ES2196035T3 - Procedimiento para la fabricacion de un recubrimiento de rozadura para partes componentes metalicas de grupos motopropulsores. - Google Patents
Procedimiento para la fabricacion de un recubrimiento de rozadura para partes componentes metalicas de grupos motopropulsores.Info
- Publication number
- ES2196035T3 ES2196035T3 ES95113444T ES95113444T ES2196035T3 ES 2196035 T3 ES2196035 T3 ES 2196035T3 ES 95113444 T ES95113444 T ES 95113444T ES 95113444 T ES95113444 T ES 95113444T ES 2196035 T3 ES2196035 T3 ES 2196035T3
- Authority
- ES
- Spain
- Prior art keywords
- lining
- procedure
- manufacture
- motor drive
- metal component
- 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.)
- Expired - Lifetime
Links
- 238000010073 coating (rubber) Methods 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
- 101150027068 DEGS1 gene Proteins 0.000 abstract 1
- 238000005299 abrasion Methods 0.000 abstract 1
- 239000000919 ceramic Substances 0.000 abstract 1
- 229910010293 ceramic material Inorganic materials 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 238000007789 sealing Methods 0.000 abstract 1
- 239000007921 spray Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
-
- 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
- C23C4/01—Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/90—Coating; Surface treatment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24355—Continuous and nonuniform or irregular surface on layer or component [e.g., roofing, etc.]
- Y10T428/24372—Particulate matter
- Y10T428/24413—Metal or metal compound
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24802—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
- Y10T428/24926—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.] including ceramic, glass, porcelain or quartz layer
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
- Y10T428/256—Heavy metal or aluminum or compound thereof
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
- Y10T428/256—Heavy metal or aluminum or compound thereof
- Y10T428/257—Iron oxide or aluminum oxide
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Plasma & Fusion (AREA)
- Physics & Mathematics (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Coating By Spraying Or Casting (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Laminated Bodies (AREA)
- Paints Or Removers (AREA)
Abstract
LA INVENCION SE REFIERE A UN RECUBRIMIENTO DE ROZADURA PARA COMPONENTES DE TRABAJO DE ACCIONAMIENTO METALICO, QUE MUESTRA UN RECUBRIMIENTO DE ROZADURA, QUE ESTA FAMILIARIZADO EN LOS PROCESOS DE ROZADURA MEDIANTE APLICACION DE DESARROLLO. EL RECUBRIMIENTO DE ARRANCADO SE COMPONE DE UNA CAPA CERAMICA CON APLICACION TERMICA EN LA PUNTA Y LA CAPA CERAMICA ESTA PERFILADA DE TAL MODO, QUE MUESTRA UN BORDE CON CAPACIDAD DE CORTE. ENTRE LOS BORDES SE DISPONEN DE ESPACIOS LIBRES, QUE RECIBEN Y EVACUAN LA ABRASION DE LA APLICACION DE ENTRADA DE DESARROLLO, ASI COMO UN PROCEDIMIENTO PARA LA ELABORACION DE RECUBRIMIENTO DE ROZADURA PERFILADO.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE4432998A DE4432998C1 (de) | 1994-09-16 | 1994-09-16 | Anstreifbelag für metallische Triebwerkskomponente und Herstellungsverfahren |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2196035T3 true ES2196035T3 (es) | 2003-12-16 |
Family
ID=6528373
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES95113444T Expired - Lifetime ES2196035T3 (es) | 1994-09-16 | 1995-08-26 | Procedimiento para la fabricacion de un recubrimiento de rozadura para partes componentes metalicas de grupos motopropulsores. |
Country Status (5)
| Country | Link |
|---|---|
| US (2) | US5756217A (es) |
| EP (1) | EP0702130B1 (es) |
| AT (1) | ATE238489T1 (es) |
| DE (2) | DE4432998C1 (es) |
| ES (1) | ES2196035T3 (es) |
Families Citing this family (70)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19730008C1 (de) * | 1997-07-12 | 1998-10-29 | Mtu Muenchen Gmbh | Panzerung für ein metallisches Triebwerksbauteil und Verfahren zu ihrer Herstellung |
| US6004362A (en) * | 1998-02-02 | 1999-12-21 | Lockheed Martin Energy Systems | Method for forming an abrasive surface on a tool |
| JP2002055600A (ja) * | 2000-08-09 | 2002-02-20 | Laurel Seiki Kk | 視覚障害者用情報入出力装置 |
| DE10047307A1 (de) * | 2000-09-25 | 2002-08-01 | Alstom Switzerland Ltd | Dichtungsanordnung |
| DE10140742B4 (de) * | 2000-12-16 | 2015-02-12 | Alstom Technology Ltd. | Vorrichtung zur Dichtspaltreduzierung zwischen einer rotierenden und einer stationären Komponente innerhalb einer axial durchströmten Strömungsmaschine |
| US7166258B2 (en) * | 2001-01-31 | 2007-01-23 | Agilent Technologies, Inc. | Automation-optimized microarray package |
| US6528118B2 (en) * | 2001-02-06 | 2003-03-04 | General Electric Company | Process for creating structured porosity in thermal barrier coating |
| JP2002256808A (ja) * | 2001-02-28 | 2002-09-11 | Mitsubishi Heavy Ind Ltd | 燃焼エンジン、ガスタービン及び研磨層 |
| FR2825411B1 (fr) * | 2001-05-31 | 2003-09-19 | Snecma Moteurs | Aube de turbine avec lechette d'etancheite |
| WO2003010419A1 (de) * | 2001-07-23 | 2003-02-06 | Alstom Technology Ltd | Vorrichtung zur dichtspaltreduzierung zwischen bewegten und stationären komponenten innerhalb einer strömungsmaschine |
| DE10340147B4 (de) * | 2002-08-27 | 2014-04-10 | Kyocera Corp. | Trockenätzverfahren und Trockenätzvorrichtung |
| US7459098B2 (en) * | 2002-08-28 | 2008-12-02 | Kyocera Corporation | Dry etching apparatus, dry etching method, and plate and tray used therein |
| US7556741B2 (en) * | 2002-08-28 | 2009-07-07 | Kyocera Corporation | Method for producing a solar cell |
| US6887528B2 (en) * | 2002-12-17 | 2005-05-03 | General Electric Company | High temperature abradable coatings |
| US20050003172A1 (en) * | 2002-12-17 | 2005-01-06 | General Electric Company | 7FAstage 1 abradable coatings and method for making same |
| JP2005008483A (ja) * | 2003-06-19 | 2005-01-13 | Shin Etsu Chem Co Ltd | 被覆部材及びその製造方法 |
| US6890150B2 (en) * | 2003-08-12 | 2005-05-10 | General Electric Company | Center-located cutter teeth on shrouded turbine blades |
| US6905309B2 (en) * | 2003-08-28 | 2005-06-14 | General Electric Company | Methods and apparatus for reducing vibrations induced to compressor airfoils |
| GB0326235D0 (en) * | 2003-11-10 | 2003-12-17 | Boc Group Inc | Vacuum pump |
| WO2005061852A1 (en) * | 2003-12-23 | 2005-07-07 | Bp Exploration Operating Company Limited | Non-threaded expandable pipe connection system |
| DE102004042127B4 (de) * | 2004-08-30 | 2006-07-13 | Daimlerchrysler Ag | Rotor-Stator-Vorrichtung mit Anstreifbelag, Verfahren zu deren Herstellung sowie Verwendung |
| US7614847B2 (en) * | 2004-11-24 | 2009-11-10 | General Electric Company | Pattern for the surface of a turbine shroud |
| US7600968B2 (en) * | 2004-11-24 | 2009-10-13 | General Electric Company | Pattern for the surface of a turbine shroud |
| NL1029708C2 (nl) * | 2005-08-10 | 2007-02-13 | Kick Off Ltd | Turbulentiefolie. |
| US7922455B2 (en) * | 2005-09-19 | 2011-04-12 | General Electric Company | Steam-cooled gas turbine bucker for reduced tip leakage loss |
| DE102005044991A1 (de) * | 2005-09-21 | 2007-03-22 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung einer Schutzschicht, Schutzschicht und Bauteil mit einer Schutzschicht |
| EP1808508A1 (de) * | 2006-01-17 | 2007-07-18 | Siemens Aktiengesellschaft | Im Strömungskanal einer Strömungsmaschine anzuordnendes Bauteil und Spritzverfahren zum Erzeugen einer Beschichtung |
| EP1820938A1 (de) * | 2006-02-20 | 2007-08-22 | ABB Turbo Systems AG | Reinigungselemente auf Laufschaufelspitzen einer Abgasturbine |
| EP1925779A1 (de) * | 2006-11-23 | 2008-05-28 | Siemens Aktiengesellschaft | Strömungsführendes Bauteil und Verfahren zur Herstellung eines solchen |
| DE102008061800A1 (de) * | 2008-12-11 | 2010-06-17 | Rolls-Royce Deutschland Ltd & Co Kg | Segmentierte Dichtlippen für Labyrinthdichtungsringe |
| DE102009012945A1 (de) | 2009-03-12 | 2010-09-16 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung einer abrasiven Beschichtung und Bauteil für eine Turbomaschine |
| US8852720B2 (en) * | 2009-07-17 | 2014-10-07 | Rolls-Royce Corporation | Substrate features for mitigating stress |
| DE102009040298A1 (de) * | 2009-09-04 | 2011-03-10 | Mtu Aero Engines Gmbh | Strömungsmaschine und Verfahren zur Erzeugung eines strukturierten Einlaufbelags |
| EP2309098A1 (en) * | 2009-09-30 | 2011-04-13 | Siemens Aktiengesellschaft | Airfoil and corresponding guide vane, blade, gas turbine and turbomachine |
| EP2524069B1 (en) | 2010-01-11 | 2018-03-07 | Rolls-Royce Corporation | Features for mitigating thermal or mechanical stress on an environmental barrier coating |
| DE102010005389A1 (de) * | 2010-01-22 | 2011-07-28 | MTU Aero Engines GmbH, 80995 | Strukturierte Oberflächenbeschichtung mittels kinetischem Kaltgasspritzen |
| US8845283B2 (en) * | 2010-11-29 | 2014-09-30 | General Electric Company | Compressor blade with flexible tip elements and process therefor |
| EP2458157B1 (fr) * | 2010-11-30 | 2015-10-14 | Techspace Aero S.A. | Abradable de virole intérieure de stator |
| US8888446B2 (en) * | 2011-10-07 | 2014-11-18 | General Electric Company | Turbomachine rotor having patterned coating |
| DE102012200883B4 (de) | 2012-01-23 | 2015-12-03 | MTU Aero Engines AG | Strömungsmaschinen-Dichtungsanordnung |
| US20130323430A1 (en) * | 2012-05-31 | 2013-12-05 | General Electric Company | Method of coating corner interface of turbine system |
| GB201222975D0 (en) * | 2012-12-19 | 2013-01-30 | Composite Technology & Applic Ltd | An aerofoil structure |
| WO2014144152A1 (en) | 2013-03-15 | 2014-09-18 | Rolls-Royce Corporation | Improved coating interface |
| US20150078900A1 (en) * | 2013-09-19 | 2015-03-19 | David B. Allen | Turbine blade with airfoil tip having cutting tips |
| US9909428B2 (en) * | 2013-11-26 | 2018-03-06 | General Electric Company | Turbine buckets with high hot hardness shroud-cutting deposits |
| US8939707B1 (en) | 2014-02-25 | 2015-01-27 | Siemens Energy, Inc. | Turbine abradable layer with progressive wear zone terraced ridges |
| US8939706B1 (en) | 2014-02-25 | 2015-01-27 | Siemens Energy, Inc. | Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface |
| US9151175B2 (en) | 2014-02-25 | 2015-10-06 | Siemens Aktiengesellschaft | Turbine abradable layer with progressive wear zone multi level ridge arrays |
| US8939705B1 (en) | 2014-02-25 | 2015-01-27 | Siemens Energy, Inc. | Turbine abradable layer with progressive wear zone multi depth grooves |
| US8939716B1 (en) | 2014-02-25 | 2015-01-27 | Siemens Aktiengesellschaft | Turbine abradable layer with nested loop groove pattern |
| US9249680B2 (en) | 2014-02-25 | 2016-02-02 | Siemens Energy, Inc. | Turbine abradable layer with asymmetric ridges or grooves |
| US9243511B2 (en) | 2014-02-25 | 2016-01-26 | Siemens Aktiengesellschaft | Turbine abradable layer with zig zag groove pattern |
| RU2016134446A (ru) | 2014-02-25 | 2018-03-29 | Сименс Акциенгезелльшафт | Термобарьерное покрытие компонента турбины с изменяющимися по глубине свойствами материала |
| KR102318300B1 (ko) * | 2014-05-15 | 2021-10-29 | 누보 피그노네 에스알엘 | 터보기계의 구성요소의 제조 방법, 터보기계의 구성요소 및 터보기계 |
| US11066937B2 (en) | 2014-06-04 | 2021-07-20 | Raytheon Technologies Corporation | Cutting blade tips |
| US9982358B2 (en) | 2014-06-04 | 2018-05-29 | United Technologies Corporation | Abrasive tip blade manufacture methods |
| US9932839B2 (en) * | 2014-06-04 | 2018-04-03 | United Technologies Corporation | Cutting blade tips |
| DE102014212652A1 (de) * | 2014-06-30 | 2016-01-14 | MTU Aero Engines AG | Strömungsmaschine |
| FR3026428B1 (fr) * | 2014-09-30 | 2019-10-25 | Safran Aircraft Engines | Aube de rotor de turbomachine a lechettes radiales |
| EP3006672A1 (de) * | 2014-10-10 | 2016-04-13 | Universität Stuttgart | Vorrichtung zur Beeinflussung der Strömung in einer Turbomaschine |
| GB201419412D0 (en) * | 2014-10-31 | 2014-12-17 | Rolls Royce Plc | Rotary device |
| FR3029813B1 (fr) * | 2014-12-16 | 2019-07-19 | Airbus Operations (S.A.S.) | Procede de fabrication d'un revetement microstructure |
| EP3259452A2 (en) | 2015-02-18 | 2017-12-27 | Siemens Aktiengesellschaft | Forming cooling passages in combustion turbine superalloy castings |
| US10190435B2 (en) | 2015-02-18 | 2019-01-29 | Siemens Aktiengesellschaft | Turbine shroud with abradable layer having ridges with holes |
| KR102630007B1 (ko) | 2015-11-10 | 2024-01-26 | 오를리콘 서피스 솔루션스 아크티엔게젤샤프트, 페피콘 | 터빈 틈새 제어 코팅 및 방법 |
| US10801097B2 (en) * | 2015-12-23 | 2020-10-13 | Praxair S.T. Technology, Inc. | Thermal spray coatings onto non-smooth surfaces |
| FR3065482B1 (fr) * | 2017-04-20 | 2019-07-05 | Safran Aircraft Engines | Element d'anneau d'etancheite pour turbine comportant une cavite inclinee dans un materiau abradable |
| US10954803B2 (en) * | 2019-01-17 | 2021-03-23 | Rolls-Royce Corporation | Abrasive coating for high temperature mechanical systems |
| FR3118990B1 (fr) * | 2021-01-21 | 2023-09-15 | Safran Aircraft Engines | Rotor de turbine pour une turbomachine. |
| US20250250900A1 (en) * | 2023-11-21 | 2025-08-07 | Rolls-Royce Plc | Aerofoil structure for a gas turbine engine |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3042365A (en) * | 1957-11-08 | 1962-07-03 | Gen Motors Corp | Blade shrouding |
| US3964877A (en) * | 1975-08-22 | 1976-06-22 | General Electric Company | Porous high temperature seal abradable member |
| US4169020A (en) * | 1977-12-21 | 1979-09-25 | General Electric Company | Method for making an improved gas seal |
| DE3413534A1 (de) * | 1984-04-10 | 1985-10-24 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Gehaeuse einer stroemungsmaschine |
| DE8411277U1 (de) * | 1984-04-10 | 1986-08-14 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Gehäuse einer Strömungsmaschine |
| US4744725A (en) * | 1984-06-25 | 1988-05-17 | United Technologies Corporation | Abrasive surfaced article for high temperature service |
| US4799939A (en) * | 1987-02-26 | 1989-01-24 | Minnesota Mining And Manufacturing Company | Erodable agglomerates and abrasive products containing the same |
| US4822248A (en) * | 1987-04-15 | 1989-04-18 | Metallurgical Industries, Inc. | Rebuilt shrouded turbine blade and method of rebuilding the same |
| US4884820A (en) * | 1987-05-19 | 1989-12-05 | Union Carbide Corporation | Wear resistant, abrasive laser-engraved ceramic or metallic carbide surfaces for rotary labyrinth seal members |
| IE892863L (en) * | 1988-09-09 | 1990-03-09 | Galderma Rech Dermatologique | Abrasive compacts |
| US5133782A (en) * | 1989-02-14 | 1992-07-28 | Wiand Ronald C | Multilayer abrading tool having an irregular abrading surface and process |
| US5223332A (en) * | 1990-05-31 | 1993-06-29 | Praxair S.T. Technology, Inc. | Duplex coatings for various substrates |
| JPH06104817B2 (ja) * | 1990-10-09 | 1994-12-21 | 日本研磨材工業株式会社 | アルミナ―ジルコニア系ラップ研磨材とその製造方法及び研磨用組成物 |
| DE4306966C1 (de) * | 1992-10-19 | 1994-01-20 | Starck H C Gmbh Co Kg | Schleifkorn auf der Basis von Zirkonkorund, Verfahren zu seiner Herstellung und dessen Verwendung |
| US5398455A (en) * | 1993-01-14 | 1995-03-21 | United Technologies Corporation | Grinding tool |
| US5443418A (en) * | 1993-03-29 | 1995-08-22 | Norton Company | Superabrasive tool |
| US5453312A (en) * | 1993-10-29 | 1995-09-26 | Minnesota Mining And Manufacturing Company | Abrasive article, a process for its manufacture, and a method of using it to reduce a workpiece surface |
| US5603603A (en) * | 1993-12-08 | 1997-02-18 | United Technologies Corporation | Abrasive blade tip |
| EP0661415A1 (de) * | 1993-12-17 | 1995-07-05 | Sulzer Innotec Ag | Einrichtung mit rotierfähigem Körper, Gehäuse und dazwischen liegendem Dichtspalt |
-
1994
- 1994-09-16 DE DE4432998A patent/DE4432998C1/de not_active Expired - Fee Related
-
1995
- 1995-08-26 DE DE59510655T patent/DE59510655D1/de not_active Expired - Lifetime
- 1995-08-26 ES ES95113444T patent/ES2196035T3/es not_active Expired - Lifetime
- 1995-08-26 AT AT95113444T patent/ATE238489T1/de not_active IP Right Cessation
- 1995-08-26 EP EP95113444A patent/EP0702130B1/de not_active Expired - Lifetime
- 1995-09-15 US US08/529,274 patent/US5756217A/en not_active Expired - Fee Related
-
1997
- 1997-09-25 US US08/937,581 patent/US6171351B1/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US5756217A (en) | 1998-05-26 |
| DE59510655D1 (de) | 2003-05-28 |
| ATE238489T1 (de) | 2003-05-15 |
| EP0702130B1 (de) | 2003-04-23 |
| US6171351B1 (en) | 2001-01-09 |
| EP0702130A2 (de) | 1996-03-20 |
| DE4432998C1 (de) | 1996-04-04 |
| EP0702130A3 (de) | 1998-06-10 |
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