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EP3575435B1 - Plasma spray method for coating a cylinder a cylinder liner of a cylinder crankcase of a reciprocating piston combustion engine - Google Patents

Plasma spray method for coating a cylinder a cylinder liner of a cylinder crankcase of a reciprocating piston combustion engine Download PDF

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Publication number
EP3575435B1
EP3575435B1 EP19176247.5A EP19176247A EP3575435B1 EP 3575435 B1 EP3575435 B1 EP 3575435B1 EP 19176247 A EP19176247 A EP 19176247A EP 3575435 B1 EP3575435 B1 EP 3575435B1
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EP
European Patent Office
Prior art keywords
coating
plasma spraying
spraying process
process according
cylinder
Prior art date
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Application number
EP19176247.5A
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German (de)
French (fr)
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EP3575435A1 (en
Inventor
Klaus Klimek
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Volkswagen AG
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Volkswagen AG
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/08Metallic material containing only metal elements
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • C23C4/11Oxides
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/134Plasma spraying
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/137Spraying in vacuum or in an inert atmosphere
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/14Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying for coating elongate material
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/14Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying for coating elongate material
    • C23C4/16Wires; Tubes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B13/00Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
    • B05B13/06Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00 specially designed for treating the inside of hollow bodies
    • B05B13/0627Arrangements of nozzles or spray heads specially adapted for treating the inside of hollow bodies
    • B05B13/0636Arrangements of nozzles or spray heads specially adapted for treating the inside of hollow bodies by means of rotatable spray heads or nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/16Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed
    • B05B7/22Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed electrically, magnetically or electromagnetically, e.g. by arc
    • B05B7/222Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed electrically, magnetically or electromagnetically, e.g. by arc using an arc
    • B05B7/226Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed electrically, magnetically or electromagnetically, e.g. by arc using an arc the material being originally a particulate material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F7/00Casings, e.g. crankcases
    • F02F7/0085Materials for constructing engines or their parts

Definitions

  • the invention relates to a plasma spraying method for coating a cylinder bore of a cylinder crankcase of a reciprocating piston internal combustion engine.
  • a coating method for coating a curved surface, a thermal coating and a cylinder with a thermal coating are known.
  • a thermal spray device in particular a plasma spray device or HVOF spray device with a burner that rotates on a burner shaft about a shaft axis at a predetermined rotation frequency, wherein the coating jet for applying a coating to the curved surface is directed at least partially radially away from the shaft axis towards the curved surface.
  • the aforementioned publication discloses a linear dependence of rotation frequency and feed rate, with the parameter combinations 200 rpm - 25 g/min, 400 rpm - 50 g/min, 600 rpm - 75 g/min and 800 rpm - 100 g/min being specifically mentioned.
  • the US 5 080 056 A discloses a method for plasma coating cylinder bores with a high rotation rate of the plasma torch of 800 rpm, whereby an axial feed rate of approximately 4.2 mm/s is expressly specified.
  • the above-mentioned publication does not address the question of the preferred spray material feed rate.
  • the US 9 885 311 B1 discloses a similar process and addresses the problem of reducing the heat input into the crankcase caused by the coating process.
  • it particularly points to an advantageous relationship between the rotation frequency and the axial feed of the burner.
  • the axial feed should be reduced to values between 16 and 25 mm/s in order to keep the residence time of the burner and thus the applied layer thickness constant.
  • the US 9 885 311 B1 a linear relationship, the extrapolation of which leads to feed rates of well below 25 mm/s at rotation frequencies of well above 500 rpm.
  • the DE 10 2008 053 642 A1 also discloses a method for cylinder liner coating and focuses primarily on the spray materials optimally used for this purpose.
  • cylinder crankcases for reciprocating piston internal combustion engines
  • cylinder crankcases made of aluminum are used, but these require a protective layer in the area of the cylinder bore, e.g. a protective layer applied by plasma spraying.
  • a positive side effect of the coating is not only an increase in the robustness of the cylinder bore, but also a significantly reduced friction in the area of the piston group (and thus also a reduction in CO2 emissions) as well as positive effects on corrosive media.
  • Coating processes known from the state of the art are powder plasma spraying (APS process), wire spraying processes, such as plasma transferred wire arc (PTWA/RSW) coating processes, arc wire spraying (LDS) and high-velocity flame spraying (HVOF spraying).
  • APS process powder plasma spraying
  • wire spraying processes such as plasma transferred wire arc (PTWA/RSW) coating processes, arc wire spraying (LDS) and high-velocity flame spraying (HVOF spraying).
  • PTWA/RSW plasma transferred wire arc
  • LDS arc wire spraying
  • HVOF spraying high-velocity flame spraying
  • a roughening process is carried out to clamp the coating, i.e. to improve the adhesion of the coating, or is necessary so that the coating can be applied at all.
  • This roughening process is carried out by blasting processes using corundum and water (medium-pressure/high-pressure water jets), laser beam roughening or roughening with a geometrically defined cutting edge.
  • the invention is based on the object of providing a coating process by means of which the formation of oxides is limited or oxide lines in the layer formation and thus negative influences due to oxide breakouts and micro-grooving - particularly caused by such oxide breakouts or existing due to a high oxide lineage - are avoided.
  • the coating is at least partially applied to the cylinder bore of the cylinder crankcase using the following parameter combination: a) rotation speed: 600 - 700 rpm, b) Spray material feed rate: 100 - 120 g/min and c) feed rate: 24 - 75 mm/s.
  • the value range between 100 and 120 g/min has proven to be optimal.
  • the coating is applied using 5-8 spraying cycles, each in the form of double strokes.
  • application using 6-7 spraying cycles is particularly preferred. It has been shown that the thickness and structure of a corresponding coating in conjunction with the processing time required in each case is particularly high-quality and efficient in this case.
  • a steel layer or a ceramic layer is preferably applied as a coating.
  • steel layers particular reference is made to low-alloy and high-alloy steel layers, i.e. steel layers with steels in which the sum of the alloying elements does not exceed 5% by mass (low-alloy steels) or steels in which the average mass content of at least one alloying element is greater than or equal to 5% (high-alloy steels).
  • low-alloy steels low-alloy steels
  • high-alloy steels are preferred over high-alloy steels.
  • high-alloy steels also achieve results that are advantageous compared to the results known from the previous state of the art.
  • a ceramic layer With regard to the application of a ceramic layer, particular reference is made to layers made of titanium dioxide (TiO 2 ).
  • a ceramic layer is preferably applied in conjunction with a previous roughening process and the previous application of an adhesion-promoting layer.
  • a nickel-aluminum layer, a bronze layer or a low-alloy steel layer are particularly suitable as an adhesion-promoting layer.
  • the thickness of an adhesion-promoting layer is preferably less than 100 ⁇ m, preferably less than 60 ⁇ m and particularly preferably a maximum of 40 ⁇ m.
  • this coating is preferably applied using a low-alloy steel powder.
  • Steel powder with a predominantly spherical morphology with small proportions of satellites is particularly preferred.
  • the coating is applied by means of a steel powder which contains less than 2 wt.% carbon (C), less than 2 wt.% manganese (Mn), less than 2 wt.% chromium (Cr), less than 1 wt.% nickel (Ni), less than 1 wt.% oxygen (O 2 ) and less than 1 wt.% nitrogen (N 2 ).
  • C carbon
  • Mn manganese
  • Cr chromium
  • Ni nickel
  • O 2 oxygen
  • N 2 nitrogen
  • proportion of carbon particular reference is made to a proportion by weight of 1.0 to 1.3.
  • the proportion of manganese particular reference is made to a proportion by weight of 1.2 to 1.6.
  • the proportion by weight of chromium particular reference is made to a value range of 1.2 to 1.6.
  • the proportion by weight of nickel particular reference is made to the value range of less than 0.5.
  • the proportion by weight of oxygen particular reference is made to values of less than 0.2.
  • the proportion by weight of nitrogen particular reference is made to the value range of less than 0.5.
  • the value ranges mentioned above preferably apply cumulatively, ie linked to one another in this combination.
  • a particularly high-quality coating is obtained when a steel layer is applied using a steel powder whose grain size is exclusively smaller than 60 ⁇ m and/or whose grain size is predominantly smaller than 42 ⁇ m.
  • the proportion in weight percent of steel powder with a grain size of less than 42 ⁇ m is preferably a maximum of 90 percent.
  • the proportion with a grain size of less than 26 ⁇ m is preferably a maximum of 50 percent.
  • the proportion with a grain size of less than 16 ⁇ m is preferably a maximum of 10 percent.
  • the coating is applied under the influence of the atmosphere.
  • the process is also referred to as an atmospheric plasma spraying process or APS process.
  • APS process is also referred to as an atmospheric plasma spraying process or APS process.
  • the coating can also be applied using a protective gas or in a vacuum in a plasma spraying process according to the invention. In this case, the costs of carrying out the process are higher, but in individual cases a qualitatively significantly better coating result can be achieved, i.e. in particular a coating can be achieved that has a lower oxide content or has a lower oxide row density.
  • the plasma spraying process according to the invention is particularly advantageous if, before applying the coating, at least one radiant roughening process is carried out using corundum and/or water, using laser beam roughening or using roughening with a geometrically defined cutting edge. In this case, the adhesion of the coating to be applied and at the same time the durability of the resulting coating is increased.
  • Figure 1 shows a section of a cylinder crankcase of a reciprocating piston internal combustion engine with a section of a cylinder bore of an aluminum base body 10 of a cylinder crankcase 14, wherein the aluminum base body 10 is provided with a coating 12 and the surface 16 facing away from the aluminum base body 10 is part of the cylinder bore 18 of the cylinder crankcase 14.
  • the partially marked black areas 20 are oxides that have formed during the application of the coating 12 by means of a plasma spraying process.
  • Figure 2 shows the surface 16 of the cylinder bore 18.
  • individual oxide lines 22a, 22b, 22c, 22d have formed on the surface 16, which are formed by black dots that are arranged approximately in a row. This is the oxide line structure mentioned at the beginning.
  • Figure 3 shows a view analogous to Figure 1 , wherein the coating 12 was applied by means of a plasma spraying process according to the invention.
  • Figure 4 shows an enlarged view of the Figure 3 .
  • the surface 16, which forms the cylinder bore 18 of the cylinder crankcase 14 has a significantly increased quality in that oxide lines are no longer visible.
  • significantly fewer oxides have formed in the coating 12 than in the coating 12 according to the prior art, which in Figure 1 is shown.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Description

Gebiet der Erfindungfield of the invention

Die Erfindung betrifft ein Plasmaspritzverfahren zur Beschichtung einer Zylinderlaufbahn eines Zylinderkurbelgehäuses einer Hubkolbenbrennkraftmaschine.The invention relates to a plasma spraying method for coating a cylinder bore of a cylinder crankcase of a reciprocating piston internal combustion engine.

Stand der TechnikState of the art

Aus WO 2017/202852 A1 sind ein Beschichtungsverfahren zur Beschichtung einer gekrümmten Oberfläche, eine thermische Beschichtung sowie ein Zylinder mit einer thermischen Beschichtung bekannt. Dabei wird insbesondere Bezug genommen auf die Verwendung von pulverförmigem Beschichtungsmaterial unter Verwendung einer thermischen Spritzgerätes, insbesondere ein Plasmaspritzgerät oder HVOF Spritzgerät mit einem Brenner, der an einem Brennerschaft um eine Schaftachse mit einer vorgegebenen Rotationsfrequenz rotiert, wobei der Beschichtungsstrahl zum Aufbringen einer Beschichtung auf die gekrümmte Oberfläche zumindest teilweise radial von der Schaftachse weg zur gekrümmten Oberfläche hin gerichtet wird. Dabei wird auf die Verwendung von erhöhten Rotationsfrequenzen über 200 Umdrehungen/Minute (U/min) verwiesen, insbesondere bis zu 800 U/min oder sogar mehr, wobei die Förderrate des pulverförmigen Beschichtungsmaterials entsprechend "geeignet gesteigert" werden soll. Hierzu offenbart die genannte Druckschrift eine lineare Abhängigkeit von Rotationsfrequenz und Förderrate, wobei speziell die Parameterkombinationen 200 U/min - 25 g/min, 400 U/min - 50 g/min, 600 U/min - 75 g/min und 800 U/min - 100g/min ausdrücklich genannt werden.Out of WO 2017/202852 A1 A coating method for coating a curved surface, a thermal coating and a cylinder with a thermal coating are known. In this case, particular reference is made to the use of powdered coating material using a thermal spray device, in particular a plasma spray device or HVOF spray device with a burner that rotates on a burner shaft about a shaft axis at a predetermined rotation frequency, wherein the coating jet for applying a coating to the curved surface is directed at least partially radially away from the shaft axis towards the curved surface. Reference is made to the use of increased rotation frequencies above 200 revolutions per minute (rpm), in particular up to 800 rpm or even more, wherein the feed rate of the powdered coating material is to be "suitably increased" accordingly. In this regard, the aforementioned publication discloses a linear dependence of rotation frequency and feed rate, with the parameter combinations 200 rpm - 25 g/min, 400 rpm - 50 g/min, 600 rpm - 75 g/min and 800 rpm - 100 g/min being specifically mentioned.

Auch die US 5 080 056 A offenbart ein Verfahren zur Plasmabeschichtung von Zylinderbohrungen mit hoher Rotationsrate des Plasmabrenners von 800 U/min, wobei ausdrücklich eine axiale Vorschubgeschwindigkeit von ca.4,2 mm/s angegeben wird. Zur Frage der bevorzugten Spritzgutförderrate verhält sich die genannte Druckschrift hingegen nicht.The US 5 080 056 A discloses a method for plasma coating cylinder bores with a high rotation rate of the plasma torch of 800 rpm, whereby an axial feed rate of approximately 4.2 mm/s is expressly specified. However, the above-mentioned publication does not address the question of the preferred spray material feed rate.

Das Dokument WO 2017/202852 A1 nimmt keinen Bezug auf den Vorschub während der Beschichtung und geht auch nicht auf die sogenannte Oxidzeiligkeit der zu erzielenden Beschichtung ein.The document WO 2017/202852 A1 does not refer to the feed rate during coating and does not address the so-called oxide lineation of the coating to be achieved.

Die US 9 885 311 B1 offenbart ein ähnliches Verfahren und nimmt sich der Problematik an, den durch den Beschichtungsprozess bedingten Wärmeeintrag in das Kurbelgehäuse zu verringern. Sie weist diesbezüglich insbesondere auf einen vorteilhafterweise einzuhaltenden Zusammenhang zwischen der Rotationsfrequenz und dem Axialvorschub des Brenners hin. Speziell soll bei hohen Rotationsfrequenzen über 500 U/min der Axialvorschub auf Werte zwischen 16 und 25 mm/s reduziert werden, um die Verweildauer der Brenners und damit die aufgetragene Schichtdicke konstant zu halten. Mit anderen Worten offenbart also auch die US 9 885 311 B1 einen linearen Zusammenhang, dessen Extrapolation zu Vorschubwerten von deutlich unter 25 mm/s bei Rotationsfrequenzen von deutlich über 500 U/min führt.The US 9 885 311 B1 discloses a similar process and addresses the problem of reducing the heat input into the crankcase caused by the coating process. In this regard, it particularly points to an advantageous relationship between the rotation frequency and the axial feed of the burner. In particular, at high rotation frequencies above 500 rpm, the axial feed should be reduced to values between 16 and 25 mm/s in order to keep the residence time of the burner and thus the applied layer thickness constant. In other words, the US 9 885 311 B1 a linear relationship, the extrapolation of which leads to feed rates of well below 25 mm/s at rotation frequencies of well above 500 rpm.

Die DE 10 2008 053 642 A1 offenbart ebenfalls eine Verfahren zur Zylinderbuchsenbeschichtung und konzentriert sich primär auf die hierfür optimalerweise verwendeten Spritzgutmaterialien.The DE 10 2008 053 642 A1 also discloses a method for cylinder liner coating and focuses primarily on the spray materials optimally used for this purpose.

Ein im Hinblick auf die allgemeinen Hintergründe interessanter Artikel findet sich bei Bobzin, K. et al.: "Coating Bores of Light Metal Engine Blocks with a Nonocomposite Material Using the Plasma Transfer Wire Arc Thermal Spray Process", Journal of Thermal Spray Technology, Bd. 17, Nr. 3, 3. Juli 2008 (2008-07-03), Seiten 344-351, XP055258217, US, ISSN:1059-9630, DOI: 10.1007/s11666-008-9188-y . An interesting article with regard to the general background can be found at Bobzin, K. et al.: "Coating Bores of Light Metal Engine Blocks with a Nonocomposite Material Using the Plasma Transfer Wire Arc Thermal Spray Process", Journal of Thermal Spray Technology, Vol. 17, No. 3, July 3, 2008 (2008-07-03), pages 344-351, XP055258217, US, ISSN:1059-9630, DOI: 10.1007/s11666-008-9188-y .

In der Fertigung von Zylinderkurbelgehäusen für Hubkolbenbrennkraftmaschinen wird zunehmend versucht, das Gewicht der Zylinderkurbelgehäuse zu reduzieren. Dazu werden Zylinderkurbelgehäuse aus Aluminium eingesetzt, die jedoch im Bereich der Zylinderlaufbahn eine Schutzschicht benötigen, z.B. eine mittels Plasmaspritzen aufgebrachte Schutzschicht. Ein positiver Nebeneffekt der Beschichtung ist neben einer Robustheitssteigerung der Zylinderlaufbahn eine deutlich reduzierte Reibung im Bereich der Kolbengruppe (und dadurch auch ein reduzierter CO2-Ausstoß) sowie positive Effekte gegenüber korrosiven Medien. Aus dem Stand der Technik bekannte Beschichtungsverfahren sind das Pulver-Plasmaspritzen (APS-Verfahren), das Drahtspritzverfahren, wie z.B. Plasma Transferred Wire Arc (PTWA/RSW) Beschichtungsverfahren, das Lichtbogen-Draht-Spritzen (LDS) und das Hochgeschwindigkeits-Flammspritzen (HVOF-Spritzen).In the manufacture of cylinder crankcases for reciprocating piston internal combustion engines, there are increasing attempts to reduce the weight of the cylinder crankcases. For this purpose, cylinder crankcases made of aluminum are used, but these require a protective layer in the area of the cylinder bore, e.g. a protective layer applied by plasma spraying. A positive side effect of the coating is not only an increase in the robustness of the cylinder bore, but also a significantly reduced friction in the area of the piston group (and thus also a reduction in CO2 emissions) as well as positive effects on corrosive media. Coating processes known from the state of the art are powder plasma spraying (APS process), wire spraying processes, such as plasma transferred wire arc (PTWA/RSW) coating processes, arc wire spraying (LDS) and high-velocity flame spraying (HVOF spraying).

Vor einer thermischen Beschichtung von Zylinderbohrungen in Kurbelgehäusen aus Aluminium und teilweise auch aus Grauguss wird ein Aufrauprozess zur Verklammerung der Beschichtung, d.h. Verbesserung der Haftung der Beschichtung, durchgeführt bzw. ist erforderlich, damit die Beschichtung überhaupt aufgebracht werden kann. Dieser Aufrauprozess wird durch strahlende Prozesse mittels Korund und Wasser (Mitteldruck-/Hochdruck-Wasserstrahlen), Laserstrahlaufrauen oder Aufrauen mit geometrisch definierter Schneide dargestellt.Before thermally coating cylinder bores in crankcases made of aluminum and sometimes also of gray cast iron, a roughening process is carried out to clamp the coating, i.e. to improve the adhesion of the coating, or is necessary so that the coating can be applied at all. This roughening process is carried out by blasting processes using corundum and water (medium-pressure/high-pressure water jets), laser beam roughening or roughening with a geometrically defined cutting edge.

Beim Einsatz des Pulver-Plasmaspritzens (APS-Verfahren) entsteht an durch den vorstehend erwähnten Aufrauprozess bedingten Inhomogenitäten eine verstärkte Oxidbildung, wenn eine Prozessführung gemäß einem aus dem Stand der Technik bekannten Beschichtungsvorgang mit beispielsweise 4 Doppelzyklen gewählt wird. Diese kann zu einer parallel zur Oberfläche entstehenden Oxidzeiligkeit in der Beschichtung führen. Die Oxidzeiligkeit wiederum bewirkt eine verminderte Schichtstabilität und kann insbesondere bei einem Vorliegen der Oxide/Oxidzeilen nach dem Fertighonen an der Oberfläche der Beschichtung (Zylinderlaufbahn) zu einem Ausbrechen der Oxide und nachfolgend zu einer Mikroriefigkeit der Zylinderlauffläche führen. Werden die Oxide/Oxidzeilen an der Oberfläche durch den Honprozess beansprucht, kann es zu verstärkten Ausbrüchen dieser Oxide und damit zu einem erhöhten Porenflächenanteil der Laufbahnoberfläche kommen. Dieser kann einen erhöhten Ölverbrauch bewirken und damit korrespondierend zu einem erhöhten Partikelausstoß führen. Ein weiterer Nachteil des aus dem Stand der Technik bekannten Verfahrens ist, dass dieses relativ viel Zeit für den Beschichtungsvorgang benötigt.When using powder plasma spraying (APS process), increased oxide formation occurs at inhomogeneities caused by the roughening process mentioned above if a process control according to a coating process known from the state of the art with, for example, 4 double cycles is selected. This can lead to oxide lines forming in the coating parallel to the surface. The oxide lines in turn cause reduced layer stability and can lead to the oxides breaking out and subsequently to micro-grooving of the cylinder running surface, particularly if the oxides/oxide lines are present on the surface of the coating (cylinder running surface) after final honing. If the oxides/oxide lines on the surface are stressed by the honing process, this can lead to increased breakouts of these oxides and thus to an increased pore area proportion of the running surface. This can cause increased oil consumption and thus correspondingly lead to increased particle emissions. A further disadvantage of the method known from the prior art is that it requires a relatively long time for the coating process.

Aufgabenstellungtask

Der Erfindung liegt die Aufgabe zugrunde, ein Beschichtungsverfahren zur Verfügung zu stellen, mittels welchem die Ausbildung von Oxiden begrenzt bzw. Oxidzeiligkeiten in der Schichtausbildung und somit negative Einflüsse aufgrund auftretender Oxidausbrüche und einer - insbesondere durch solche Oxidausbrücke entstehenden oder aufgrund einer hohen Oxidzeiligkeit existierenden - Mikroriefigkeit zu vermeiden.The invention is based on the object of providing a coating process by means of which the formation of oxides is limited or oxide lines in the layer formation and thus negative influences due to oxide breakouts and micro-grooving - particularly caused by such oxide breakouts or existing due to a high oxide lineage - are avoided.

Darlegung der Erfindungexplanation of the invention

Die Lösung der Aufgabe erfolgt erfindungsgemäß mit den Merkmalen des unabhängigen Anspruchs 1 und der entsprechenden abhängigen Ansprüche. Weitere praktische Ausführungsformen und Vorteile der Erfindung sind in Verbindung mit den abhängigen Ansprüchen beschrieben.The object is achieved according to the invention with the features of independent claim 1 and the corresponding dependent claims. Further practical embodiments and advantages of the invention are described in connection with the dependent claims.

Gemäß dem erfindungsgemäßen Plasmaspritzverfahren zur Beschichtung einer Zylinderlaufbahn eines Zylinderkurbelgehäuses einer Hubkolbenbrennkraftmaschine wird die Beschichtung zumindest teilweise mit folgender Parameterkombination auf die Zylinderlaufbahn des Zylinderkurbelgehäuses aufgebracht: a) Rotationsgeschwindigkeit: 600 - 700 U/min, b) Spritzgutförderrate: 100 - 120 g/min und c) Vorschubgeschwindigkeit: 24 - 75 mm/s. According to the plasma spraying method according to the invention for coating a cylinder bore of a cylinder crankcase of a reciprocating piston internal combustion engine, the coating is at least partially applied to the cylinder bore of the cylinder crankcase using the following parameter combination: a) rotation speed: 600 - 700 rpm, b) Spray material feed rate: 100 - 120 g/min and c) feed rate: 24 - 75 mm/s.

Mittels ausführlicher empirischer Versuchsreihen und unter Einbeziehung modifizierter Anlagentechnik wurde ermittelt, dass mit dem vorstehend genannten Parameterbereiche, die allesamt gemäß a), b) und c) erfüllt sein müssen, damit die erfindungsgemäßen Vorteile erzielt werden, sich die Bildung von Oxiden verringern und die entstehende Oxidzeiligkeit drastisch reduziert werden kann. Dadurch kann eine besonders homogene Oberfläche erzielt werden, die weitestgehend frei von einer unerwünschten Mikroriefigkeit ist, welche durch eine erhöhte Oxidbildung und eine hohe Oxidzeiligkeit entsteht. Darüber hinaus kann eine hohe Rotationsgeschwindigkeit während des Verfahrens eingesetzt werden und damit die gewünschte Beschichtung in einer kürzeren Zeit aufgebracht werden als mit den bislang aus dem Stand der Technik bekannten Verfahren. Hinsichtlich der Rotationsgeschwindigkeit der Brennertechnik haben sich Werte zwischen 600-700 U/min als optimal herausgestellt. Bevorzugt sind Werte zwischen 630 U/min und 770 U/min, besonders bevorzugt Werte zwischen 640 U/min und 660 U/min. Besonders gute Ergebnisse wurden mit Rotationsgeschwindigkeiten von 650 U/min erzielt.By means of extensive empirical test series and by including modified plant technology, it was determined that with the above-mentioned parameter ranges, all of which must be fulfilled in accordance with a), b) and c) in order to achieve the advantages according to the invention, the formation of oxides can be reduced and the resulting oxide rows can be drastically reduced. This makes it possible to achieve a particularly homogeneous surface that is largely free of undesirable micro-grooving, which is caused by increased oxide formation and high oxide rows. In addition, a high rotation speed can be used during the process and thus the desired coating can be applied in a shorter time than with the processes known to date from the state of the art. With regard to the rotation speed of the burner technology, values between 600-700 rpm have proven to be optimal. Values between 630 rpm and 770 rpm are preferred, values between 640 rpm and 660 rpm are particularly preferred. Particularly good results were achieved with rotation speeds of 650 rpm.

Hinsichtlich der Spritzgutförderrate hat sich der Wertebereich zwischen 100 und 120 g/min als optimal erwiesen. Speziell wird auf den Wert von 110 g/min verwiesen, mit welchem, insbesondere in Verbindung mit der Rotationsgeschwindigkeit von 650 U/min ein qualitativ besonders hochwertiges Ergebnis einer Beschichtung der Zylinderlaufbahn erzielt wurde.With regard to the spray material feed rate, the value range between 100 and 120 g/min has proven to be optimal. Special reference is made to the value of 110 g/min, with which, especially in conjunction with the rotation speed of 650 rpm, a particularly high-quality result for coating the cylinder bore was achieved.

Zu der Vorschubgeschwindigkeit gemäß Merkmal c) wird auf den Wertebereich zwischen 30 und 70 mm/s, weiter bevorzugt auf den Wertebereich zwischen 40 und 65 mm/s und besonders bevorzugt auf den Wertebereich zwischen 50 und 65 mm/s verwiesen. Darüber hinaus wird auf die noch engeren Wertebereiche zwischen 52 und 60 mm/s und weiter bevorzugt zwischen 54 und 58 mm/s verwiesen.With regard to the feed rate according to feature c), reference is made to the value range between 30 and 70 mm/s, more preferably to the value range between 40 and 65 mm/s and particularly preferably to the value range between 50 and 65 mm/s. In addition, reference is made to the even narrower value ranges between 52 and 60 mm/s and more preferably between 54 and 58 mm/s.

In einer praktischen Ausführungsform des erfindungsgemäßen Plasmaspritzverfahrens wird die Beschichtung mittels 5-8 Spritzzyklen jeweils in Form von Doppelhüben aufgebracht. Besonders bevorzugt ist diesbezüglich die Aufbringung mit 6-7 Spritzzyklen zu erwähnen. Es hat sich gezeigt, dass die Dicke und die Struktur einer entsprechenden Beschichtung in Verbindung mit der jeweils benötigten Bearbeitungsdauer in diesem Fall besonders hochwertig und effizient ist.In a practical embodiment of the plasma spraying process according to the invention, the coating is applied using 5-8 spraying cycles, each in the form of double strokes. In this respect, application using 6-7 spraying cycles is particularly preferred. It has been shown that the thickness and structure of a corresponding coating in conjunction with the processing time required in each case is particularly high-quality and efficient in this case.

Als Beschichtung werden vorzugsweise eine Stahlschicht oder eine Keramikschicht aufgebracht. In Bezug auf die Stahlschichten wird insbesondere auf niedriglegierte und hochlegierte Stahlschichten verwiesen, d.h. auf Stahlschichten mit Stählen, bei denen die Summe der Legierungselemente einen Gehalt von 5 Massenprozent nicht überschreitet (niedriglegierte Stähle) bzw. Stähle, bei denen der mittlere Massengehalt mindestens eines Legierungselementes größer gleich 5 % ist (hochlegierte Stähle). Die Verwendung von niedriglegierten Stählen ist gegenüber hochlegierten Stählen bevorzugt. Mit hochlegierten Stählen werden jedoch ebenfalls Ergebnisse erzielt, die gegenüber den aus dem bisherigen Stand der Technik bekannten Ergebnissen vorteilhaft sind.A steel layer or a ceramic layer is preferably applied as a coating. With regard to the steel layers, particular reference is made to low-alloy and high-alloy steel layers, i.e. steel layers with steels in which the sum of the alloying elements does not exceed 5% by mass (low-alloy steels) or steels in which the average mass content of at least one alloying element is greater than or equal to 5% (high-alloy steels). The use of low-alloy steels is preferred over high-alloy steels. However, high-alloy steels also achieve results that are advantageous compared to the results known from the previous state of the art.

In Bezug auf die Aufbringung einer Keramikschicht wird insbesondere auf Schichten aus TitanDioxid (TiO2) verwiesen.With regard to the application of a ceramic layer, particular reference is made to layers made of titanium dioxide (TiO 2 ).

Eine Keramikschicht wird unabhängig von Vorstehendem vorzugsweise in Verbindung mit einem vorherigen Aufrauhungsprozess und dem vorherigen Aufbringen einer haftvermittelnden Schicht aufgebracht. Als haftvermittelnde Schicht kommen insbesondere eine Nickel-Aluminium-Schicht, eine Bronzeschicht oder eine niedrig legierte Stahlschicht in Frage. Die Dicke einer haftvermittelnden Schicht beträgt dabei vorzugsweise weniger als 100 µm, bevorzugt weniger als 60 µm und besonders bevorzugt maximal 40 µm.Regardless of the above, a ceramic layer is preferably applied in conjunction with a previous roughening process and the previous application of an adhesion-promoting layer. A nickel-aluminum layer, a bronze layer or a low-alloy steel layer are particularly suitable as an adhesion-promoting layer. The thickness of an adhesion-promoting layer is preferably less than 100 µm, preferably less than 60 µm and particularly preferably a maximum of 40 µm.

Wenn bei einem erfindungsgemäßen Plasmaspritzverfahren eine Beschichtung in Form einer niedriglegierten Stahlschicht erzielt werden soll, wird diese Beschichtung vorzugsweise mittels eines niedriglegierten Stahlpulvers aufgebracht. Dabei sein Stahlpulver mit einer vorwiegend kugeligen Morphologie mit geringen Anteilen an Satelliten besonders bevorzugt.If a coating in the form of a low-alloy steel layer is to be achieved in a plasma spraying process according to the invention, this coating is preferably applied using a low-alloy steel powder. Steel powder with a predominantly spherical morphology with small proportions of satellites is particularly preferred.

In einer weiteren praktischen Ausführungsform eines erfindungsgemäßen Plasmaspritzverfahrens, bei welchem als Beschichtung eine Stahlschicht aufgebracht wird, wird die Beschichtung mittels eines Stahlpulvers aufgebracht, die weniger als 2 Gew.-% Kohlenstoff (C), weniger als 2 Gew.-% Mangan (Mn), weniger als 2 Gew.-% Chrom (Cr), weniger als 1 Gew.-% Nickel (Ni), weniger als 1 Gew.-% Sauerstoff (O2) und weniger als 1 Gew.-% Stickstoff (N2) aufweist. In Bezug auf den Anteil von Kohlenstoff wird insbesondere auf einen Gew.-%-Anteil von 1,0 bis 1,3 verwiesen. In Bezug auf den Anteil von Mangan wird insbesondere auf einen Anteil von 1,2 bis 1,6 Gew.-% verwiesen. In Bezug auf den Gewichtsanteil von Chrom wird insbesondere auf einen Wertebereich von 1,2 bis 1,6 Gew.-% verwiesen. In Bezug auf den Gewichtsanteil von Nickel wird insbesondere auf den Wertebereich von weniger als 0,5 Gew.-% verwiesen. In Bezug auf den Gewichtsanteil von Sauerstoff wird insbesondere auf Werte von weniger als 0,2 Gew.-% verwiesen und in Bezug auf den Gewichtsanteil von Stickstoff wird insbesondere auf den Wertebereich von weniger als 0,5 Gew.-%. Die vorstehend genannten Wertebereiche gelten vorzugsweise kumulativ, d.h. in dieser Kombination mit einander verknüpft.In a further practical embodiment of a plasma spraying process according to the invention, in which a steel layer is applied as a coating, the coating is applied by means of a steel powder which contains less than 2 wt.% carbon (C), less than 2 wt.% manganese (Mn), less than 2 wt.% chromium (Cr), less than 1 wt.% nickel (Ni), less than 1 wt.% oxygen (O 2 ) and less than 1 wt.% nitrogen (N 2 ). With regard to the proportion of carbon, particular reference is made to a proportion by weight of 1.0 to 1.3. With regard to the proportion of manganese, particular reference is made to a proportion by weight of 1.2 to 1.6. With regard to the proportion by weight of chromium, particular reference is made to a value range of 1.2 to 1.6. With regard to the proportion by weight of nickel, particular reference is made to the value range of less than 0.5. With regard to the proportion by weight of oxygen, particular reference is made to values of less than 0.2. With regard to the proportion by weight of nitrogen, particular reference is made to the value range of less than 0.5. The value ranges mentioned above preferably apply cumulatively, ie linked to one another in this combination.

Eine qualitativ besonders hochwertige Beschichtung ergibt sich, wenn eine Stahlschicht mittels eines Stahlpulvers aufgebracht wird, dessen Korngröße ausschließlich kleiner ist als 60 µm und/oder dessen Korngröße zu einem überwiegenden Teil kleiner als 42 µm ist. Der Anteil in Gewichtsprozent von Stahlpulver mit einer Korngröße von weniger als 42 µm liegt vorzugsweise bei maximal 90 Prozent. Der Anteil mit einer Korngröße von kleiner als 26 µm liegt vorzugweise bei maximal 50 Prozent. Der Anteil mit einer Korngröße von weniger als 16 µm liegt vorzugsweise bei maximal 10 Prozent.A particularly high-quality coating is obtained when a steel layer is applied using a steel powder whose grain size is exclusively smaller than 60 µm and/or whose grain size is predominantly smaller than 42 µm. The proportion in weight percent of steel powder with a grain size of less than 42 µm is preferably a maximum of 90 percent. The proportion with a grain size of less than 26 µm is preferably a maximum of 50 percent. The proportion with a grain size of less than 16 µm is preferably a maximum of 10 percent.

In einer weiteren praktischen Ausführungsform eines erfindungsgemäßen Plasmaspritzverfahrens wird die Beschichtung unter Einfluss der Atmosphäre aufgebracht. In diesem Fall wird das Verfahren auch als atmosphärisches Plasmaspritzverfahren oder APS-Verfahren bezeichnet. Ein Vorteil des APS-Verfahrens ist, dass auf den Einsatz von Schutzgasen und die damit verbundenen zusätzlichen Kosten verzichtet werden kann. Alternativ kann die Beschichtung bei einem erfindungsgemäßen Plasmaspritzverfahren aber auch unter Einsatz eines Schutzgases oder im Vakuum aufgebracht werden. In diesem Fall sind zwar die Kosten zur Durchführung des Verfahrens erhöht, im Einzelfall kann so aber ein qualitativ noch deutlich besseres Ergebnis einer Beschichtung erzielt werden, d.h. insbesondere eine Beschichtung erzielt werden, die einen geringeren Oxidanteil aufweist bzw. eine geringere Oxidzeiligkeit aufweist.In a further practical embodiment of a plasma spraying process according to the invention, the coating is applied under the influence of the atmosphere. In this case, the process is also referred to as an atmospheric plasma spraying process or APS process. One advantage of the APS process is that the use of protective gases and the associated additional costs can be dispensed with. Alternatively, the coating can also be applied using a protective gas or in a vacuum in a plasma spraying process according to the invention. In this case, the costs of carrying out the process are higher, but in individual cases a qualitatively significantly better coating result can be achieved, i.e. in particular a coating can be achieved that has a lower oxide content or has a lower oxide row density.

Das erfindungsgemäße Plasmaspritzverfahren ist insbesondere dann von Vorteil, wenn vor dem Aufbringen der Beschichtung mindestens ein strahlender Aufrauprozess mittels Korund und/oder Wasser, mittels Laserstrahlaufrauen oder mittels Aufrauen mit geometrisch definierter Schneide durchgeführt wird. In diesem Fall verbessert sich die Haftungsfähigkeit der aufzubringenden Beschichtung und gleichzeitig erhöht sich die Dauerhaltbarkeit der erzielten Beschichtung.The plasma spraying process according to the invention is particularly advantageous if, before applying the coating, at least one radiant roughening process is carried out using corundum and/or water, using laser beam roughening or using roughening with a geometrically defined cutting edge. In this case, the adhesion of the coating to be applied and at the same time the durability of the resulting coating is increased.

Weitere praktische Ausführungsformen der Erfindung sind nachfolgend im Zusammenhang mit den Zeichnungen beschrieben.Further practical embodiments of the invention are described below in connection with the drawings.

Kurzbeschreibung der ZeichnungenShort description of the drawings

Es zeigen:

Figur 1:
eine Querschnittsdarstellung eines Ausschnitts einer Zylinderlaufbahn mit einer Beschichtung,
Figur 2:
einen Blick auf eine Oberfläche einer Beschichtung einer Zylinderlaufbahn gemäß Stand der Technik,
Figur 3:
einen Querschnitt durch eine mit einem erfindungsgemäßen Verfahren hergestellte Beschichtung auf einer Zylinderlaufbahn und
Figur 4:
eine vergrößerte Darstellung des Ausschnitts gemäß Figur 3.
They show:
Figure 1:
a cross-sectional view of a section of a cylinder bore with a coating,
Figure 2:
a view of a surface of a cylinder bore coating according to the state of the art,
Figure 3:
a cross section through a coating on a cylinder bore produced by a method according to the invention and
Figure 4:
an enlarged view of the section according to Figure 3 .

Beschreibung bevorzugter AusführungsformenDescription of preferred embodiments

Figur 1 zeigt einen Ausschnitt eines Zylinderkurbelgehäuses einer Hubkolbenbrennkraftmaschine mit einem Ausschnitt einer Zylinderlaufbahn eines Aluminiumgrundkörpers 10 eines Zylinderkurbelgehäuses 14, wobei der Aluminiumgrundkörper 10 mit einer Beschichtung 12 versehen ist und die dem Aluminiumgrundkörper 10 abgewandte Oberfläche 16 Teil der Zylinderlaufbahn 18 des Zylinderkurbelgehäuses 14 ist. Die zum Teil gekennzeichneten schwarzen Bereiche 20 sind Oxide, die sich während des Aufbringens der Beschichtung 12 mittels eines Plasmaspritzverfahrens gebildet haben. Figure 1 shows a section of a cylinder crankcase of a reciprocating piston internal combustion engine with a section of a cylinder bore of an aluminum base body 10 of a cylinder crankcase 14, wherein the aluminum base body 10 is provided with a coating 12 and the surface 16 facing away from the aluminum base body 10 is part of the cylinder bore 18 of the cylinder crankcase 14. The partially marked black areas 20 are oxides that have formed during the application of the coating 12 by means of a plasma spraying process.

Figur 2 zeigt die Oberfläche 16 der Zylinderlaufbahn 18. Wie in der Figur erkennbar ist, haben sich auf der Oberfläche 16 einzelne Oxidzeilen 22a, 22b, 22c, 22d gebildet, die durch schwarze Punkte gebildet sind, die ungefähr ein einer Reihe angeordnet sind. Hierbei handelt es sich um die eingangs erwähnte Oxidzeiligkeit. Figure 2 shows the surface 16 of the cylinder bore 18. As can be seen in the figure, individual oxide lines 22a, 22b, 22c, 22d have formed on the surface 16, which are formed by black dots that are arranged approximately in a row. This is the oxide line structure mentioned at the beginning.

Figur 3 zeigt eine Ansicht analog zu Figur 1, wobei die Beschichtung 12 mittels eines erfindungsgemäßen Plasmaspritzverfahrens aufgebracht wurde. Figure 3 shows a view analogous to Figure 1 , wherein the coating 12 was applied by means of a plasma spraying process according to the invention.

Figur 4 zeigt eine vergrößerte Darstellung der Ansicht aus Figur 3. Wie erkennbar ist, weist die Oberfläche 16, welche die Zylinderlaufbahn 18 des Zylinderkurbelgehäuses 14 bildet, eine deutlich erhöhte Qualität dadurch auf, dass keine Oxidzeiligkeit mehr erkennbar ist. Darüber hinaus ist erkennbar, dass sich in der Beschichtung 12 deutlich weniger Oxide gebildet haben, als bei der Beschichtung 12 gemäß Stand der Technik, welche in Figur 1 dargestellt ist. Figure 4 shows an enlarged view of the Figure 3 . As can be seen, the surface 16, which forms the cylinder bore 18 of the cylinder crankcase 14, has a significantly increased quality in that oxide lines are no longer visible. In addition, it can be seen that significantly fewer oxides have formed in the coating 12 than in the coating 12 according to the prior art, which in Figure 1 is shown.

Bezugszeichenlistelist of reference symbols

1010
Aluminiumgrundkörperaluminum base body
1212
Beschichtungcoating
1414
Zylinderkurbelgehäusecylinder crankcase
1616
Oberflächesurface
1818
Zylinderlaufbahncylinder bore
2020
schwarzer Bereich (Oxid)black area (oxide)
22a-d22a-d
Oxidzeilenoxide lines

Claims (11)

  1. Plasma spraying process for coating a cylinder barrel of a cylinder crankcase of a reciprocating piston internal combustion engine, characterized in that the coating (12) is at least partially applied to the cylinder barrel (18) of the cylinder crankcase (14) using the following parameter combination: a) rotation speed: 600 - 700 revolutions/minute, b) spray material flow rate: 100 - 120 grams/minute and c) feed rate: 24 - 75 mm/s.
  2. Plasma spraying process according to the preceding claim, characterized in that the coating (12) is applied by means of 5 - 8 spray cycles, each in the form of double strokes.
  3. Plasma spraying process according to either of the preceding claims,
    characterized in that a steel layer or a ceramic layer is applied as the coating (12).
  4. Plasma spraying process according to the preceding claim, characterized in that the coating (12) is applied by means of a low-alloy steel powder.
  5. Plasma spraying process according to either of the two preceding claims, characterized in that a steel layer is applied as the coating (12) by means of a steel powder having a predominantly spherical morphology with small proportions of satellites.
  6. Plasma spraying process according to any of the three preceding claims, characterized in that a steel layer is applied as the coating (12) by means of a steel powder which comprises less than 2 wt.% carbon (C), less than 2 wt.% manganese (Mn), less than 2 wt.% chromium (Cr), less than 1 wt.% nickel (Ni), less than 1 wt.% oxygen (O2) and less than 1 wt.% nitrogen (N2).
  7. Plasma spraying process according to any of the four preceding claims, characterized in that a steel layer is applied by means of a steel powder of which the particle size is exclusively smaller than 60 µm and/or predominantly smaller than 42 µm.
  8. Plasma spraying process according to any of the preceding claims,
    characterized in that the coating (12) is applied under the influence of the atmosphere.
  9. Plasma spraying process according to any of the preceding claims,
    characterized in that the coating (12) is applied using a protective gas or in a vacuum.
  10. Plasma spraying process according to any of the preceding claims,
    characterized in that, before applying the coating (12), at least one blasting abrasion process is carried out by means of corundum and/or water, by means of laser beam abrasion or by means of abrasion with a geometrically defined cutting edge.
  11. Plasma spraying process according to any of the preceding claims, characterized in that the feed rate is 52 - 60 mm/s.
EP19176247.5A 2018-05-29 2019-05-23 Plasma spray method for coating a cylinder a cylinder liner of a cylinder crankcase of a reciprocating piston combustion engine Active EP3575435B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102018208435.1A DE102018208435A1 (en) 2018-05-29 2018-05-29 Plasma spraying method for coating a cylinder bore of a cylinder crankcase of a reciprocating internal combustion engine

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EP3575435A1 EP3575435A1 (en) 2019-12-04
EP3575435B1 true EP3575435B1 (en) 2025-02-26

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EP (1) EP3575435B1 (en)
CN (1) CN110607495B (en)
DE (1) DE102018208435A1 (en)
RU (1) RU2723491C1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10941766B2 (en) * 2019-06-10 2021-03-09 Halliburton Energy Sendees, Inc. Multi-layer coating for plunger and/or packing sleeve
HUE067596T2 (en) * 2020-04-16 2024-10-28 Sturm Maschinen & Anlagenbau Gmbh Installation and method for producing a metallic coating on a borehole wall
CN112746272A (en) * 2020-12-28 2021-05-04 洛阳清科激光技术有限公司 Engine cylinder sleeve strengthening method

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US9885311B2 (en) * 2011-11-22 2018-02-06 Nissan Motor Co., Ltd. Method for manufacturing cylinder block and cylinder block

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US4976948A (en) * 1989-09-29 1990-12-11 Gte Products Corporation Process for producing free-flowing chromium oxide powders having a low free chromium content
RU2165995C1 (en) * 1999-10-05 2001-04-27 Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" Highly string aluminium-based alloy and product made of said alloy
RU2245388C1 (en) * 2003-12-19 2005-01-27 Государственное образовательное учреждение высшего профессионального образования "Московский государственный институт стали и сплавов" (технологический университет) Aluminum-based material
FR2872172B1 (en) * 2004-06-25 2007-04-27 Pechiney Rhenalu Sa ALUMINUM ALLOY PRODUCTS WITH HIGH TENACITY AND HIGH FATIGUE RESISTANCE
DE102008053642A1 (en) * 2008-10-29 2010-05-06 Daimler Ag Thermally sprayed cylinder liner for a combustion engine, is made of iron based alloy, steel, stainless steel and/or light metal based on aluminum, titanium and/or magnesium
RU2478132C1 (en) * 2012-01-23 2013-03-27 Федеральное государственное автономное образовательное учреждение высшего профессионального образования "Национальный исследовательский технологический университет "МИСиС" High-strength alloy based on aluminium with calcium addition
BR112018074291B1 (en) 2016-05-27 2022-08-23 Oerlikon Metco Ag, Wohlen COATING PROCESS, THERMAL COATING, AS WELL AS CYLINDER WITH A THERMAL COATING

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US9885311B2 (en) * 2011-11-22 2018-02-06 Nissan Motor Co., Ltd. Method for manufacturing cylinder block and cylinder block

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Publication number Publication date
EP3575435A1 (en) 2019-12-04
DE102018208435A1 (en) 2019-12-05
CN110607495A (en) 2019-12-24
US20190368023A1 (en) 2019-12-05
RU2723491C1 (en) 2020-06-11
CN110607495B (en) 2022-03-25

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