EP2279279B1 - Method for preparing a surface for applying a thermally sprayed layer - Google Patents

Method for preparing a surface for applying a thermally sprayed layer Download PDF

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Publication number
EP2279279B1
EP2279279B1 EP09735658.8A EP09735658A EP2279279B1 EP 2279279 B1 EP2279279 B1 EP 2279279B1 EP 09735658 A EP09735658 A EP 09735658A EP 2279279 B1 EP2279279 B1 EP 2279279B1
Authority
EP
European Patent Office
Prior art keywords
brush
groove
wires
percussion
process according
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP09735658.8A
Other languages
German (de)
French (fr)
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EP2279279A1 (en
Inventor
Clemens Maria Verpoort
Mark Silk
Spencer Lindon
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Ford Global Technologies LLC
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Ford Global Technologies LLC
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Publication of EP2279279A1 publication Critical patent/EP2279279A1/en
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Classifications

    • 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
    • AHUMAN NECESSITIES
    • A46BRUSHWARE
    • A46BBRUSHES
    • A46B3/00Brushes characterised by the way in which the bristles are fixed or joined in or on the brush body or carrier
    • A46B3/08Brushes characterised by the way in which the bristles are fixed or joined in or on the brush body or carrier by clamping
    • AHUMAN NECESSITIES
    • A46BRUSHWARE
    • A46BBRUSHES
    • A46B7/00Bristle carriers arranged in the brush body
    • A46B7/06Bristle carriers arranged in the brush body movably during use, i.e. the normal brushing action causing movement
    • AHUMAN NECESSITIES
    • A46BRUSHWARE
    • A46BBRUSHES
    • A46B7/00Bristle carriers arranged in the brush body
    • A46B7/06Bristle carriers arranged in the brush body movably during use, i.e. the normal brushing action causing movement
    • A46B7/10Bristle carriers arranged in the brush body movably during use, i.e. the normal brushing action causing movement as a rotating cylinder
    • AHUMAN NECESSITIES
    • A46BRUSHWARE
    • A46BBRUSHES
    • A46B9/00Arrangements of the bristles in the brush body
    • A46B9/02Position or arrangement of bristles in relation to surface of the brush body, e.g. inclined, in rows, in groups
    • AHUMAN NECESSITIES
    • A46BRUSHWARE
    • A46BBRUSHES
    • A46B9/00Arrangements of the bristles in the brush body
    • A46B9/08Supports or guides for bristles
    • A46B9/12Non-adjustable supports
    • AHUMAN NECESSITIES
    • A46BRUSHWARE
    • A46BBRUSHES
    • A46B2200/00Brushes characterized by their functions, uses or applications
    • A46B2200/30Brushes for cleaning or polishing
    • A46B2200/3093Brush with abrasive properties, e.g. wire bristles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/45Scale remover or preventor
    • Y10T29/4506Scale remover or preventor for hollow workpiece
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/47Burnishing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12201Width or thickness variation or marginal cuts repeating longitudinally
    • Y10T428/12208Variation in both width and thickness

Definitions

  • the invention relates to a method for preparing a surface on a workpiece made of metal for applying a thermally sprayed layer according to the preamble of claim 1, a hammer or impact brush for performing the method and a workpiece produced by this method.
  • a known method is also the preparation of the surface by sandblasting with corundum particles and subsequent cleaning before the surface coating can be applied by means of thermal spraying.
  • a significant disadvantage of sand blasting with corundum particles is, in particular, that the smallest corundum particles can penetrate into the surface to be coated and remain there despite intensive cleaning.
  • Such jet particles can significantly affect the adhesive tensile strength of the coating on the previously cleaned surface after application of the surface coating.
  • particles of the blasting material can also adhere to surface areas of the workpiece to be coated, which are not coated and therefore have not previously been irradiated.
  • Such blasting material particles can lead to significant problems when using the workpiece. This can for example be done on the cylinder surfaces of engines that have been processed in this form. Corundum particles that are left in or on the engine components can thus lead to significant problems and may cause a failure of the engine under certain circumstances.
  • the US 53633821 describes a method for preparing a surface on workpieces made of metal for the application of a thermally sprayed layer.
  • the surface is roughened either by wire brushing or by rough mechanical processing to a certain surface roughness.
  • DE 10 2006 004769 A1 discloses a method for preparing a previously mechanically roughened surface having sharp-edged ridges and depressions on metal workpieces for applying a thermally sprayed layer, wherein the ridge edges are fractured to improve adhesiveness of the subsequently applied thermally sprayed layer and / or to form undercuts be at least partially bent, characterized in that the sharp-edged ridges and depressions of the mechanically roughened surface resulting from machining are grooves.
  • the impact wires impinge parallel to the grooves, an advantageous shape of the undercuts is generated because the material of the groove webs thereby predominantly flows transversely to the grooves and thus a favorable shape of the undercuts is produced.
  • the impact wires have a direction of movement which is predominantly parallel to the groove direction. This is z.
  • the axis of rotation of the brush is oriented predominantly parallel to the surface and predominantly transverse to the groove direction.
  • the grooves are formed as grooves in z. B. turning, drilling or milling the surface, z. B. in the mechanical machining of cylinder bores. Equivalently, the grooves can also be introduced by rolling or pressing. For the purposes of this application, all methods are suitable to produce the mechanically roughened surface having a corresponding groove structure in the Bring in the surface.
  • the grooves advantageously have a trapezoidal to rectangular cross section.
  • the necessary undercuts form very simple when the impact strikes striking in parallel deform the edges and ridges of the groove webs transversely to the groove direction.
  • a rectangular cross-section only slight deformations of the groove web transverse to the groove direction are required to form the undercuts.
  • trapezoidal cross-section is advantageous that this is easy to produce, and still can be produced by the impact brushes, the necessary undercuts.
  • the impact wires have a diameter which is greater than the groove width.
  • the groove width is the mean distance between the groove webs.
  • the impact wires can never hit the bottom of the grooves, which would theoretically be possible in the parallel brushing, but will always impinge on at least one groove web to produce the undercut there.
  • the impact wires may also have a diameter which corresponds at least once to the groove spacing, preferably two to three times the groove spacing. Such impact wires will definitely hit a groove web, but can also hit two grooved webs. Due to the relatively large diameter relative to the groove spacing, a wide undercut is formed, since a large area of a groove web is plastically deformed.
  • the groove distance is to be understood as the distance from the center of the groove to the middle of the groove or from the center of the groove center to the groove bridge center.
  • the ratio of groove depth to groove width is between 0.2 and 1, preferably between 0.5 and 0.7.
  • the groove depth is understood to mean the average distance from the surface of the groove web to the bottom of the groove.
  • the grooves can easily be introduced into the surface at these proportions and yet have enough depth to effect a sufficient clamping of the sprayed layer to be applied with the undercuts produced. Too deep grooves could not be filled by the spray material, with too shallow grooves, the undercuts would be ineffective, since the spray material would not get behind it.
  • the ratio of groove spacing to groove width is between 1.2 and 4, preferably between 1.8 and 2.2.
  • the groove spacing is the average groove width plus the average width of the groove webs.
  • groove lands and the grooves have similar widths.
  • the widths can then be chosen so that on the one hand a good filling of the grooves is granted with the spray material, on the other hand, the width of the groove web is sufficient to firmly bind the sprayed layer to the base material.
  • the groove spacing is between 0.1 mm and 1 mm, preferably between 0.15 mm and 0.25 mm.
  • the resulting grooves and grooved ridges are easy to manufacture, can be formed with the impact wires favorable for the undercuts, can be filled well with the spray material and have sufficient strength to hold the sprayed layer.
  • the combined hammer-brushing process also produces residual compressive stresses in the machined surface areas, increasing the fatigue strength of the various components.
  • the hammer or impact brush impact or torsion springs are provided with diffusion hard chromium plating containing about 53% chromium in the surface of the wires, corresponding to a Vickers hardness HV of about 1800, so that the life of the brush is so great as possible, and to avoid any contamination of steel with aluminum beams, which could otherwise lead to galvanic corrosion problems.
  • the surface treatment in particular in the repair of engine blocks, takes place only in the area of the worn cylinder running surfaces and the honed cylinder surfaces still present above and / or below remain unprocessed. This avoids adhesion problems for the coating which would otherwise be too thin Coating in the honed surface areas can often occur.
  • the areas to be coated can be processed very well without damaging or roughening the adjacent honed cylinder surface.
  • a thermally sprayed layer can be applied only in the area of the worn cylinder surface, which adheres very well to the engine block by the surface treatment with the brush.
  • the inventive method is suitable for preparing a thermal sprayed coating produced by the PTWA wire-plasma spraying process.
  • the claimed method is used to prepare a previously mechanically roughened surface on a workpiece 1 made of metal by brushing for the application of a thermally sprayed layer. It is characterized in that the surface 2 to be processed on the workpiece 1 by hammer or impact brushes with a rotating hammer or impact brush 3 is processed with a plurality of radially outwardly directed impact wires 4 such that the edges of the ridges for improvement the adhesion of the subsequently applied thermally sprayed layer broken or at least partially bent to form undercuts.
  • the brush 3 rotates at a high speed of about 3000 to 6000 revolutions per minute and is in the machining process with its axis of rotation 13 in such a constant parallel distance relative to the surface 2 of the workpiece 1 so laterally displaced that over the circumference of the brush.
  • 3 distributed Impact wires 4 abruptly impinge with their ends 5 at an oblique angle of less than 90 ° in rapid succession on adjacent surface areas on the workpiece 1.
  • the freely rotatably mounted on the brush body 7 in the direction of rotation 6 Impact wires 4 when hitting the workpiece resiliently and slide with their ends 5 along the surface to be machined to immediately lifted from the surface due to the resilient deflection and in the Continued rotation of the brush 3 against the direction of rotation 6 to be thrown back and then to return by centrifugal action in their radial orientation for a renewed surface contact.
  • the impact wires 4 of the brush have a length such that they are pulled in the rapid rotation of the brush after its sudden impact on the surface to be machined 2 at this in the direction of rotation 6 of the brush 3 a piece along, then with the further rotation of the brush from the working surface lift again and thus stop the impact.
  • the brush 3 consists of a substantially cylindrical rotationally symmetrical brush body 7 with a plurality of axially parallel support rods 11 which are clamped over the circumference of the brush between the front side brush discs 9, 10 and a plurality of axially in the axial direction of the brush 3 next to each other arranged impact wires (4) wear.
  • the rotating at high speed hammer or impact brush 3 is in the embodiment of Fig. 1 to Fig. 8 from a substantially cylindrical rotationally symmetrical brush body 7 with a plurality of axially parallel longitudinal grooves 8 in which between the front side brush discs 9, 10 each axially parallel support rods 11 (FIGS. Fig. 1, Fig. 2 and Fig. 9 ) are clamped for a plurality of in the axial direction of the brush closely juxtaposed impact wires 4.
  • the hammer or impact brush 3 shown has on the brush body 7 six evenly distributed over the circumference longitudinal grooves 8 with six support rods 11, where the punch wires 4 are freely rotatably mounted.
  • the legs 4a, 4b of the percussion wires 4 each have the same length, and the supporting rods 11 have a round cross-section, so that the percussion wires 4 can move freely on the support rods 11 in the direction of rotation 6 of the brush back and forth.
  • the punch wires 4 with two parallel spaced legs 4a, 4b U-shaped, so that they enclose the support rod 11 with an annular eye 4c.
  • the impact wires 4 of the brush 3 are hard-ingrained with about 53% Cr on the wire surface and a Vickers hardness HV of at least 1800.
  • the receptacles 12 are formed for the ends of the support rods 11 on at least one brush disc 9 or 10 by means of adjustable bearing bushes 14 radially adjustable to the rotational axis 13 of the brush 3.
  • the brush body 7 with brush discs 9, 10, Support rods 11, impact wires 4 and brush shaft 15 suitably made of a high-strength stainless steel.
  • a hammer or impact brush of Fig. 11 to 14 are the percussion wires 4 as leg springs formed in the axial direction of the support rods 11 closely adjacent parallel legs 4a, 4b and enclose the support rods 11 also with an annular eye 4c. When hitting the surface to be machined 2 they are bent and then spring back in the direction of a counter to the direction of rotation 6 following adjacent support rod 11.
  • the brush body 7 consists in this embodiment of two attached to the brush shaft 15 brush discs 9, 10, where the support rods 11 for the percussion wires or torsion springs (4) are fixed with its two ends in about the circumference of the brush body 7 also uniformly distributed receptacles 12 , Again, the receptacles 12 may be adjustable for the ends of the support rods 11 on at least one brush disc 9 or 10 by means of adjustable bearing bushes 14 radially to the axis of rotation 13 of the brush.
  • the brush body 7 with brush discs 9, 10, support rods 11, impact wires or torsion springs 4 and brush shaft 15 made of a high-strength stainless steel.
  • the materials used for the brush have the same quality as brushes Fig. 1 to Fig. 10 ,
  • FIG. 2 shows a cross section through an inventive surface 2 of a workpiece 1, which is provided with a spray layer 16, transversely to the grooves 17.
  • the grooves 17 are defined at regular intervals by the groove webs 18.
  • the grooves 17 are defined by their mean groove width B, their mean groove spacing A, the mean width S of the groove webs 18, the mean groove depth T and the mean groove web height H, the groove spacing A is the sum of groove width B and width S of the groove webs 18 and the groove depth T is equal to the groove web height H.
  • “Middle" width or depth or height should mean here that a is formed by the cross-sectional area of a groove 17 and a groove web 18 respectively expressed by two average values.
  • the undercuts 22 are formed in the grooves 17.
  • the sprayed layer 16 is clamped together at these undercuts 22 and is thus firmly connected to the workpiece 1. It can be seen that the plastic deformations 20 occur transversely to the grooves 17 irregularly. This also applies in the longitudinal direction to the grooves 17, where the plastic deformations 20 are introduced into the groove structure more or less frequently, depending on the intensity of the brushing. Overall, this surface structure with the irregular undercuts 22 leads to a very high adhesive strength of the sprayed layer 16 on the workpiece 1.
  • the grooves 17 have approximately a groove width B of 0.2 mm, a groove spacing A of 0.5 mm, so that a width S of the groove webs 18 of 0.3 mm and a groove depth S or groove web height H of 0.09 mm up.
  • This macroscopic structure applied in a first process step has a size in the preferred magnitudes for these processes of 0.1-1 mm in width and about 0.05-0.2 mm in depth.
  • the introduced in the second process step by the brush plastic deformation 20 have microscopic dimensions of about 5 - 50 microns on the surface 19 of the groove webs 18.
  • the plastically deformed surface 19 of the groove webs 18, similar to a shot peened surface, has a layer provided with residual compressive stresses.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
  • Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
  • Coating By Spraying Or Casting (AREA)

Description

Die Erfindung betrifft ein Verfahren zum Vorbereiten einer Oberfläche an einem Werkstück aus Metall für das Aufbringen einer thermisch gespritzten Schicht nach dem Oberbegriff des Anspruchs 1, eine Hammer- oder Schlagbürste zum Durchführen des Verfahrens sowie ein Werkstück hergestellt nach diesem Verfahren.The invention relates to a method for preparing a surface on a workpiece made of metal for applying a thermally sprayed layer according to the preamble of claim 1, a hammer or impact brush for performing the method and a workpiece produced by this method.

Oberflächen an Werkstücken aus Metall für eine Beschichtung durch thermisches Spritzen müssen bekanntlich entsprechend vorbereitet werden. Dies kann durch Aufrauhen der Oberfläche geschehen. Hierfür werden verschiedene Verfahren industriell eingesetzt, wie Sandstrahlen, Hochdruck-Wasserstrahlen, Bürsten, Fräsen und ähnliche Bearbeitungsverfahren. Mit diesen Bearbeitungsverfahren sind jedoch Probleme verbunden. So können Späne und Rückstände von den Bearbeitungsprozessen in Rillen und Nuten an den bearbeiteten Oberflächen verbleiben und zu Problemen führen, wenn sie von der Beschichtung überdeckt und eingeschlossen werden und diese Schicht anschließend gehont worden ist. Die Rillen und Nuten, die durch mechanisches Aufrauhen erzeugt worden sind, haben eine Tiefe von ca. 100 µm. Dieser Bereich ist eben und glatt, so dass die thermisch gespritzte Schicht an diesen Stellen nicht gut haften kann.Surfaces on workpieces made of metal for a coating by thermal spraying must be prepared accordingly. This can be done by roughening the surface. For this purpose, various methods are used industrially, such as sandblasting, high-pressure water jets, brushing, milling and similar machining processes. However, there are problems associated with these processing methods. Thus, chips and debris from the machining processes may remain in grooves and grooves on the machined surfaces and cause problems when they are covered and trapped by the coating and this layer has subsequently been honed. The grooves and grooves created by mechanical roughening have a depth of about 100 μm. This area is flat and smooth, so that the thermally sprayed layer can not adhere well at these locations.

In Fällen, in denen ein Motor bei Servicearbeiten mittels thermischen Spritzens repariert werden muss, ist es erforderlich, eine innen liegende Verschleißzone innerhalb der Zylinderbohrung zu bearbeiten, wobei oberhalb und unterhalb dieser Zone ein Bereich mit der ursprünglichen glatten Oberflächenstruktur, die beispielsweise gehont ist, verbleibt. Wenn eine solche Zylinderbohrung mittels thermischen Spritzens repariert wird, kann die Beschichtung an der gehonten Oberfläche nicht anhaften. Besonders für Motorblöcke aus Aluminiumlegierung mit eingegossenen Zylinderlaufbuchsen ist eine Reparatur mittels thermischen Spritzens schwierig wegen der die Zylinderlaufbuchse übergreifenden Aluminiumlippe und des Zwischenbereiches von der Aluminiumlippe zu dem zu beschichtenden Oberflächenbereich an der Zylinderlaufbuchse. - Das mechanische Aufrauhen führt zu Dehnungs-Restspannungen, die die Ermüdungsfestigkeit des Werkstückes reduzieren.In cases where a motor needs to be repaired during service by thermal spraying, it is necessary to machine an internal wear zone within the cylinder bore, leaving above and below this zone an area with the original smooth surface structure, for example honed , When such a cylinder bore is repaired by thermal spraying, the coating can not adhere to the honed surface. Especially for engine blocks made of aluminum alloy with cast-in cylinder liners is a repair by means of thermal spraying difficult because of the cylinder lip cross-aluminum lip and the intermediate region of the aluminum lip to be coated surface area at the cylinder liner. - Mechanical roughening leads to residual strain stresses which reduce the fatigue strength of the workpiece.

Ein bekanntes Verfahren ist auch die Vorbereitung der Oberfläche durch Sandstrahlen mit Korundpartikeln und anschließender Reinigung, bevor die Oberflächenbeschichtung mittels des thermischen Spritzens aufgetragen werden kann. Neben dem vergleichsweise aufwendigen Verfahrensschritt der Oberflächenreinigung besteht ein wesentlicher Nachteil des Sandstrahlens mit Korundpartikeln insbesondere darin, dass kleinste Korundteilchen in die zu beschichtende Oberfläche eindringen und dort trotz intensiver Reinigung verbleiben können. Solche Strahlpartikel können nach dem Aufbringen der Oberflächenbeschichtung die Haftzugfestigkeit der Beschichtung an der zuvor gereinigten Oberfläche erheblich beeinträchtigen.A known method is also the preparation of the surface by sandblasting with corundum particles and subsequent cleaning before the surface coating can be applied by means of thermal spraying. In addition to the comparatively complicated process step of surface cleaning, a significant disadvantage of sand blasting with corundum particles is, in particular, that the smallest corundum particles can penetrate into the surface to be coated and remain there despite intensive cleaning. Such jet particles can significantly affect the adhesive tensile strength of the coating on the previously cleaned surface after application of the surface coating.

Außerdem können Partikel des Strahlgutes auch noch an Oberflächenbereichen des zu beschichtenden Werkstückes anhaften, die nicht beschichtet werden und dementsprechend auch zuvor nicht bestrahlt worden sind. Solche Strahlgutpartikel können beim Einsatz des Werkstückes zu erheblichen Problemen führen. Dies kann beispielsweise an den Zylinderlaufflächen von Motoren geschehen, die in dieser Form bearbeitet worden sind. Korundpartikel, die in oder an den Motorbauteilen verblieben sind, können so zu erheblichen Problemen führen und unter Umständen ein Versagen des Motors herbeiführen.In addition, particles of the blasting material can also adhere to surface areas of the workpiece to be coated, which are not coated and therefore have not previously been irradiated. Such blasting material particles can lead to significant problems when using the workpiece. This can for example be done on the cylinder surfaces of engines that have been processed in this form. Corundum particles that are left in or on the engine components can thus lead to significant problems and may cause a failure of the engine under certain circumstances.

Um hier Abhilfe zu schaffen, ist aus DE 198 40 117 A1 ein Verfahren zur spanabhebenden Oberflächenbearbeitung der Innenseite von Hohlkörpern als Vorbereitung zum Aufbringen einer thermisch gespritzten Schicht bekannt, wobei ein Teil des die Innenseite der Hohlkörper bildenden Materials abgetragen und eine Oberfläche mit einer definierten Struktur und/oder Güte erzeugt wird. Dieses bekannte Verfahren weist jedoch den Nachteil auf, dass damit keine Oberflächenprofile erzeugt werden können, die einen Sägezahneffekt und damit Hinterschnitte aufweisen. Da derartige Oberflächenstrukturen jedoch entscheidende Vorteile bei der Haftzugfestigkeit der thermisch aufgebrachten Beschichtung ermöglichen, stellt dies einen entscheidenden Nachteil dar. Durch das spanabhebende Verfahren kann außerdem keine Konstanz hinsichtlich der Oberflächenwerte erzielt werden, da die Bearbeitungswerkzeuge einem notwendigen Verschleiß unterliegen und somit auch eine mit dem Verschleiß des Werkstücks variierende Oberflächenstruktur erzeugen. Außerdem wird die mechanische Festigkeit der durch dieses Verfahren vorbereiteten Oberfläche durch das Spanabheben nachteilig beeinflusst.To remedy this situation is out DE 198 40 117 A1 a method for machining the surface of the inside of hollow bodies in preparation for applying a thermally sprayed layer, wherein a part of the material forming the inside of the hollow body is removed and a surface having a defined structure and / or quality is produced. However, this known method has the disadvantage that no Surface profiles can be generated, which have a sawtooth effect and thus undercuts. However, since such surface structures allow decisive advantages in the adhesive tensile strength of the thermally applied coating, this represents a decisive disadvantage. In addition, no consistency in terms of surface values can be achieved by the machining process, since the machining tools are subject to a necessary wear and thus also to wear produce varying surface texture of the workpiece. In addition, the mechanical strength of the surface prepared by this method is adversely affected by chip removal.

In DE 27 12 863 A1 ist weiterhin ein Schlagwerkzeug zum Abtragen von Oberflächen beschrieben, das an einem Ende ein Bündel von metallischen Abtragsnadeln trägt, die in ihrer Längsrichtung oszillieren und so in schneller Folge gegen eine Oberfläche schlagen können. Üblicherweise werden derartige Nadelgeräte eingesetzt, um Rost oder Lacke von Oberflächen zu entfernen. Aber auch bei der Reinigung von Betonbauteilen werden derartige Nadelgeräte verwendet.In DE 27 12 863 A1 Furthermore, a striking tool for removing surfaces is described, which carries at one end a bunch of metallic Abtragsnadeln that oscillate in their longitudinal direction and can beat in rapid succession against a surface. Usually, such needle devices are used to remove rust or varnish from surfaces. But also in the cleaning of concrete components such needle devices are used.

Die US 53633821 beschreibt ein Verfahren zum Vorbereiten einer Oberfläche an Werkstücken aus Metall für das Aufbringen einer thermisch gespritzten Schicht. Dabei wird die Oberfläche entweder durch Drahtbürsten oder durch grobes mechanisches Bearbeiten auf eine bestimmte Rauhtiefe aufgerauht. Durch diese Bearbeitung entstehen jedoch nur wenig Hinterschnitte, die für die Haftzugfestigkeit der thermisch gespritzten Schicht notwendig sind.The US 53633821 describes a method for preparing a surface on workpieces made of metal for the application of a thermally sprayed layer. The surface is roughened either by wire brushing or by rough mechanical processing to a certain surface roughness. However, only a few undercuts, which are necessary for the adhesive tensile strength of the thermally sprayed layer, result from this processing.

In der JP 2006 097045 A ist ein weiteres Verfahren zum Aufrauhen einer Oberfläche als Vorbereitung für eine thermische Beschichtung beschrieben. In eine Zylinderlaufbahn werden in einem ersten Arbeitsschritt durch ein rundes, mehrstufiges Räumwerkzeug in Richtung der Zylinderachse eine Vielzahl von Längsrillen eingebracht. In einem zweiten Arbeitsschritt werden die Spitzen der Längsrillen durch eine parallel zur Zylinderachse rotierende Drahtbürste abgetragen. Dabei entsteht eine Oberfläche, die Längsrillen und zwischen den Längsrillen in Umfangsrichtung des Zylinders gebürstete Umfangsriefenriefen aufweist. Dabei weisen die gebürsteten Umfangsriefen eine wesentlich geringere Rautiefe als die geräumten Längsrillen. Durch dieses Verfahren entstehen jedoch keine Hinterschnitte in der Oberfläche, die für eine gute Haftung der thermisch gespritzten Schicht notwendig sind.In the JP 2006 097045 A Another method for roughening a surface in preparation for a thermal coating is described. In a cylinder bore a plurality of longitudinal grooves are introduced in a first step by a round, multi-stage broach in the direction of the cylinder axis. In a second step, the tips of the longitudinal grooves are removed by a wire brush rotating parallel to the cylinder axis. This results in a surface having longitudinal grooves and between the longitudinal grooves in the circumferential direction of the cylinder brushed Umfangsriefenriefen. The brushed Umfangsriefen have a much lower roughness than the cleared longitudinal grooves. By this method, however, no undercuts in the surface, which are necessary for a good adhesion of the thermally sprayed layer.

DE 10 2006 004769 A1 offenbart ein Verfahren zum Vorbereiten einer zuvor mechanisch aufgerauhten Oberfläche mit scharfkantigen Graten und Vertiefungen an Werkstücken aus Metall für das Aufbringen einer thermisch gespritzten Schicht, wobei die Kanten der Grate zur Verbesserung der Haftfähigkeit der anschließend aufgebrachten thermisch gespritzten Schicht gebrochen und/oder unter Bildung von Hinterschnitten zumindest teilweise umgebogen werden, dadurch gekennzeichnet, dass die scharfkantigen Grate und Vertiefungen der mechanisch aufgerauhten Oberfläche durch mechanische Bearbeitung entstandene Rillen sind. DE 10 2006 004769 A1 discloses a method for preparing a previously mechanically roughened surface having sharp-edged ridges and depressions on metal workpieces for applying a thermally sprayed layer, wherein the ridge edges are fractured to improve adhesiveness of the subsequently applied thermally sprayed layer and / or to form undercuts be at least partially bent, characterized in that the sharp-edged ridges and depressions of the mechanically roughened surface resulting from machining are grooves.

Der Erfindung liegt die Aufgabe zugrunde, die vorstehend beschriebenen Probleme beim Vorbereiten einer Oberfläche an einem Werkstück aus Metall für das Aufbringen einer thermisch gespritzten Schicht in einem bestimmten Oberflächenbereich zu beseitigen.It is an object of the present invention to overcome the above-described problems in preparing a surface on a metal workpiece for applying a thermally sprayed layer in a particular surface area.

Gelöst wird diese Aufgabe mit den Merkmalen des Anspruchs 1. Die Kombination von mechanischem Aufrauhen und Bürsten führt im Vergleich zum herkömmlichen Bürsten zu einer Oberflächenstruktur mit Eigenschaften, die sehr ähnlich mit einem Sand- oder Korundstrahlen oder einem Kugelstrahlen, also einem Beschuss mit Schrot oder einem anderen geeigneten Strahlgut ist. Die Bürste rotiert bei diesem Verfahren mit einer sehr hohen Drehzahl von etwa 3000 bis 6000 Umdrehungen pro Minute, wodurch die Schlagdrähte eine hohe örtliche Energie auf die Oberfläche des Werkstückes übertragen. Dies führt zu einer plastischen Verformung und einer erhöhten Rauhigkeit nur in dem bearbeiteten Oberflächenbereich des Werkstückes, wobei die scharfkantigen Grate an der aufgerauhten Oberfläche zur Verbesserung der Haftfähigkeit der anschließend aufgebrachten thermisch gespritzten Schicht gebrochen oder unter Bildung von Hinterschnitten zumindest teilweise umgebogen werden. Dabei werden auch Späne und Rückstände von den bearbeiteten Oberflächenbereichen mit entfernt, was eine weiter verbesserte Haftfähigkeit und somit eine erhöhte Oberflächenfestigkeit der gespritzten Beschichtung zur Folge hat.This object is achieved with the features of claim 1. The combination of mechanical roughening and brushing leads in comparison to conventional brushing to a surface structure with properties that are very similar to a Sand or corundum or shot peening, so a bombardment with shot or other suitable blasting material is. The brush rotates in this process at a very high speed of about 3000 to 6000 revolutions per minute, whereby the impact wires transmit a high local energy to the surface of the workpiece. This leads to a plastic deformation and an increased roughness only in the machined surface area of the workpiece, wherein the sharp-edged ridges on the roughened surface to improve the adhesion of the subsequently applied thermally sprayed layer broken or at least partially bent to form undercuts. It also chips and residues from the machined surface areas are removed, which has a further improved adhesion and thus increased surface strength of the sprayed coating result.

Dies ist insbesondere dann der Fall, wenn die scharfkantigen Grate und Vertiefungen der mechanisch aufgerauhten Oberfläche durch mechanische Bearbeitung entstandene Rillen sind und die Schlagdrähte überwiegend parallel zu den Rillen auftreffen. Durch das Auftreffen eines Schlagdrahtes auf die Oberfläche eines Rillensteges, der zwischen den Rillen gebildet ist, wird kinetische Energie übertragen, die zu einer plastischen Verformung der Oberfläche des Rillensteges führt, wodurch das Material des Rillensteges in den Bereich zumindest einer der beiseitigen Rillen fließt. Dies kann auch als eine örtlich begrenzte Bördelung des Rillensteges in Richtung der Rille betrachtet werden, wodurch der für die Erhöhung der Haftfestigkeit benötigte Hinterschnitt entsteht.This is especially the case when the sharp-edged ridges and depressions of the mechanically roughened surface are formed by mechanical processing grooves and impingement wires predominantly parallel to the grooves. The impact of a striking wire on the surface of a groove web formed between the grooves transmits kinetic energy, which results in plastic deformation of the surface of the groove land, whereby the material of the groove land flows into the area of at least one of the side grooves. This can also be considered as a localized curling of the groove web in the direction of the groove, whereby the undercut required for increasing the adhesion strength arises.

Indem die Schlagdrähte parallel zu den Rillen auftreffen, wird eine vorteilhafte Form der Hinterschnitte erzeugt, da das Material der Rillenstege dadurch überwiegend quer zu den Rillen fließt und damit eine günstige Form der Hinterschnitte erzeugt wird. Als überwiegend parallel ist hier zu verstehen, daß die Schlagdrähte eine Bewegungsrichtung aufweisen, die überwiegend parallel zur Rillenrichtung ist. Dies ist z. B. der Fall, wenn bei einer rotierenden Bürste die Drehachse der Bürste überwiegend parallel zur Oberfläche und überwiegend quer zur Rillenrichtung ausgerichtet ist.By the impact wires impinge parallel to the grooves, an advantageous shape of the undercuts is generated because the material of the groove webs thereby predominantly flows transversely to the grooves and thus a favorable shape of the undercuts is produced. As a predominantly parallel is to be understood here that the impact wires have a direction of movement which is predominantly parallel to the groove direction. This is z. As is the case when in a rotating brush, the axis of rotation of the brush is oriented predominantly parallel to the surface and predominantly transverse to the groove direction.

Die Rillen entstehen als Nuten beim z. B. Drehen, Bohren oder Fräsen der Oberfläche, z. B. bei der mechanischen Bearbeitung von Zylinderbohrungen. Äquivalent können die Rillen auch durch Walzen oder Pressen eingebracht werden. Im Sinne dieser Anmeldung sind alle Verfahren geeignet, die mechanisch aufgerauhte Oberfläche zu erzeugen, die eine entsprechende Rillenstruktur in die Oberfläche einbringen.The grooves are formed as grooves in z. B. turning, drilling or milling the surface, z. B. in the mechanical machining of cylinder bores. Equivalently, the grooves can also be introduced by rolling or pressing. For the purposes of this application, all methods are suitable to produce the mechanically roughened surface having a corresponding groove structure in the Bring in the surface.

Vorteilhaft weisen die Rillen vorteilhaft einen trapezförmig bis rechteckigen Querschnitt auf. Bei dieser Querschnittsform bilden sich die erforderlichen Hinterschnitte sehr einfach, wenn die parallel auftreffenden Schlagdrähte die Kanten und Grate der Rillenstege quer zur Rillenrichtung verformen. Insbesondere bei einem rechteckigen Querschnitt sind nur geringe Verformungen des Rillensteges quer zur Rillenrichtung erforderlich, um die Hinterschnitte zu bilden. Beim trapezförmigen Querschnitt ist vorteilhaft, daß dieser einfach zu erzeugen ist, und trotzdem können durch das Schlagbürsten die erforderlichen Hinterschnitte erzeugt werden.Advantageously, the grooves advantageously have a trapezoidal to rectangular cross section. In this cross-sectional shape, the necessary undercuts form very simple when the impact strikes striking in parallel deform the edges and ridges of the groove webs transversely to the groove direction. Especially with a rectangular cross-section only slight deformations of the groove web transverse to the groove direction are required to form the undercuts. When trapezoidal cross-section is advantageous that this is easy to produce, and still can be produced by the impact brushes, the necessary undercuts.

Vorteilhaft weisen die Schlagdrähte einen Durchmesser auf, der größer als die Rillenbreite ist. Als Rillenbreite ist dabei der mittlere Abstand zwischen den Rillenstegen zu betrachten. In diesem Fall können die Schlagdrähte nie auf den Grund der Rillen auftreffen, was bei dem parallelen Bürsten theoretisch möglich wäre, sondern werden immer auf zumindest einen Rillensteg auftreffen, um dort den Hinterschnitt zu erzeugen.Advantageously, the impact wires have a diameter which is greater than the groove width. The groove width is the mean distance between the groove webs. In this case, the impact wires can never hit the bottom of the grooves, which would theoretically be possible in the parallel brushing, but will always impinge on at least one groove web to produce the undercut there.

Dabei können die Schlagdrähte auch einen Durchmesser aufweisen, der mindestens einmal dem Rillenabstand entspricht, bevorzugt zwei- bis dreimal dem Rillenabstand. Derartige Schlagdrähte werden auf jeden Fall einen Rillensteg treffen, können aber auch zwei Rillenstege treffen. Durch den relativ großen Durchmesser relativ zum Rillenabstand bildet sich ein breiter Hinterschnitt aus, da ein großer Bereich eines Rillensteges plastisch verformt wird. Als Rillenabstand ist der Abstand von Rillenmitte zu Rillenmitte bzw. von Rillstegmitte zu Rillenstegmitte zu verstehen.The impact wires may also have a diameter which corresponds at least once to the groove spacing, preferably two to three times the groove spacing. Such impact wires will definitely hit a groove web, but can also hit two grooved webs. Due to the relatively large diameter relative to the groove spacing, a wide undercut is formed, since a large area of a groove web is plastically deformed. The groove distance is to be understood as the distance from the center of the groove to the middle of the groove or from the center of the groove center to the groove bridge center.

Vorteilhaft beträgt das Verhältnis Rillentiefe zu Rillenbreite zwischen 0,2 und 1, bevorzugt zwischen 0,5 und 0,7. Als Rillentiefe wird die mittlere Entfernung von der Oberfläche des Rillensteges zum Boden der Rille verstanden. Die Rillen können bei diesen Proportionen leicht in die Oberfläche eingebracht werden und weisen dennoch genug Tiefe aus, um mit den erzeugten Hinterschnitten eine ausreichende Verklammerung der aufzubringenden Spritzschicht zu bewirken. Zu tiefe Rillen könnten nicht vom Spritzmaterial gefüllt werden, bei zu flachen Rillen wären die Hinterschnitte wirkungslos, da das Spritzmaterial nicht dahinter gelangen würde.Advantageously, the ratio of groove depth to groove width is between 0.2 and 1, preferably between 0.5 and 0.7. The groove depth is understood to mean the average distance from the surface of the groove web to the bottom of the groove. The grooves can easily be introduced into the surface at these proportions and yet have enough depth to effect a sufficient clamping of the sprayed layer to be applied with the undercuts produced. Too deep grooves could not be filled by the spray material, with too shallow grooves, the undercuts would be ineffective, since the spray material would not get behind it.

Vorteilhaft beträgt das Verhältnis Rillenabstand zu Rillenbreite zwischen 1,2 und 4, bevorzugt zwischen 1,8 und 2,2. Dabei ist der Rillenabstand die mittlere Rillenbreite plus die mittlere Breite der Rillenstege. Somit weisen Rillenstege und die Rillen ähnliche Breiten auf. Die Breiten können dann so gewählt werden, daß sich zum einen eine gute Füllung der Rillen mit dem Spritzmaterial gewährt ist, zum anderen die Breite des Rillensteges ausreichend ist, um die Spritzschicht fest an das Grundmaterial zu binden.Advantageously, the ratio of groove spacing to groove width is between 1.2 and 4, preferably between 1.8 and 2.2. The groove spacing is the average groove width plus the average width of the groove webs. Thus, groove lands and the grooves have similar widths. The widths can then be chosen so that on the one hand a good filling of the grooves is granted with the spray material, on the other hand, the width of the groove web is sufficient to firmly bind the sprayed layer to the base material.

Vorteilhaft beträgt der Rillenabstand zwischen 0,1 mm und 1 mm, bevorzugt zwischen 0,15 mm und 0,25 mm. Die daraus resultierenden Rillen und Rillenstege sind einfach herzustellen, lassen sich mit den Schlagdrähten günstig für die Hinterschnitte umformen, können gut mit dem Spritzmaterial gefüllt werden und weisen eine ausreichende Festigkeit auf, um die Spritzschicht zu halten.Advantageously, the groove spacing is between 0.1 mm and 1 mm, preferably between 0.15 mm and 0.25 mm. The resulting grooves and grooved ridges are easy to manufacture, can be formed with the impact wires favorable for the undercuts, can be filled well with the spray material and have sufficient strength to hold the sprayed layer.

Das kombinierte Hammer-Bürstverfahren erzeugt auch Rest-Druckspannungen in den bearbeiteten Oberflächenbereichen, wodurch die Ermüdungsfestigkeit der verschiedenen Komponenten erhöht wird. Zur Verbesserung der Bearbeitungsgüte und der Dauerfestigkeit sind die Schlagdrähte oder Schenkelfedern der Hammer- oder Schlagbürste mit einer Diffusions-Hartinchromierung mit etwa 53 % Chrom in der Oberfläche der Drähte versehen, entsprechend einer Vickershärte HV von etwa 1800, so dass die Lebensdauer der Bürste so groß wie möglich ist und jegliche Verunreinigung von Stahl mit Aluminiumträgern, die sonst zu galvanischen Korrosionsproblemen führen könnten, vermieden wird.The combined hammer-brushing process also produces residual compressive stresses in the machined surface areas, increasing the fatigue strength of the various components. To improve the quality of workmanship and fatigue strength, the hammer or impact brush impact or torsion springs are provided with diffusion hard chromium plating containing about 53% chromium in the surface of the wires, corresponding to a Vickers hardness HV of about 1800, so that the life of the brush is so great as possible, and to avoid any contamination of steel with aluminum beams, which could otherwise lead to galvanic corrosion problems.

Besonders vorteilhaft ist es auch, wenn die Oberflächenbearbeitung insbesondere bei der Reparatur von Motorblöcken nur im Bereich der verschlissenen Zylinderlaufflächen erfolgt und die oberhalb und/oder unterhalb davon noch vorhandenen gehonten Zylinderflächen unbearbeitet bleiben. Hierdurch werden Haftungsprobleme für die Beschichtung vermieden, die sonst bei einer zu dünnen Beschichtung in den gehonten Oberflächenbereichen häufig auftreten können. Mittels des erfinderischen Verfahrens lassen sich die zu beschichtenden Bereiche sehr gut bearbeiten, ohne die angrenzende, gehonte Zylinderfläche zu beschädigen bzw. mit aufzurauhen.It is also particularly advantageous if the surface treatment, in particular in the repair of engine blocks, takes place only in the area of the worn cylinder running surfaces and the honed cylinder surfaces still present above and / or below remain unprocessed. This avoids adhesion problems for the coating which would otherwise be too thin Coating in the honed surface areas can often occur. By means of the inventive method, the areas to be coated can be processed very well without damaging or roughening the adjacent honed cylinder surface.

Damit läßt sich nur im Bereich der verschlissenen Zylinderlauffläche eine thermisch gespritzten Schicht aufbringen, die durch die Oberflächenbearbeitung mit der Schlagbürste eine sehr gut auf Motorblock haftet. Insbesondere eignet sich das erfinderische Verfahren zur Vorbereitung einer thermischen Spritzschicht, die durch das PTWA Draht-Plasma Spritzverfahren hergestellt ist.Thus, a thermally sprayed layer can be applied only in the area of the worn cylinder surface, which adheres very well to the engine block by the surface treatment with the brush. In particular, the inventive method is suitable for preparing a thermal sprayed coating produced by the PTWA wire-plasma spraying process.

Bevorzugte Ausführungsbeispiele einer Hammer- oder Schlagbürste zum Durchführen des Verfahrens gemäß der Erfindung sind in der Zeichnung schematisch dargestellt. Es zeigen:

Fig. 1
den Einsatz einer Hammer- oder Schlagbürste bei der Bearbeitung von Zylinderlaufbuchsen an Verbrennungsmotoren,
Fig. 2
eine derartige Bürste in perspektivischer Seitenansicht,
Fig. 3 und Fig. 3a
den Bürstenkörper einer derartigen Bürste in Seitenansicht mit zugehöriger Stirnansicht,
Fig. 4 und Fig. 4a
eine gegenüber Fig. 3 und Fig. 3a vergrößerte teilweise Seitenansicht des Bürstenkörpers mit zugehöriger Stirnansicht,
Fig. 5 und Fig. 5a
eine teilweise Seitenansicht des Bürstenkörpers mit einer Schnittdarstellung gemäß Schnittlinie V - V von Fig. 5,
Fig. 6 und Fig. 6a
eine Stirnansicht einer endseitigen Bürstenscheibe gemäß den vorherigen Darstellungen mit einer Schnittdarstellung gemäß Schnittlinie VI - VI von Fig. 6,
Fig. 7 und Fig. 7a
eine Seitenansicht des Bürstenkörpers mit Bürstenwelle und einer mit dem Bürstenkörper verschweißten Bürstenscheibe sowie eine zugehörige Stirnansicht,
Fig. 8
eine Seitenansicht des kompletten Bürstenkörpers mit Bürstenwelle und verschweißter Bürstenscheibe,
Fig. 9
eine weitere Ausführungsform einer Hammer- oder Schlagbürste mit einem abgewandelten Bürstenkörper in perspektivischer Ansicht,
Fig. 10
in einem vergrößerten Ausschnitt X von Fig. 9 die Ausbildung und die Arbeitsweise der Schlagdrähte von solchen Bürsten beim Bearbeiten von Oberflächen an Werkstücken nach dem erfindungsgemäßen Verfahren, während in
Fig. 11
eine weitere Ausführungsform einer Hammer- oder Schlagbürste nach Fig. 9 mit geänderten Schlagdrähten in Form von Schenkelfedern gezeigt ist, von denen eine Schenkelfeder in
Fig. 12
in perspektivischer Darstellung und in
Fig. 13 und Fig. 14
jeweils in zwei zugehörigen Längsseitenansichten wiedergegeben ist; und
Fig. 15
einen Querschnitt durch eine mit einer Spritzschicht versehenen erfinderischen Oberfläche.
Preferred embodiments of a hammer or impact brush for carrying out the method according to the invention are shown schematically in the drawing. Show it:
Fig. 1
the use of a hammer or impact brush when machining cylinder liners on internal combustion engines,
Fig. 2
Such a brush in a perspective side view,
Fig. 3 and Fig. 3a
the brush body of such a brush in side view with associated front view,
Fig. 4 and Fig. 4a
one opposite Fig. 3 and Fig. 3a enlarged partial side view of the brush body with associated front view,
Fig. 5 and Fig. 5a
a partial side view of the brush body with a sectional view along section line V - V of Fig. 5 .
Fig. 6 and Fig. 6a
an end view of an end brush disc according to the previous representations with a sectional view along section line VI - VI of Fig. 6 .
Fig. 7 and Fig. 7a
a side view of the brush body with brush shaft and a welded to the brush body brush disc and an associated end view,
Fig. 8
a side view of the complete brush body with brush shaft and welded brush disc,
Fig. 9
a further embodiment of a hammer or impact brush with a modified brush body in perspective view,
Fig. 10
in an enlarged section X of Fig. 9 the formation and operation of the impact wires of such brushes when machining surfaces on workpieces according to the inventive method, while in
Fig. 11
another embodiment of a hammer or impact brush after Fig. 9 is shown with modified impact wires in the form of torsion springs, one leg of which in
Fig. 12
in perspective and in
FIGS. 13 and 14
each reproduced in two associated longitudinal side views; and
Fig. 15
a cross section through an inventive surface provided with a sprayed layer.

Das beanspruchte Verfahren dient zum Vorbereiten einer zuvor mechanisch aufgerauhten Oberfläche an einem Werkstück 1 aus Metall durch Bürsten für das Aufbringen einer thermisch gespritzten Schicht. Es zeichnet sich dadurch aus, dass die zu bearbeitende Oberfläche 2 an dem Werkstück 1 durch Hammer- oder Schlagbürsten mit einer rotierenden Hammer- oder Schlagbürste 3 mit einer Vielzahl von radial nach außen gerichteten Schlagdrähten 4 derart bearbeitet wird, dass die Kanten der Grate zur Verbesserung der Haftfähigkeit der anschließend aufgebrachten thermisch gespritzten Schicht gebrochen oder unter Bildung von Hinterschnitten zumindest teilweise umgebogen werden. Die Bürste 3 rotiert mit einer hohen Drehzahl von etwa 3000 bis 6000 Umdrehungen pro Minute und wird bei dem Bearbeitungsvorgang mit ihrer Drehachse 13 in einem solchen gleichbleibenden parallelen Abstand gegenüber der Oberfläche 2 des Werkstückes 1 derart seitlich verlagert, dass die über den Umfang der Bürste 3 verteilten Schlagdrähte 4 mit ihren Enden 5 in einem schrägen Winkel von weniger als 90° in schneller Aufeinanderfolge auf nebeneinander liegende Oberflächenbereiche an dem Werkstück 1 schlagartig auftreffen.The claimed method is used to prepare a previously mechanically roughened surface on a workpiece 1 made of metal by brushing for the application of a thermally sprayed layer. It is characterized in that the surface 2 to be processed on the workpiece 1 by hammer or impact brushes with a rotating hammer or impact brush 3 is processed with a plurality of radially outwardly directed impact wires 4 such that the edges of the ridges for improvement the adhesion of the subsequently applied thermally sprayed layer broken or at least partially bent to form undercuts. The brush 3 rotates at a high speed of about 3000 to 6000 revolutions per minute and is in the machining process with its axis of rotation 13 in such a constant parallel distance relative to the surface 2 of the workpiece 1 so laterally displaced that over the circumference of the brush. 3 distributed Impact wires 4 abruptly impinge with their ends 5 at an oblique angle of less than 90 ° in rapid succession on adjacent surface areas on the workpiece 1.

Wie in Fig. 10 und Fig. 11 gezeigt ist, werden die am Bürstenkörper 7 in Drehrichtung 6 frei drehbar gelagerten Schlagdrähte 4 beim Auftreffen auf das Werkstück federnd durchgebogen und gleiten mit ihren Enden 5 an der zu bearbeitenden Oberfläche entlang, um unmittelbar darauf infolge der federnden Durchbiegung von der Oberfläche abgehoben und bei der Weiterdrehung der Bürste 3 entgegen der Drehrichtung 6 zurückgeschleudert zu werden und anschließend durch Fliehkraftwirkung wieder in ihre radiale Ausrichtung für einen erneuten Oberflächenkontakt zurück zu gelangen.As in Fig. 10 and Fig. 11 is shown, the freely rotatably mounted on the brush body 7 in the direction of rotation 6 Impact wires 4 when hitting the workpiece resiliently and slide with their ends 5 along the surface to be machined to immediately lifted from the surface due to the resilient deflection and in the Continued rotation of the brush 3 against the direction of rotation 6 to be thrown back and then to return by centrifugal action in their radial orientation for a renewed surface contact.

Wie in Fig. 10 und Fig. 11 ebenfalls zu erkennen ist, haben die Schlagdrähte 4 der Bürste eine solche Länge, dass sie bei der schnellen Rotation der Bürste nach ihrem schlagartigen Auftreffen auf die zu bearbeitende Oberfläche 2 an dieser in Drehrichtung 6 der Bürste 3 ein Stück entlang gezogen werden, um anschließend mit der Weiterdrehung der Bürste von der Bearbeitungsfläche wieder abzuheben und damit die Schlagwirkung zu beenden.As in Fig. 10 and Fig. 11 can also be seen, the impact wires 4 of the brush have a length such that they are pulled in the rapid rotation of the brush after its sudden impact on the surface to be machined 2 at this in the direction of rotation 6 of the brush 3 a piece along, then with the further rotation of the brush from the working surface lift again and thus stop the impact.

Bei allen gezeigten Ausführungsformen besteht die Bürste 3 aus einem im wesentlichen zylindrischen rotationssymmetrischen Bürstenkörper 7 mit einer Vielzahl von achsparallelen Tragstangen 11, die über den Umfang der Bürste zwischen stirnseitigen Bürstenscheiben 9, 10 eingespannt sind und jeweils eine Vielzahl von in Achsrichtung der Bürste 3 eng nebeneinander angeordneten Schlagdrähten (4) tragen.In all the embodiments shown, the brush 3 consists of a substantially cylindrical rotationally symmetrical brush body 7 with a plurality of axially parallel support rods 11 which are clamped over the circumference of the brush between the front side brush discs 9, 10 and a plurality of axially in the axial direction of the brush 3 next to each other arranged impact wires (4) wear.

Die mit hoher Drehzahl rotierende Hammer- oder Schlagbürste 3 besteht in der Ausführungsform von Fig. 1 bis Fig. 8 aus einem im wesentlichen zylindrischen rotationssymmetrischen Bürstenkörper 7 mit einer Vielzahl von achsparallelen Längsnuten 8, in denen zwischen stirnseitigen Bürstenscheiben 9, 10 jeweils achsparallele Tragstangen 11 (Fig. 1, Fig. 2 und Fig. 9) für eine Vielzahl von in Achsrichtung der Bürste eng nebeneinander angeordneten Schlagdrähten 4 eingespannt sind. Die gezeigte Hammer- oder Schlagbürste 3 hat am Bürstenkörper 7 sechs über den Umfang gleichmäßig verteilte Längsnuten 8 mit ebenfalls sechs Tragstangen 11, an denen die Schlagdrähte 4 frei drehbar gelagert sind. Die Schenkel 4a, 4b der Schlagdrähte 4 haben jeweils gleiche Länge, und die Tragstangen 11 haben einen runden Querschnitt, so dass sich die Schlagdrähte 4 an den Tragstangen 11 in Drehrichtung 6 der Bürste frei hin und her bewegen können. Bei dem Ausführungsbeispiel von Fig. 9 und Fig. 10 sind die Schlagdrähte 4 mit zwei im Abstand parallelen Schenkeln 4a, 4b U-förmig ausgebildet, so dass sie die Tragstange 11 mit einem ringförmigen Auge 4c umschließen. Die Schlagdrähte 4 der Bürste 3 sind hartinchromiert mit etwa 53 % Cr an der Drahtoberfläche und einer Vickershärte HV von mindestens 1800.The rotating at high speed hammer or impact brush 3 is in the embodiment of Fig. 1 to Fig. 8 from a substantially cylindrical rotationally symmetrical brush body 7 with a plurality of axially parallel longitudinal grooves 8 in which between the front side brush discs 9, 10 each axially parallel support rods 11 (FIGS. Fig. 1, Fig. 2 and Fig. 9 ) are clamped for a plurality of in the axial direction of the brush closely juxtaposed impact wires 4. The hammer or impact brush 3 shown has on the brush body 7 six evenly distributed over the circumference longitudinal grooves 8 with six support rods 11, where the punch wires 4 are freely rotatably mounted. The legs 4a, 4b of the percussion wires 4 each have the same length, and the supporting rods 11 have a round cross-section, so that the percussion wires 4 can move freely on the support rods 11 in the direction of rotation 6 of the brush back and forth. In the embodiment of FIGS. 9 and 10 are the punch wires 4 with two parallel spaced legs 4a, 4b U-shaped, so that they enclose the support rod 11 with an annular eye 4c. The impact wires 4 of the brush 3 are hard-ingrained with about 53% Cr on the wire surface and a Vickers hardness HV of at least 1800.

Wie in Fig. 5 und Fig. 5a außerdem gezeigt ist, sind die Aufnahmen 12 für die Enden der Tragstangen 11 an mindestens einer Bürstenscheibe 9 oder 10 mittels verstellbarer Lagerbuchsen 14 radial zur Drehachse 13 der Bürste 3 einstellbar ausgebildet. Außerdem besteht der Bürstenkörper 7 mit Bürstenscheiben 9, 10, Tragstangen 11, Schlagdrähten 4 und Bürstenwelle 15 zweckmäßig aus einem hochfesten nichtrostenden Edelstahl.As in Fig. 5 and Fig. 5a is also shown, the receptacles 12 are formed for the ends of the support rods 11 on at least one brush disc 9 or 10 by means of adjustable bearing bushes 14 radially adjustable to the rotational axis 13 of the brush 3. In addition, the brush body 7 with brush discs 9, 10, Support rods 11, impact wires 4 and brush shaft 15 suitably made of a high-strength stainless steel.

Bei dem weiteren Ausführungsbeispiel einer Hammer- oder Schlagbürste von Fig. 11 bis 14 sind die Schlagdrähte 4 als Schenkelfedern mit in Achsrichtung der Tragstangen 11 eng nebeneinanderliegenden parallelen Schenkeln 4a, 4b ausgebildet und umschließen die Tragstangen 11 ebenfalls mit einem ringförmigen Auge 4c. Beim Auftreffen auf die zu bearbeitende Oberfläche 2 werden sie durchgebogen und federn anschließend in Richtung auf eine entgegen der Drehrichtung 6 folgende benachbarte Tragstange 11 zurück.In the further embodiment of a hammer or impact brush of Fig. 11 to 14 are the percussion wires 4 as leg springs formed in the axial direction of the support rods 11 closely adjacent parallel legs 4a, 4b and enclose the support rods 11 also with an annular eye 4c. When hitting the surface to be machined 2 they are bent and then spring back in the direction of a counter to the direction of rotation 6 following adjacent support rod 11.

Der Bürstenkörper 7 besteht bei diesem Ausführungsbeispiel aus zwei an der Bürstenwelle 15 befestigten Bürstenscheiben 9, 10, an denen die Tragstangen 11 für die Schlagdrähte oder Schenkelfedern (4) mit ihren beiden Enden in über den Umfang des Bürstenkörpers 7 ebenfalls gleichmäßig verteilten Aufnahmen 12 befestigt sind. Auch hierbei können die Aufnahmen 12 für die Enden der Tragstangen 11 an mindestens einer Bürstenscheibe 9 oder 10 mittels verstellbarer Lagerbuchsen 14 radial zur Drehachse 13 der Bürste einstellbar sein. Ebenso besteht der Bürstenkörper 7 mit Bürstenscheiben 9, 10, Tragstangen 11, Schlagdrähten oder Schenkelfedern 4 und Bürstenwelle 15 aus einem hochfesten nichtrostenden Edelstahl. Im übrigen haben die für die Bürste verwendeten Werkstoffe die gleiche Qualität wie bei Bürsten nach Fig. 1 bis Fig. 10.The brush body 7 consists in this embodiment of two attached to the brush shaft 15 brush discs 9, 10, where the support rods 11 for the percussion wires or torsion springs (4) are fixed with its two ends in about the circumference of the brush body 7 also uniformly distributed receptacles 12 , Again, the receptacles 12 may be adjustable for the ends of the support rods 11 on at least one brush disc 9 or 10 by means of adjustable bearing bushes 14 radially to the axis of rotation 13 of the brush. Likewise, the brush body 7 with brush discs 9, 10, support rods 11, impact wires or torsion springs 4 and brush shaft 15 made of a high-strength stainless steel. Moreover, the materials used for the brush have the same quality as brushes Fig. 1 to Fig. 10 ,

In Figur 15 ist ein Querschnitt durch eine mit einer Spritzschicht 16 versehene erfinderischen Oberfläche 2 eines Werkstücks 1 quer zu den Rillen 17 dargestellt. Zwischen den Rillen 17 befinden sich in regelmäßigen Abständen die Rillenstege 18. Die Rillen 17 sind definiert durch ihre mittlere Rillenbreite B, ihren mittleren Rillenabstand A, die mittlere Breite S der Rillenstege 18, die mittlere Rillentiefe T und die mittlere Rillensteghöhe H, wobei der Rillenabstand A der Summe von Rillenbreite B und Breite S der Rillenstege 18 entspricht und die Rillentiefe T gleich der Rillensteghöhe H ist. "Mittlere" Breite bzw. Tiefe oder Höhe soll hier heißen, daß ein ungefährer Mittelwert gebildet wird, indem die Querschnittsfläche einer Rille 17 bzw. eines Rillensteges 18 jeweils durch zwei mittlere Werte ausgedrückt werden.In FIG. 15 FIG. 2 shows a cross section through an inventive surface 2 of a workpiece 1, which is provided with a spray layer 16, transversely to the grooves 17. The grooves 17 are defined at regular intervals by the groove webs 18. The grooves 17 are defined by their mean groove width B, their mean groove spacing A, the mean width S of the groove webs 18, the mean groove depth T and the mean groove web height H, the groove spacing A is the sum of groove width B and width S of the groove webs 18 and the groove depth T is equal to the groove web height H. "Middle" width or depth or height should mean here that a is formed by the cross-sectional area of a groove 17 and a groove web 18 respectively expressed by two average values.

Auf den Oberflächen 19 der Rillenstege 18 sind die durch das Schlagbürsten entstandenen plastischen Ausformungen 20 der Rillenkanten 21 zu sehen, wodurch die Hinterschnitte 22 in den Rillen 17 gebildet werden. Nachdem die Rillen 17 durch die Spritzschicht 16a ausgefüllt sind, verklammert sich die Spritzschicht 16 insgesamt an diesen Hinterschnitten 22 und ist somit mit dem Werkstück 1 fest verbunden. Es ist erkennbar, daß die plastischen Verformungen 20 quer zu den Rillen 17 unregelmäßig auftreten. Dies gilt auch in Längsrichtung zu den Rillen 17, wo die plastischen Verformungen 20 je nach Intensität des Bürstens mehr oder weniger häufiger in die Rillenstruktur eingebracht sind. Diese Oberflächestruktur mit den unregelmäßigen Hinterschnitten 22 führt insgesamt zu einer sehr hohen Haftfestigkeit der Spritzschicht 16 auf dem Werkstück 1.On the surfaces 19 of the groove webs 18, the formed by the brush brushing plastic formations 20 of the groove edges 21 can be seen, whereby the undercuts 22 are formed in the grooves 17. After the grooves 17 are filled by the sprayed layer 16 a, the sprayed layer 16 is clamped together at these undercuts 22 and is thus firmly connected to the workpiece 1. It can be seen that the plastic deformations 20 occur transversely to the grooves 17 irregularly. This also applies in the longitudinal direction to the grooves 17, where the plastic deformations 20 are introduced into the groove structure more or less frequently, depending on the intensity of the brushing. Overall, this surface structure with the irregular undercuts 22 leads to a very high adhesive strength of the sprayed layer 16 on the workpiece 1.

Wie aus der Größenangabe in Figur 15 zu entnehmen, weisen die Rillen 17 etwa eine Rillenbreite B von 0,2 mm, einen Rillenabstand A von 0,5 mm, damit eine Breite S der Rillenstege 18 von 0,3 mm und eine Rillentiefe S bzw. Rillensteghöhe H von 0,09 mm auf. Diese in einem ersten Prozeßschritt aufgebrachte makroskopische Struktur weist eine Größe in der bevorzugten Größenordnungen für diese Verfahren von 0,1 - 1 mm in der Breite und etwa 0,05 - 0.2 mm in der Tiefe aus.As from the size in FIG. 15 can be seen, the grooves 17 have approximately a groove width B of 0.2 mm, a groove spacing A of 0.5 mm, so that a width S of the groove webs 18 of 0.3 mm and a groove depth S or groove web height H of 0.09 mm up. This macroscopic structure applied in a first process step has a size in the preferred magnitudes for these processes of 0.1-1 mm in width and about 0.05-0.2 mm in depth.

Die im zweiten Prozeßschritt durch das Bürsten eingeführten plastischen Verformungen 20 weisen mikroskopische Abmessungen von etwa 5 - 50 µm an der Oberfläche 19 der Rillenstege 18 auf. Die plastisch umgeformte Oberfläche 19 der Rillenstege 18 weist ähnlich wie eine kugelgestrahlte Oberfläche eine mit Druckeigenspannungen versehene Schicht auf.The introduced in the second process step by the brush plastic deformation 20 have microscopic dimensions of about 5 - 50 microns on the surface 19 of the groove webs 18. The plastically deformed surface 19 of the groove webs 18, similar to a shot peened surface, has a layer provided with residual compressive stresses.

BEZUGSZEICHENLISTELIST OF REFERENCE NUMBERS

11
Werkstückworkpiece
22
Oberflächesurface
33
Hammer- oder SchlagbürsteHammer or impact brush
44
Schlagdrähte - SchenkelfederImpact Wires - Thigh Spring
4a4a
Schenkel der als Schenkelfeder ausgebildeten SchlagdrähteLegs of trained as a leg spring percussion wires
4b4b
Schenkel der als Schenkelfeder ausgebildeten SchlagdrähteLegs of trained as a leg spring percussion wires
4c4c
ringförmiges Auge der Schlagdrähte bzw. Schenkelfedernannular eye of the percussion wires or torsion springs
55
Enden der Schlagdrähte 4Ends of the punch wires 4
66
Drehrichtung der BürsteDirection of rotation of the brush
77
Bürstenkörperbrush body
88th
Längsnutenlongitudinal grooves
99
Bürstenscheibebrush disc
1010
Bürstenscheibebrush disc
1111
Tragstangen - AchsenSupport rods - axles
1212
Aufnahmen für die Tragstangen 11Shooting for the support rods 11
1313
Drehachseaxis of rotation
1414
Lagerbuchsenbushings
1515
Bürstenwellebrush shaft
1616
Spritzschichtspray layer
16a16a
Spritzschicht in einer RilleSprayed layer in a groove
1717
Rillengrooves
1818
Rillenstegegrooved ridges
1919
Oberflächen der RillenstegeSurfaces of the grooved webs
2020
Plastische Ausformung einer Rillenkante 21Plastic shaping of a grooved edge 21
2121
Rillenkantegroove edge
2222
Hinterschnitteundercuts

Claims (9)

  1. Process for preparing a previously mechanically roughened surface (2) having sharp-edged burrs and depressions on metal workpieces (1) for the application of a thermally sprayed layer, the roughened surface (2) being machined by hammer or percussion brushing using a rapidly rotating hammer or percussion brush (3) having a multiplicity of radially outwardly oriented, resilient percussion wires (4), in such a manner that the edges of the burrs are broken in order to improve the adhesion of the subsequently applied thermally sprayed layer and/or are at least partially bent over to form undercuts (22),
    where
    the sharp-edged burrs and depressions on the mechanically roughened surface (2) are grooves (17) formed by machining, and the percussion wires (4) impinge predominantly parallel to the grooves (17).
  2. Process according to Claim 1,
    characterized in that
    the grooves (17) have a trapezoidal to rectangular cross section.
  3. Process according to Claim 1 or 2,
    characterized in that
    the diameter of the percussion wires (4) is greater than the groove width (B).
  4. Process according to one of the preceding claims,
    characterized in that
    the diameter of the percussion wires (4) corresponds to at least one times the groove spacing (A), preferably two to three times the groove spacing (A).
  5. Process according to one of the preceding claims,
    characterized in that
    the ratio of groove depth (T) to groove width (B) is between 0.2 and 1, preferably between 0.5 and 0.7.
  6. Process according to one of the preceding claims,
    characterized in that
    the ratio of groove spacing (A) to groove width (B) is between 1.2 and 4, preferably between 1.8 and 2.2.
  7. Process according to one of the preceding claims,
    characterized in that
    the groove spacing (A) is between 0.1 mm and 1 mm, preferably between 0.15 mm and 0.25 mm.
  8. Process according to one of the preceding claims,
    characterized in that
    the brush (3) rotates at a high rotational speed of about 3000 to 6000 revolutions per minute and is displaced laterally with the axis of rotation (13) thereof at such a constant parallel distance in relation to the surface (2) of the workpiece (1), and in such a manner, that the ends (5) of the percussion wires (4) distributed over the circumference of the brush (3) impinge on adjacent surface regions on the workpiece (1) in bursts at an oblique angle of less than 90° in quick succession.
  9. Process according to one of the preceding claims,
    characterized in that
    the percussion wires (4) mounted so as to be freely rotatable in the direction of rotation (6) of the brush (3) are bent resiliently when they impinge on the workpiece, slide along the surface to be machined with the ends (5) thereof, are then immediately lifted off from the surface owing to the resilient bending and, when the brush (3) continues to rotate, are thrown back counter to the direction of rotation (6), in order to then return to their radial orientation for renewed surface contact as a result of the effect of centrifugal force.
EP09735658.8A 2008-04-21 2009-04-20 Method for preparing a surface for applying a thermally sprayed layer Not-in-force EP2279279B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008019933A DE102008019933A1 (en) 2008-04-21 2008-04-21 Apparatus and method for preparing a metal surface for applying a thermally sprayed layer
PCT/EP2009/054670 WO2009130184A1 (en) 2008-04-21 2009-04-20 Method for preparing a surface for applying a thermally sprayed layer

Publications (2)

Publication Number Publication Date
EP2279279A1 EP2279279A1 (en) 2011-02-02
EP2279279B1 true EP2279279B1 (en) 2017-06-14

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EP (1) EP2279279B1 (en)
CN (1) CN102016098A (en)
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WO (1) WO2009130184A1 (en)

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EP2279279A1 (en) 2011-02-02
US8752256B2 (en) 2014-06-17
DE102008019933A1 (en) 2009-10-22
WO2009130184A1 (en) 2009-10-29
CN102016098A (en) 2011-04-13
US20110030663A1 (en) 2011-02-10

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