IN2014DN05853A - - Google Patents

Info

Publication number
IN2014DN05853A
IN2014DN05853A IN5853DEN2014A IN2014DN05853A IN 2014DN05853 A IN2014DN05853 A IN 2014DN05853A IN 5853DEN2014 A IN5853DEN2014 A IN 5853DEN2014A IN 2014DN05853 A IN2014DN05853 A IN 2014DN05853A
Authority
IN
India
Prior art keywords
shroud
upstream
platform
turbomachine
downstream
Prior art date
Application number
Other languages
English (en)
Inventor
Slim Bensalah
Arnaud Negri
BROU DE CUISSART Sébastien DIGARD
Guillaume Klein
Ba Phuc TANG
David Mathieu
Sibylle Doremus
Original Assignee
Snecma
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=46826732&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=IN2014DN05853(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Snecma filed Critical Snecma
Publication of IN2014DN05853A publication Critical patent/IN2014DN05853A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Component Parts Of Construction Machinery (AREA)
IN5853DEN2014 2012-01-17 2013-01-16 IN2014DN05853A (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1250435A FR2985759B1 (fr) 2012-01-17 2012-01-17 Aube mobile de turbomachine
FR1255586A FR2985760B1 (fr) 2012-01-17 2012-06-14 Aube mobile de turbomachine
PCT/FR2013/050096 WO2013107982A1 (fr) 2012-01-17 2013-01-16 Aube mobile de turbomachine et turbomachine correspondante

Publications (1)

Publication Number Publication Date
IN2014DN05853A true IN2014DN05853A (fr) 2015-05-22

Family

ID=46826732

Family Applications (1)

Application Number Title Priority Date Filing Date
IN5853DEN2014 IN2014DN05853A (fr) 2012-01-17 2013-01-16

Country Status (9)

Country Link
US (1) US10196907B2 (fr)
EP (1) EP2805020B2 (fr)
JP (2) JP6199309B2 (fr)
CN (1) CN104053857B (fr)
BR (1) BR112014017505B1 (fr)
CA (1) CA2861076C (fr)
FR (2) FR2985759B1 (fr)
IN (1) IN2014DN05853A (fr)
WO (1) WO2013107982A1 (fr)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013224199A1 (de) * 2013-11-27 2015-05-28 MTU Aero Engines AG Gasturbinen-Laufschaufel
WO2016072473A1 (fr) * 2014-11-06 2016-05-12 三菱日立パワーシステムズ株式会社 Pale de rotor de turbine à vapeur, procédé de fabrication de pale de rotor de turbine à vapeur et turbine à vapeur
PL3056677T3 (pl) 2015-02-12 2020-06-01 MTU Aero Engines AG Łopatka i maszyna przepływowa
US10710317B2 (en) * 2016-06-16 2020-07-14 Rolls-Royce North American Technologies Inc. Composite rotatable assembly for an axial-flow compressor
FR3065483B1 (fr) 2017-04-24 2020-08-07 Safran Aircraft Engines Dispositif d'etancheite entre rotor et stator de turbomachine
FR3066780B1 (fr) 2017-05-24 2019-07-19 Safran Aircraft Engines Piece amovible anti-usure pour talon d'aube
US10294801B2 (en) * 2017-07-25 2019-05-21 United Technologies Corporation Rotor blade having anti-wear surface
FR3072716B1 (fr) * 2017-10-20 2019-09-27 Safran Aircraft Engines Aube de rotor de turbomachine, turbomachine associee
FR3074838B1 (fr) * 2017-12-07 2020-10-16 Safran Aircraft Engines Aube mobile a calage variable sur la hauteur pour une turbomachine
FR3074813B1 (fr) * 2017-12-12 2022-05-06 Safran Aircraft Engines Procede de depot d'un materiau anti-usure sur un element aubage pour une turbomachine d'aeronef
FR3077601B1 (fr) * 2018-02-08 2020-01-17 Safran Aircraft Engines Aube de turbomachine d'aeronef
FR3077600B1 (fr) 2018-02-08 2020-03-06 Safran Aircraft Engines Aube de turbomachine d'aeronef
FR3078907B1 (fr) * 2018-03-15 2022-11-18 Safran Aircraft Engines Procede de fabrication d'une aube de rotor
FR3079847B1 (fr) * 2018-04-10 2023-11-10 Safran Aircraft Engines Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef
FR3079848B1 (fr) * 2018-04-10 2020-11-06 Safran Aircraft Engines Procede de depot d'un materiau anti-usure sur un element aubage pour une turbomachine d'aeronef
FR3084398B1 (fr) 2018-07-24 2021-04-16 Safran Aircraft Engines Aube de turbine
FR3085419B1 (fr) * 2018-09-05 2020-08-07 Safran Aircraft Engines Aube mobile
FR3085993B1 (fr) * 2018-09-17 2020-12-25 Safran Aircraft Engines Aube mobile pour une roue d'une turbomachine
DE102018215728A1 (de) 2018-09-17 2020-03-19 MTU Aero Engines AG Gasturbinen-Laufschaufel
FR3095833B1 (fr) 2019-05-07 2021-05-28 Safran Helicopter Engines Anneau d’etancheite pour une turbomachine d’aeronef
FR3107079B1 (fr) 2020-02-07 2022-01-21 Safran Aircraft Engines Aube de turbomachine d’aeronef
EP3865665A1 (fr) * 2020-02-11 2021-08-18 MTU Aero Engines AG Pale pour turbomachine avec un carénage

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6193203A (ja) * 1984-10-15 1986-05-12 Toshiba Corp 蒸気タ−ビン用羽根
JPH0240002A (ja) * 1988-07-29 1990-02-08 Hitachi Ltd ガスタービン動翼
US5083903A (en) * 1990-07-31 1992-01-28 General Electric Company Shroud insert for turbomachinery blade
DE4439950C2 (de) * 1994-11-09 2001-03-01 Mtu Muenchen Gmbh Metallisches Bauteil mit einer Verbundbeschichtung, Verwendung, sowie Verfahren zur Herstellung von metallischen Bauteilen
US6190124B1 (en) * 1997-11-26 2001-02-20 United Technologies Corporation Columnar zirconium oxide abrasive coating for a gas turbine engine seal system
US20040124231A1 (en) * 1999-06-29 2004-07-01 Hasz Wayne Charles Method for coating a substrate
JP4410357B2 (ja) * 1999-11-30 2010-02-03 三菱重工業株式会社 シュラウドコンタクト面のコーティング方法およびシュラウド付き動翼
US6793878B2 (en) 2000-10-27 2004-09-21 Wayne C. Blake Cobalt-based hard facing alloy
FR2825411B1 (fr) * 2001-05-31 2003-09-19 Snecma Moteurs Aube de turbine avec lechette d'etancheite
US6491498B1 (en) 2001-10-04 2002-12-10 Power Systems Mfg, Llc. Turbine blade pocket shroud
TWI272993B (en) 2002-10-09 2007-02-11 Ishikawajima Harima Heavy Ind Method for coating rotary member, rotary member, labyrinth seal structure and method for manufacturing rotary member
JP4096301B2 (ja) * 2002-10-09 2008-06-04 株式会社Ihi 動翼及びそのコーティング方法
JP4305928B2 (ja) 2002-10-09 2009-07-29 株式会社Ihi 回転体及びそのコーティング方法
JP4191621B2 (ja) * 2004-01-22 2008-12-03 三菱重工業株式会社 タービン動翼
JP4425746B2 (ja) 2004-08-25 2010-03-03 株式会社日立製作所 ガスタービン
US20060110254A1 (en) * 2004-11-24 2006-05-25 General Electric Company Thermal barrier coating for turbine bucket platform side faces and methods of application
GB0524735D0 (en) 2005-12-03 2006-01-11 Rolls Royce Plc Turbine blade
US8703044B2 (en) * 2006-01-03 2014-04-22 General Electric Company Machine components and methods of fabricating and repairing
US7527477B2 (en) * 2006-07-31 2009-05-05 General Electric Company Rotor blade and method of fabricating same
US7500824B2 (en) * 2006-08-22 2009-03-10 General Electric Company Angel wing abradable seal and sealing method
US7771171B2 (en) * 2006-12-14 2010-08-10 General Electric Company Systems for preventing wear on turbine blade tip shrouds
US20090097979A1 (en) 2007-07-31 2009-04-16 Omer Duane Erdmann Rotor blade
US8182228B2 (en) * 2007-08-16 2012-05-22 General Electric Company Turbine blade having midspan shroud with recessed wear pad and methods for manufacture
RU2486349C2 (ru) * 2007-10-25 2013-06-27 Сименс Акциенгезелльшафт Уплотнительный гребень, узел лопаток турбины и газовая турбина, содержащая такой узел лопаток
FR2923524B1 (fr) * 2007-11-12 2013-12-06 Snecma Aube metallique fabriquee par moulage et procede de fabrication de l'aube
US20090202344A1 (en) 2008-02-13 2009-08-13 General Electric Company Rotating assembly for a turbomachine
US8471168B2 (en) * 2008-06-19 2013-06-25 General Electric Company Methods of treating metal articles and articles made therefrom
ES2457846T3 (es) 2008-10-23 2014-04-29 Alstom Technology Ltd Paleta para una turbina de gas
EP2390466B1 (fr) * 2010-05-27 2018-04-25 Ansaldo Energia IP UK Limited Ensemble refroidissement d'une turbine à gaz
ES2698368T3 (es) 2010-07-01 2019-02-04 MTU Aero Engines AG Pala de turbina con cubierta de punta
JP5374563B2 (ja) * 2011-10-03 2013-12-25 三菱重工業株式会社 軸流タービン
US8894368B2 (en) * 2012-01-04 2014-11-25 General Electric Company Device and method for aligning tip shrouds

Also Published As

Publication number Publication date
FR2985760B1 (fr) 2014-03-07
US20150023793A1 (en) 2015-01-22
BR112014017505A2 (pt) 2017-06-13
BR112014017505B1 (pt) 2021-10-19
US10196907B2 (en) 2019-02-05
CN104053857A (zh) 2014-09-17
CN104053857B (zh) 2016-02-10
EP2805020B2 (fr) 2022-10-19
FR2985759B1 (fr) 2014-03-07
FR2985759A1 (fr) 2013-07-19
JP6199309B2 (ja) 2017-09-20
JP2018009576A (ja) 2018-01-18
CA2861076A1 (fr) 2013-07-25
BR112014017505A8 (pt) 2017-07-04
RU2014133548A (ru) 2016-03-10
WO2013107982A1 (fr) 2013-07-25
EP2805020A1 (fr) 2014-11-26
EP2805020B1 (fr) 2016-04-06
FR2985760A1 (fr) 2013-07-19
JP6518735B2 (ja) 2019-05-22
JP2015506438A (ja) 2015-03-02
CA2861076C (fr) 2020-03-24

Similar Documents

Publication Publication Date Title
IN2014DN05853A (fr)
WO2008120748A1 (fr) Paroi de turbomachine et turbomachine
GB201116666D0 (en) Sealing arrangement
BR112013030931A2 (pt) elemento de turbomáquina
FR2971539B1 (fr) Ensemble pale-plateforme pour ecoulement subsonique
JP2014134200A5 (fr)
EP2573364A3 (fr) Turbocompresseur à géometrie variable avec joint à labyrinthe pour ailettes
JP2013139770A5 (fr)
GB201312222D0 (en) Turbomachine with variable-pitch vortex generator
IN2014DN10346A (fr)
FR2971540B1 (fr) Ensemble pale-plateforme pour ecoulement supersonique
BR112015020506A2 (pt) lâmina de turbina
WO2013130181A3 (fr) Bord de fuite de plateforme de profil à faible perte
RU2011142880A (ru) Уплотнительное устройство турбоустановки и турбоустановка
RU2013116442A (ru) Турбомашина, турбина и установка, содержащая турбину
GB201212384D0 (en) A gas turbine engine
BR112014007517B8 (pt) Turbomáquina com ventoinha não carenada
WO2014099082A3 (fr) Profil d'emplanture de pale de turbine
MX2015011663A (es) Pala de turbina con una ranura para sello de pasador.
WO2013156725A3 (fr) Carter de compresseur a cavités au calage optimisé
FR2973829B1 (fr) Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant
IN2015DN00342A (fr)
RU2013104538A (ru) Комбинированная уплотнительная и балансировочная система для турбинного диска
MX2015011666A (es) Sello de pasador de pala de turbina.
RU2014146428A (ru) Пакет лопаток vtg турбонагнетателя в сборе с истираемым покрытием