DE3467017D1 - Sealing means for rotor blades of a gas-turbine - Google Patents
Sealing means for rotor blades of a gas-turbineInfo
- Publication number
- DE3467017D1 DE3467017D1 DE8484400155T DE3467017T DE3467017D1 DE 3467017 D1 DE3467017 D1 DE 3467017D1 DE 8484400155 T DE8484400155 T DE 8484400155T DE 3467017 T DE3467017 T DE 3467017T DE 3467017 D1 DE3467017 D1 DE 3467017D1
- Authority
- DE
- Germany
- Prior art keywords
- turbine
- gas
- sealing means
- rotor blades
- blades
- 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
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
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8301671A FR2540560B1 (fr) | 1983-02-03 | 1983-02-03 | Dispositif d'etancheite d'aubages mobiles de turbomachine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3467017D1 true DE3467017D1 (en) | 1987-12-03 |
Family
ID=9285561
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8484400155T Expired DE3467017D1 (en) | 1983-02-03 | 1984-01-25 | Sealing means for rotor blades of a gas-turbine |
Country Status (5)
Country | Link |
---|---|
US (1) | US4527385A (de) |
EP (1) | EP0115984B1 (de) |
JP (1) | JPS59147802A (de) |
DE (1) | DE3467017D1 (de) |
FR (1) | FR2540560B1 (de) |
Families Citing this family (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2548733B1 (fr) * | 1983-07-07 | 1987-07-10 | Snecma | Dispositif d'etancheite d'aubages mobiles de turbomachine |
FR2570763B1 (fr) * | 1984-09-27 | 1986-11-28 | Snecma | Dispositif de controle automatique du jeu d'un joint a labyrinthe de turbomachine |
FR2577281B1 (fr) * | 1985-02-13 | 1987-03-20 | Snecma | Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter |
US4728257A (en) * | 1986-06-18 | 1988-03-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal stress minimized, two component, turbine shroud seal |
FR2614073B1 (fr) * | 1987-04-15 | 1992-02-14 | Snecma | Dispositif d'ajustement en temps reel du jeu radial entre un rotor et un stator de turbomachine |
US4825640A (en) * | 1987-06-22 | 1989-05-02 | Sundstrand Corporation | Combustor with enhanced turbine nozzle cooling |
US4826397A (en) * | 1988-06-29 | 1989-05-02 | United Technologies Corporation | Stator assembly for a gas turbine engine |
JP2539259B2 (ja) * | 1988-11-25 | 1996-10-02 | 積水ハウス株式会社 | 壁体構造 |
FR2640687B1 (fr) * | 1988-12-21 | 1991-02-08 | Snecma | Carter de compresseur de turbomachine a pilotage de son diametre interne |
US5116199A (en) * | 1990-12-20 | 1992-05-26 | General Electric Company | Blade tip clearance control apparatus using shroud segment annular support ring thermal expansion |
US5224822A (en) * | 1991-05-13 | 1993-07-06 | General Electric Company | Integral turbine nozzle support and discourager seal |
GB9210642D0 (en) * | 1992-05-19 | 1992-07-08 | Rolls Royce Plc | Rotor shroud assembly |
FR2751694B1 (fr) * | 1996-07-25 | 1998-09-04 | Snecma | Agencement et procede de reglage de diametre d'anneau de stator |
US6227800B1 (en) * | 1998-11-24 | 2001-05-08 | General Electric Company | Bay cooled turbine casing |
US7033138B2 (en) * | 2002-09-06 | 2006-04-25 | Mitsubishi Heavy Industries, Ltd. | Ring segment of gas turbine |
US6910851B2 (en) * | 2003-05-30 | 2005-06-28 | Honeywell International, Inc. | Turbofan jet engine having a turbine case cooling valve |
US6896484B2 (en) * | 2003-09-12 | 2005-05-24 | Siemens Westinghouse Power Corporation | Turbine engine sealing device |
US6926495B2 (en) * | 2003-09-12 | 2005-08-09 | Siemens Westinghouse Power Corporation | Turbine blade tip clearance control device |
US7278820B2 (en) * | 2005-10-04 | 2007-10-09 | Siemens Power Generation, Inc. | Ring seal system with reduced cooling requirements |
US7491029B2 (en) * | 2005-10-14 | 2009-02-17 | United Technologies Corporation | Active clearance control system for gas turbine engines |
US9039358B2 (en) * | 2007-01-03 | 2015-05-26 | United Technologies Corporation | Replaceable blade outer air seal design |
US8783027B2 (en) * | 2009-09-18 | 2014-07-22 | Siemens Energy, Inc. | Pressure regulation circuit for turbine generators |
US8790067B2 (en) * | 2011-04-27 | 2014-07-29 | United Technologies Corporation | Blade clearance control using high-CTE and low-CTE ring members |
US9169739B2 (en) * | 2012-01-04 | 2015-10-27 | United Technologies Corporation | Hybrid blade outer air seal for gas turbine engine |
US9200530B2 (en) | 2012-07-20 | 2015-12-01 | United Technologies Corporation | Radial position control of case supported structure |
US9238971B2 (en) * | 2012-10-18 | 2016-01-19 | General Electric Company | Gas turbine casing thermal control device |
WO2014143311A1 (en) | 2013-03-14 | 2014-09-18 | Uskert Richard C | Turbine shrouds |
US10001022B2 (en) * | 2013-06-21 | 2018-06-19 | United Technologies Corporation | Seals for gas turbine engine |
EP3055513B1 (de) * | 2013-10-07 | 2019-09-18 | United Technologies Corporation | Spaltregelungssystem für eine gasturbine und verfahren für die regelung eines radialspaltes in einer gasturbine |
US10323535B2 (en) * | 2013-12-10 | 2019-06-18 | United Technologies Corporation | Blade tip clearance systems |
US10221713B2 (en) * | 2015-05-26 | 2019-03-05 | Rolls-Royce Corporation | Shroud cartridge having a ceramic matrix composite seal segment |
US10197069B2 (en) * | 2015-11-20 | 2019-02-05 | United Technologies Corporation | Outer airseal for gas turbine engine |
US10422241B2 (en) | 2016-03-16 | 2019-09-24 | United Technologies Corporation | Blade outer air seal support for a gas turbine engine |
US10138750B2 (en) | 2016-03-16 | 2018-11-27 | United Technologies Corporation | Boas segmented heat shield |
US10337346B2 (en) | 2016-03-16 | 2019-07-02 | United Technologies Corporation | Blade outer air seal with flow guide manifold |
US10443616B2 (en) | 2016-03-16 | 2019-10-15 | United Technologies Corporation | Blade outer air seal with centrally mounted seal arc segments |
US10132184B2 (en) | 2016-03-16 | 2018-11-20 | United Technologies Corporation | Boas spring loaded rail shield |
US10563531B2 (en) | 2016-03-16 | 2020-02-18 | United Technologies Corporation | Seal assembly for gas turbine engine |
US10422240B2 (en) | 2016-03-16 | 2019-09-24 | United Technologies Corporation | Turbine engine blade outer air seal with load-transmitting cover plate |
US10138749B2 (en) | 2016-03-16 | 2018-11-27 | United Technologies Corporation | Seal anti-rotation feature |
US10415414B2 (en) | 2016-03-16 | 2019-09-17 | United Technologies Corporation | Seal arc segment with anti-rotation feature |
US10161258B2 (en) | 2016-03-16 | 2018-12-25 | United Technologies Corporation | Boas rail shield |
US10107129B2 (en) | 2016-03-16 | 2018-10-23 | United Technologies Corporation | Blade outer air seal with spring centering |
US10513943B2 (en) | 2016-03-16 | 2019-12-24 | United Technologies Corporation | Boas enhanced heat transfer surface |
US10443424B2 (en) | 2016-03-16 | 2019-10-15 | United Technologies Corporation | Turbine engine blade outer air seal with load-transmitting carriage |
EP3330498B1 (de) * | 2016-11-30 | 2020-01-08 | Rolls-Royce Corporation | Turbinenummantelung mit hängevorrichtungsbefestigung |
US11761343B2 (en) * | 2019-03-13 | 2023-09-19 | Rtx Corporation | BOAS carrier with dovetail attachments |
US11220928B1 (en) * | 2020-08-24 | 2022-01-11 | Rolls-Royce Corporation | Turbine shroud assembly with ceramic matrix composite components and cooling features |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1248198A (en) * | 1970-02-06 | 1971-09-29 | Rolls Royce | Sealing device |
US3807891A (en) * | 1972-09-15 | 1974-04-30 | United Aircraft Corp | Thermal response turbine shroud |
US3864056A (en) * | 1973-07-27 | 1975-02-04 | Westinghouse Electric Corp | Cooled turbine blade ring assembly |
GB1484936A (en) * | 1974-12-07 | 1977-09-08 | Rolls Royce | Gas turbine engines |
US3966354A (en) * | 1974-12-19 | 1976-06-29 | General Electric Company | Thermal actuated valve for clearance control |
GB1484288A (en) * | 1975-12-03 | 1977-09-01 | Rolls Royce | Gas turbine engines |
US4019320A (en) * | 1975-12-05 | 1977-04-26 | United Technologies Corporation | External gas turbine engine cooling for clearance control |
US4127357A (en) * | 1977-06-24 | 1978-11-28 | General Electric Company | Variable shroud for a turbomachine |
JPS554933A (en) * | 1978-06-26 | 1980-01-14 | Hitachi Ltd | Helium gas recovering device |
DE2907749C2 (de) * | 1979-02-28 | 1985-04-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur Minimierung von Konstanthaltung des bei Axialturbinen von Gasturbinentriebwerken vorhandenen Schaufelspitzenspiels |
DE2907748C2 (de) * | 1979-02-28 | 1987-02-12 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur Minimierung und Konstanthaltung des Schaufelspitzenspiels einer axial durchströmten Hochdruckturbine eines Gasturbinentriebwerks |
GB2047354B (en) * | 1979-04-26 | 1983-03-30 | Rolls Royce | Gas turbine engines |
FR2467292A1 (fr) * | 1979-10-09 | 1981-04-17 | Snecma | Dispositif de reglage du jeu entre les aubes mobiles et l'anneau de turbine |
US4363599A (en) * | 1979-10-31 | 1982-12-14 | General Electric Company | Clearance control |
FR2515734A1 (fr) * | 1981-11-05 | 1983-05-06 | Snecma | Systeme d'ajustement du centrage d'une roue de turbomachine et turbomachine munie de moyens permettant l'application dudit systeme |
-
1983
- 1983-02-03 FR FR8301671A patent/FR2540560B1/fr not_active Expired
-
1984
- 1984-01-25 EP EP84400155A patent/EP0115984B1/de not_active Expired
- 1984-01-25 DE DE8484400155T patent/DE3467017D1/de not_active Expired
- 1984-01-30 US US06/575,319 patent/US4527385A/en not_active Expired - Fee Related
- 1984-02-01 JP JP59018157A patent/JPS59147802A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
EP0115984A1 (de) | 1984-08-15 |
FR2540560B1 (fr) | 1987-06-12 |
JPH0377363B2 (de) | 1991-12-10 |
JPS59147802A (ja) | 1984-08-24 |
EP0115984B1 (de) | 1987-10-28 |
FR2540560A1 (fr) | 1984-08-10 |
US4527385A (en) | 1985-07-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |