DE602005000026D1 - Dichtungsanordnung für die Hochdruckturbine einer Turbomaschine - Google Patents
Dichtungsanordnung für die Hochdruckturbine einer TurbomaschineInfo
- Publication number
- DE602005000026D1 DE602005000026D1 DE602005000026T DE602005000026T DE602005000026D1 DE 602005000026 D1 DE602005000026 D1 DE 602005000026D1 DE 602005000026 T DE602005000026 T DE 602005000026T DE 602005000026 T DE602005000026 T DE 602005000026T DE 602005000026 D1 DE602005000026 D1 DE 602005000026D1
- Authority
- DE
- Germany
- Prior art keywords
- turbomachine
- pressure turbine
- sealing arrangement
- sealing
- arrangement
- 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.)
- Active
Links
Classifications
-
- 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
- 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
- F01D11/003—Preventing or minimising internal leakage of working-fluid, e.g. between stages by packing rings; Mechanical seals
-
- 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
- F16J15/3204—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings with at least one lip
- F16J15/322—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings with at least one lip supported in a direction perpendicular to the surfaces
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sealing Devices (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0400213A FR2865012B1 (fr) | 2004-01-12 | 2004-01-12 | Dispositif d'etancheite pour turbine haute-pression de turbomachine |
FR0400213 | 2004-01-12 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE602005000026D1 true DE602005000026D1 (de) | 2006-08-10 |
DE602005000026T2 DE602005000026T2 (de) | 2007-03-08 |
Family
ID=34684929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005000026T Active DE602005000026T2 (de) | 2004-01-12 | 2005-01-04 | Dichtungsanordnung für die Hochdruckturbine einer Turbomaschine |
Country Status (8)
Country | Link |
---|---|
US (1) | US7290769B2 (de) |
EP (1) | EP1564455B1 (de) |
JP (1) | JP4444842B2 (de) |
CA (1) | CA2493065C (de) |
DE (1) | DE602005000026T2 (de) |
FR (1) | FR2865012B1 (de) |
RU (1) | RU2296866C2 (de) |
UA (1) | UA85539C2 (de) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1878912B1 (de) | 2006-07-14 | 2011-12-21 | OpenHydro Group Limited | Unter Wasser gesetzte hydroelektrische Turbinen mit Schwimmern |
EP1878913B1 (de) | 2006-07-14 | 2013-03-13 | OpenHydro Group Limited | Bidirektionale Gezeitenturbine |
EP1879280B1 (de) | 2006-07-14 | 2014-03-05 | OpenHydro Group Limited | Hydroelektrische Turbine |
DE602006002883D1 (de) | 2006-07-14 | 2008-11-06 | Openhydro Group Ltd | Turbinen mit einer Rutsche zum Durchfluss von Fremdkörpern |
DE102006049634A1 (de) * | 2006-10-20 | 2008-04-24 | Mtu Aero Engines Gmbh | Dichtungsanordnung |
ATE472056T1 (de) | 2007-04-11 | 2010-07-15 | Openhydro Group Ltd | Verfahren zum installieren von hydroelektrischen turbinen |
DE102008006486A1 (de) * | 2008-01-29 | 2009-07-30 | Mtu Aero Engines Gmbh | Bürstendichtung und Verfahren zur Montage einer Bürstendichtung |
EP2088311B1 (de) | 2008-02-05 | 2015-10-14 | OpenHydro Group Limited | Hydroelektrische Turbine mit schwimmendem Rotor |
EP2110910A1 (de) | 2008-04-17 | 2009-10-21 | OpenHydro Group Limited | Verbessertes Turbineninstallationsverfahren |
EP2199598B1 (de) | 2008-12-18 | 2012-05-02 | OpenHydro IP Limited | Hydroelektrische Turbine mit passiver Bremse und Verfahren zum Betrieb |
EP2199599A1 (de) * | 2008-12-18 | 2010-06-23 | OpenHydro IP Limited | Eine hydroelektrische Turbine mit einer Ablagerungsausstoßvorrichtung |
DE602008002602D1 (de) | 2008-12-19 | 2010-10-28 | Openhydro Ip Ltd | Verfahren zum Installieren eines hydroelektrischen Turbinengenerators |
EP2241749B1 (de) | 2009-04-17 | 2012-03-07 | OpenHydro IP Limited | Verbessertes Verfahren zur Steuerung der Ausgabe eines hydroelektrischen Turbinengenerators |
US20100270747A1 (en) * | 2009-04-24 | 2010-10-28 | General Electric Company | Non-metallic brush seal |
EP2302755B1 (de) | 2009-09-29 | 2012-11-28 | OpenHydro IP Limited | Elektrisches Stromumwandlungssystem und Verfahren |
EP2302766B1 (de) | 2009-09-29 | 2013-03-13 | OpenHydro IP Limited | Hydroelektrische Turbine mit Spulenkühlung |
EP2302204A1 (de) | 2009-09-29 | 2011-03-30 | OpenHydro IP Limited | Hydroelektrisches Turbinensystem |
DE102010021923B4 (de) * | 2010-05-28 | 2013-12-19 | MTU Aero Engines AG | Dichtungssystem für ein Gehäusesegment einer thermischen Strömungsmaschine |
CN111473530A (zh) * | 2010-09-16 | 2020-07-31 | 威尔逊太阳能公司 | 使用太阳能接收器的太阳能发电***及其相关装置和方法 |
EP2450562B1 (de) | 2010-11-09 | 2015-06-24 | Openhydro IP Limited | Bergungssystem für eine hydroelektrische Turbine und Bergungsverfahren |
EP2469257B1 (de) | 2010-12-23 | 2014-02-26 | Openhydro IP Limited | Hydroelektrisches Turbinenprüfverfahren |
US9701388B2 (en) | 2011-05-11 | 2017-07-11 | Aviation Devices & Electronic Components, Llc | Gasket having a pliable resilient body with a perimeter having characteristics different than the body |
WO2012174426A1 (en) | 2011-06-17 | 2012-12-20 | Aviation Devices & Electronic Components, L.L.C. | Single-sided sticky gasket |
US8863625B2 (en) | 2011-06-21 | 2014-10-21 | Aviation Devices & Electronics Components, LLC | Elastomeric gasket squeeze out removal method and kit |
US8691033B1 (en) | 2011-07-06 | 2014-04-08 | Aviation Devices & Electronic Components, Llc | Positioning a workpiece on a sticky gasket |
US9702464B1 (en) | 2011-10-03 | 2017-07-11 | The Patent Well LLC | Non-planar stick gaskets for receipt between a base and a workpiece |
ITCO20110058A1 (it) | 2011-12-05 | 2013-06-06 | Nuovo Pignone Spa | Turbomacchina |
GB201202104D0 (en) * | 2012-02-08 | 2012-03-21 | Rolls Royce Plc | Leaf seal |
US9751244B2 (en) | 2012-05-15 | 2017-09-05 | The Patent Well LLC | Elastomeric gasket for fuel access door of an aircraft wing and a method for making the same |
US9303447B1 (en) | 2012-05-15 | 2016-04-05 | Aviation Devices & Electronic Components LLC | Elastomeric gasket for fuel access door of an aircraft wing and a method for making the same |
US9671023B2 (en) | 2012-07-10 | 2017-06-06 | Aviation Devices & Electronic Components, Llc | Spacer and gasket assembly for use on an aircraft |
US9016697B2 (en) | 2012-07-10 | 2015-04-28 | Aviation Devices & Electronic Components, Llc | Spacer and gasket assembly for use on an aircraft |
FR2998611B1 (fr) * | 2012-11-29 | 2018-08-10 | Safran Aircraft Engines | Ensemble formant joint d'etancheite pour une turbomachine comportant un joint a brosse |
DE102013219832B3 (de) | 2013-09-30 | 2015-03-12 | MTU Aero Engines AG | Bürstendichtung für eine Turbomaschine |
WO2015053935A1 (en) | 2013-10-11 | 2015-04-16 | United Technologies Corporation | Non-linearly deflecting brush seal land |
US9587505B2 (en) | 2013-12-05 | 2017-03-07 | General Electric Company | L brush seal for turbomachinery application |
US9322287B2 (en) * | 2014-06-03 | 2016-04-26 | General Electric Company | Brush seal for turbine |
US10400896B2 (en) | 2014-08-28 | 2019-09-03 | United Technologies Corporation | Dual-ended brush seal assembly and method of manufacture |
EP3280933B1 (de) | 2015-04-08 | 2022-08-31 | The Patent Well LLC | Metallnetz mit einer umwandlungsbeschichtung mit geringem elektrischen widerstand zur verwendung mit flugzeugstrukturen |
US11486497B2 (en) * | 2017-07-19 | 2022-11-01 | Raytheon Technologies Corporation | Compact brush seal |
RU2705103C1 (ru) * | 2019-04-05 | 2019-11-05 | Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК - УМПО") | Щеточное уплотнение турбомашины |
RU2719753C1 (ru) * | 2019-11-25 | 2020-04-23 | Акционерное общество "ОДК-Климов" | Щёточное уплотнение |
Family Cites Families (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3514382C1 (de) | 1985-04-20 | 1986-06-12 | Motoren Turbinen Union | Buerstendichtung |
GB2250790B (en) * | 1990-12-12 | 1994-04-27 | Rolls Royce Plc | Brush seal |
US5265412A (en) * | 1992-07-28 | 1993-11-30 | General Electric Company | Self-accommodating brush seal for gas turbine combustor |
US5568931A (en) * | 1992-08-20 | 1996-10-29 | General Electric Company | Brush seal |
US5480162A (en) | 1993-09-08 | 1996-01-02 | United Technologies Corporation | Axial load carrying brush seal |
IT1284468B1 (it) * | 1995-07-28 | 1998-05-21 | Mtu Muenchen Gmbh | Guarnizione a spazzola per turbomacchine |
DE19529655C2 (de) * | 1995-08-11 | 1999-04-22 | Mtu Muenchen Gmbh | Bürstendichtung für Turbomaschinen |
DE29600193U1 (de) * | 1996-01-08 | 1996-03-14 | MTU Motoren- und Turbinen-Union München GmbH, 80995 München | Bürstendichtung mit C-förmigem Klemmring |
DE19613510C1 (de) * | 1996-04-04 | 1997-04-24 | Mtu Muenchen Gmbh | Bürstendichtung mit einem von Borstenbündeln umschlungenen Kernring |
DE19618475B4 (de) * | 1996-05-08 | 2005-10-20 | Mtu Aero Engines Gmbh | Bürstendichtung |
DE19720648C2 (de) * | 1997-05-16 | 2000-07-13 | Mtu Muenchen Gmbh | Bürstendichtung mit Front- und Stützplatte |
DE19720649C2 (de) * | 1997-05-16 | 2000-09-28 | Mtu Muenchen Gmbh | Bürstendichtung |
DE19855742C1 (de) * | 1998-12-03 | 2000-09-14 | Mtu Muenchen Gmbh | Bürstendichtung mit abgewinkelten Borsten |
US6170831B1 (en) | 1998-12-23 | 2001-01-09 | United Technologies Corporation | Axial brush seal for gas turbine engines |
GB9900102D0 (en) * | 1999-01-06 | 1999-02-24 | Rolls Royce Plc | A seal arrangement |
DE19962316C2 (de) * | 1999-12-23 | 2002-07-18 | Mtu Aero Engines Gmbh | Bürstendichtung |
GB9930620D0 (en) * | 1999-12-24 | 2000-02-16 | Cross Mfg Co | Brush seals |
DE10017643B4 (de) * | 2000-04-08 | 2005-10-20 | Mtu Aero Engines Gmbh | Dichtung in nicht-hermetischer Ausführung |
DE10018273B4 (de) * | 2000-04-13 | 2005-10-20 | Mtu Aero Engines Gmbh | Bürstendichtung |
JP4644378B2 (ja) * | 2001-03-27 | 2011-03-02 | イーグル・エンジニアリング・エアロスペース株式会社 | ブラシシール装置 |
GB0126220D0 (en) * | 2001-11-01 | 2002-01-02 | Alstom Switzerland Ltd | Brush seals |
DE10163804B4 (de) * | 2001-12-22 | 2005-07-07 | Mtu Aero Engines Gmbh | Bürstendichtung |
GB0201666D0 (en) * | 2002-01-25 | 2002-03-13 | Cross Mfg 1938 Company Ltd | A brush seal element |
US7677847B2 (en) * | 2002-03-26 | 2010-03-16 | Siemens Aktiengesellschaft | Sealing assembly for a spindle |
US6685427B1 (en) * | 2002-07-23 | 2004-02-03 | General Electric Company | Brush seal for a rotary machine and method of retrofitting |
US6779799B2 (en) * | 2002-11-27 | 2004-08-24 | General Electric Company | Sealing apparatus for electrical generator ventilation system |
DE10259381A1 (de) * | 2002-12-18 | 2004-07-15 | Mtu Aero Engines Gmbh | Dichtungsanordnung |
DE10337867B4 (de) * | 2003-08-18 | 2020-04-23 | MTU Aero Engines AG | Bürstendichtung |
-
2004
- 2004-01-12 FR FR0400213A patent/FR2865012B1/fr not_active Expired - Fee Related
-
2005
- 2005-01-04 DE DE602005000026T patent/DE602005000026T2/de active Active
- 2005-01-04 EP EP05290003A patent/EP1564455B1/de active Active
- 2005-01-04 US US11/028,232 patent/US7290769B2/en active Active
- 2005-01-05 JP JP2005000455A patent/JP4444842B2/ja active Active
- 2005-01-11 UA UAA200500250A patent/UA85539C2/ru unknown
- 2005-01-11 RU RU2005100808/06A patent/RU2296866C2/ru active
- 2005-01-12 CA CA2493065A patent/CA2493065C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
US20050151324A1 (en) | 2005-07-14 |
CA2493065C (fr) | 2011-10-18 |
EP1564455A1 (de) | 2005-08-17 |
JP4444842B2 (ja) | 2010-03-31 |
RU2296866C2 (ru) | 2007-04-10 |
CA2493065A1 (fr) | 2005-07-12 |
EP1564455B1 (de) | 2006-06-28 |
DE602005000026T2 (de) | 2007-03-08 |
JP2005201445A (ja) | 2005-07-28 |
FR2865012A1 (fr) | 2005-07-15 |
UA85539C2 (ru) | 2009-02-10 |
FR2865012B1 (fr) | 2006-03-17 |
US7290769B2 (en) | 2007-11-06 |
RU2005100808A (ru) | 2006-06-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE602005000026D1 (de) | Dichtungsanordnung für die Hochdruckturbine einer Turbomaschine | |
DE602005004447D1 (de) | Manschettendichtung für Turbinenleitschaufeln | |
DE602005007408D1 (de) | Dichtungsanordnung für eine Turbomaschine | |
ITMI20061784A1 (it) | Guarnizioni per turbine e macchinario di turbine | |
DE602005021428D1 (de) | Turbinentriebwerk und Montageverfahren für ein Turbinentriebwerk | |
NO20070239L (no) | System for a vaske en gassturbinmotor | |
DE60208870D1 (de) | Dichtung für die Verbindungsstelle Düse-Mantel einer Gasturbine | |
DE602006001430D1 (de) | Turbinenmodul für einen Gasturbinentriebwerk | |
DE602008003377D1 (de) | Dämpfungsblech für die Schaufel einer Turbomaschine | |
DE602005000935D1 (de) | Befestigungsvorrichtung für die Brennkammerwand einer Turbine | |
FR2913050B1 (fr) | Turbine haute-pression d'une turbomachine | |
DK1903188T3 (da) | Gasturbine | |
DE602007008001D1 (de) | Dichtung für segmentierte Gasturbinenkomponenten | |
FR2858649B1 (fr) | Turbine basse-pression de turbomachine | |
DE602004006922D1 (de) | Leitschaufelanordnung für ein Gasturbinentriebwerk | |
DE502007000155D1 (de) | Axialkompressor für ein Gasturbinentriebwerk | |
EP1745213A4 (de) | Druckflüssigkeitsbetriebener turbinenmotor | |
FR2867223B1 (fr) | Turbomachine comme par exemple un turboreacteur pour avion | |
DE602005007297D1 (de) | Turbine eines Gasturbinentriebwerks | |
DE602004000301D1 (de) | Vorrichtung für die Belüftung eines Rotor einer Hochdruckturbine | |
GB2422641B (en) | Vane for a gas turbine engine | |
DE602008001945D1 (de) | Laminierte Gasdichtung für eine Gasturbine | |
DE602006014269D1 (de) | Dichtungsanordnung für eine gebläserotoranordnung einer spitzenturbine | |
NO20054322D0 (no) | Rotorblad for forste trinn i en gassturbin | |
DE602006020376D1 (de) | ugehörige Gasturbine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |