent/DE50102738D1/de not_active Expired - Lifetime
- 2001-01-05 WO PCT/EP2001/000088 patent/WO2001068293A1/de not_active Ceased
- 2001-01-05 MX MXPA02008871A patent/MXPA02008871A/es active IP Right Grant
- 2001-01-05 HU HU0300086A patent/HU225711B1/hu not_active IP Right Cessation
- 2001-01-05 AT AT01900129T patent/ATE270163T1/de active
- 2001-01-05 US US10/221,534 patent/US6953627B2/en not_active Expired - Fee Related
- 2001-01-05 EP EP01900129A patent/EP1263540B1/de not_active Expired - Lifetime
- 2001-01-05 SK SK1327-2002A patent/SK286356B6/sk not_active IP Right Cessation
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12031613B2 (en) | 2019-05-28 | 2024-07-09 | Schaeffler Technologies AG & Co. KG | Profiled nut of a screw drive, in particular a ball screw nut of a ball screw drive, and method for the production thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| HU225711B1 (en) | 2007-06-28 |
| CZ303019B6 (cs) | 2012-02-29 |
| DE50102738D1 (de) | 2004-08-05 |
| CA2404361A1 (en) | 2001-09-20 |
| ATE270163T1 (de) | 2004-07-15 |
| ES2223770T3 (es) | 2005-03-01 |
| CA2404361C (en) | 2007-03-06 |
| BR0109190B1 (pt) | 2011-04-05 |
| AU2372701A (en) | 2001-09-24 |
| EP1263540A1 (de) | 2002-12-11 |
| US20030029530A1 (en) | 2003-02-13 |
| SK13272002A3 (sk) | 2003-07-01 |
| MXPA02008871A (es) | 2004-10-14 |
| SK286356B6 (sk) | 2008-08-05 |
| DE10011758A1 (de) | 2001-09-27 |
| BR0109190A (pt) | 2003-05-27 |
| WO2001068293A1 (de) | 2001-09-20 |
| HUP0300086A2 (en) | 2003-04-28 |
| US6953627B2 (en) | 2005-10-11 |
| CZ20023038A3 (cs) | 2003-06-18 |
| DE10011758C2 (de) | 2003-10-16 |
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