CA2769217A1 - Secteur de virole exterieure pour couronne aubagee de stator de turbomachine d'aeronef, comprenant des cales amortisseuses de vibrations - Google Patents
Secteur de virole exterieure pour couronne aubagee de stator de turbomachine d'aeronef, comprenant des cales amortisseuses de vibrations Download PDFInfo
- Publication number
- CA2769217A1 CA2769217A1 CA2769217A CA2769217A CA2769217A1 CA 2769217 A1 CA2769217 A1 CA 2769217A1 CA 2769217 A CA2769217 A CA 2769217A CA 2769217 A CA2769217 A CA 2769217A CA 2769217 A1 CA2769217 A1 CA 2769217A1
- Authority
- CA
- Canada
- Prior art keywords
- sector
- outer shell
- shim
- vibration damping
- elementary sectors
- 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.)
- Abandoned
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
-
- 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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- 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
- F01D25/04—Antivibration arrangements
- F01D25/06—Antivibration arrangements for preventing blade vibration
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
- F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
-
- 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
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)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0955439A FR2948736B1 (fr) | 2009-07-31 | 2009-07-31 | Secteur de virole exterieure pour couronne aubagee de stator de turbomachine d'aeronef, comprenant des cales amortisseuses de vibrations |
FR0955439 | 2009-07-31 | ||
PCT/EP2010/061037 WO2011012679A2 (fr) | 2009-07-31 | 2010-07-29 | Secteur de virole exterieure pour couronne aubagee de stator de turbomachine d'aeronef, comprenant des cales amortisseuses de vibrations |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2769217A1 true CA2769217A1 (fr) | 2011-02-03 |
Family
ID=41800367
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2769217A Abandoned CA2769217A1 (fr) | 2009-07-31 | 2010-07-29 | Secteur de virole exterieure pour couronne aubagee de stator de turbomachine d'aeronef, comprenant des cales amortisseuses de vibrations |
Country Status (9)
Country | Link |
---|---|
US (1) | US20120128482A1 (fr) |
EP (1) | EP2459884B1 (fr) |
JP (1) | JP5697667B2 (fr) |
CN (1) | CN102472297A (fr) |
BR (1) | BR112012002304A2 (fr) |
CA (1) | CA2769217A1 (fr) |
FR (1) | FR2948736B1 (fr) |
RU (1) | RU2537997C2 (fr) |
WO (1) | WO2011012679A2 (fr) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2971022B1 (fr) | 2011-02-02 | 2013-01-04 | Snecma | Etage redresseur de compresseur pour une turbomachine |
US9610644B2 (en) * | 2011-02-08 | 2017-04-04 | United Technologies Corporation | Mate face brazing for turbine components |
US9546557B2 (en) * | 2012-06-29 | 2017-01-17 | General Electric Company | Nozzle, a nozzle hanger, and a ceramic to metal attachment system |
US9334756B2 (en) | 2012-09-28 | 2016-05-10 | United Technologies Corporation | Liner and method of assembly |
US10066548B2 (en) | 2013-03-15 | 2018-09-04 | United Technologies Corporation | Acoustic liner with varied properties |
DE102013212252A1 (de) * | 2013-06-26 | 2014-12-31 | Siemens Aktiengesellschaft | Turbine und Verfahren zur Anstreiferkennung |
FR3008455B1 (fr) * | 2013-07-09 | 2015-08-21 | Snecma | Redresseur pour compresseur comportant des moyens de rattrapage de jeu |
CN104440153B (zh) * | 2014-11-04 | 2017-06-06 | 中国南方航空工业(集团)有限公司 | 机匣内叶片加工阻尼装置 |
FR3029242B1 (fr) | 2014-11-28 | 2016-12-30 | Snecma | Aube de turbomachine, comprenant des cloisons entrecroisees pour la circulation d'air en direction du bord de fuite |
US10655482B2 (en) * | 2015-02-05 | 2020-05-19 | Rolls-Royce Corporation | Vane assemblies for gas turbine engines |
JP6689117B2 (ja) * | 2016-03-31 | 2020-04-28 | 三菱日立パワーシステムズ株式会社 | 軸流回転機械に装備される静翼環及び軸流回転機械 |
CN106988794B (zh) * | 2017-06-02 | 2018-12-14 | 中国航发南方工业有限公司 | 静子组合件夹紧方法及静子组合件 |
CN107747563B (zh) * | 2017-09-30 | 2020-04-10 | 中国航发沈阳发动机研究所 | 带阻尼的风扇机匣 |
US11242762B2 (en) * | 2019-11-21 | 2022-02-08 | Raytheon Technologies Corporation | Vane with collar |
FR3115819B1 (fr) * | 2020-11-02 | 2023-04-14 | Safran Aircraft Engines | Ensemble de stator de turbomachine d’aéronef, comprenant une structure externe formée de deux tronçons annulaires entourant une couronne aubagée de stator |
FR3119196B1 (fr) * | 2021-01-27 | 2022-12-23 | Safran Aircraft Engines | Rangée annulaire sectorisée d’aubes fixes |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2661147A (en) * | 1949-01-19 | 1953-12-01 | Ingersoll Rand Co | Blower blade fastening device |
SU453486A1 (ru) * | 1973-04-11 | 1974-12-15 | УСТРОЙСТВО дл ДЕМПФИРОВАНИЯ КОЛЕБАНИЙ РАБОЧИХ ЛОПАТОК ОСЕВОЙ ТУРБОМАШИНЫ | |
JPS5239807A (en) * | 1975-09-25 | 1977-03-28 | Mitsubishi Heavy Ind Ltd | Moving vane vibration controlling apparatus |
US5201850A (en) * | 1991-02-15 | 1993-04-13 | General Electric Company | Rotor tip shroud damper including damper wires |
DE4436731A1 (de) * | 1994-10-14 | 1996-04-18 | Abb Management Ag | Verdichter |
FR2831615B1 (fr) * | 2001-10-31 | 2004-01-02 | Snecma Moteurs | Redresseur fixe sectorise pour compresseur d'une turbomachine |
US6984108B2 (en) * | 2002-02-22 | 2006-01-10 | Drs Power Technology Inc. | Compressor stator vane |
US6733237B2 (en) * | 2002-04-02 | 2004-05-11 | Watson Cogeneration Company | Method and apparatus for mounting stator blades in axial flow compressors |
EP1510654A1 (fr) * | 2003-08-25 | 2005-03-02 | Siemens Aktiengesellschaft | Matrice unitaire d'aubes de turbine et procédé de fabrication d' une matrice unitaire d'aubes de turbine |
US7104752B2 (en) * | 2004-10-28 | 2006-09-12 | Florida Turbine Technologies, Inc. | Braided wire damper for segmented stator/rotor and method |
FR2902843A1 (fr) * | 2006-06-23 | 2007-12-28 | Snecma Sa | Secteur de redresseur de compresseur ou secteur de distributeur de turbomachine |
US7591634B2 (en) * | 2006-11-21 | 2009-09-22 | General Electric Company | Stator shim welding |
US7806655B2 (en) * | 2007-02-27 | 2010-10-05 | General Electric Company | Method and apparatus for assembling blade shims |
-
2009
- 2009-07-31 FR FR0955439A patent/FR2948736B1/fr active Active
-
2010
- 2010-07-29 US US13/386,496 patent/US20120128482A1/en not_active Abandoned
- 2010-07-29 RU RU2012107522/06A patent/RU2537997C2/ru not_active IP Right Cessation
- 2010-07-29 EP EP10739591.5A patent/EP2459884B1/fr active Active
- 2010-07-29 JP JP2012522172A patent/JP5697667B2/ja not_active Expired - Fee Related
- 2010-07-29 CA CA2769217A patent/CA2769217A1/fr not_active Abandoned
- 2010-07-29 BR BR112012002304A patent/BR112012002304A2/pt not_active IP Right Cessation
- 2010-07-29 WO PCT/EP2010/061037 patent/WO2011012679A2/fr active Application Filing
- 2010-07-29 CN CN2010800340319A patent/CN102472297A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
EP2459884A2 (fr) | 2012-06-06 |
US20120128482A1 (en) | 2012-05-24 |
FR2948736A1 (fr) | 2011-02-04 |
JP2013501181A (ja) | 2013-01-10 |
FR2948736B1 (fr) | 2011-09-23 |
EP2459884B1 (fr) | 2018-06-27 |
JP5697667B2 (ja) | 2015-04-08 |
WO2011012679A2 (fr) | 2011-02-03 |
RU2537997C2 (ru) | 2015-01-10 |
WO2011012679A3 (fr) | 2011-04-21 |
CN102472297A (zh) | 2012-05-23 |
BR112012002304A2 (pt) | 2016-05-31 |
RU2012107522A (ru) | 2013-09-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20120128482A1 (en) | Outer shell sector for a bladed ring for an aircraft turbomachine stator, including vibration damping shims | |
US9726033B2 (en) | Rotor wheel for a turbine engine | |
US5622475A (en) | Double rabbet rotor blade retention assembly | |
JP5995958B2 (ja) | ターボ機械タービンノズル用の封止装置 | |
EP2568121B1 (fr) | Support conique en gradin de garniture d'étanchéité et joint annulaire associé | |
EP2859188B1 (fr) | Plateforme d'aube de ventilateur | |
JP5427398B2 (ja) | ターボ機械のセクタ化されたノズル | |
EP2615256B1 (fr) | Joint à ressort en forme de t des turbines à gas | |
EP3042043B1 (fr) | Aube de turbomachine ayant un joint d'étanchéité à aile d'ange pour dissuadeurs de tailles différentes et procédé d'ajustement associé | |
US10184345B2 (en) | Cover plate assembly for a gas turbine engine | |
US9702259B2 (en) | Turbomachine compressor guide vanes assembly | |
US10871079B2 (en) | Turbine sealing assembly for turbomachinery | |
EP2636852B1 (fr) | Joint d'air interne hybride pour moteurs à turbine à gaz | |
WO2014168862A1 (fr) | Couvercle pour un ensemble rotor d'une turbine à gaz | |
CN115443370A (zh) | 用于涡轮发动机的涡轮 | |
US20200217217A1 (en) | Inter-blade platform seal | |
WO2018203924A1 (fr) | Moteur à turbine à gaz à joint de bordure | |
US20210172324A1 (en) | Pre-formed faceted turbine blade damper seal | |
EP3904638B1 (fr) | Ensemble rotor | |
EP3284911B1 (fr) | Moteur à turbine à gaz ayant une couche anti-usure pour carter de soufflante | |
US20230250732A1 (en) | Turbine for a turbine engine comprising heat-shielding foils | |
US20230125862A1 (en) | Turbomachine rotary assembly comprising an annular clamping part | |
US20200063590A1 (en) | Sealing member for gas turbine engine | |
US20200392855A1 (en) | Multi-blade vane for a turbomachine rotor and rotor comprising same |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Discontinued |
Effective date: 20160729 |