BR112014000168A2 - roda de estator de motor de turbina e uma turbina ou um compressor que inclui tal roda de estator - Google Patents

roda de estator de motor de turbina e uma turbina ou um compressor que inclui tal roda de estator

Info

Publication number
BR112014000168A2
BR112014000168A2 BR112014000168A BR112014000168A BR112014000168A2 BR 112014000168 A2 BR112014000168 A2 BR 112014000168A2 BR 112014000168 A BR112014000168 A BR 112014000168A BR 112014000168 A BR112014000168 A BR 112014000168A BR 112014000168 A2 BR112014000168 A2 BR 112014000168A2
Authority
BR
Brazil
Prior art keywords
stator wheel
turbine
compressor
turbine engine
wheel
Prior art date
Application number
BR112014000168A
Other languages
English (en)
Other versions
BR112014000168B1 (pt
Inventor
Jean-Philippe Beaujard Antoine
Belmonte Olivier
Original Assignee
Herakles
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
Application filed by Herakles, Snecma filed Critical Herakles
Publication of BR112014000168A2 publication Critical patent/BR112014000168A2/pt
Publication of BR112014000168B1 publication Critical patent/BR112014000168B1/pt

Links

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F05D2300/222—Silicon
    • 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
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6033—Ceramic matrix composites [CMC]
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BR112014000168-5A 2011-07-22 2012-07-18 Roda de estator de turbomáquina, turbina de turbomáquina e compressor de turbomáquina que inclui tal roda de estator BR112014000168B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1156710A FR2978197B1 (fr) 2011-07-22 2011-07-22 Distributeur de turbine de turbomachine et turbine comportant un tel distributeur
FR1156710 2011-07-22
PCT/FR2012/051698 WO2013014367A1 (fr) 2011-07-22 2012-07-18 Roue fixe de turbomachine et turbine ou compresseur comportant une telle roue fixe

Publications (2)

Publication Number Publication Date
BR112014000168A2 true BR112014000168A2 (pt) 2017-02-07
BR112014000168B1 BR112014000168B1 (pt) 2021-08-31

Family

ID=46614554

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014000168-5A BR112014000168B1 (pt) 2011-07-22 2012-07-18 Roda de estator de turbomáquina, turbina de turbomáquina e compressor de turbomáquina que inclui tal roda de estator

Country Status (8)

Country Link
US (1) US9518472B2 (pt)
EP (1) EP2734708B1 (pt)
CN (1) CN103649469B (pt)
BR (1) BR112014000168B1 (pt)
CA (1) CA2842080C (pt)
FR (1) FR2978197B1 (pt)
RU (1) RU2611539C2 (pt)
WO (1) WO2013014367A1 (pt)

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DE102013210427A1 (de) * 2013-06-05 2014-12-11 Rolls-Royce Deutschland Ltd & Co Kg Deckbandanordnung für eine Strömungsmaschine
WO2014204574A2 (en) * 2013-06-21 2014-12-24 United Technologies Corporation Seals for gas turbine engine
ES2935815T3 (es) * 2013-09-06 2023-03-10 MTU Aero Engines AG (Des)montaje de un rotor de una turbina de gas, en particular delantero
GB201414587D0 (en) * 2014-08-18 2014-10-01 Rolls Royce Plc Mounting Arrangement For Aerofoil Body
FR3037097B1 (fr) * 2015-06-03 2017-06-23 Snecma Aube composite comprenant une plateforme munie d'un raidisseur
US10094239B2 (en) 2014-10-31 2018-10-09 Rolls-Royce North American Technologies Inc. Vane assembly for a gas turbine engine
US20160169033A1 (en) * 2014-12-15 2016-06-16 General Electric Company Apparatus and system for ceramic matrix composite attachment
US10982564B2 (en) 2014-12-15 2021-04-20 General Electric Company Apparatus and system for ceramic matrix composite attachment
EP3075471B1 (de) 2015-03-30 2021-11-03 MTU Aero Engines AG Verfahren zum generativen herstellen eines gasturbinengehäuseteils
JP6614407B2 (ja) * 2015-06-10 2019-12-04 株式会社Ｉｈｉ タービン
US10428665B2 (en) * 2015-12-11 2019-10-01 General Electric Company CMC thermal clamps
JP6763157B2 (ja) * 2016-03-11 2020-09-30 株式会社Ihi タービンノズル
FR3064024B1 (fr) * 2017-03-16 2019-09-13 Safran Aircraft Engines Ensemble d'anneau de turbine
US10301953B2 (en) * 2017-04-13 2019-05-28 General Electric Company Turbine nozzle with CMC aft Band
FR3069014B1 (fr) * 2017-07-11 2021-02-26 Safran Aircraft Engines Partie de turbomachine a tole ressort
WO2019240785A1 (en) * 2018-06-13 2019-12-19 Siemens Aktiengesellschaft Attachment arrangement for connecting components with different coefficient of thermal expansion
CN110284929B (zh) * 2019-07-19 2021-10-22 中国航发沈阳发动机研究所 一种涡轮机匣封严结构
FR3109402B1 (fr) 2020-04-15 2022-07-15 Safran Aircraft Engines Turbine pour une turbomachine

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BE533039A (pt) * 1953-11-06
US2968468A (en) * 1957-08-13 1961-01-17 Gen Motors Corp Sheet metal compressor casing
GB1484936A (en) * 1974-12-07 1977-09-08 Rolls Royce Gas turbine engines
US4639189A (en) * 1984-02-27 1987-01-27 Rockwell International Corporation Hollow, thermally-conditioned, turbine stator nozzle
US5226789A (en) * 1991-05-13 1993-07-13 General Electric Company Composite fan stator assembly
US5201846A (en) * 1991-11-29 1993-04-13 General Electric Company Low-pressure turbine heat shield
US5246756A (en) 1992-01-29 1993-09-21 Mobil Oil Corporation Release sheet
FR2732338B1 (fr) 1995-03-28 1997-06-13 Europ Propulsion Materiau composite protege contre l'oxydation par matrice auto-cicatrisante et son procede de fabrication
US6164903A (en) * 1998-12-22 2000-12-26 United Technologies Corporation Turbine vane mounting arrangement
EP1130218A1 (de) * 2000-03-02 2001-09-05 Siemens Aktiengesellschaft Turbine mit Dichtelement für die Fussplatten der Leitschaufeln
US6921246B2 (en) * 2002-12-20 2005-07-26 General Electric Company Methods and apparatus for assembling gas turbine nozzles
US20050135923A1 (en) * 2003-12-22 2005-06-23 Todd Coons Cooled vane cluster
RU2280767C2 (ru) * 2004-10-14 2006-07-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Способ изготовления рабочего колеса турбины из композиционных материалов
FR2883599B1 (fr) * 2005-03-23 2010-04-23 Snecma Moteurs Dispositif de liaison entre une enceinte de passage d'air de refroidissement et un aubage de distributeur dans une turbomachine
US8251652B2 (en) 2008-09-18 2012-08-28 Siemens Energy, Inc. Gas turbine vane platform element
FR2939129B1 (fr) 2008-11-28 2014-08-22 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.
FR2942638B1 (fr) * 2009-02-27 2015-08-21 Snecma Secteur angulaire de redresseur pour compresseur de turbomachine
FR2943942B1 (fr) 2009-04-06 2016-01-29 Snecma Procede de fabrication d'une aube de turbomachine en materiau composite
FR2946999B1 (fr) * 2009-06-18 2019-08-09 Safran Aircraft Engines Element de distributeur de turbine en cmc, procede pour sa fabrication, et distributeur et turbine a gaz l'incorporant.
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FR2953885B1 (fr) 2009-12-14 2012-02-10 Snecma Aube de turbomachine en materiau composite et procede pour sa fabrication

Also Published As

Publication number Publication date
CN103649469A (zh) 2014-03-19
CA2842080C (fr) 2018-10-30
FR2978197A1 (fr) 2013-01-25
FR2978197B1 (fr) 2015-12-25
US20140147264A1 (en) 2014-05-29
EP2734708B1 (fr) 2017-04-05
BR112014000168B1 (pt) 2021-08-31
EP2734708A1 (fr) 2014-05-28
CA2842080A1 (fr) 2013-01-31
CN103649469B (zh) 2015-11-25
WO2013014367A1 (fr) 2013-01-31
RU2014106552A (ru) 2015-08-27
US9518472B2 (en) 2016-12-13
RU2611539C2 (ru) 2017-02-28

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 18/07/2012, OBSERVADAS AS CONDICOES LEGAIS.