DE69504053T2 - Unterstützung einer bürstendichtung und eine strömungsgünstige leitschaufelverkleidung - Google Patents
Unterstützung einer bürstendichtung und eine strömungsgünstige leitschaufelverkleidungInfo
- Publication number
- DE69504053T2 DE69504053T2 DE69504053T DE69504053T DE69504053T2 DE 69504053 T2 DE69504053 T2 DE 69504053T2 DE 69504053 T DE69504053 T DE 69504053T DE 69504053 T DE69504053 T DE 69504053T DE 69504053 T2 DE69504053 T2 DE 69504053T2
- Authority
- DE
- Germany
- Prior art keywords
- proof
- flow
- support
- brush gasket
- van
- 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
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
- F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
- F16J15/3284—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
- F16J15/3288—Filamentary structures, e.g. brush 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- 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
- F05D2240/55—Seals
- F05D2240/56—Brush seals
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/235,824 US5522698A (en) | 1994-04-29 | 1994-04-29 | Brush seal support and vane assembly windage cover |
PCT/US1995/004359 WO1995030071A1 (en) | 1994-04-29 | 1995-04-07 | Brush seal support and vane assembly windage cover |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69504053D1 DE69504053D1 (de) | 1998-09-17 |
DE69504053T2 true DE69504053T2 (de) | 1999-04-15 |
Family
ID=22887057
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69504053T Expired - Lifetime DE69504053T2 (de) | 1994-04-29 | 1995-04-07 | Unterstützung einer bürstendichtung und eine strömungsgünstige leitschaufelverkleidung |
Country Status (5)
Country | Link |
---|---|
US (1) | US5522698A (de) |
EP (1) | EP0757750B1 (de) |
JP (1) | JP3683272B2 (de) |
DE (1) | DE69504053T2 (de) |
WO (1) | WO1995030071A1 (de) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5707064A (en) * | 1993-01-08 | 1998-01-13 | The Texas A&M University System | Modulated pressure damper seal |
US5630590A (en) * | 1996-03-26 | 1997-05-20 | United Technologies Corporation | Method and apparatus for improving the airsealing effectiveness in a turbine engine |
US5961279A (en) * | 1996-05-31 | 1999-10-05 | Atlantic Richfield Company | Turbine power plant having minimal-contact brush seal augmented labyrinth seal |
US5755445A (en) * | 1996-08-23 | 1998-05-26 | Alliedsignal Inc. | Noncontacting finger seal with hydrodynamic foot portion |
JPH10259703A (ja) * | 1997-03-18 | 1998-09-29 | Mitsubishi Heavy Ind Ltd | ガスタービンのシュラウド及びプラットフォームシールシステム |
DE19712088C2 (de) * | 1997-03-22 | 1999-06-24 | Mtu Muenchen Gmbh | Bürstendichtung mit in Umfangsrichtung schräg gestellten Borsten |
US6206642B1 (en) * | 1998-12-17 | 2001-03-27 | United Technologies Corporation | Compressor blade for a gas turbine engine |
US6226975B1 (en) | 1999-09-14 | 2001-05-08 | Steven G. Ingistov | Turbine power plant having a floating brush seal |
DE19962244A1 (de) | 1999-12-22 | 2001-06-28 | Rolls Royce Deutschland | Kühlluft-Führungssystem im Hochdruck-Turbinenabschnitt eines Gasturbinen Triebwerkes |
US6471472B1 (en) | 2000-05-03 | 2002-10-29 | Siemens Canada Limited | Turbomachine shroud fibrous tip seal |
US6761034B2 (en) * | 2000-12-08 | 2004-07-13 | General Electroc Company | Structural cover for gas turbine engine bolted flanges |
US6517314B1 (en) * | 2001-11-05 | 2003-02-11 | General Electric Company | Method and apparatus for eliminating thermal bowing and axial thrust loads of steam turbine rotors |
US6644668B1 (en) | 2002-06-13 | 2003-11-11 | General Electric Company | Brush seal support |
JP4016845B2 (ja) | 2003-02-05 | 2007-12-05 | 株式会社Ihi | ガスタービンエンジン |
GB0424883D0 (en) * | 2004-11-11 | 2004-12-15 | Rolls Royce Plc | Seal structure |
US20060275108A1 (en) * | 2005-06-07 | 2006-12-07 | Memmen Robert L | Hammerhead fluid seal |
US20060275107A1 (en) * | 2005-06-07 | 2006-12-07 | Ioannis Alvanos | Combined blade attachment and disk lug fluid seal |
US20060275106A1 (en) * | 2005-06-07 | 2006-12-07 | Ioannis Alvanos | Blade neck fluid seal |
US8517666B2 (en) | 2005-09-12 | 2013-08-27 | United Technologies Corporation | Turbine cooling air sealing |
US7445424B1 (en) | 2006-04-22 | 2008-11-04 | Florida Turbine Technologies, Inc. | Passive thermostatic bypass flow control for a brush seal application |
US20080044284A1 (en) * | 2006-08-16 | 2008-02-21 | United Technologies Corporation | Segmented fluid seal assembly |
US20080061515A1 (en) * | 2006-09-08 | 2008-03-13 | Eric Durocher | Rim seal for a gas turbine engine |
US20080095616A1 (en) * | 2006-10-20 | 2008-04-24 | Ioannis Alvanos | Fluid brush seal with segment seal land |
US7578653B2 (en) * | 2006-12-19 | 2009-08-25 | General Electric Company | Ovate band turbine stage |
US20080145208A1 (en) * | 2006-12-19 | 2008-06-19 | General Electric Company | Bullnose seal turbine stage |
US8562285B2 (en) * | 2007-07-02 | 2013-10-22 | United Technologies Corporation | Angled on-board injector |
US8079803B2 (en) * | 2008-06-30 | 2011-12-20 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and cooling air supply structure thereof |
US8794640B2 (en) * | 2010-03-25 | 2014-08-05 | United Technologies Corporation | Turbine sealing system |
US8690527B2 (en) | 2010-06-30 | 2014-04-08 | Honeywell International Inc. | Flow discouraging systems and gas turbine engines |
US9169849B2 (en) | 2012-05-08 | 2015-10-27 | United Technologies Corporation | Gas turbine engine compressor stator seal |
US9291071B2 (en) | 2012-12-03 | 2016-03-22 | United Technologies Corporation | Turbine nozzle baffle |
EP2938868B1 (de) | 2012-12-29 | 2019-08-07 | United Technologies Corporation | Anordnung zur strömungsumlenkung |
JP6078353B2 (ja) * | 2013-01-23 | 2017-02-08 | 三菱日立パワーシステムズ株式会社 | ガスタービン |
EP2762684B1 (de) * | 2013-01-30 | 2021-03-03 | MTU Aero Engines AG | Dichtungsträger aus titanaluminid für eine strömungsmaschine |
EP3055512B1 (de) * | 2013-10-11 | 2019-07-31 | United Technologies Corporation | Nichtlinear ablenkende bürstendichtungsfläche |
US9677423B2 (en) | 2014-06-20 | 2017-06-13 | Solar Turbines Incorporated | Compressor aft hub sealing system |
US10094229B2 (en) | 2014-07-28 | 2018-10-09 | United Technologies Corporation | Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation |
EP3173670B1 (de) * | 2015-11-24 | 2020-07-29 | MTU Aero Engines GmbH | Bürstendichtungsanordnung für eine strömungsmaschine, einbausicherungsanordnung und strömungsmaschine |
US10633992B2 (en) | 2017-03-08 | 2020-04-28 | Pratt & Whitney Canada Corp. | Rim seal |
US11021962B2 (en) * | 2018-08-22 | 2021-06-01 | Raytheon Technologies Corporation | Turbulent air reducer for a gas turbine engine |
IT202100009716A1 (it) | 2021-04-16 | 2022-10-16 | Ge Avio Srl | Copertura di un dispositivo di fissaggio per una giunzione flangiata |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US885032A (en) * | 1907-06-24 | 1908-04-21 | Sebastian Ziani De Ferranti | Fluid packing. |
US4218189A (en) * | 1977-08-09 | 1980-08-19 | Rolls-Royce Limited | Sealing means for bladed rotor for a gas turbine engine |
US4411594A (en) * | 1979-06-30 | 1983-10-25 | Rolls-Royce Limited | Support member and a component supported thereby |
GB2070700B (en) * | 1980-03-01 | 1983-10-05 | Rolls Royce | Gas turbine seals |
GB2250790B (en) * | 1990-12-12 | 1994-04-27 | Rolls Royce Plc | Brush seal |
GB2258277B (en) * | 1991-07-29 | 1995-02-22 | Europ Gas Turbines Ltd | Brush seals |
US5114159A (en) * | 1991-08-05 | 1992-05-19 | United Technologies Corporation | Brush seal and damper |
US5181728A (en) * | 1991-09-23 | 1993-01-26 | General Electric Company | Trenched brush seal |
FR2691749B1 (fr) * | 1992-05-27 | 1994-07-22 | Snecma | Dispositif d'etancheite entre des etages d'aubes et un tambour tournant notamment pour eviter les fuites autour des etages d'aubes de redresseur . |
US5217348A (en) * | 1992-09-24 | 1993-06-08 | United Technologies Corporation | Turbine vane assembly with integrally cast cooling fluid nozzle |
-
1994
- 1994-04-29 US US08/235,824 patent/US5522698A/en not_active Expired - Lifetime
-
1995
- 1995-04-07 JP JP52824395A patent/JP3683272B2/ja not_active Expired - Lifetime
- 1995-04-07 WO PCT/US1995/004359 patent/WO1995030071A1/en active IP Right Grant
- 1995-04-07 EP EP95916262A patent/EP0757750B1/de not_active Expired - Lifetime
- 1995-04-07 DE DE69504053T patent/DE69504053T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH09512607A (ja) | 1997-12-16 |
WO1995030071A1 (en) | 1995-11-09 |
US5522698A (en) | 1996-06-04 |
DE69504053D1 (de) | 1998-09-17 |
EP0757750A1 (de) | 1997-02-12 |
JP3683272B2 (ja) | 2005-08-17 |
EP0757750B1 (de) | 1998-08-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |