TR201905293T4 - Turbo maki̇nelerde kullanima yöneli̇k sizdirmazlik si̇stemleri̇ ve bunlarin üreti̇lmesi̇ne yöneli̇k yöntemler - Google Patents
Turbo maki̇nelerde kullanima yöneli̇k sizdirmazlik si̇stemleri̇ ve bunlarin üreti̇lmesi̇ne yöneli̇k yöntemler Download PDFInfo
- Publication number
- TR201905293T4 TR201905293T4 TR2019/05293T TR201905293T TR201905293T4 TR 201905293 T4 TR201905293 T4 TR 201905293T4 TR 2019/05293 T TR2019/05293 T TR 2019/05293T TR 201905293 T TR201905293 T TR 201905293T TR 201905293 T4 TR201905293 T4 TR 201905293T4
- Authority
- TR
- Turkey
- Prior art keywords
- al2o3
- abrasive
- zro2
- production
- methods
- Prior art date
Links
- 238000007789 sealing Methods 0.000 title abstract 3
- 238000000034 method Methods 0.000 title 1
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 abstract 8
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 abstract 6
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 abstract 3
- 229910003468 tantalcarbide Inorganic materials 0.000 abstract 3
- 230000003628 erosive effect Effects 0.000 abstract 2
- 239000002245 particle Substances 0.000 abstract 2
- 239000000758 substrate Substances 0.000 abstract 2
- 229910052582 BN Inorganic materials 0.000 abstract 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 abstract 1
- 238000005299 abrasion Methods 0.000 abstract 1
- 239000003082 abrasive agent 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
- F01D11/122—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 with erodable or abradable material
-
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/445—Free-space packings with means for adjusting the clearance
-
- 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
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
-
- 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
-
- 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
- F05D2300/22—Non-oxide ceramics
- F05D2300/226—Carbides
-
- 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
- F05D2300/22—Non-oxide ceramics
- F05D2300/228—Nitrides
-
- 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
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/506—Hardness
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Combustion & Propulsion (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
- Coating By Spraying Or Casting (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Polishing Bodies And Polishing Tools (AREA)
- Ceramic Products (AREA)
Abstract
Buraya bağlanan kanat profillerine sahip bir döndürülebilir bölümü ve bir iç yüzeye sahip bir sabit bölümü kapsayan sızdırmazlık sistemi, iç yüzeyin üzerinden oluşturulan bir aşındırılabilir malzemenin en az bir aşındırılabilir katmanını kapsayan bir aşındırılabilir bölümü kapsamaktadır. Sızdırmazlık sistemi, ayrıca, kanat profilinin bir substratının en az bir bölümü üzerinden düzenlenen bir aşındırma bölümünü kapsamaktadır. Aşındırma bölümü, substratın en az bir bölümünün üstünde oluşturulan en az bir aşındırma katmanını ve aşındırma katmanının içerisine yerleştirilen birden çok aşındırıcı partikülü kapsamaktadır. Birden çok aşındırıcı partikül, tantal karbür (TaC), alüminyum oksit (Al2O3) ve zirkonyadan (ZrO2) en az birinin büyük ölçüde tamamı, önceden belirlenmiş oranlarda kübik bor nitrür (cBN) ve Al2O3, önceden belirlenmiş oranlarda cBN, Al2O3 ve ZrO2, önceden belirlenmiş oranlarda birleştirilmiş Al2O3 ve ZrO2 ve önceden belirlenmiş oranlarda TaC ve Al2O3’#&ten en az birini kapsamaktadır.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/687,369 US9598973B2 (en) | 2012-11-28 | 2012-11-28 | Seal systems for use in turbomachines and methods of fabricating the same |
Publications (1)
Publication Number | Publication Date |
---|---|
TR201905293T4 true TR201905293T4 (tr) | 2019-05-21 |
Family
ID=49726728
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TR2019/05293T TR201905293T4 (tr) | 2012-11-28 | 2013-11-27 | Turbo maki̇nelerde kullanima yöneli̇k sizdirmazlik si̇stemleri̇ ve bunlarin üreti̇lmesi̇ne yöneli̇k yöntemler |
Country Status (11)
Country | Link |
---|---|
US (1) | US9598973B2 (tr) |
EP (1) | EP2925971B1 (tr) |
JP (1) | JP6340010B2 (tr) |
KR (1) | KR102170569B1 (tr) |
CN (1) | CN104937217A (tr) |
AU (1) | AU2013351191A1 (tr) |
BR (1) | BR112015012277B8 (tr) |
CA (1) | CA2891497A1 (tr) |
MX (1) | MX2015006730A (tr) |
TR (1) | TR201905293T4 (tr) |
WO (1) | WO2014083069A1 (tr) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20160356165A1 (en) * | 2014-02-14 | 2016-12-08 | United Technologies Corporation | Abrasive Tip Blade Manufacture Methods |
EP3143259B1 (en) | 2014-05-15 | 2020-08-05 | Nuovo Pignone S.r.l. | Method of manufacturing a component of a turbomachine, component of a turbomachine and turbomachine |
US10072506B2 (en) * | 2014-06-30 | 2018-09-11 | Rolls-Royce Corporation | Coated gas turbine engine components |
US10786875B2 (en) * | 2014-07-02 | 2020-09-29 | Raytheon Technologies Corporation | Abrasive preforms and manufacture and use methods |
DE102015202070A1 (de) | 2015-02-05 | 2016-08-25 | MTU Aero Engines AG | Gasturbinenbauteil |
US20160237832A1 (en) * | 2015-02-12 | 2016-08-18 | United Technologies Corporation | Abrasive blade tip with improved wear at high interaction rate |
US20160305319A1 (en) * | 2015-04-17 | 2016-10-20 | General Electric Company | Variable coating porosity to influence shroud and rotor durability |
US10030532B2 (en) * | 2015-04-22 | 2018-07-24 | United Technologies Corporation | Abradable seal with thermally conductive microspheres |
US11268183B2 (en) * | 2015-05-06 | 2022-03-08 | Raytheon Technologies Corporation | Method of forming an abrasive coating on a fan blade tip |
US10052724B2 (en) * | 2016-03-02 | 2018-08-21 | General Electric Company | Braze composition, brazing process, and brazed article |
US10544698B2 (en) * | 2016-06-20 | 2020-01-28 | United Technologies Corporation | Air seal abrasive coating and method |
US10415579B2 (en) * | 2016-09-28 | 2019-09-17 | General Electric Company | Ceramic coating compositions for compressor blade and methods for forming the same |
US10294962B2 (en) * | 2017-06-30 | 2019-05-21 | United Technologies Corporation | Turbine engine seal for high erosion environment |
US10900371B2 (en) | 2017-07-27 | 2021-01-26 | Rolls-Royce North American Technologies, Inc. | Abradable coatings for high-performance systems |
US10858950B2 (en) | 2017-07-27 | 2020-12-08 | Rolls-Royce North America Technologies, Inc. | Multilayer abradable coatings for high-performance systems |
US11149744B2 (en) * | 2017-09-19 | 2021-10-19 | Raytheon Technologies Corporation | Turbine engine seal for high erosion environment |
US11976013B2 (en) * | 2017-09-27 | 2024-05-07 | Rolls-Royce Corporation | Composite coating layer for ceramic matrix composite substrate |
JP6939682B2 (ja) | 2018-04-06 | 2021-09-22 | トヨタ自動車株式会社 | 内燃機関 |
JP2019183716A (ja) * | 2018-04-06 | 2019-10-24 | トヨタ自動車株式会社 | 内燃機関 |
US11346232B2 (en) * | 2018-04-23 | 2022-05-31 | Rolls-Royce Corporation | Turbine blade with abradable tip |
US10995623B2 (en) | 2018-04-23 | 2021-05-04 | Rolls-Royce Corporation | Ceramic matrix composite turbine blade with abrasive tip |
US10808565B2 (en) * | 2018-05-22 | 2020-10-20 | Rolls-Royce Plc | Tapered abradable coatings |
US11028721B2 (en) * | 2018-07-19 | 2021-06-08 | Ratheon Technologies Corporation | Coating to improve oxidation and corrosion resistance of abrasive tip system |
FR3085172B1 (fr) | 2018-08-22 | 2021-03-05 | Safran Aircraft Engines | Revetement abradable pour aubes tournantes d'une turbomachine |
CN109236382A (zh) * | 2018-09-11 | 2019-01-18 | 大唐淮北发电厂 | 一种汽轮机轴封及其低压外缸缸面处的密封方法 |
US12116285B2 (en) | 2018-10-05 | 2024-10-15 | Fuji Chemical Industries Co., Ltd. | Porous silica particle composition |
US11015474B2 (en) | 2018-10-19 | 2021-05-25 | Raytheon Technologies Corporation | Geometrically segmented abradable ceramic thermal barrier coating with improved spallation resistance |
US11686208B2 (en) | 2020-02-06 | 2023-06-27 | Rolls-Royce Corporation | Abrasive coating for high-temperature mechanical systems |
FR3115811B1 (fr) * | 2020-10-30 | 2023-02-24 | Safran Ceram | Assemblage pour turbine comprenant des secteurs avec languettes d’étanchéité lamifiées |
CN113215513B (zh) * | 2021-05-11 | 2022-06-03 | 成都中科翼能科技有限公司 | 用于燃气轮机零件可磨耗Al/BN封严涂层新后处理工艺 |
US11976571B1 (en) * | 2022-12-13 | 2024-05-07 | Rtx Corporation | Machinable coating with thermal protection |
Family Cites Families (83)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4227703A (en) * | 1978-11-27 | 1980-10-14 | General Electric Company | Gas seal with tip of abrasive particles |
US4249913A (en) * | 1979-05-21 | 1981-02-10 | United Technologies Corporation | Alumina coated silicon carbide abrasive |
IL75564A (en) * | 1984-06-25 | 1988-02-29 | United Technologies Corp | Abrasive surfaced article for high temperature service |
US4851188A (en) * | 1987-12-21 | 1989-07-25 | United Technologies Corporation | Method for making a turbine blade having a wear resistant layer sintered to the blade tip surface |
US4936745A (en) | 1988-12-16 | 1990-06-26 | United Technologies Corporation | Thin abradable ceramic air seal |
US5059095A (en) * | 1989-10-30 | 1991-10-22 | The Perkin-Elmer Corporation | Turbine rotor blade tip coated with alumina-zirconia ceramic |
US5064727A (en) | 1990-01-19 | 1991-11-12 | Avco Corporation | Abradable hybrid ceramic wall structures |
GB2241506A (en) * | 1990-02-23 | 1991-09-04 | Baj Ltd | Method of producing a gas turbine blade having an abrasive tip by electrodepo- sition. |
US5134032A (en) | 1991-02-25 | 1992-07-28 | General Electric Company | Abrasive particle and rotary seal therewith |
US5453329A (en) | 1992-06-08 | 1995-09-26 | Quantum Laser Corporation | Method for laser cladding thermally insulated abrasive particles to a substrate, and clad substrate formed thereby |
US5551959A (en) | 1994-08-24 | 1996-09-03 | Minnesota Mining And Manufacturing Company | Abrasive article having a diamond-like coating layer and method for making same |
US5704759A (en) | 1996-10-21 | 1998-01-06 | Alliedsignal Inc. | Abrasive tip/abradable shroud system and method for gas turbine compressor clearance control |
US5951892A (en) * | 1996-12-10 | 1999-09-14 | Chromalloy Gas Turbine Corporation | Method of making an abradable seal by laser cutting |
US6946208B2 (en) | 1996-12-10 | 2005-09-20 | Siemens Westinghouse Power Corporation | Sinter resistant abradable thermal barrier coating |
US5935407A (en) * | 1997-11-06 | 1999-08-10 | Chromalloy Gas Turbine Corporation | Method for producing abrasive tips for gas turbine blades |
US6190124B1 (en) | 1997-11-26 | 2001-02-20 | United Technologies Corporation | Columnar zirconium oxide abrasive coating for a gas turbine engine seal system |
SG72959A1 (en) | 1998-06-18 | 2000-05-23 | United Technologies Corp | Article having durable ceramic coating with localized abradable portion |
JP3426987B2 (ja) | 1998-11-13 | 2003-07-14 | 三菱重工業株式会社 | 高温用耐食・耐摩耗コーティング部材及び製造方法並びにガスタービン翼 |
US6089825A (en) | 1998-12-18 | 2000-07-18 | United Technologies Corporation | Abradable seal having improved properties and method of producing seal |
DE19859477B4 (de) | 1998-12-22 | 2005-06-23 | Mtu Aero Engines Gmbh | Verschleißschutzschicht |
US6432487B1 (en) | 2000-12-28 | 2002-08-13 | General Electric Company | Dense vertically cracked thermal barrier coating process to facilitate post-coat surface finishing |
US6533285B2 (en) | 2001-02-05 | 2003-03-18 | Caterpillar Inc | Abradable coating and method of production |
JP3801452B2 (ja) * | 2001-02-28 | 2006-07-26 | 三菱重工業株式会社 | 耐摩耗性コーティング及びその施工方法 |
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 |
JP3790440B2 (ja) * | 2001-05-24 | 2006-06-28 | 三菱重工業株式会社 | 燃焼エンジン動翼の製造方法 |
US6537021B2 (en) | 2001-06-06 | 2003-03-25 | Chromalloy Gas Turbine Corporation | Abradeable seal system |
JP2002371803A (ja) * | 2001-06-13 | 2002-12-26 | Mitsubishi Heavy Ind Ltd | 動翼用耐摩耗層の形成方法、耐摩耗層及びその再生方法 |
US6547522B2 (en) | 2001-06-18 | 2003-04-15 | General Electric Company | Spring-backed abradable seal for turbomachinery |
US20030203224A1 (en) * | 2001-07-30 | 2003-10-30 | Diconza Paul Josesh | Thermal barrier coating of intermediate density |
JP2003148103A (ja) * | 2001-11-09 | 2003-05-21 | Mitsubishi Heavy Ind Ltd | タービンおよびその製造方法 |
JP4058294B2 (ja) | 2002-04-30 | 2008-03-05 | 株式会社荏原製作所 | 回転部材の耐摩耗表面処理方法、羽根車及びその羽根車を有する流体機械 |
US6887530B2 (en) | 2002-06-07 | 2005-05-03 | Sulzer Metco (Canada) Inc. | Thermal spray compositions for abradable seals |
US6884470B2 (en) | 2002-10-03 | 2005-04-26 | General Electric Company | Application method for abradable material |
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 |
US6916529B2 (en) * | 2003-01-09 | 2005-07-12 | General Electric Company | High temperature, oxidation-resistant abradable coatings containing microballoons and method for applying same |
US6808756B2 (en) | 2003-01-17 | 2004-10-26 | Sulzer Metco (Canada) Inc. | Thermal spray composition and method of deposition for abradable seals |
DE502004010739D1 (de) | 2003-12-17 | 2010-03-25 | Sulzer Metco Us Inc | Strömungsmaschine mit einer keramischen Anstreifschicht |
US7165946B2 (en) | 2004-06-21 | 2007-01-23 | Solar Turbine Incorporated | Low-mid turbine temperature abradable coating |
US7927189B2 (en) | 2004-08-16 | 2011-04-19 | United Technologies Corporation | Superabrasive tool |
US7614847B2 (en) | 2004-11-24 | 2009-11-10 | General Electric Company | Pattern for the surface of a turbine shroud |
US7449254B2 (en) | 2005-01-21 | 2008-11-11 | General Electric Company | Environmental barrier coating with physical barrier layer for silicon-comprising materials |
US7354651B2 (en) | 2005-06-13 | 2008-04-08 | General Electric Company | Bond coat for corrosion resistant EBC for silicon-containing substrate and processes for preparing same |
US7442444B2 (en) | 2005-06-13 | 2008-10-28 | General Electric Company | Bond coat for silicon-containing substrate for EBC and processes for preparing same |
ATE405686T1 (de) | 2005-06-16 | 2008-09-15 | Sulzer Metco Us Inc | Aluminiumoxid dotierter verschleissbarer keramischer werkstoff |
EP1743957A1 (de) | 2005-07-14 | 2007-01-17 | Sulzer Metco (US) Inc. | Verfahren zum Behandeln der Schaufelspitze einer Turbinenschaufel sowie mit einem solchen Verfahren behandelte Turbinenschaufel |
US20080107920A1 (en) * | 2006-01-06 | 2008-05-08 | Raymond Grant Rowe | Thermal barrier coated articles and methods of making the same |
CA2585992C (en) | 2006-06-08 | 2014-06-17 | Sulzer Metco (Us) Inc. | Dysprosia stabilized zirconia abradable |
US7604455B2 (en) | 2006-08-15 | 2009-10-20 | Siemens Energy, Inc. | Rotor disc assembly with abrasive insert |
US8017240B2 (en) | 2006-09-28 | 2011-09-13 | United Technologies Corporation | Ternary carbide and nitride thermal spray abradable seal material |
US8038388B2 (en) | 2007-03-05 | 2011-10-18 | United Technologies Corporation | Abradable component for a gas turbine engine |
EP2171124B1 (en) * | 2007-05-04 | 2011-09-14 | MTU Aero Engines AG | Method for manufacturing an abrasive coating on a gas turbine component |
JP5074123B2 (ja) * | 2007-08-08 | 2012-11-14 | 株式会社日立製作所 | 高温耐摩耗性部材及び高温用耐摩耗部材の製造方法 |
US8047773B2 (en) | 2007-08-23 | 2011-11-01 | General Electric Company | Gas turbine shroud support apparatus |
US20100028711A1 (en) * | 2008-07-29 | 2010-02-04 | General Electric Company | Thermal barrier coatings and methods of producing same |
US8365405B2 (en) | 2008-08-27 | 2013-02-05 | United Technologies Corp. | Preforms and related methods for repairing abradable seals of gas turbine engines |
GB0822703D0 (en) | 2008-12-15 | 2009-01-21 | Rolls Royce Plc | A component having an abrasive layer and a method of applying an abrasive layer on a component |
US8309197B2 (en) | 2008-12-17 | 2012-11-13 | Teledyne Scientific & Imaging, Llc | Integral abradable seals |
EP2202264B1 (fr) | 2008-12-24 | 2018-04-18 | Safran Aero Boosters SA | Procédé de fabrication par moulage d'un élément structurel de machine avec une surface abradable |
JP5112286B2 (ja) * | 2008-12-26 | 2013-01-09 | 株式会社東芝 | 蒸気タービン翼及び蒸気タービン |
DE102009012945A1 (de) | 2009-03-12 | 2010-09-16 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung einer abrasiven Beschichtung und Bauteil für eine Turbomaschine |
US8186946B2 (en) | 2009-04-17 | 2012-05-29 | United Technologies Corporation | Abrasive thermal coating |
US8172519B2 (en) | 2009-05-06 | 2012-05-08 | General Electric Company | Abradable seals |
JP5210984B2 (ja) | 2009-06-29 | 2013-06-12 | 株式会社日立製作所 | タービン用高信頼性メタルシール材 |
US20110164961A1 (en) | 2009-07-14 | 2011-07-07 | Thomas Alan Taylor | Coating system for clearance control in rotating machinery |
WO2011008211A1 (en) | 2009-07-16 | 2011-01-20 | Bell Helicopter Textron Inc. | Method of applying abrasion resistant materials to rotors |
KR20110008398A (ko) | 2009-07-20 | 2011-01-27 | 삼성전자주식회사 | 막 구조물, 이를 포함하는 커패시터 및 그 제조 방법 |
US20110027573A1 (en) | 2009-08-03 | 2011-02-03 | United Technologies Corporation | Lubricated Abradable Coating |
IT1396362B1 (it) | 2009-10-30 | 2012-11-19 | Nuovo Pignone Spa | Macchina con righe in rilievo che possono essere abrase e metodo. |
EP2317079B1 (en) | 2009-10-30 | 2020-05-20 | Ansaldo Energia Switzerland AG | Abradable coating system |
GB2475850A (en) | 2009-12-02 | 2011-06-08 | Rolls Royce Plc | An Abrasive Layer and a Method Of Applying an Abrasive Layer on a Turbomachine Component |
IT1397706B1 (it) | 2009-12-22 | 2013-01-24 | Nuovo Pignone Spa | Tenuta che si puo' abradere con spostamento assiale. |
DE102009060570A1 (de) | 2009-12-23 | 2011-07-28 | Lufthansa Technik AG, 22335 | Verfahren zum Herstellen einer Rotor/Statordichtung einer Gasturbine |
JP5767248B2 (ja) | 2010-01-11 | 2015-08-19 | ロールス−ロイス コーポレイション | 環境障壁コーティングに加わる熱又は機械的応力を軽減するための特徴体 |
JP5490736B2 (ja) | 2010-01-25 | 2014-05-14 | 株式会社日立製作所 | セラミックアブレーダブルコーテイングを有するガスタービン用シュラウド |
WO2011100311A1 (en) | 2010-02-09 | 2011-08-18 | Rolls-Royce Corporation | Abradable ceramic coatings and coating systems |
SG173932A1 (en) | 2010-02-25 | 2011-09-29 | United Technologies Corp | Repair of a coating on a turbine component |
DE102010010595A1 (de) | 2010-03-08 | 2011-09-08 | Lufthansa Technik Ag | Verfahren zur Reparatur von Dichtsegmenten in der Rotor-/Statordichtung einer Gasturbine |
CH702980A1 (de) | 2010-03-31 | 2011-10-14 | Alstom Technology Ltd | Dichtstruktur an einem Deckband einer Turbinenlaufschaufel. |
DE102010019958B4 (de) | 2010-05-08 | 2016-05-04 | MTU Aero Engines AG | Verfahren zur Herstellung eines Einlaufbelags |
US8770926B2 (en) | 2010-10-25 | 2014-07-08 | United Technologies Corporation | Rough dense ceramic sealing surface in turbomachines |
US9169740B2 (en) | 2010-10-25 | 2015-10-27 | United Technologies Corporation | Friable ceramic rotor shaft abrasive coating |
US20120099971A1 (en) | 2010-10-25 | 2012-04-26 | United Technologies Corporation | Self dressing, mildly abrasive coating for clearance control |
-
2012
- 2012-11-28 US US13/687,369 patent/US9598973B2/en active Active
-
2013
- 2013-11-27 AU AU2013351191A patent/AU2013351191A1/en not_active Abandoned
- 2013-11-27 CA CA2891497A patent/CA2891497A1/en not_active Abandoned
- 2013-11-27 BR BR112015012277A patent/BR112015012277B8/pt not_active IP Right Cessation
- 2013-11-27 CN CN201380062147.7A patent/CN104937217A/zh active Pending
- 2013-11-27 MX MX2015006730A patent/MX2015006730A/es unknown
- 2013-11-27 EP EP13802299.1A patent/EP2925971B1/en active Active
- 2013-11-27 JP JP2015543477A patent/JP6340010B2/ja active Active
- 2013-11-27 WO PCT/EP2013/074893 patent/WO2014083069A1/en active Application Filing
- 2013-11-27 KR KR1020157016152A patent/KR102170569B1/ko active IP Right Grant
- 2013-11-27 TR TR2019/05293T patent/TR201905293T4/tr unknown
Also Published As
Publication number | Publication date |
---|---|
US9598973B2 (en) | 2017-03-21 |
JP2016508202A (ja) | 2016-03-17 |
CA2891497A1 (en) | 2014-06-05 |
WO2014083069A1 (en) | 2014-06-05 |
KR102170569B1 (ko) | 2020-10-28 |
CN104937217A (zh) | 2015-09-23 |
BR112015012277B8 (pt) | 2022-10-18 |
EP2925971B1 (en) | 2019-01-09 |
AU2013351191A1 (en) | 2015-07-09 |
MX2015006730A (es) | 2015-08-06 |
US20140147242A1 (en) | 2014-05-29 |
JP6340010B2 (ja) | 2018-06-06 |
KR20150088278A (ko) | 2015-07-31 |
BR112015012277B1 (pt) | 2021-12-07 |
EP2925971A1 (en) | 2015-10-07 |
BR112015012277A2 (pt) | 2018-12-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
TR201905293T4 (tr) | Turbo maki̇nelerde kullanima yöneli̇k sizdirmazlik si̇stemleri̇ ve bunlarin üreti̇lmesi̇ne yöneli̇k yöntemler | |
ES2565657T3 (es) | Cuchillas de máquina de afeitar con un radio de punta grande | |
GB2547605A (en) | Rotating superhard cutting element | |
PH12016000209A1 (en) | Semiconductor die singulation method | |
CL2014002509A1 (es) | Una composicion que comprende por lo menos una fuente de boro y por lo menos una fuente de silicio; producto que comprende sustrato y la composicion; un metodo para proporcionar un producto recubierto; uso de la composicion. | |
IN2012DN06723A (tr) | ||
JP2013014129A5 (ja) | スクライビングホイール及びスクライブ方法 | |
EP2537822A3 (en) | Composite article including silicon oxycarbide layer | |
MX2019009858A (es) | Cuchilla de rasuradora. | |
EP3615705A4 (en) | HIGHLY ADHESIVE DIAMOND LAYER WITH BORON-DOPED GRADIENT ON A WC-CO CUTTING TOOL | |
MX2011012194A (es) | Recubrimiento de hoja de rasuradora. | |
WO2011150326A3 (en) | Non-abrasive back coat for coated abrasives | |
MX2019009460A (es) | Cuchilla de rasuradora. | |
MX2017008324A (es) | Hoja de afeitar. | |
MX2015006855A (es) | Cuchilla de sierra que tiene dientes de diferentes materiales y metodo para su fabricación. | |
RU2016122446A (ru) | Режущий инструмент с износостойким покрытием | |
MY185161A (en) | Fixed abrasive grain wire saw, its manufacturing method, and method of cutting workpiece by using it | |
JP2019513161A5 (tr) | ||
MX352925B (es) | Papel de lija de grano grueso con capa de recubrimiento no deslizante. | |
EP3067194A3 (en) | Manufacturing method of honeycomb structure, and grinding wheel | |
SE0800538L (sv) | Oxidbelagt skärverktygsskär för spånavskiljande bearbetning av stål | |
IN2013CH05964A (tr) | ||
CN104441111A (zh) | 木工铣刀 | |
MX2020002034A (es) | Elemento de lijado y metodo para fabricar un elemento de lijado. | |
JP2013107204A5 (tr) |