DE102020122935A1 - plain bearing element - Google Patents
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- DE102020122935A1 DE102020122935A1 DE102020122935.6A DE102020122935A DE102020122935A1 DE 102020122935 A1 DE102020122935 A1 DE 102020122935A1 DE 102020122935 A DE102020122935 A DE 102020122935A DE 102020122935 A1 DE102020122935 A1 DE 102020122935A1
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/122—Multilayer structures of sleeves, washers or liners
- F16C33/124—Details of overlays
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D15/00—Electrolytic or electrophoretic production of coatings containing embedded materials, e.g. particles, whiskers, wires
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D7/00—Electroplating characterised by the article coated
- C25D7/10—Bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/122—Multilayer structures of sleeves, washers or liners
- F16C33/125—Details of bearing layers, i.e. the lining
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/122—Multilayer structures of sleeves, washers or liners
- F16C33/127—Details of intermediate layers, e.g. nickel dams
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/14—Special methods of manufacture; Running-in
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/20—Sliding surface consisting mainly of plastics
- F16C33/203—Multilayer structures, e.g. sleeves comprising a plastic lining
- F16C33/205—Multilayer structures, e.g. sleeves comprising a plastic lining with two layers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/20—Sliding surface consisting mainly of plastics
- F16C33/208—Methods of manufacture, e.g. shaping, applying coatings
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/56—Electroplating: Baths therefor from solutions of alloys
- C25D3/60—Electroplating: Baths therefor from solutions of alloys containing more than 50% by weight of tin
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
- F16C17/022—Sliding-contact bearings for exclusively rotary movement for radial load only with a pair of essentially semicircular bearing sleeves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2202/00—Solid materials defined by their properties
- F16C2202/50—Lubricating properties
- F16C2202/52—Graphite
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2202/00—Solid materials defined by their properties
- F16C2202/50—Lubricating properties
- F16C2202/54—Molybdenum disulfide
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/30—Alloys based on one of tin, lead, antimony, bismuth, indium, e.g. materials for providing sliding surfaces
- F16C2204/34—Alloys based on tin
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2206/00—Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents
- F16C2206/40—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal
- F16C2206/42—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic oxides
- F16C2206/44—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic oxides based on aluminium oxide (Al2O3)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2206/00—Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents
- F16C2206/40—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal
- F16C2206/56—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic carbides, e.g. silicon carbide (SiC)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2206/00—Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents
- F16C2206/40—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal
- F16C2206/58—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic nitrides
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2208/00—Plastics; Synthetic resins, e.g. rubbers
- F16C2208/20—Thermoplastic resins
- F16C2208/40—Imides, e.g. polyimide [PI], polyetherimide [PEI]
- F16C2208/42—Polyamideimide [PAI]
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/30—Coating surfaces
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2240/00—Specified values or numerical ranges of parameters; Relations between them
- F16C2240/40—Linear dimensions, e.g. length, radius, thickness, gap
- F16C2240/60—Thickness, e.g. thickness of coatings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/22—Internal combustion engines
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- Metallurgy (AREA)
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- Sliding-Contact Bearings (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
Die Erfindung betrifft ein Gleitlagerelement (2) in Form einer Gleitlagerschale (4) oder einer Anlaufscheibe (6) jeweils aus einem Gleitlagerverbundwerkstoff mit einer metallischen Stützschicht (16), insbesondere aus Stahl, mit einer auf die Stützschicht (16) aufgebrachten Lagermetallschicht (18) und mit einer auf die Lagermetallschicht (18) aufgebrachten Gleitschicht (22) auf Polymerbasis; erfindungsgemäß wird vorgeschlagen, dass die Lagermetallschicht (18) eine galvanisch auf die Stützschicht (16) abgeschiedene Zinn-Basis-Schicht (20) ist und eine Dicke von 8,0 - 50,0 µm aufweist und dass die Gleitschicht (22) auf Polymerbasis eine Gleitlackschicht (24) mit einer Dicke von 8,0 - 15,0 µm ist.The invention relates to a plain bearing element (2) in the form of a plain bearing shell (4) or a thrust washer (6), each made of a plain bearing composite material with a metallic supporting layer (16), in particular made of steel, with a bearing metal layer (18) applied to the supporting layer (16). and having a polymer-based sliding layer (22) applied to the bearing metal layer (18); According to the invention, it is proposed that the bearing metal layer (18) is a tin base layer (20) galvanically deposited on the supporting layer (16) and has a thickness of 8.0 - 50.0 µm and that the sliding layer (22) is polymer-based a bonded lacquer layer (24) with a thickness of 8.0 - 15.0 µm.
Description
Die Erfindung betrifft ein Gleitlagerelement in Form einer Gleitlagerschale, insbesondere Pleuellagerschale, oder einer Anlaufscheibe, insbesondere für eine Kurbelwelle, jeweils aus einem Gleitlagerverbundwerkstoff mit einer metallischen Stützschicht, insbesondere aus Stahl, mit einer auf die Stützschicht aufgebrachten Lagermetallschicht und mit einer auf die Lagermetallschicht aufgebrachten Gleitschicht auf Polymerbasis.The invention relates to a plain bearing element in the form of a plain bearing shell, in particular a connecting rod bearing shell, or a thrust washer, in particular for a crankshaft, each made of a plain bearing composite material with a metallic supporting layer, in particular made of steel, with a bearing metal layer applied to the supporting layer and with a sliding layer applied to the bearing metal layer polymer based.
Bei derartigen bekannten Gleitlagerelementen für insbesondere motorische oder motorennahe Anwendungen als Pleuellagerschale oder Anlaufscheibe ist auf die Stützschicht aus Stahl eine üblicherweise wenigstens 150 µm, typischerweise 200 - 500 µm dicke Lagermetallschicht auf Alu-, Bronze-, Messing- oder Weißmetallbasis aufgegossen oder aufplattiert. Darauf kann noch eine in unmittelbarem Kontakt mit dem Gleitpartner stehende Gleitlackschicht als Sputterschicht, als galvanische Schicht oder als Polymerschicht aufgebracht sein.In such known plain bearing elements for engine or engine-related applications in particular as a connecting rod bearing shell or thrust washer, a usually at least 150 μm, typically 200-500 μm thick bearing metal layer based on aluminum, bronze, brass or white metal is cast or plated onto the steel supporting layer. A bonded coating layer that is in direct contact with the sliding partner can also be applied as a sputter layer, as a galvanic layer or as a polymer layer.
Der vorliegenden Erfindung liegt die Aufgabe zugrunde, ein Gleitlagerelement der eingangs genannten Art zu schaffen, dass kostengünstiger herstellbar ist als vorbekannte Gleitlagerelemente und dennoch hinsichtlich der Verschleißbeständigkeit und des Reibwerts keine Nachteile mit sich bringt.The present invention is based on the object of creating a plain bearing element of the type mentioned at the outset that can be produced more cost-effectively than previously known plain bearing elements and yet does not entail any disadvantages with regard to wear resistance and the coefficient of friction.
Diese Aufgabe wird bei einem Gleitlagerelement der genannten Art erfindungsgemäß dadurch gelöst, dass die Lagermetallschicht eine galvanisch auf die Stützschicht abgeschiedene Zinn-Basis-Schicht ist und eine Dicke von 8,0 - 50,0 µm aufweist und dass die Gleitschicht auf Polymerbasis eine Gleitlackschicht mit einer Dicke von 8,0 - 15,0 µm ist.In the case of a plain bearing element of the type mentioned, this object is achieved according to the invention in that the bearing metal layer is a tin-based layer which is electroplated onto the supporting layer and has a thickness of 8.0-50.0 μm and that the polymer-based sliding layer has a bonded coating layer with a thickness of 8.0 - 15.0 µm.
Mit der vorliegenden Erfindung wurde erkannt, dass es möglich ist, auf eine dicke aufgegossene oder aufplattierte Lagermetallschicht zu verzichten und die Lagermetallschicht stattdessen als dünne galvanisch abgeschiedene Zinn-Basis-Schicht auszubilden. Diese dünne Zinn-Basis-Schicht bildet einerseits eine belastbare Unterlage für die darauf vorzugsweise unmittelbar aufgebrachte Gleitlackschicht, obschon sich Zinn für den Einsatz als lasttragende Schicht eher nicht empfiehlt. Jedoch tragen dünne Schichten im Allgemeinen besser als dicke Schichten. Durch die Reduzierung der Dicke der Lagermetallschicht vermag daher auch eine galvanische Zinn-Basis-Schicht den hier auftretenden Belastungen standzuhalten. Neben ihrer Funktion als tragende Unterlage für die Gleitlackschicht vermag die Zinn-Basis-Schicht aber auch eine Einbettungsfähigkeit für Fremdpartikel zu gewährleisten, welche in die polymere Gleitlackschicht, insbesondere im Einlaufbetrieb des Gleitlagerelements, eingedrungen oder durch diese hindurchgedrungen sind.With the present invention, it was recognized that it is possible to dispense with a thick cast or plated-on bearing metal layer and instead to form the bearing metal layer as a thin galvanically deposited tin base layer. On the one hand, this thin tin base layer forms a resilient base for the bonded coating layer that is preferably applied directly to it, although tin is not recommended for use as a load-bearing layer. However, thin layers generally wear better than thick layers. By reducing the thickness of the bearing metal layer, a galvanic tin base layer can withstand the loads that occur here. In addition to its function as a supporting base for the anti-friction layer, the tin-base layer can also ensure embedding for foreign particles which have penetrated or penetrated the polymer anti-friction layer, particularly during running-in of the plain bearing element.
Ein erfindungsgemäßes Gleitlagerelement und ein zugrundeliegender Gleitlagerverbundwerkstoff lassen sich aufgrund reduzierter Komplexität des Herstellprozesses durch Anwendung von zwei Nassprozessen und einer wesentlichen Reduzierung des Materials kostengünstiger herstellen, ohne dass hiermit Performanceeinbußen verbunden sind.A plain bearing element according to the invention and a plain bearing composite material on which it is based can be produced more cost-effectively due to the reduced complexity of the production process by using two wet processes and a significant reduction in the material, without any losses in performance being associated with this.
Die Zinn-Basis-Schicht kann Zinn oder eine Zinn-Legierung, insbesondere eine Zinn-Kupfer-Legierung, insbesondere eine SnCu6-Legierung, umfassen.The tin base layer can comprise tin or a tin alloy, in particular a tin-copper alloy, in particular an SnCu6 alloy.
Es erweist sich als vorteilhaft, wenn die Zinn-Basis-Schicht eine Dicke von wenigstens 9,0 µm, insbesondere von wenigstens 10,0 µm, insbesondere von wenigstens 11,0 µm, insbesondere von wenigstens 12,0 µm, insbesondere von wenigstens 13,0 µm, insbesondere von wenigstens 14,0 µm, insbesondere von von wenigstens 15,0 µm, insbesondere von höchstens 45,0 µm, insbesondere von höchstens 40,0 µm, insbesondere von höchstens 35,0 µm aufweist. Je geringer die Dicke der Zinn-Basis-Schicht ist, desto tragfähiger und belastbarer wird die durch sie gebildete Lagermetallschicht, und es reduzieren sich auch die Herstellkosten. Je größer die Dicke der Zinn-Basis-Schicht ist, desto mehr Potenzial bildet sie für die Einbettung von Fremdpartikeln. Optimale Ergebnisse werden mit Schichtdicken zwischen 10,0 und 40,0 µm insbesondere zwischen 15,0 und 35,0 µm erzielt.It has proven to be advantageous if the tin base layer has a thickness of at least 9.0 µm, in particular at least 10.0 µm, in particular at least 11.0 µm, in particular at least 12.0 µm, in particular at least 13 .0 μm, in particular at least 14.0 μm, in particular at least 15.0 μm, in particular at most 45.0 μm, in particular at most 40.0 μm, in particular at most 35.0 μm. The smaller the thickness of the tin base layer, the more stable and resilient the bearing metal layer it forms, and the production costs are also reduced. The greater the thickness of the tin base layer, the more potential it creates for embedding foreign particles. Optimum results are achieved with layer thicknesses between 10.0 and 40.0 µm, in particular between 15.0 and 35.0 µm.
Es ist weiter denkbar und kann sich als vorteilhaft erweisen, wenn die Zinn-Basis-Schicht eingelagerte Hartpartikel, insbesondere aus ... und/oder Festschmierstoffpartikel, insbesondere aus MoS2, Graphit, PTFE, aufweist. Solche Partikel lassen sich in das galvanische Bad einbringen, aus dem die Zinn-Basis-Schicht abgeschieden wird, so dass sie beim Aufwachsen der Zinn-Basis-Schicht auch darin eingeschlossen und Bestandteil der Lagermetallschicht werden.It is also conceivable and can prove to be advantageous if the tin base layer has embedded hard particles, in particular made of ... and/or solid lubricant particles, in particular made of MoS 2 , graphite, PTFE. Such particles can be introduced into the galvanic bath from which the tin base layer is deposited, so that when the tin base layer is grown they are also included therein and become part of the bearing metal layer.
Im Zusammenwirken mit der beanspruchten Zinn-Basis-Schicht als Lagermetallschicht erweist es sich als vorteilhaft, wenn die Gleitlackschicht eine Dicke von wenigstens 9,0 µm und insbesondere von höchstens 14,0 µm, insbesondere von höchstens 13,0 µm aufweist. Bei diesen Schichtdicken wird eine noch sehr gute Tragfähigkeit erzielt, und die Gleitlagerschicht selbst bietet auch ein gewisses Potenzial für die Einbettung kleiner Fremdpartikel.In conjunction with the claimed tin base layer as a bearing metal layer, it has proven to be advantageous if the anti-friction coating layer has a thickness of at least 9.0 μm and in particular at most 14.0 μm, in particular at most at least 13.0 µm. With these layer thicknesses, a very good load-bearing capacity is still achieved, and the plain bearing layer itself also offers a certain potential for embedding small foreign particles.
Die Polymerbasis der Gleitlackschicht ist bevorzugt Polyamidimid (PAI).The polymer basis of the bonded coating layer is preferably polyamideimide (PAI).
Bei herkömmlichen Gleitlagerelementen wird eine finale Formgebung der Geometrie des Gleitlagerelements, insbesondere eine sogenannte Ovalisierung eines halbschalenförmigen Gleitlagerelements, an einem zuvor hergestellten Verbund aus metallischer Stützschicht und verhältnismäßig dicker Lagermetallschicht durch spanabhebende Bearbeitung der Lagermetallschicht erreicht. Man erhält so eine Lagermetallschicht mit über den Umfang des Gleitlagerelements variierender Wandstärke bei gleichbleibender Wandstärke der metallischen Stützschicht. Dies kann unerwünschte Variationen der Belastbarkeit und der sonstigen tribologischen Eigenschaften des Gleitlagerelements in Umfangsrichtung bedeuten. - Es wird in Weiterbildung der vorliegenden Erfindung weiter vorgeschlagen, dass die metallische Stützschicht ausgehend von einem metallischen Flachmaterialabschnitt gleichförmiger Dicke gebildet ist, indem der Flachmaterialabschnitt auf Schalenform gebracht wurde und im Anschluss daran auf einer radial inneren Seite der Schalenform spanabhebend bearbeitet und auf eine Endform mit variierender Wanddicke gebracht wurde und dass die Zinn-Basis-Schicht unmittelbar auf die spanabhebend bearbeitete radial innere Seite des Flachmaterialabschnitts galvanisch abgeschieden und darauf die Gleitlackschicht aufgebracht ist. Solchenfalls wird eine bewusst herzustellende Innenkontur des Gleitlagerelements, also eine Abweichung von der idealen zylindrischen Geometrie, insbesondere in Form einer sogenannten Ovalisierung, durch eine spanabhebende Bearbeitung der metallischen Stützschicht und nicht der Lagermetallschicht erhalten, so dass die Lagermetallschicht in Form der galvanisch aufgebrachten Zinn-Basis-Schicht mit gleichförmiger Wanddicke auf die zuvor bearbeitete metallische Stützschicht aufgebracht werden kann. Die spanabhebende Bearbeitung der metallischen Stützschicht ist demzufolge auch am fertigen Produkt ohne weiteres anhand einer variierenden Wanddicke dieser Stützschicht erkennbar.In conventional plain bearing elements, a final shape of the geometry of the plain bearing element, in particular a so-called ovalization of a half-shell-shaped plain bearing element, is achieved on a previously produced composite of metallic support layer and relatively thick bearing metal layer by machining the bearing metal layer. In this way, a bearing metal layer is obtained with a wall thickness that varies over the circumference of the plain bearing element, while the wall thickness of the metal support layer remains the same. This can mean undesirable variations in the load capacity and other tribological properties of the plain bearing element in the circumferential direction. - In a further development of the present invention, it is further proposed that the metallic support layer is formed starting from a metallic flat material section of uniform thickness, by bringing the flat material section into a shell shape and then machining it on a radially inner side of the shell shape and machining it to a final shape varying wall thickness was brought and that the tin base layer is electroplated directly onto the machined radially inner side of the flat material section and the bonded coating layer is applied to it. In such a case, an inner contour of the plain bearing element that is to be deliberately produced, i.e. a deviation from the ideal cylindrical geometry, in particular in the form of a so-called ovalization, is obtained by machining the metallic support layer and not the bearing metal layer, so that the bearing metal layer is in the form of the galvanically applied tin base -layer with uniform wall thickness can be applied to the previously machined metallic backing layer. The machining of the metallic support layer can consequently also be readily recognized on the finished product by means of a varying wall thickness of this support layer.
Weiter wird Schutz beansprucht für ein Verfahren mit den Merkmalen des Anspruchs 8 und für ein Verfahren mit den Merkmalen des Anspruchs 9.Protection is also claimed for a method having the features of
Weitere Merkmale, Einzelheiten und Vorteile der Erfindung ergeben sich aus den beigefügten Patentansprüchen und aus der zeichnerischen Darstellung und nachfolgenden Beschreibung einer bevorzugten Ausführungsform des erfindungsgemäßen Gleitlagerelements. In der Zeichnung zeigt:
-
1 eine Seitenansicht eines erfindungsgemäßen Gleitlagerelements in Form einer Gleitlagerschale; -
2 eine schematische nicht maßstabsgetreue Querschnittsdarstellung mit Schnittebene II-II des Gleitlagerelements nach1 ; und -
3 eine Draufsicht auf ein erfindungsgemäßes Gleitlagerelement in Form einer Anlaufscheibe.
-
1 a side view of a plain bearing element according to the invention in the form of a plain bearing shell; -
2 a schematic cross-sectional representation, not true to scale, with section plane II-II of the plain bearing element1 ; and -
3 a plan view of a plain bearing element according to the invention in the form of a thrust washer.
Die Figuren zeigen ein Gleitlagerelement 2 in Form einer Gleitlagerschale 4 (
Nachfolgend wird der Schichtenaufbau des Gleitlagerelements 2 anhand der schematischen Querschnittsdarstellung der
Zur Herstellung des Gleitlagerelements 2 nach
Schließlich zeigt
ZITATE ENTHALTEN IN DER BESCHREIBUNGQUOTES INCLUDED IN DESCRIPTION
Diese Liste der vom Anmelder aufgeführten Dokumente wurde automatisiert erzeugt und ist ausschließlich zur besseren Information des Lesers aufgenommen. Die Liste ist nicht Bestandteil der deutschen Patent- bzw. Gebrauchsmusteranmeldung. Das DPMA übernimmt keinerlei Haftung für etwaige Fehler oder Auslassungen.This list of the documents cited by the applicant was generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.
Zitierte PatentliteraturPatent Literature Cited
- WO 2020/118327 A1 [0003]WO 2020/118327 A1 [0003]
Claims (9)
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2224868A1 (en) | 1972-05-20 | 1973-11-29 | Schmidt Gmbh Karl | MOLDING BOARD FOR THE IMPROVED MANUFACTURING OF FLOOR BEARING SHELLS |
EP1717469A2 (en) | 2005-04-29 | 2006-11-02 | Miba Gleitlager GmbH | Bearing element |
DE102015202631A1 (en) | 2015-02-13 | 2016-08-18 | Schaeffler Technologies AG & Co. KG | Coating for bearings, bearings and procedures |
WO2020118327A1 (en) | 2018-12-13 | 2020-06-18 | Miba Gleitlager Austria Gmbh | Slide bearing, in particular for a gearbox of a wind turbine |
-
2020
- 2020-09-02 DE DE102020122935.6A patent/DE102020122935B4/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2224868A1 (en) | 1972-05-20 | 1973-11-29 | Schmidt Gmbh Karl | MOLDING BOARD FOR THE IMPROVED MANUFACTURING OF FLOOR BEARING SHELLS |
EP1717469A2 (en) | 2005-04-29 | 2006-11-02 | Miba Gleitlager GmbH | Bearing element |
DE102015202631A1 (en) | 2015-02-13 | 2016-08-18 | Schaeffler Technologies AG & Co. KG | Coating for bearings, bearings and procedures |
WO2020118327A1 (en) | 2018-12-13 | 2020-06-18 | Miba Gleitlager Austria Gmbh | Slide bearing, in particular for a gearbox of a wind turbine |
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