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WO1996033837A1 - Procede permettant de preparer la surface d'une piece comportant un materiau support metallique, et piece munie d'un materiau support metallique - Google Patents

Procede permettant de preparer la surface d'une piece comportant un materiau support metallique, et piece munie d'un materiau support metallique Download PDF

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Publication number
WO1996033837A1
WO1996033837A1 PCT/CH1996/000131 CH9600131W WO9633837A1 WO 1996033837 A1 WO1996033837 A1 WO 1996033837A1 CH 9600131 W CH9600131 W CH 9600131W WO 9633837 A1 WO9633837 A1 WO 9633837A1
Authority
WO
WIPO (PCT)
Prior art keywords
workpiece
depressions
carrier material
metal substrate
substrate material
Prior art date
Application number
PCT/CH1996/000131
Other languages
German (de)
English (en)
Inventor
Max Dätwyler
Original Assignee
Mdc Max Dätwyler Bleienbach Ag
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mdc Max Dätwyler Bleienbach Ag filed Critical Mdc Max Dätwyler Bleienbach Ag
Publication of WO1996033837A1 publication Critical patent/WO1996033837A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K15/00—Electron-beam welding or cutting
    • B23K15/08—Removing material, e.g. by cutting, by hole drilling
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas

Definitions

  • the invention relates to a method for surface preparation of a workpiece with a metallic carrier material according to the preamble of patent claim 1 and a workpiece with a metallic carrier material according to the preamble of patent claim 9.
  • DD-A-242 638 discloses such a method for improving the adhesive strength of metal sprayed layers, in which the component surface is cleaned by melting using a continuous or pulsating laser beam with a specific power density or by controlled thermal exposure.
  • the energy beam is intended to roughen and activate the area near the surface before thermal coating with metal or ceramic.
  • the laser beam is guided in such a way that the traces of melting just touch each other, as a result of which the affected surface area is homogenized.
  • the alignment of the tracks and the speed of movement of a pulsating laser beam are selected in such a way that the zones of influence overlap.
  • the energizing impulses cause contaminants to evaporate or explode and activate the surface.
  • the present invention has for its object to provide a method of the aforementioned type, which allows the surface of the carrier material of a workpiece to be pretreated in such a way that a substrate is formed with an even adhesive strength for a metal or ceramic layer to be sprayed on, which is also possible with a high level Stress on the workpiece shows no cracks or other signs of detachment in the sprayed-on layer.
  • this object is achieved by a method having the features of claim 1 and by a workpiece having the features of claim 5.
  • the invention has the great advantage that an improved mechanical connection or clamping of the sprayed-on metal or ceramic layer with the surface of the metallic carrier material is produced.
  • the process is considerably less expensive than the conventional roughening processes, such as sandblasting, since there is no need for subsequent cleaning.
  • the throughput times in the case of the invention are also Processes significantly lower, which is why it is more economical.
  • Fig. 1 is a schematic representation of a treatment process for surface preparation for the subsequent metal or ceramic coating
  • Fig. 2 cross sections through a part of a workpiece with different types of recesses, the carrier material surface has been prepared with the treatment method explained with reference to FIG. 1.
  • a workpiece 1 here a metallic circular cylindrical hollow body, with its surface 2 and small recesses 3 located therein.
  • the hollow body 1 is rotatably supported in a known manner about an axis of rotation 5.
  • a schematically indicated laser cannon 7 with a mirror 8 is shown to the side of the hollow body 1, with which a laser beam 9 is directed onto the workpiece 1, here the circular cylindrical hollow body.
  • the mirror 8 is mounted in a manner known to those skilled in the art by means of servomotors so that it can rotate in all directions.
  • the depressions 3 are worked into the surface 2 in a predetermined pattern or grid indicated by the arrow 11.
  • the geometric shape of the recesses 3 is the performance control of the laser beam 9 and achieved by the continuous and targeted deflection of the laser beam 9 with the mirror 8 in the desired manner.
  • suitable control of the laser beam 9 almost any geometrical shape of the depressions 3 can thus be obtained in a predetermined pattern or grid.
  • the depressions 3 can be provided on the surface 2 in any pattern, a regular grid is preferred, however, which is formed by the nodes of sets of parallel straight lines which are perpendicular or at an oblique angle to one another.
  • FIG. 2 shows various examples of the depressions 3 produced by means of the laser beam 9 in a cross section through part of a workpiece 1.
  • the metallic carrier material 13 of the workpiece 1 is shown below, on which a metal or ceramic layer 14 applied in the plasma spraying process is anchored.
  • FIG. 2a shows a recess 3 which is frustoconical. The geometric shape shown is achieved in that the mirror 8 is brought to a certain distance from the workpiece 1 and the laser beam 9 is deflected in a predetermined angular range. The aforementioned distance is formed from the apex of a cone through the truncated cone-shaped recess 3. The depth of the recess 3 is in the range from 10 to 100 ⁇ m, in particular between 2 to 10 ⁇ m.
  • the width of the recess 3 is also of the same order of magnitude.
  • the circular-cylindrical depression in FIG. 2b is obtained in that the mirror 8 is continuously shifted in directions perpendicular to the normal to the flat surface of the carrier material 13 while the power density of the laser beam 9 remains the same.
  • the depression 3 in FIG Laser beam 9 reached with such a shift.
  • the depressions 3 shown in FIGS. 2a to 2c are all rotationally symmetrical. This means that the depressions 3 all have a circular cross section. However, it goes without saying that other types of depressions 3 can also be provided, for example with a square or triangular shape in cross section. However, the rotationally symmetrical shape is preferred.
  • the targeted and defined shape of the depressions 3 results in an improved mechanical clamping of the carrier material 13 with the sprayed-on metal or ceramic layer 14.
  • the adhesion of this layer 14 is significantly improved by this measure.
  • the geometric dimensions of the depressions 3 can largely be adapted to the requirements of the required adhesion of the coating material. Subsequent cleaning, as with the mechanical roughening process, such as. such as sandblasting, is completely eliminated.
  • the method described above can also be carried out with an electron beam, which is directed onto the workpiece by electromagnetic means in a manner known to those skilled in the art.
  • the method described is particularly suitable for the production of cylinder liners for internal combustion engines, the depressions 3 preferably being incorporated after a dot matrix 11, as indicated purely schematically in FIG. 1.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Laser Beam Processing (AREA)

Abstract

L'invention concerne un procédé permettant de préparer la surface d'une pièce (1) comportant un matériau support, selon lequel des cavités (3) de forme géométrique prédéfinie sont pratiquées dans ladite surface, à l'aide d'un faisceau laser ou électronique.
PCT/CH1996/000131 1995-04-25 1996-04-12 Procede permettant de preparer la surface d'une piece comportant un materiau support metallique, et piece munie d'un materiau support metallique WO1996033837A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH1179/95-2 1995-04-25
CH117995 1995-04-25

Publications (1)

Publication Number Publication Date
WO1996033837A1 true WO1996033837A1 (fr) 1996-10-31

Family

ID=4204349

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CH1996/000131 WO1996033837A1 (fr) 1995-04-25 1996-04-12 Procede permettant de preparer la surface d'une piece comportant un materiau support metallique, et piece munie d'un materiau support metallique

Country Status (1)

Country Link
WO (1) WO1996033837A1 (fr)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0899053A2 (fr) * 1997-08-29 1999-03-03 Sintokogio Ltd. Produit plaqué et procédé et dispositif pour sa fabrication
EP1247874A1 (fr) * 2001-04-06 2002-10-09 ALSTOM (Switzerland) Ltd Construction composite avec matériaux métalliques et non-métalliques
EP1854903A1 (fr) 2006-05-08 2007-11-14 Ford-Werke GmbH Procédé de fabrication de revêtements résistant à l'usure sur un corps de base métallique et un revêtement fabriqué avec ce procédé
WO2008110835A1 (fr) * 2007-03-13 2008-09-18 Airbus Uk Limited Préparation d'un composant destiné à être utilisé dans un joint
EP2112359A1 (fr) * 2001-01-20 2009-10-28 KS Aluminium-Technologie GmbH Surface de glissement d'un cylindre
US20100000069A1 (en) * 2004-03-08 2010-01-07 Ceramic Sciences, Inc. Orthodontic bracket
DE10325910B4 (de) * 2002-08-02 2010-03-18 Mauser-Werke Oberndorf Maschinenbau Gmbh Verfahren zur Einbringung von Strukturen in Anlageflächen, Vorrichtung zum Einbringen derartiger Strukturen und kraftschlüssig verbundene Körper
US20110097538A1 (en) * 2009-07-17 2011-04-28 Rolls-Royce Corporation Substrate Features for Mitigating Stress
CN103153524A (zh) * 2010-10-13 2013-06-12 陶瓷技术有限责任公司 利用激光射线接合两个接合伙伴、即陶瓷与金属/陶瓷的方法
EP2937392A1 (fr) * 2014-04-23 2015-10-28 Roller Bearing Company of America, Inc. Procédé et appareil permettant la préparation d'une surface pour la liaison d'un matériau à celui-ci
EP3047934A1 (fr) 2013-04-16 2016-07-27 Volkswagen AG Dispositif de structuration de surface d'un élément de machine
DE102015210359A1 (de) 2015-06-05 2016-12-08 Volkswagen Aktiengesellschaft Verfahren zur Erzeugung eines Vertiefungsmusters in der Reibfläche eines Reibelements sowie ein nach diesem Verfahren hergestelltes Reibelement
US9643265B2 (en) 2008-08-05 2017-05-09 Guehring Kg Method and tool for producing a surface of predetermined roughness
US9713912B2 (en) 2010-01-11 2017-07-25 Rolls-Royce Corporation Features for mitigating thermal or mechanical stress on an environmental barrier coating
US10040094B2 (en) 2013-03-15 2018-08-07 Rolls-Royce Corporation Coating interface
DE102017210639A1 (de) * 2017-06-23 2018-12-27 Robert Bosch Gmbh Verbundbauteil, Verfahren zur Herstellung desselben und dessen Verwendung
RU2752821C1 (ru) * 2020-10-07 2021-08-06 Федеральное государственное бюджетное учреждение науки Институт электрофизики и электроэнергетики Российской академии наук (ИЭЭ РАН) Способ получения наноструктурированной поверхности металлической заготовки лазерной обработкой
RU2833917C1 (ru) * 2023-12-15 2025-01-31 Федеральное Автономное Учреждение "Центральный институт авиационного моторостроения имени П.И. Баранова" Способ наноструктурирования поверхности металлического материала для изготовления электродов или электролитических мембран твердоокисных топливных ячеек путем лазерной абляции

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB222179A (en) * 1923-06-20 1924-09-22 English Electric Co Ltd Improvements in electro-magnetic control devices for electric switches and other apparatus
JPS59146986A (ja) * 1983-02-03 1984-08-23 三井造船株式会社 セラミツク部材の接合方法
DD242638A1 (de) * 1985-11-18 1987-02-04 Ibr Fuer Entwickl Techn U Rat Verfahren zur haftfestigkeitsverbesserung von metallspritzschichten
US5354581A (en) * 1990-01-17 1994-10-11 Hjl Projects & Developments Ltd. Surface treatment of sheet- or plate-like blanks
EP0626228A1 (fr) * 1993-05-26 1994-11-30 The Welding Institute Modification de la surface

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB222179A (en) * 1923-06-20 1924-09-22 English Electric Co Ltd Improvements in electro-magnetic control devices for electric switches and other apparatus
JPS59146986A (ja) * 1983-02-03 1984-08-23 三井造船株式会社 セラミツク部材の接合方法
DD242638A1 (de) * 1985-11-18 1987-02-04 Ibr Fuer Entwickl Techn U Rat Verfahren zur haftfestigkeitsverbesserung von metallspritzschichten
US5354581A (en) * 1990-01-17 1994-10-11 Hjl Projects & Developments Ltd. Surface treatment of sheet- or plate-like blanks
EP0626228A1 (fr) * 1993-05-26 1994-11-30 The Welding Institute Modification de la surface

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
DATABASE WPI Section Ch Week 8440, Derwent World Patents Index; Class L02, AN 84-246050, XP002003962 *

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0899053A3 (fr) * 1997-08-29 2000-04-05 Sintokogio Ltd. Produit plaqué et procédé et dispositif pour sa fabrication
EP0899053A2 (fr) * 1997-08-29 1999-03-03 Sintokogio Ltd. Produit plaqué et procédé et dispositif pour sa fabrication
EP2112359A1 (fr) * 2001-01-20 2009-10-28 KS Aluminium-Technologie GmbH Surface de glissement d'un cylindre
EP1247874A1 (fr) * 2001-04-06 2002-10-09 ALSTOM (Switzerland) Ltd Construction composite avec matériaux métalliques et non-métalliques
DE10325910C5 (de) * 2002-08-02 2017-01-26 Mauser-Werke Oberndorf Maschinenbau Gmbh Verfahren zur Einbringung von Strukturen in Anlageflächen, Vorrichtung zum Einbringen derartiger Strukturen und kraftschlüssig verbundene Körper
DE10325910B4 (de) * 2002-08-02 2010-03-18 Mauser-Werke Oberndorf Maschinenbau Gmbh Verfahren zur Einbringung von Strukturen in Anlageflächen, Vorrichtung zum Einbringen derartiger Strukturen und kraftschlüssig verbundene Körper
US8726510B2 (en) * 2004-03-08 2014-05-20 John C. Voudouris Method of making a clip for a self-ligating orthodontic bracket
US20100000069A1 (en) * 2004-03-08 2010-01-07 Ceramic Sciences, Inc. Orthodontic bracket
EP1854903A1 (fr) 2006-05-08 2007-11-14 Ford-Werke GmbH Procédé de fabrication de revêtements résistant à l'usure sur un corps de base métallique et un revêtement fabriqué avec ce procédé
US9192990B2 (en) 2007-03-13 2015-11-24 Airbus Operations Limited Preparation of a component for use in a joint
WO2008110835A1 (fr) * 2007-03-13 2008-09-18 Airbus Uk Limited Préparation d'un composant destiné à être utilisé dans un joint
US10155266B2 (en) 2007-03-13 2018-12-18 Airbus Operations Limited Preparation of a component for use in a joint
JP2010522849A (ja) * 2007-03-13 2010-07-08 エアバス・ユ―ケ―・リミテッド ジョイントで用いるための構成部材の準備
US10259059B2 (en) 2008-08-05 2019-04-16 Martinrea Honsel Germany Gmbh Method and tool for producing a surface of predetermined roughness
US9643265B2 (en) 2008-08-05 2017-05-09 Guehring Kg Method and tool for producing a surface of predetermined roughness
EP2307162B1 (fr) 2008-08-05 2017-08-30 Martinrea Honsel Germany GmbH Procédé et outil pour produire une surface présentant une rugosité prédéfinie
US8852720B2 (en) * 2009-07-17 2014-10-07 Rolls-Royce Corporation Substrate features for mitigating stress
US9194243B2 (en) 2009-07-17 2015-11-24 Rolls-Royce Corporation Substrate features for mitigating stress
US20110097538A1 (en) * 2009-07-17 2011-04-28 Rolls-Royce Corporation Substrate Features for Mitigating Stress
US9713912B2 (en) 2010-01-11 2017-07-25 Rolls-Royce Corporation Features for mitigating thermal or mechanical stress on an environmental barrier coating
CN103153524A (zh) * 2010-10-13 2013-06-12 陶瓷技术有限责任公司 利用激光射线接合两个接合伙伴、即陶瓷与金属/陶瓷的方法
US10040094B2 (en) 2013-03-15 2018-08-07 Rolls-Royce Corporation Coating interface
EP3047934A1 (fr) 2013-04-16 2016-07-27 Volkswagen AG Dispositif de structuration de surface d'un élément de machine
EP2937392A1 (fr) * 2014-04-23 2015-10-28 Roller Bearing Company of America, Inc. Procédé et appareil permettant la préparation d'une surface pour la liaison d'un matériau à celui-ci
US9919502B2 (en) 2014-04-23 2018-03-20 Schaublin Sa Method and apparatus for preparing a surface for bonding a material thereto
DE102015210359A1 (de) 2015-06-05 2016-12-08 Volkswagen Aktiengesellschaft Verfahren zur Erzeugung eines Vertiefungsmusters in der Reibfläche eines Reibelements sowie ein nach diesem Verfahren hergestelltes Reibelement
DE102017210639A1 (de) * 2017-06-23 2018-12-27 Robert Bosch Gmbh Verbundbauteil, Verfahren zur Herstellung desselben und dessen Verwendung
RU2752821C1 (ru) * 2020-10-07 2021-08-06 Федеральное государственное бюджетное учреждение науки Институт электрофизики и электроэнергетики Российской академии наук (ИЭЭ РАН) Способ получения наноструктурированной поверхности металлической заготовки лазерной обработкой
RU2833917C1 (ru) * 2023-12-15 2025-01-31 Федеральное Автономное Учреждение "Центральный институт авиационного моторостроения имени П.И. Баранова" Способ наноструктурирования поверхности металлического материала для изготовления электродов или электролитических мембран твердоокисных топливных ячеек путем лазерной абляции

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