HK1107387A1 - A device for attaching ring sectors around a turbine rotor of a turbomachine - Google Patents
A device for attaching ring sectors around a turbine rotor of a turbomachineInfo
- Publication number
- HK1107387A1 HK1107387A1 HK08101072.1A HK08101072A HK1107387A1 HK 1107387 A1 HK1107387 A1 HK 1107387A1 HK 08101072 A HK08101072 A HK 08101072A HK 1107387 A1 HK1107387 A1 HK 1107387A1
- Authority
- HK
- Hong Kong
- Prior art keywords
- turbomachine
- turbine rotor
- ring sectors
- attaching ring
- sectors around
- Prior art date
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
-
- 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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- 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
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0602746A FR2899274B1 (fr) | 2006-03-30 | 2006-03-30 | Dispositif de fixation de secteurs d'anneau autour d'une roue de turbine d'une turbomachine |
Publications (1)
Publication Number | Publication Date |
---|---|
HK1107387A1 true HK1107387A1 (en) | 2008-04-03 |
Family
ID=37401478
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
HK08101072.1A HK1107387A1 (en) | 2006-03-30 | 2008-01-28 | A device for attaching ring sectors around a turbine rotor of a turbomachine |
Country Status (9)
Country | Link |
---|---|
US (1) | US7789619B2 (xx) |
EP (1) | EP1840339B1 (xx) |
JP (1) | JP4820321B2 (xx) |
KR (1) | KR101369067B1 (xx) |
CN (1) | CN101046161B (xx) |
CA (1) | CA2582401C (xx) |
FR (1) | FR2899274B1 (xx) |
HK (1) | HK1107387A1 (xx) |
RU (1) | RU2403405C2 (xx) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005013797A1 (de) * | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
DE102005013796A1 (de) * | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
US20090014964A1 (en) * | 2007-07-09 | 2009-01-15 | Siemens Power Generation, Inc. | Angled honeycomb seal between turbine rotors and turbine stators in a turbine engine |
FR2923526B1 (fr) | 2007-11-13 | 2013-12-13 | Snecma | Etage de turbine ou de compresseur de turbomachine |
FR2923525B1 (fr) * | 2007-11-13 | 2009-12-18 | Snecma | Etancheite d'un anneau de rotor dans un etage de turbine |
FR2923527B1 (fr) * | 2007-11-13 | 2013-12-27 | Snecma | Etage de turbine ou de compresseur, en particulier de turbomachine |
FR2930593B1 (fr) * | 2008-04-23 | 2013-05-31 | Snecma | Piece thermomecanique de revolution autour d'un axe longitudinal, comprenant au moins une couronne abradable destinee a un labyrinthe d'etancheite |
FR2931197B1 (fr) * | 2008-05-16 | 2010-06-18 | Snecma | Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages axiaux pour sa prehension |
US8608424B2 (en) * | 2009-10-09 | 2013-12-17 | General Electric Company | Contoured honeycomb seal for a turbomachine |
FR2954400B1 (fr) * | 2009-12-18 | 2012-03-09 | Snecma | Etage de turbine dans une turbomachine |
FR2960591B1 (fr) * | 2010-06-01 | 2012-08-24 | Snecma | Dispositif pour caler en rotation un segment de distributeur dans un carter de turbomachine ; pion antirotation |
FR2961556B1 (fr) * | 2010-06-16 | 2015-12-11 | Snecma | Isolation du carter externe d'une turbine de turbomachine vis-a-vis d'un anneau sectorise |
JP5751950B2 (ja) * | 2011-06-20 | 2015-07-22 | 三菱日立パワーシステムズ株式会社 | ガスタービン及びガスタービンの補修方法 |
FR2983518B1 (fr) * | 2011-12-06 | 2014-02-07 | Snecma | Dispositif deverrouillable d'arret axial d'une couronne d'etancheite contactee par une roue mobile de module de turbomachine d'aeronef |
US9097136B2 (en) * | 2012-01-03 | 2015-08-04 | General Electric Company | Contoured honeycomb seal for turbine shroud |
US9410441B2 (en) * | 2012-09-13 | 2016-08-09 | Pratt & Whitney Canada Corp. | Turboprop engine with compressor turbine shroud |
FR2995949B1 (fr) * | 2012-09-25 | 2018-05-25 | Safran Aircraft Engines | Carter de turbomachine |
US10087771B2 (en) * | 2013-02-20 | 2018-10-02 | United Technologies Corporation | Gas turbine engine seal assembly |
RU2519656C1 (ru) * | 2013-03-01 | 2014-06-20 | Открытое акционерное общество "Авиадвигатель" | Турбина низкого давления |
EP2846001B1 (de) | 2013-09-06 | 2023-01-11 | MTU Aero Engines AG | Montage- und Demontageverfahren eines Gasturbinenrotors und zugehörige Werkzeug |
RU2534333C1 (ru) * | 2013-11-25 | 2014-11-27 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | Статор газовой турбины |
JP6233578B2 (ja) * | 2013-12-05 | 2017-11-22 | 株式会社Ihi | タービン |
EP2886802B1 (fr) * | 2013-12-20 | 2019-04-10 | Safran Aero Boosters SA | Joint de virole interne de dernier étage de compresseur de turbomachine axiale |
EP2896796B1 (fr) * | 2014-01-20 | 2019-09-18 | Safran Aero Boosters SA | Stator de turbomachine axiale et turbomachine associée |
FR3022578B1 (fr) * | 2014-06-23 | 2016-06-03 | Snecma | Procede de realisation et de reparation d’un distributeur de turbine d’une turbomachine |
FR3022944B1 (fr) * | 2014-06-26 | 2020-02-14 | Safran Aircraft Engines | Ensemble rotatif pour turbomachine |
US20170211407A1 (en) * | 2016-01-21 | 2017-07-27 | General Electric Company | Flow alignment devices to improve diffuser performance |
US20180347399A1 (en) * | 2017-06-01 | 2018-12-06 | Pratt & Whitney Canada Corp. | Turbine shroud with integrated heat shield |
FR3072713B1 (fr) * | 2017-10-23 | 2021-09-10 | Safran Aircraft Engines | Secteur d'anneau de turbine pour turbomachine d'aeronef |
FR3083563B1 (fr) | 2018-07-03 | 2020-07-24 | Safran Aircraft Engines | Module d'etancheite de turbomachine d'aeronef |
FR3100838B1 (fr) * | 2019-09-13 | 2021-10-01 | Safran Aircraft Engines | Anneau d’etancheite de turbomachine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2468741A1 (fr) * | 1979-10-26 | 1981-05-08 | Snecma | Perfectionnements aux anneaux a joint d'etancheite refroidi par l'air pour roues de turbine a gaz |
GB2206651B (en) * | 1987-07-01 | 1991-05-08 | Rolls Royce Plc | Turbine blade shroud structure |
GB2236147B (en) * | 1989-08-24 | 1993-05-12 | Rolls Royce Plc | Gas turbine engine with turbine tip clearance control device and method of operation |
US5609469A (en) * | 1995-11-22 | 1997-03-11 | United Technologies Corporation | Rotor assembly shroud |
JPH09329003A (ja) * | 1996-06-12 | 1997-12-22 | Ishikawajima Harima Heavy Ind Co Ltd | ガスシール装置を備えたタービンシュラウド |
JPH1162509A (ja) * | 1997-08-18 | 1999-03-05 | Ishikawajima Harima Heavy Ind Co Ltd | ジェットエンジンのタービンシュラウド支持構造 |
US6120242A (en) * | 1998-11-13 | 2000-09-19 | General Electric Company | Blade containing turbine shroud |
US6652226B2 (en) * | 2001-02-09 | 2003-11-25 | General Electric Co. | Methods and apparatus for reducing seal teeth wear |
DE10122464C1 (de) * | 2001-05-09 | 2002-03-07 | Mtu Aero Engines Gmbh | Mantelring |
FR2835563B1 (fr) * | 2002-02-07 | 2004-04-02 | Snecma Moteurs | Agencement d'accrochage de secteurs en arc de cercle de distributeur porteur d'aubes |
US7033138B2 (en) * | 2002-09-06 | 2006-04-25 | Mitsubishi Heavy Industries, Ltd. | Ring segment of gas turbine |
FR2852053B1 (fr) * | 2003-03-06 | 2007-12-28 | Snecma Moteurs | Turbine haute pression pour turbomachine |
WO2005003520A1 (en) * | 2003-07-04 | 2005-01-13 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine shroud segment |
JP4200846B2 (ja) | 2003-07-04 | 2008-12-24 | 株式会社Ihi | シュラウドセグメント |
-
2006
- 2006-03-30 FR FR0602746A patent/FR2899274B1/fr active Active
-
2007
- 2007-03-14 EP EP07290322.2A patent/EP1840339B1/fr active Active
- 2007-03-27 US US11/691,749 patent/US7789619B2/en active Active
- 2007-03-28 CA CA2582401A patent/CA2582401C/fr active Active
- 2007-03-29 RU RU2007111675/06A patent/RU2403405C2/ru active
- 2007-03-29 KR KR1020070030889A patent/KR101369067B1/ko active IP Right Grant
- 2007-03-29 JP JP2007086701A patent/JP4820321B2/ja active Active
- 2007-03-30 CN CN2007100906444A patent/CN101046161B/zh active Active
-
2008
- 2008-01-28 HK HK08101072.1A patent/HK1107387A1/xx unknown
Also Published As
Publication number | Publication date |
---|---|
US7789619B2 (en) | 2010-09-07 |
CN101046161B (zh) | 2011-06-15 |
JP2007270836A (ja) | 2007-10-18 |
KR20070098660A (ko) | 2007-10-05 |
RU2403405C2 (ru) | 2010-11-10 |
JP4820321B2 (ja) | 2011-11-24 |
FR2899274B1 (fr) | 2012-08-17 |
CA2582401A1 (fr) | 2007-09-30 |
FR2899274A1 (fr) | 2007-10-05 |
CA2582401C (fr) | 2014-01-28 |
CN101046161A (zh) | 2007-10-03 |
US20070231127A1 (en) | 2007-10-04 |
RU2007111675A (ru) | 2008-10-10 |
EP1840339A1 (fr) | 2007-10-03 |
KR101369067B1 (ko) | 2014-02-28 |
EP1840339B1 (fr) | 2018-01-03 |
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