EP2083148A3 - Turbine à gaz dotée d'un compresseur muni d'un revêtement de rodage et procédé de rodage des extrémités libres des aubes d'un compresseur de turbine à gaz - Google Patents
Turbine à gaz dotée d'un compresseur muni d'un revêtement de rodage et procédé de rodage des extrémités libres des aubes d'un compresseur de turbine à gaz Download PDFInfo
- Publication number
- EP2083148A3 EP2083148A3 EP09000952A EP09000952A EP2083148A3 EP 2083148 A3 EP2083148 A3 EP 2083148A3 EP 09000952 A EP09000952 A EP 09000952A EP 09000952 A EP09000952 A EP 09000952A EP 2083148 A3 EP2083148 A3 EP 2083148A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- gas turbine
- compressor
- blades
- lapping
- run
- 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.)
- Withdrawn
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
- 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
- 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
- F01D11/10—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using sealing fluid, e.g. steam
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/0238—Details or means for fluid reinjection
-
- 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
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
-
- 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
- F05D2300/50—Intrinsic material properties or characteristics
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200810005480 DE102008005480A1 (de) | 2008-01-23 | 2008-01-23 | Gasturbine mit einem Verdichter mit Einlaufschicht mit luftaushärtendem Material |
DE102008005479A DE102008005479A1 (de) | 2008-01-23 | 2008-01-23 | Gasturbine mit einem Verdichter mit flüssigkeitsbeaufschlagter Einlaufschicht |
DE102008005482A DE102008005482A1 (de) | 2008-01-23 | 2008-01-23 | Gasturbine mit einem Verdichter mit selbstheilender Einlaufschicht |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2083148A2 EP2083148A2 (fr) | 2009-07-29 |
EP2083148A3 true EP2083148A3 (fr) | 2012-06-06 |
Family
ID=40469804
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09000952A Withdrawn EP2083148A3 (fr) | 2008-01-23 | 2009-01-23 | Turbine à gaz dotée d'un compresseur muni d'un revêtement de rodage et procédé de rodage des extrémités libres des aubes d'un compresseur de turbine à gaz |
Country Status (2)
Country | Link |
---|---|
US (1) | US8257016B2 (fr) |
EP (1) | EP2083148A3 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9068507B2 (en) * | 2011-11-16 | 2015-06-30 | General Electric Company | Compressor having purge circuit and method of purging |
EP2886804B1 (fr) * | 2013-12-20 | 2017-08-16 | Safran Aero Boosters SA | Dispositif d'étanchéité pour un compresseur de turbomachine |
BE1024735B1 (fr) | 2016-11-15 | 2018-06-19 | Safran Aero Boosters Sa | Virole antigivre de compresseur de turbomachine axiale |
CN108412761B (zh) * | 2018-04-12 | 2024-03-01 | 河北昊方新能源科技有限公司 | 喷液冷却涡旋式空气压缩机 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0751280A1 (fr) * | 1995-05-31 | 1997-01-02 | United Technologies Corporation | Paroi avec plenum pour l'alignement de l'écoulement dans les aubes de compresseur |
US20050141990A1 (en) * | 2003-11-26 | 2005-06-30 | Volker Guemmer | Turbomachine wtih fluid supply |
WO2005114013A1 (fr) * | 2004-05-20 | 2005-12-01 | Rolls-Royce Plc | Dispositif de confinement |
DE102004031255A1 (de) * | 2004-06-29 | 2006-01-19 | Mtu Aero Engines Gmbh | Einlaufbelag |
US20060153673A1 (en) * | 2004-11-17 | 2006-07-13 | Volker Guemmer | Turbomachine exerting dynamic influence on the flow |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1061467B (de) | 1956-12-22 | 1959-07-16 | Gen Electric | Abdichtung zwischen Laeufer und Gehaeuse eines Kreiselverdichters, bei der der Laeufer das noetige Spiel selbst aus der Dichtung herausschabt |
DE1913065C3 (de) | 1969-03-14 | 1974-10-10 | General Electric Co., Schenectady, N.Y. (V.St.A.) | Flüssigkeitskühlung von Laufschaufeln einer Gasturbine |
FR2401310A1 (fr) | 1977-08-26 | 1979-03-23 | Snecma | Carter de turbine de moteur a reaction |
FR2438165A1 (fr) | 1978-10-06 | 1980-04-30 | Snecma | Dispositif de regulation de temperature pour turbines a gaz |
GB2053367B (en) | 1979-07-12 | 1983-01-26 | Rolls Royce | Cooled shroud for a gas turbine engine |
US4269903A (en) * | 1979-09-06 | 1981-05-26 | General Motors Corporation | Abradable ceramic seal and method of making same |
GB2095749B (en) | 1981-03-25 | 1984-12-12 | Rolls Royce | Gas turbine engine having improved resistance for foreign object ingestion damage |
JPS6345402A (ja) | 1986-08-11 | 1988-02-26 | Nagasu Hideo | 流体機械 |
US5161942A (en) | 1990-10-24 | 1992-11-10 | Westinghouse Electric Corp. | Moisture drainage of honeycomb seals |
US6196790B1 (en) | 1998-12-17 | 2001-03-06 | United Technologies Corporation | Seal assembly for an intershaft seal in a gas turbine engine |
US6425736B1 (en) | 1999-08-09 | 2002-07-30 | United Technologies Corporation | Stator assembly for a rotary machine and method for making the stator assembly |
EP1245792A1 (fr) | 2001-03-30 | 2002-10-02 | Siemens Aktiengesellschaft | Virole de turbine refroidie et procédé pour sa fabrication |
GB0117110D0 (en) | 2001-07-13 | 2001-09-05 | Siemens Ag | Coolable segment for a turbomachinery and combustion turbine |
DE10337094A1 (de) | 2003-08-12 | 2005-03-03 | Mtu Aero Engines Gmbh | Einlaufbelag für Gasturbinen sowie Verfahren zur Herstellung desselben |
SE525924C2 (sv) * | 2003-09-25 | 2005-05-24 | Gas Turbine Efficiency Ab | Munstycke samt metod för rengöring av gasturbinkompressorer |
US7086233B2 (en) | 2003-11-26 | 2006-08-08 | Siemens Power Generation, Inc. | Blade tip clearance control |
DE10360164A1 (de) | 2003-12-20 | 2005-07-21 | Mtu Aero Engines Gmbh | Gasturbinenbauteil |
DE602004028871D1 (de) * | 2004-02-16 | 2010-10-07 | Gas Turbine Efficiency Ab | Verfahren und vorrichtung zum reinigen eines turbofan-gasturbinentriebwerks |
EP1717419B1 (fr) | 2005-04-28 | 2010-10-13 | Siemens Aktiengesellschaft | Méthode et dispositif pour l'adjustement d'un jeu radial d'un compresseur axial dans une turbomachine |
DE102005058324A1 (de) | 2005-12-07 | 2007-06-14 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen eines Einlaufbelags |
-
2009
- 2009-01-23 EP EP09000952A patent/EP2083148A3/fr not_active Withdrawn
- 2009-01-23 US US12/320,368 patent/US8257016B2/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0751280A1 (fr) * | 1995-05-31 | 1997-01-02 | United Technologies Corporation | Paroi avec plenum pour l'alignement de l'écoulement dans les aubes de compresseur |
US20050141990A1 (en) * | 2003-11-26 | 2005-06-30 | Volker Guemmer | Turbomachine wtih fluid supply |
WO2005114013A1 (fr) * | 2004-05-20 | 2005-12-01 | Rolls-Royce Plc | Dispositif de confinement |
DE102004031255A1 (de) * | 2004-06-29 | 2006-01-19 | Mtu Aero Engines Gmbh | Einlaufbelag |
US20060153673A1 (en) * | 2004-11-17 | 2006-07-13 | Volker Guemmer | Turbomachine exerting dynamic influence on the flow |
Also Published As
Publication number | Publication date |
---|---|
US8257016B2 (en) | 2012-09-04 |
EP2083148A2 (fr) | 2009-07-29 |
US20090196730A1 (en) | 2009-08-06 |
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