DE60302077D1 - Befestiganordnung für den Statorring einer Turbomaschine - Google Patents
Befestiganordnung für den Statorring einer TurbomaschineInfo
- Publication number
- DE60302077D1 DE60302077D1 DE60302077T DE60302077T DE60302077D1 DE 60302077 D1 DE60302077 D1 DE 60302077D1 DE 60302077 T DE60302077 T DE 60302077T DE 60302077 T DE60302077 T DE 60302077T DE 60302077 D1 DE60302077 D1 DE 60302077D1
- Authority
- DE
- Germany
- Prior art keywords
- turbomachine
- fastening arrangement
- stator ring
- stator
- ring
- 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.)
- Expired - Lifetime
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
- F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
-
- 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
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0201460A FR2835563B1 (fr) | 2002-02-07 | 2002-02-07 | Agencement d'accrochage de secteurs en arc de cercle de distributeur porteur d'aubes |
FR0201460 | 2002-02-07 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60302077D1 true DE60302077D1 (de) | 2005-12-08 |
DE60302077T2 DE60302077T2 (de) | 2006-07-20 |
Family
ID=27589603
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60302077T Expired - Lifetime DE60302077T2 (de) | 2002-02-07 | 2003-02-05 | Befestiganordnung für den Statorring einer Turbomaschine |
Country Status (11)
Country | Link |
---|---|
US (2) | US20030146578A1 (de) |
EP (1) | EP1335113B1 (de) |
JP (1) | JP4087720B2 (de) |
CN (1) | CN100357569C (de) |
CA (1) | CA2418357C (de) |
DE (1) | DE60302077T2 (de) |
ES (1) | ES2250844T3 (de) |
FR (1) | FR2835563B1 (de) |
MA (1) | MA25948A1 (de) |
RU (1) | RU2311539C2 (de) |
UA (1) | UA76424C2 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2829525B1 (fr) * | 2001-09-13 | 2004-03-12 | Snecma Moteurs | Assemblage de secteurs d'un distributeur de turbine a un carter |
DE102004016222A1 (de) * | 2004-03-26 | 2005-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Anordnung zur selbsttätigen Laufspalteinstellung bei einer zwei- oder mehrstufigen Turbine |
US7637110B2 (en) * | 2005-11-30 | 2009-12-29 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
US7493771B2 (en) * | 2005-11-30 | 2009-02-24 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
US7523616B2 (en) * | 2005-11-30 | 2009-04-28 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
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 |
US7665960B2 (en) * | 2006-08-10 | 2010-02-23 | United Technologies Corporation | Turbine shroud thermal distortion control |
US7771160B2 (en) * | 2006-08-10 | 2010-08-10 | United Technologies Corporation | Ceramic shroud assembly |
FR2923525B1 (fr) * | 2007-11-13 | 2009-12-18 | Snecma | Etancheite d'un anneau de rotor dans un etage de turbine |
FR2928963B1 (fr) * | 2008-03-19 | 2017-12-08 | Snecma | Distributeur de turbine pour une turbomachine. |
FR2928961B1 (fr) * | 2008-03-19 | 2015-11-13 | Snecma | Distributeur sectorise pour une turbomachine. |
FR2930592B1 (fr) * | 2008-04-24 | 2010-04-30 | Snecma | Distributeur de turbine pour une turbomachine |
FR2939836B1 (fr) * | 2008-12-12 | 2015-05-15 | Snecma | Joint d'etancheite de plateforme dans un rotor de turbomachine |
FR2944554B1 (fr) * | 2009-04-16 | 2014-06-13 | Snecma | Turbine haute-pression de turbomachine |
US8167546B2 (en) * | 2009-09-01 | 2012-05-01 | United Technologies Corporation | Ceramic turbine shroud support |
US8608424B2 (en) * | 2009-10-09 | 2013-12-17 | General Electric Company | Contoured honeycomb seal for a turbomachine |
US8647055B2 (en) * | 2011-04-18 | 2014-02-11 | General Electric Company | Ceramic matrix composite shroud attachment system |
FR2974841B1 (fr) * | 2011-05-04 | 2013-06-07 | Snecma | Dispositif d'etancheite pour distributeur de turbine de turbomachine |
FR2981602B1 (fr) * | 2011-10-25 | 2017-02-17 | Snecma Propulsion Solide | Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs |
US9291061B2 (en) * | 2012-04-13 | 2016-03-22 | General Electric Company | Turbomachine blade tip shroud with parallel casing configuration |
WO2014163673A2 (en) | 2013-03-11 | 2014-10-09 | Bronwyn Power | Gas turbine engine flow path geometry |
EP2896796B1 (de) * | 2014-01-20 | 2019-09-18 | Safran Aero Boosters SA | Stator einer axialen Strömungsmaschine und zugehörige Strömungsmaschine |
FR3057015B1 (fr) * | 2016-09-30 | 2018-12-07 | Safran Aircraft Engines | Disque de rotor comportant une toile a epaisseur variable |
FR3083564B1 (fr) * | 2018-07-05 | 2021-07-09 | Safran Aircraft Engines | Turbine comportant un element abradable a position radiale ajustable |
RU190280U1 (ru) * | 2019-01-09 | 2019-06-25 | Публичное Акционерное Общество "Одк-Сатурн" | Устройство для фиксации сегментов сопловых лопаток в силовом корпусе статора турбины |
BE1027280B1 (fr) * | 2019-05-16 | 2020-12-15 | Safran Aero Boosters Sa | Carter de compresseur pour turbomachine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2623728A (en) * | 1945-01-16 | 1952-12-30 | Power Jets Res & Dev Ltd | Mounting of blades in compressors, turbines, and the like |
US2693904A (en) * | 1950-11-14 | 1954-11-09 | A V Roe Canada Ltd | Air bleed for compressors |
US2942844A (en) * | 1952-12-22 | 1960-06-28 | Gen Motors Corp | Turbine nozzle |
US2834537A (en) * | 1954-01-18 | 1958-05-13 | Ryan Aeronautical Co | Compressor stator structure |
US2858104A (en) * | 1954-02-04 | 1958-10-28 | A V Roe Canada Ltd | Adjustable gas turbine shroud ring segments |
GB856599A (en) * | 1958-06-16 | 1960-12-21 | Gen Motors Corp | Improvements relating to axial-flow compressors |
GB2078309B (en) * | 1980-05-31 | 1983-05-25 | Rolls Royce | Mounting nozzle guide vane assemblies |
GB2117843B (en) * | 1982-04-01 | 1985-11-06 | Rolls Royce | Compressor shrouds |
FR2683851A1 (fr) * | 1991-11-20 | 1993-05-21 | Snecma | Turbomachine equipee de moyens facilitant le reglage des jeux du stator entree stator et rotor. |
FR2685936A1 (fr) * | 1992-01-08 | 1993-07-09 | Snecma | Dispositif de controle des jeux d'un carter de compresseur de turbomachine. |
US5299910A (en) * | 1992-01-23 | 1994-04-05 | General Electric Company | Full-round compressor casing assembly in a gas turbine engine |
US5288208A (en) * | 1993-06-01 | 1994-02-22 | Cummins Richard L | Marine propeller block apparatus |
US5462403A (en) * | 1994-03-21 | 1995-10-31 | United Technologies Corporation | Compressor stator vane assembly |
US6341938B1 (en) * | 2000-03-10 | 2002-01-29 | General Electric Company | Methods and apparatus for minimizing thermal gradients within turbine shrouds |
-
2002
- 2002-02-07 FR FR0201460A patent/FR2835563B1/fr not_active Expired - Fee Related
-
2003
- 2003-01-31 JP JP2003024269A patent/JP4087720B2/ja not_active Expired - Lifetime
- 2003-02-04 CA CA2418357A patent/CA2418357C/en not_active Expired - Lifetime
- 2003-02-04 MA MA27026A patent/MA25948A1/fr unknown
- 2003-02-05 EP EP03290288A patent/EP1335113B1/de not_active Expired - Lifetime
- 2003-02-05 DE DE60302077T patent/DE60302077T2/de not_active Expired - Lifetime
- 2003-02-05 ES ES03290288T patent/ES2250844T3/es not_active Expired - Lifetime
- 2003-02-06 UA UA2003021092A patent/UA76424C2/uk unknown
- 2003-02-06 RU RU2003103610/06A patent/RU2311539C2/ru active
- 2003-02-06 US US10/359,222 patent/US20030146578A1/en not_active Abandoned
- 2003-02-07 CN CNB031217737A patent/CN100357569C/zh not_active Expired - Lifetime
-
2004
- 2004-10-05 US US10/957,690 patent/US7290982B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
UA76424C2 (uk) | 2006-08-15 |
FR2835563B1 (fr) | 2004-04-02 |
CA2418357C (en) | 2010-10-26 |
DE60302077T2 (de) | 2006-07-20 |
US7290982B2 (en) | 2007-11-06 |
CN1443927A (zh) | 2003-09-24 |
EP1335113B1 (de) | 2005-11-02 |
FR2835563A1 (fr) | 2003-08-08 |
US20050042081A1 (en) | 2005-02-24 |
JP2003269111A (ja) | 2003-09-25 |
CA2418357A1 (en) | 2003-08-07 |
EP1335113A1 (de) | 2003-08-13 |
ES2250844T3 (es) | 2006-04-16 |
MA25948A1 (fr) | 2003-12-31 |
CN100357569C (zh) | 2007-12-26 |
RU2311539C2 (ru) | 2007-11-27 |
JP4087720B2 (ja) | 2008-05-21 |
US20030146578A1 (en) | 2003-08-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |