BR112014013617A2 - dispositivo desbloqueável de parada axial de uma coroa de estanqueidade contatada por uma roda móvel de módulo de turbomáquina de aeronave - Google Patents
dispositivo desbloqueável de parada axial de uma coroa de estanqueidade contatada por uma roda móvel de módulo de turbomáquina de aeronaveInfo
- Publication number
- BR112014013617A2 BR112014013617A2 BR112014013617A BR112014013617A BR112014013617A2 BR 112014013617 A2 BR112014013617 A2 BR 112014013617A2 BR 112014013617 A BR112014013617 A BR 112014013617A BR 112014013617 A BR112014013617 A BR 112014013617A BR 112014013617 A2 BR112014013617 A2 BR 112014013617A2
- Authority
- BR
- Brazil
- Prior art keywords
- axis
- axial stop
- movable wheel
- stop device
- unlockable
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- 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
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/28—Arrangement of seals
-
- 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
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/644—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins for adjusting the position or the alignment, e.g. wedges or eccenters
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/14—Casings or housings protecting or supporting assemblies within
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/312—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being parallel to each other
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/35—Arrangement of components rotated
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
-
- 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
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Abstract
resumo patente de invenção: "dispositivo desbloqueável de parada axial de uma coroa de estanqueidade contatada por uma roda móvel de módulo de turbomáquina de aeronave". a presente invenção refere-se a um dispositivo (20) de parada axial de uma coroa de estanqueidade (12) em material passível de abrasão contatada pela periferia de uma roda móvel de módulo de turbomáquina de aero, o dispositivo apresentando um eixo central de referência, dito primeiro eixo (4) e compreendendo: - um suporte (30) que apresenta uma abertura de suporte (32) que define uma pista circular (34) centrada sobre um segundo eixo (36) espaçado do eixo (4); - uma peça de batente axial (46) apresentando uma passagem de extração (48) centrada sobre um terceiro eixo (50) espaçado do eixo (36) e definindo em sua periferia uma pista circular complementar (52) que coopera com a pista (34), de maneira a permitir uma rotação da peça (46), segundo o eixo (36), entre uma posição de batente axial para a coroa de estanqueidade , e uma posição de extração dessa coroa pela passagem de extração (48).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1161233 | 2011-12-06 | ||
FR1161233A FR2983518B1 (fr) | 2011-12-06 | 2011-12-06 | Dispositif deverrouillable d'arret axial d'une couronne d'etancheite contactee par une roue mobile de module de turbomachine d'aeronef |
PCT/FR2012/052788 WO2013083905A1 (fr) | 2011-12-06 | 2012-12-04 | Dispositif deverrouillable d'arret axial d'une couronne d'etancheite contactee par une roue mobile de module de turbomachine d'aeronef |
Publications (3)
Publication Number | Publication Date |
---|---|
BR112014013617A8 BR112014013617A8 (pt) | 2017-06-13 |
BR112014013617A2 true BR112014013617A2 (pt) | 2017-06-13 |
BR112014013617B1 BR112014013617B1 (pt) | 2021-09-21 |
Family
ID=47505198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014013617-3A BR112014013617B1 (pt) | 2011-12-06 | 2012-12-04 | Dispositivo de parada axial de uma coroa de estanqueidade, módulo de turbomáquina de aeronave e turbomáquina de aeronave |
Country Status (9)
Country | Link |
---|---|
US (1) | US9957896B2 (pt) |
EP (1) | EP2788589B1 (pt) |
JP (1) | JP6013501B2 (pt) |
CN (1) | CN103975132B (pt) |
BR (1) | BR112014013617B1 (pt) |
CA (1) | CA2856702C (pt) |
FR (1) | FR2983518B1 (pt) |
RU (1) | RU2604475C2 (pt) |
WO (1) | WO2013083905A1 (pt) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9759427B2 (en) * | 2013-11-01 | 2017-09-12 | General Electric Company | Interface assembly for a combustor |
US10215099B2 (en) * | 2015-02-06 | 2019-02-26 | United Technologies Corporation | System and method for limiting movement of a retainer ring of a gas turbine engine |
US10415622B2 (en) * | 2016-05-03 | 2019-09-17 | General Electric Company | Method and system for hybrid gang channel bolted joint |
US11421555B2 (en) | 2018-12-07 | 2022-08-23 | Raytheon Technologies Corporation | Case flange with scallop features |
FR3100838B1 (fr) * | 2019-09-13 | 2021-10-01 | Safran Aircraft Engines | Anneau d’etancheite de turbomachine |
GB202203012D0 (en) | 2022-03-04 | 2022-04-20 | Rolls Royce Plc | Brush seal |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4222708A (en) * | 1978-06-26 | 1980-09-16 | General Electric Company | Method and apparatus for reducing eccentricity in a turbomachine |
FR2452601A1 (fr) * | 1979-03-30 | 1980-10-24 | Snecma | Support amovible de revetement d'etancheite pour carter de soufflante de turboreacteur |
EP0844369B1 (en) * | 1996-11-23 | 2002-01-30 | ROLLS-ROYCE plc | A bladed rotor and surround assembly |
DE19756734A1 (de) * | 1997-12-19 | 1999-06-24 | Bmw Rolls Royce Gmbh | Passives Spalthaltungssystem einer Gasturbine |
US6435820B1 (en) * | 1999-08-25 | 2002-08-20 | General Electric Company | Shroud assembly having C-clip retainer |
DE10122464C1 (de) * | 2001-05-09 | 2002-03-07 | Mtu Aero Engines Gmbh | Mantelring |
JP4200846B2 (ja) * | 2003-07-04 | 2008-12-24 | 株式会社Ihi | シュラウドセグメント |
FR2875534B1 (fr) * | 2004-09-21 | 2006-12-22 | Snecma Moteurs Sa | Module de turbine pour moteur a turbine a gaz avec rotor comportant un corps monobloc |
FR2891583B1 (fr) * | 2005-09-30 | 2010-06-18 | Snecma | Turbine comportant des secteurs d'etancheite demontables par l'amont |
FR2899275A1 (fr) * | 2006-03-30 | 2007-10-05 | Snecma Sa | Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine |
FR2899274B1 (fr) * | 2006-03-30 | 2012-08-17 | Snecma | Dispositif de fixation de secteurs d'anneau autour d'une roue de turbine d'une turbomachine |
US7878756B2 (en) * | 2007-10-31 | 2011-02-01 | United Technologies Corporation | Systems and methods for controlling seal clearance in a turbine engine |
FR2938292B1 (fr) * | 2008-11-07 | 2010-12-24 | Snecma | Bride annulaire de fixation d'un element de rotor ou de stator dans une turbomachine |
FR2939470B1 (fr) | 2008-12-10 | 2011-01-07 | Snecma | Soufflante pour turbomachine comprenant un systeme d'equilibrage a trous borgnes de logement de masses |
-
2011
- 2011-12-06 FR FR1161233A patent/FR2983518B1/fr not_active Expired - Fee Related
-
2012
- 2012-12-04 WO PCT/FR2012/052788 patent/WO2013083905A1/fr active Application Filing
- 2012-12-04 CN CN201280060117.8A patent/CN103975132B/zh active Active
- 2012-12-04 CA CA2856702A patent/CA2856702C/fr active Active
- 2012-12-04 JP JP2014545329A patent/JP6013501B2/ja active Active
- 2012-12-04 RU RU2014127525/06A patent/RU2604475C2/ru active
- 2012-12-04 EP EP12810333.0A patent/EP2788589B1/fr active Active
- 2012-12-04 US US14/361,954 patent/US9957896B2/en active Active
- 2012-12-04 BR BR112014013617-3A patent/BR112014013617B1/pt active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
FR2983518A1 (fr) | 2013-06-07 |
JP6013501B2 (ja) | 2016-10-25 |
WO2013083905A1 (fr) | 2013-06-13 |
RU2604475C2 (ru) | 2016-12-10 |
CN103975132B (zh) | 2015-11-25 |
CA2856702A1 (fr) | 2013-06-13 |
CN103975132A (zh) | 2014-08-06 |
US20140341722A1 (en) | 2014-11-20 |
CA2856702C (fr) | 2019-07-16 |
JP2015500424A (ja) | 2015-01-05 |
BR112014013617A8 (pt) | 2017-06-13 |
EP2788589B1 (fr) | 2015-10-14 |
RU2014127525A (ru) | 2016-02-10 |
EP2788589A1 (fr) | 2014-10-15 |
BR112014013617B1 (pt) | 2021-09-21 |
US9957896B2 (en) | 2018-05-01 |
FR2983518B1 (fr) | 2014-02-07 |
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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] | ||
B350 | Update of information on the portal [chapter 15.35 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 04/12/2012, OBSERVADAS AS CONDICOES LEGAIS. |