FR2631656B1 - Dispositif d'etancheite pour interieur de turbine a gaz - Google Patents
Dispositif d'etancheite pour interieur de turbine a gazInfo
- Publication number
- FR2631656B1 FR2631656B1 FR898906742A FR8906742A FR2631656B1 FR 2631656 B1 FR2631656 B1 FR 2631656B1 FR 898906742 A FR898906742 A FR 898906742A FR 8906742 A FR8906742 A FR 8906742A FR 2631656 B1 FR2631656 B1 FR 2631656B1
- Authority
- FR
- France
- Prior art keywords
- interior
- gas turbine
- sealing device
- sealing
- turbine
- 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 - Fee Related
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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/197,726 US4820119A (en) | 1988-05-23 | 1988-05-23 | Inner turbine seal |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2631656A1 FR2631656A1 (fr) | 1989-11-24 |
FR2631656B1 true FR2631656B1 (fr) | 1992-01-24 |
Family
ID=22730511
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR898906742A Expired - Fee Related FR2631656B1 (fr) | 1988-05-23 | 1989-05-23 | Dispositif d'etancheite pour interieur de turbine a gaz |
Country Status (3)
Country | Link |
---|---|
US (1) | US4820119A (fr) |
FR (1) | FR2631656B1 (fr) |
GB (1) | GB2219353B (fr) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5215435A (en) * | 1991-10-28 | 1993-06-01 | General Electric Company | Angled cooling air bypass slots in honeycomb seals |
FR2722240B1 (fr) * | 1994-07-06 | 1996-08-14 | Snecma | Joint metallique a levre et turbomachine equipee de ce joint |
DE19507673C2 (de) * | 1995-03-06 | 1997-07-03 | Mtu Muenchen Gmbh | Leitrad für Turbomaschinen |
US5639211A (en) * | 1995-11-30 | 1997-06-17 | United Technology Corporation | Brush seal for stator of a gas turbine engine case |
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 |
US6471216B1 (en) * | 1999-05-24 | 2002-10-29 | General Electric Company | Rotating seal |
US6499742B1 (en) * | 2001-08-20 | 2002-12-31 | General Electric Company | Brush seal assembly and method of using brush seal assembly |
FR2832543B1 (fr) * | 2001-11-21 | 2006-04-14 | Jeumont Sa | Ecran de protection thermique pour un arbre tournant |
US20040017050A1 (en) * | 2002-07-29 | 2004-01-29 | Burdgick Steven Sebastian | Endface gap sealing for steam turbine diaphragm interstage packing seals and methods of retrofitting |
US20040239040A1 (en) * | 2003-05-29 | 2004-12-02 | Burdgick Steven Sebastian | Nozzle interstage seal for steam turbines |
WO2004113771A2 (fr) * | 2003-06-20 | 2004-12-29 | Elliott Company | Joint hybride labyrinthe abradable/amortisseur |
WO2004113770A2 (fr) * | 2003-06-20 | 2004-12-29 | Elliott Company | Presse-garniture a labyrinthe abradable a inversion de tourbillon |
EP1508672A1 (fr) * | 2003-08-21 | 2005-02-23 | Siemens Aktiengesellschaft | Anneau de fixation segmenté pour une turbine |
US20110150640A1 (en) * | 2003-08-21 | 2011-06-23 | Peter Tiemann | Labyrinth Seal in a Stationary Gas Turbine |
US7059829B2 (en) | 2004-02-09 | 2006-06-13 | Siemens Power Generation, Inc. | Compressor system with movable seal lands |
US7520718B2 (en) * | 2005-07-18 | 2009-04-21 | Siemens Energy, Inc. | Seal and locking plate for turbine rotor assembly between turbine blade and turbine vane |
ES2357754T3 (es) * | 2005-09-19 | 2011-04-29 | Ingersoll Rand Company | Impulsor para un compresor centrífugo. |
WO2007035701A2 (fr) * | 2005-09-19 | 2007-03-29 | Ingersoll-Rand Company | Anneau d'etancheite stationnaire destine a un compresseur centrifuge |
US20070132193A1 (en) * | 2005-12-13 | 2007-06-14 | Wolfe Christopher E | Compliant abradable sealing system and method for rotary machines |
FR2930592B1 (fr) * | 2008-04-24 | 2010-04-30 | Snecma | Distributeur de turbine pour une turbomachine |
US8177495B2 (en) * | 2009-03-24 | 2012-05-15 | General Electric Company | Method and apparatus for turbine interstage seal ring |
US8613590B2 (en) * | 2010-07-27 | 2013-12-24 | United Technologies Corporation | Blade outer air seal and repair method |
US8511976B2 (en) | 2010-08-02 | 2013-08-20 | General Electric Company | Turbine seal system |
US8434766B2 (en) | 2010-08-18 | 2013-05-07 | General Electric Company | Turbine engine seals |
US8821113B2 (en) | 2010-12-21 | 2014-09-02 | Hamilton Sundstrand Corporation | Air cycle machine seal land |
US8770928B2 (en) | 2010-12-21 | 2014-07-08 | Hamilton Sundstrand Corporation | Air cycle machine seal plate and seal land |
FR2971022B1 (fr) * | 2011-02-02 | 2013-01-04 | Snecma | Etage redresseur de compresseur pour une turbomachine |
US20130264779A1 (en) * | 2012-04-10 | 2013-10-10 | General Electric Company | Segmented interstage seal system |
US9145786B2 (en) | 2012-04-17 | 2015-09-29 | General Electric Company | Method and apparatus for turbine clearance flow reduction |
US9327368B2 (en) * | 2012-09-27 | 2016-05-03 | United Technologies Corporation | Full ring inner air-seal with locking nut |
US10822980B2 (en) | 2013-04-11 | 2020-11-03 | Raytheon Technologies Corporation | Gas turbine engine stress isolation scallop |
US9267387B2 (en) | 2013-07-15 | 2016-02-23 | General Electric Company | Seal platform |
CN103541776B (zh) * | 2013-10-15 | 2015-12-30 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机轮盘间的轴向密封结构 |
US9745864B2 (en) * | 2014-04-16 | 2017-08-29 | United Technologies Corporation | Systems and methods for anti-rotational features |
EP3020929A1 (fr) | 2014-11-17 | 2016-05-18 | United Technologies Corporation | Ensemble joint de bordure pour plate-forme portante |
US12037926B2 (en) | 2016-02-05 | 2024-07-16 | Siemens Energy Global GmbH & Co. KG | Rotor comprising a rotor component arranged between two rotor discs |
US10344869B2 (en) * | 2016-05-31 | 2019-07-09 | Rolls-Royce Corporation | Labyrinth seal with lubricant directing projection |
WO2018132084A1 (fr) * | 2017-01-10 | 2018-07-19 | Siemens Aktiengesellschaft | Rotor et turbomachine |
FR3071541B1 (fr) * | 2017-09-26 | 2019-09-13 | Safran Aircraft Engines | Joint d'etancheite a labyrinthe pour une turbomachine d'aeronef |
EP3540180A1 (fr) * | 2018-03-14 | 2019-09-18 | General Electric Company | Conduites de purge de cavité inter-étage |
JP7394979B2 (ja) * | 2019-10-18 | 2023-12-08 | シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | 2つのロータディスクの間に配置されたロータコンポーネントを有するロータ |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2427244A (en) * | 1944-03-07 | 1947-09-09 | Gen Electric | Gas turbine |
GB772394A (en) * | 1955-07-28 | 1957-04-10 | Gen Electric | Improved seal for turbojet engines |
GB816288A (en) * | 1957-03-25 | 1959-07-08 | Gen Motors Corp | Improvements relating to labyrinth seals in turbines or compressors |
GB979749A (en) * | 1963-10-18 | 1965-01-06 | Rolls Royce | Axial flow compressors particularly for gas turbine engines |
GB1008526A (en) * | 1964-04-09 | 1965-10-27 | Rolls Royce | Axial flow bladed rotor, e.g. for a turbine |
US3529904A (en) * | 1968-10-28 | 1970-09-22 | Westinghouse Electric Corp | Diaphragm seal structure |
US3941500A (en) * | 1974-06-10 | 1976-03-02 | Westinghouse Electric Corporation | Turbomachine interstage seal assembly |
FR2427469A1 (fr) * | 1978-06-01 | 1979-12-28 | Snecma | Dispositif de fixation d'une garniture d'etancheite sur un distributeur de turbomachine |
GB2092243B (en) * | 1981-01-31 | 1984-12-05 | Rolls Royce | Non-contacting gas seal |
GB2092242B (en) * | 1981-01-31 | 1984-12-19 | Rolls Royce | Non-contacting gas seal |
US4659289A (en) * | 1984-07-23 | 1987-04-21 | United Technologies Corporation | Turbine side plate assembly |
US4645424A (en) * | 1984-07-23 | 1987-02-24 | United Technologies Corporation | Rotating seal for gas turbine engine |
US4655683A (en) * | 1984-12-24 | 1987-04-07 | United Technologies Corporation | Stator seal land structure |
US4767267A (en) * | 1986-12-03 | 1988-08-30 | General Electric Company | Seal assembly |
-
1988
- 1988-05-23 US US07/197,726 patent/US4820119A/en not_active Expired - Fee Related
-
1989
- 1989-05-18 GB GB8911408A patent/GB2219353B/en not_active Expired - Fee Related
- 1989-05-23 FR FR898906742A patent/FR2631656B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2219353A (en) | 1989-12-06 |
GB8911408D0 (en) | 1989-07-05 |
US4820119A (en) | 1989-04-11 |
GB2219353B (en) | 1992-04-08 |
FR2631656A1 (fr) | 1989-11-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |