CA2366363A1 - Agencement de reglage de diametre d'un stator de turbine a gaz - Google Patents
Agencement de reglage de diametre d'un stator de turbine a gaz Download PDFInfo
- Publication number
- CA2366363A1 CA2366363A1 CA002366363A CA2366363A CA2366363A1 CA 2366363 A1 CA2366363 A1 CA 2366363A1 CA 002366363 A CA002366363 A CA 002366363A CA 2366363 A CA2366363 A CA 2366363A CA 2366363 A1 CA2366363 A1 CA 2366363A1
- Authority
- CA
- Canada
- Prior art keywords
- stator
- regulating
- array
- diameter
- gas 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.)
- 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
- 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
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Abstract
Du gaz de ventilation est soufflé vers un anneau de stator (3) pour régler sa distance du bout d'aubes mobiles (5) et diminuer les fuites dans une turbine de machine. On propose d'opérer des communications entre chambres successives (18, 19, 20) à travers des crochets (26, 27, 28 et 29) de fixation d'une entretoise (10) de support de l'anneau (3) au carter (2), afin de réduire les concentrations de contrainte dans cette entretoise (10).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR00/00371 | 2000-01-13 | ||
FR0000371A FR2803871B1 (fr) | 2000-01-13 | 2000-01-13 | Agencement de reglage de diametre d'un stator de turbine a gaz |
PCT/FR2001/000101 WO2001051771A2 (fr) | 2000-01-13 | 2001-01-12 | Agencement de reglage de diametre d'un stator de turbine a gaz |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2366363A1 true CA2366363A1 (fr) | 2001-07-19 |
CA2366363C CA2366363C (fr) | 2008-12-09 |
Family
ID=8845853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002366363A Expired - Lifetime CA2366363C (fr) | 2000-01-13 | 2001-01-12 | Agencement de reglage de diametre d'un stator de turbine a gaz |
Country Status (10)
Country | Link |
---|---|
US (1) | US6666645B1 (fr) |
EP (1) | EP1134360B1 (fr) |
JP (1) | JP4248785B2 (fr) |
CA (1) | CA2366363C (fr) |
DE (1) | DE60114910T2 (fr) |
ES (1) | ES2248248T3 (fr) |
FR (1) | FR2803871B1 (fr) |
RU (1) | RU2292466C2 (fr) |
UA (1) | UA70353C2 (fr) |
WO (1) | WO2001051771A2 (fr) |
Families Citing this family (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2816352B1 (fr) * | 2000-11-09 | 2003-01-31 | Snecma Moteurs | Ensemble de ventilation d'un anneau de stator |
US6893217B2 (en) * | 2002-12-20 | 2005-05-17 | General Electric Company | Methods and apparatus for assembling gas turbine nozzles |
US6892931B2 (en) * | 2002-12-27 | 2005-05-17 | General Electric Company | Methods for replacing portions of turbine shroud supports |
FR2857406B1 (fr) * | 2003-07-10 | 2005-09-30 | Snecma Moteurs | Refroidissement des anneaux de turbine |
DE102005013796A1 (de) * | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
DE102005013797A1 (de) * | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
US7600967B2 (en) * | 2005-07-30 | 2009-10-13 | United Technologies Corporation | Stator assembly, module and method for forming a rotary machine |
FR2899281B1 (fr) * | 2006-03-30 | 2012-08-10 | Snecma | Dispositif de refroidissement d'un carter de turbine d'une turbomachine |
US20070249823A1 (en) * | 2006-04-20 | 2007-10-25 | Chemagis Ltd. | Process for preparing gemcitabine and associated intermediates |
US7785063B2 (en) * | 2006-12-15 | 2010-08-31 | Siemens Energy, Inc. | Tip clearance control |
US7597533B1 (en) | 2007-01-26 | 2009-10-06 | Florida Turbine Technologies, Inc. | BOAS with multi-metering diffusion cooling |
US7665962B1 (en) | 2007-01-26 | 2010-02-23 | Florida Turbine Technologies, Inc. | Segmented ring for an industrial gas turbine |
AU2009216831B2 (en) * | 2008-02-20 | 2014-11-20 | General Electric Technology Gmbh | Gas turbine |
US8123473B2 (en) * | 2008-10-31 | 2012-02-28 | General Electric Company | Shroud hanger with diffused cooling passage |
JP5254774B2 (ja) * | 2008-12-22 | 2013-08-07 | 三菱重工業株式会社 | 熱機関の流体シール構造 |
EP2415969A1 (fr) * | 2010-08-05 | 2012-02-08 | Siemens Aktiengesellschaft | Composant d'une turbine avec des joints lamelles et procédé d'étanchéification contre les fuites entre une pale et un élément porteur |
RU2465466C1 (ru) * | 2011-05-05 | 2012-10-27 | Открытое акционерное общество "Авиадвигатель" | Высокотемпературная турбина газотурбинного двигателя |
US8826668B2 (en) * | 2011-08-02 | 2014-09-09 | Siemens Energy, Inc. | Two stage serial impingement cooling for isogrid structures |
US9080458B2 (en) | 2011-08-23 | 2015-07-14 | United Technologies Corporation | Blade outer air seal with multi impingement plate assembly |
US9745854B2 (en) | 2012-04-27 | 2017-08-29 | General Electric Company | Shroud assembly and seal for a gas turbine engine |
EP2719867B1 (fr) * | 2012-10-12 | 2015-01-21 | MTU Aero Engines GmbH | Structure de boîtier avec étanchéification et refroidissement améliorés |
EP2728255A1 (fr) * | 2012-10-31 | 2014-05-07 | Alstom Technology Ltd | Agencement de segment de gaz chaud |
US9752451B2 (en) * | 2012-12-19 | 2017-09-05 | United Technologies Corporation | Active clearance control system with zone controls |
FR3002971B1 (fr) * | 2013-03-06 | 2015-04-17 | Snecma | Dispositif de ventilation d'un carter de stator d'une turbomachine, comprenant un ajustement sur des circonferences |
FR3002972B1 (fr) * | 2013-03-06 | 2015-04-17 | Snecma | Dispositif de ventilation d'un carter de stator d'une turbomachine comprenant un ajustement en direction axiale |
DE102013212501A1 (de) * | 2013-06-27 | 2014-12-31 | MTU Aero Engines AG | Leitschaufelsegment mit stirnseitiger Ausnehmung |
US9464538B2 (en) * | 2013-07-08 | 2016-10-11 | General Electric Company | Shroud block segment for a gas turbine |
FR3009579B1 (fr) * | 2013-08-07 | 2015-09-25 | Snecma | Carter de turbine en deux materiaux |
WO2015038906A1 (fr) | 2013-09-12 | 2015-03-19 | United Technologies Corporation | Système de réglage de garde en extrémité des aubes comprenant un support de joint d'aube externe étanche à l'air (boas) |
WO2015138027A2 (fr) | 2013-12-17 | 2015-09-17 | United Technologies Corporation | Plaque de dosge pour élément d'étanchéité à l'air externe d'aube |
EP3183431B1 (fr) | 2014-08-22 | 2018-10-10 | Siemens Aktiengesellschaft | Système de refroidissement de carénage pour des carénages adjacents à des surfaces portantes dans des moteurs à turbine à gaz |
US10100659B2 (en) * | 2014-12-16 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Hanger system for a turbine engine component |
US20170248030A1 (en) * | 2016-02-26 | 2017-08-31 | General Electric Company | Encapsulated Cooling for Turbine Shrouds |
FR3049003B1 (fr) * | 2016-03-21 | 2018-04-06 | Safran Aircraft Engines | Ensemble d'anneau de turbine sans jeu de montage a froid |
US10815814B2 (en) * | 2017-05-08 | 2020-10-27 | Raytheon Technologies Corporation | Re-use and modulated cooling from tip clearance control system for gas turbine engine |
GB201708744D0 (en) * | 2017-06-01 | 2017-07-19 | Rolls Royce Plc | Clearance control arrangement |
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 |
US20190218928A1 (en) * | 2018-01-17 | 2019-07-18 | United Technologies Corporation | Blade outer air seal for gas turbine engine |
FR3082872B1 (fr) * | 2018-06-25 | 2021-06-04 | Safran Aircraft Engines | Dispositif de refroidissement d'un carter de turbomachine |
US10634010B2 (en) | 2018-09-05 | 2020-04-28 | United Technologies Corporation | CMC BOAS axial retaining clip |
US11761343B2 (en) * | 2019-03-13 | 2023-09-19 | Rtx Corporation | BOAS carrier with dovetail attachments |
US10995626B2 (en) * | 2019-03-15 | 2021-05-04 | Raytheon Technologies Corporation | BOAS and methods of making a BOAS having fatigue resistant cooling inlets |
FR3109406B1 (fr) * | 2020-04-17 | 2022-10-07 | Safran Aircraft Engines | Dispositif de refroidissement d’un carter de turbine |
FR3127981A1 (fr) * | 2021-10-08 | 2023-04-14 | Safran Aircraft Engines | Virole annulaire de turbine |
US11788425B2 (en) * | 2021-11-05 | 2023-10-17 | General Electric Company | Gas turbine engine with clearance control system |
EP4332351A1 (fr) * | 2022-09-05 | 2024-03-06 | General Electric Company Polska Sp. Z o.o | Ensemble boîtier externe de rotor de turbine |
US20240110487A1 (en) * | 2022-09-30 | 2024-04-04 | Rtx Corporation | Blade outer air seal with retainer ring |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3391904A (en) * | 1966-11-02 | 1968-07-09 | United Aircraft Corp | Optimum response tip seal |
US4177004A (en) * | 1977-10-31 | 1979-12-04 | General Electric Company | Combined turbine shroud and vane support structure |
US4573866A (en) * | 1983-05-02 | 1986-03-04 | United Technologies Corporation | Sealed shroud for rotating body |
JPH07503298A (ja) * | 1992-11-24 | 1995-04-06 | ユナイテッド テクノロジーズ コーポレイション | タービン用の冷却可能なアウタエアシール装置 |
-
2000
- 2000-01-13 FR FR0000371A patent/FR2803871B1/fr not_active Expired - Fee Related
-
2001
- 2001-01-11 ES ES01400059T patent/ES2248248T3/es not_active Expired - Lifetime
- 2001-01-11 DE DE60114910T patent/DE60114910T2/de not_active Expired - Lifetime
- 2001-01-11 EP EP01400059A patent/EP1134360B1/fr not_active Expired - Lifetime
- 2001-01-12 WO PCT/FR2001/000101 patent/WO2001051771A2/fr active Application Filing
- 2001-01-12 CA CA002366363A patent/CA2366363C/fr not_active Expired - Lifetime
- 2001-01-12 US US09/926,122 patent/US6666645B1/en not_active Expired - Lifetime
- 2001-01-12 RU RU2001127713/06A patent/RU2292466C2/ru active
- 2001-01-12 JP JP2001551951A patent/JP4248785B2/ja not_active Expired - Fee Related
- 2001-12-01 UA UA2001096296A patent/UA70353C2/uk unknown
Also Published As
Publication number | Publication date |
---|---|
US6666645B1 (en) | 2003-12-23 |
FR2803871A1 (fr) | 2001-07-20 |
EP1134360A3 (fr) | 2002-07-31 |
EP1134360A2 (fr) | 2001-09-19 |
WO2001051771A3 (fr) | 2002-01-17 |
ES2248248T3 (es) | 2006-03-16 |
WO2001051771A2 (fr) | 2001-07-19 |
DE60114910T2 (de) | 2006-08-10 |
RU2292466C2 (ru) | 2007-01-27 |
FR2803871B1 (fr) | 2002-06-07 |
UA70353C2 (uk) | 2004-10-15 |
JP4248785B2 (ja) | 2009-04-02 |
CA2366363C (fr) | 2008-12-09 |
JP2003519742A (ja) | 2003-06-24 |
EP1134360B1 (fr) | 2005-11-16 |
DE60114910D1 (de) | 2005-12-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request |