FR2428141A1 - Dispositif perfectionne de support de virole de turbine - Google Patents
Dispositif perfectionne de support de virole de turbineInfo
- Publication number
- FR2428141A1 FR2428141A1 FR7905594A FR7905594A FR2428141A1 FR 2428141 A1 FR2428141 A1 FR 2428141A1 FR 7905594 A FR7905594 A FR 7905594A FR 7905594 A FR7905594 A FR 7905594A FR 2428141 A1 FR2428141 A1 FR 2428141A1
- Authority
- FR
- France
- Prior art keywords
- support device
- rubber support
- improved turbine
- percussion
- turbine rubber
- 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.)
- Granted
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/14—Casings modified therefor
-
- 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
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Dispositif assurant le support et le refroidissement de la virole du rotor de turbine. Il comprend une chicane perforée de percussion 38, fixée sur la structure de support 17 et délimitant en partie une chambre de pression d'air de refroidissement et assurant la percussion de l'air de refroidissement sur la virole 12. Application aux turbines à gaz.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/912,904 US4303371A (en) | 1978-06-05 | 1978-06-05 | Shroud support with impingement baffle |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2428141A1 true FR2428141A1 (fr) | 1980-01-04 |
FR2428141B1 FR2428141B1 (fr) | 1986-03-14 |
Family
ID=25432669
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7905594A Expired FR2428141B1 (fr) | 1978-06-05 | 1979-03-05 | Dispositif perfectionne de support de virole de turbine |
Country Status (6)
Country | Link |
---|---|
US (1) | US4303371A (fr) |
JP (1) | JPS54159516A (fr) |
DE (1) | DE2907769C2 (fr) |
FR (1) | FR2428141B1 (fr) |
GB (1) | GB2035466B (fr) |
IT (1) | IT1110149B (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0243274A1 (fr) * | 1986-04-24 | 1987-10-28 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Anneau de turbine sectorisé |
EP1903186A1 (fr) * | 2006-09-22 | 2008-03-26 | Snecma | Dispositif d' écran thermique sur le carter de turbine pour le contrôle du jeu en sommet d'aube |
FR2922589A1 (fr) * | 2007-10-22 | 2009-04-24 | Snecma Sa | Controle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine |
FR2972760A1 (fr) * | 2011-03-16 | 2012-09-21 | Snecma | Anneau de carter de turbomachine |
Families Citing this family (61)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4693667A (en) * | 1980-04-29 | 1987-09-15 | Teledyne Industries, Inc. | Turbine inlet nozzle with cooling means |
US4551064A (en) * | 1982-03-05 | 1985-11-05 | Rolls-Royce Limited | Turbine shroud and turbine shroud assembly |
GB2117451B (en) * | 1982-03-05 | 1985-11-06 | Rolls Royce | Gas turbine shroud |
FR2576637B1 (fr) * | 1985-01-30 | 1988-11-18 | Snecma | Anneau de turbine a gaz. |
JPS6345402A (ja) * | 1986-08-11 | 1988-02-26 | Nagasu Hideo | 流体機械 |
US5054997A (en) * | 1989-11-22 | 1991-10-08 | General Electric Company | Blade tip clearance control apparatus using bellcrank mechanism |
US5127793A (en) * | 1990-05-31 | 1992-07-07 | General Electric Company | Turbine shroud clearance control assembly |
US5167487A (en) * | 1991-03-11 | 1992-12-01 | General Electric Company | Cooled shroud support |
US5152666A (en) * | 1991-05-03 | 1992-10-06 | United Technologies Corporation | Stator assembly for a rotary machine |
US5165847A (en) * | 1991-05-20 | 1992-11-24 | General Electric Company | Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines |
US5169287A (en) * | 1991-05-20 | 1992-12-08 | General Electric Company | Shroud cooling assembly for gas turbine engine |
US5238365A (en) * | 1991-07-09 | 1993-08-24 | General Electric Company | Assembly for thermal shielding of low pressure turbine |
US5160241A (en) * | 1991-09-09 | 1992-11-03 | General Electric Company | Multi-port air channeling assembly |
US5188507A (en) * | 1991-11-27 | 1993-02-23 | General Electric Company | Low-pressure turbine shroud |
US5201846A (en) * | 1991-11-29 | 1993-04-13 | General Electric Company | Low-pressure turbine heat shield |
US5205708A (en) * | 1992-02-07 | 1993-04-27 | General Electric Company | High pressure turbine component interference fit up |
US5593276A (en) * | 1995-06-06 | 1997-01-14 | General Electric Company | Turbine shroud hanger |
US5562408A (en) * | 1995-06-06 | 1996-10-08 | General Electric Company | Isolated turbine shroud |
US5553999A (en) * | 1995-06-06 | 1996-09-10 | General Electric Company | Sealable turbine shroud hanger |
US5593277A (en) * | 1995-06-06 | 1997-01-14 | General Electric Company | Smart turbine shroud |
US5641267A (en) * | 1995-06-06 | 1997-06-24 | General Electric Company | Controlled leakage shroud panel |
US6139257A (en) * | 1998-03-23 | 2000-10-31 | General Electric Company | Shroud cooling assembly for gas turbine engine |
US6412149B1 (en) * | 1999-08-25 | 2002-07-02 | General Electric Company | C-clip for shroud assembly |
DE19963371A1 (de) * | 1999-12-28 | 2001-07-12 | Alstom Power Schweiz Ag Baden | Gekühltes Hitzeschild |
EP1124039A1 (fr) * | 2000-02-09 | 2001-08-16 | General Electric Company | Dispositif de refroidissement par impact pour une bande de protection de turbine à gaz |
US6340285B1 (en) | 2000-06-08 | 2002-01-22 | General Electric Company | End rail cooling for combined high and low pressure turbine shroud |
US6354795B1 (en) | 2000-07-27 | 2002-03-12 | General Electric Company | Shroud cooling segment and assembly |
US6902371B2 (en) * | 2002-07-26 | 2005-06-07 | General Electric Company | Internal low pressure turbine case cooling |
ITMI20022418A1 (it) * | 2002-11-15 | 2004-05-16 | Nuovo Pignone Spa | Assieme migliorato di cassa interna a dispositivo di |
US6892931B2 (en) * | 2002-12-27 | 2005-05-17 | General Electric Company | Methods for replacing portions of turbine shroud supports |
FR2867224B1 (fr) * | 2004-03-04 | 2006-05-19 | Snecma Moteurs | Dispositif de maintien axial de secteur d'entretoise pour anneau d'une turbine haute-pression de turbomachine |
US7063503B2 (en) * | 2004-04-15 | 2006-06-20 | Pratt & Whitney Canada Corp. | Turbine shroud cooling system |
US20070009349A1 (en) * | 2005-07-11 | 2007-01-11 | General Electric Company | Impingement box for gas turbine shroud |
FR2907841B1 (fr) * | 2006-10-30 | 2011-04-15 | Snecma | Secteur d'anneau de turbine de turbomachine |
US8123466B2 (en) * | 2007-03-01 | 2012-02-28 | United Technologies Corporation | Blade outer air seal |
US8240980B1 (en) | 2007-10-19 | 2012-08-14 | Florida Turbine Technologies, Inc. | Turbine inter-stage gap cooling and sealing arrangement |
EP2078837A1 (fr) | 2008-01-11 | 2009-07-15 | Siemens Aktiengesellschaft | Dispositif de prélèvement d'air pour un compresseur d'un moteur à turbine à gaz |
US8021109B2 (en) * | 2008-01-22 | 2011-09-20 | General Electric Company | Turbine casing with false flange |
US8439639B2 (en) * | 2008-02-24 | 2013-05-14 | United Technologies Corporation | Filter system for blade outer air seal |
DE102008052372A1 (de) * | 2008-10-20 | 2010-04-22 | Mtu Aero Engines Gmbh | Verdichter |
US8740551B2 (en) * | 2009-08-18 | 2014-06-03 | Pratt & Whitney Canada Corp. | Blade outer air seal cooling |
EP2299063B1 (fr) * | 2009-09-17 | 2015-08-26 | Siemens Aktiengesellschaft | Plaque de refroidissement d'impact pour moteur de turbine à gaz et moteur de turbine à gaz |
US9482107B2 (en) * | 2009-09-28 | 2016-11-01 | Siemens Aktiengesellschaft | Gas turbine nozzle arrangement and gas turbine |
RU2547541C2 (ru) * | 2010-11-29 | 2015-04-10 | Альстом Текнолоджи Лтд | Осевая газовая турбина |
IT1403415B1 (it) * | 2010-12-21 | 2013-10-17 | Avio Spa | Turbina a gas per motori aeronautici |
US8876458B2 (en) | 2011-01-25 | 2014-11-04 | United Technologies Corporation | Blade outer air seal assembly and support |
FR2972483B1 (fr) * | 2011-03-07 | 2013-04-19 | Snecma | Carter de turbine comportant des moyens de fixation de secteurs d'anneau |
US9169739B2 (en) * | 2012-01-04 | 2015-10-27 | United Technologies Corporation | Hybrid blade outer air seal for gas turbine engine |
EP2964936A4 (fr) * | 2013-03-08 | 2016-11-02 | United Technologies Corp | Ensemble de montage de boîte de vitesse |
EP2789803A1 (fr) | 2013-04-09 | 2014-10-15 | Siemens Aktiengesellschaft | Fixation et étanchéification d'élément d'anneau d'impact |
EP2881545B1 (fr) * | 2013-12-04 | 2017-05-31 | MTU Aero Engines GmbH | Élément d'étanchéité, dispositif d'étanchéité et turbomachine |
US10690055B2 (en) * | 2014-05-29 | 2020-06-23 | General Electric Company | Engine components with impingement cooling features |
DE102015215144B4 (de) * | 2015-08-07 | 2017-11-09 | MTU Aero Engines AG | Vorrichtung und Verfahren zum Beeinflussen der Temperaturen in Innenringsegmenten einer Gasturbine |
US10422240B2 (en) * | 2016-03-16 | 2019-09-24 | United Technologies Corporation | Turbine engine blade outer air seal with load-transmitting cover plate |
US10337346B2 (en) * | 2016-03-16 | 2019-07-02 | United Technologies Corporation | Blade outer air seal with flow guide manifold |
FR3056632B1 (fr) * | 2016-09-27 | 2020-06-05 | Safran Aircraft Engines | Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement |
US10677084B2 (en) | 2017-06-16 | 2020-06-09 | Honeywell International Inc. | Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement |
US10900378B2 (en) | 2017-06-16 | 2021-01-26 | Honeywell International Inc. | Turbine tip shroud assembly with plural shroud segments having internal cooling passages |
US10822973B2 (en) | 2017-11-28 | 2020-11-03 | General Electric Company | Shroud for a gas turbine engine |
US11242764B2 (en) * | 2018-05-17 | 2022-02-08 | Raytheon Technologies Corporation | Seal assembly with baffle for gas turbine engine |
FR3115814B1 (fr) * | 2020-11-05 | 2023-06-23 | Safran Aircraft Engines | Ensemble d’anneau de turbine ameliore |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1308771A (en) * | 1966-11-02 | 1973-03-07 | Gen Electric | Fluid cooled porous stator structure |
US3825364A (en) * | 1972-06-09 | 1974-07-23 | Gen Electric | Porous abradable turbine shroud |
US3864056A (en) * | 1973-07-27 | 1975-02-04 | Westinghouse Electric Corp | Cooled turbine blade ring assembly |
FR2280791A1 (fr) * | 1974-07-31 | 1976-02-27 | Snecma | Perfectionnements au reglage du jeu entre les aubes et le stator d'une turbine |
FR2293594A1 (fr) * | 1974-12-07 | 1976-07-02 | Rolls Royce | Perfectionnements aux turbomoteurs |
GB1483532A (en) * | 1974-09-13 | 1977-08-24 | Rolls Royce | Stator structure for a gas turbine engine |
US4053254A (en) * | 1976-03-26 | 1977-10-11 | United Technologies Corporation | Turbine case cooling system |
GB1524956A (en) * | 1975-10-30 | 1978-09-13 | Rolls Royce | Gas tubine engine |
FR2416345A1 (fr) * | 1978-01-31 | 1979-08-31 | Snecma | Dispositif de refroidissement par impact des segments d'etancheite de turbine d'un turboreacteur |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE756582A (fr) * | 1969-10-02 | 1971-03-01 | Gen Electric | Ecran circulaire et support d'ecran avec dispositif de reglage de la temperature pour turbomachine |
BE755567A (fr) * | 1969-12-01 | 1971-02-15 | Gen Electric | Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe |
US3742705A (en) * | 1970-12-28 | 1973-07-03 | United Aircraft Corp | Thermal response shroud for rotating body |
US3844343A (en) * | 1973-02-02 | 1974-10-29 | Gen Electric | Impingement-convective cooling system |
GB1519590A (en) * | 1974-11-11 | 1978-08-02 | Rolls Royce | Gas turbine engine |
GB1484288A (en) * | 1975-12-03 | 1977-09-01 | Rolls Royce | Gas turbine engines |
US4126405A (en) * | 1976-12-16 | 1978-11-21 | General Electric Company | Turbine nozzle |
-
1978
- 1978-06-05 US US05/912,904 patent/US4303371A/en not_active Expired - Lifetime
-
1979
- 1979-02-28 DE DE2907769A patent/DE2907769C2/de not_active Expired - Lifetime
- 1979-02-28 GB GB7906994A patent/GB2035466B/en not_active Expired
- 1979-02-28 IT IT20610/79A patent/IT1110149B/it active
- 1979-03-02 JP JP2348979A patent/JPS54159516A/ja active Granted
- 1979-03-05 FR FR7905594A patent/FR2428141B1/fr not_active Expired
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1308771A (en) * | 1966-11-02 | 1973-03-07 | Gen Electric | Fluid cooled porous stator structure |
US3825364A (en) * | 1972-06-09 | 1974-07-23 | Gen Electric | Porous abradable turbine shroud |
US3864056A (en) * | 1973-07-27 | 1975-02-04 | Westinghouse Electric Corp | Cooled turbine blade ring assembly |
FR2238838A1 (fr) * | 1973-07-27 | 1975-02-21 | Westinghouse Electric Corp | |
FR2280791A1 (fr) * | 1974-07-31 | 1976-02-27 | Snecma | Perfectionnements au reglage du jeu entre les aubes et le stator d'une turbine |
GB1483532A (en) * | 1974-09-13 | 1977-08-24 | Rolls Royce | Stator structure for a gas turbine engine |
FR2293594A1 (fr) * | 1974-12-07 | 1976-07-02 | Rolls Royce | Perfectionnements aux turbomoteurs |
GB1524956A (en) * | 1975-10-30 | 1978-09-13 | Rolls Royce | Gas tubine engine |
US4053254A (en) * | 1976-03-26 | 1977-10-11 | United Technologies Corporation | Turbine case cooling system |
FR2416345A1 (fr) * | 1978-01-31 | 1979-08-31 | Snecma | Dispositif de refroidissement par impact des segments d'etancheite de turbine d'un turboreacteur |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0243274A1 (fr) * | 1986-04-24 | 1987-10-28 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Anneau de turbine sectorisé |
FR2597921A1 (fr) * | 1986-04-24 | 1987-10-30 | Snecma | Anneau de turbine sectorise |
US4759687A (en) * | 1986-04-24 | 1988-07-26 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Turbine ring incorporating elements of a ceramic composition divided into sectors |
EP1903186A1 (fr) * | 2006-09-22 | 2008-03-26 | Snecma | Dispositif d' écran thermique sur le carter de turbine pour le contrôle du jeu en sommet d'aube |
FR2906295A1 (fr) * | 2006-09-22 | 2008-03-28 | Snecma Sa | Dispositif de toles isolantes sur carter pour amelioration du jeu en sommet d'aube |
US7946807B2 (en) | 2006-09-22 | 2011-05-24 | Snecma | Set of insulating sheets on a casing to improve blade tip clearance |
FR2922589A1 (fr) * | 2007-10-22 | 2009-04-24 | Snecma Sa | Controle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine |
EP2053200A1 (fr) | 2007-10-22 | 2009-04-29 | Snecma | Contrôle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine |
US8100635B2 (en) | 2007-10-22 | 2012-01-24 | Snecma | Control of clearance at blade tips in a high-pressure turbine of a turbine engine |
FR2972760A1 (fr) * | 2011-03-16 | 2012-09-21 | Snecma | Anneau de carter de turbomachine |
Also Published As
Publication number | Publication date |
---|---|
GB2035466A (en) | 1980-06-18 |
GB2035466B (en) | 1982-12-15 |
IT7920610A0 (it) | 1979-02-28 |
JPS54159516A (en) | 1979-12-17 |
DE2907769C2 (de) | 1994-02-03 |
DE2907769A1 (de) | 1979-12-13 |
JPH0228683B2 (fr) | 1990-06-26 |
IT1110149B (it) | 1985-12-23 |
US4303371A (en) | 1981-12-01 |
FR2428141B1 (fr) | 1986-03-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
DL | Decision of the director general to leave to make available licences of right |