CA2806401A1 - Enveloppe de turbine a faible ductilite - Google Patents
Enveloppe de turbine a faible ductilite Download PDFInfo
- Publication number
- CA2806401A1 CA2806401A1 CA2806401A CA2806401A CA2806401A1 CA 2806401 A1 CA2806401 A1 CA 2806401A1 CA 2806401 A CA2806401 A CA 2806401A CA 2806401 A CA2806401 A CA 2806401A CA 2806401 A1 CA2806401 A1 CA 2806401A1
- Authority
- CA
- Canada
- Prior art keywords
- shroud segment
- wall
- walls
- aft
- hanger
- 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.)
- Abandoned
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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- 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
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
- F05D2300/6033—Ceramic matrix composites [CMC]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/402,616 | 2012-02-22 | ||
US13/402,616 US9175579B2 (en) | 2011-12-15 | 2012-02-22 | Low-ductility turbine shroud |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2806401A1 true CA2806401A1 (fr) | 2013-08-22 |
Family
ID=47790007
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2806401A Abandoned CA2806401A1 (fr) | 2012-02-22 | 2013-02-14 | Enveloppe de turbine a faible ductilite |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP2631434A3 (fr) |
JP (1) | JP6063285B2 (fr) |
CN (1) | CN103291387B (fr) |
CA (1) | CA2806401A1 (fr) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
JP6114878B2 (ja) * | 2013-05-17 | 2017-04-12 | ゼネラル・エレクトリック・カンパニイ | Cmcシュラウド支持システム |
WO2015088869A1 (fr) | 2013-12-12 | 2015-06-18 | General Electric Company | Système de support de carénage cmc |
US10472989B2 (en) | 2014-01-17 | 2019-11-12 | General Electric Company | CMC hanger sleeve for CMC shroud |
EP2930308B1 (fr) * | 2014-04-11 | 2021-07-28 | Safran Aero Boosters SA | Carter à facettes de turbomachine axiale |
RU2700848C2 (ru) * | 2014-05-15 | 2019-09-23 | Нуово Пиньоне СРЛ | Способ изготовления компонента турбомашины, компонент турбомашины и турбомашина |
JP6363232B2 (ja) * | 2014-06-12 | 2018-07-25 | ゼネラル・エレクトリック・カンパニイ | シュラウドハンガーアセンブリ |
JP6574208B2 (ja) * | 2014-06-12 | 2019-09-11 | ゼネラル・エレクトリック・カンパニイ | シュラウドハンガアセンブリ |
EP3155231B1 (fr) * | 2014-06-12 | 2019-07-03 | General Electric Company | Ensemble dispositif de suspension de carénage |
US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
US10422244B2 (en) * | 2015-03-16 | 2019-09-24 | General Electric Company | System for cooling a turbine shroud |
FR3034132B1 (fr) * | 2015-03-23 | 2018-06-15 | Safran Ceramics | Ensemble d'anneau de turbine comprenant une pluralite de secteurs d'anneau en materiau composite a matrice ceramique |
CA2925588A1 (fr) | 2015-04-29 | 2016-10-29 | Rolls-Royce Corporation | Sillage de pale brase destine a une turbine a gaz |
US10550709B2 (en) | 2015-04-30 | 2020-02-04 | Rolls-Royce North American Technologies Inc. | Full hoop blade track with flanged segments |
US9932901B2 (en) | 2015-05-11 | 2018-04-03 | General Electric Company | Shroud retention system with retention springs |
US9915153B2 (en) * | 2015-05-11 | 2018-03-13 | General Electric Company | Turbine shroud segment assembly with expansion joints |
FR3036433B1 (fr) | 2015-05-22 | 2019-09-13 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien par crabotage |
CA2936977A1 (fr) * | 2015-07-24 | 2017-01-24 | Rolls-Royce Corporation | Un segment de joint destine a une turbine a gaz |
US10100654B2 (en) | 2015-11-24 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Impingement tubes for CMC seal segment cooling |
FR3048016B1 (fr) * | 2016-02-18 | 2018-03-16 | Safran Ceramics | Secteur d'anneau de turbine avec barriere environnementale dopee par un element electriquement conducteur |
US20170370583A1 (en) * | 2016-06-22 | 2017-12-28 | General Electric Company | Ceramic Matrix Composite Component for a Gas Turbine Engine |
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 |
US10633996B2 (en) | 2016-11-17 | 2020-04-28 | Rolls-Royce Corporation | Turbine cooling system |
US10619514B2 (en) | 2017-10-18 | 2020-04-14 | Rolls-Royce Corporation | Ceramic matrix composite assembly with compliant pin attachment features |
US20190170013A1 (en) * | 2017-12-06 | 2019-06-06 | General Electric Company | Discontinuous Molded Tape Wear Interface for Composite Components |
US10801350B2 (en) | 2018-02-23 | 2020-10-13 | Rolls-Royce Corporation | Actively cooled engine assembly with ceramic matrix composite components |
US11408300B2 (en) * | 2018-12-03 | 2022-08-09 | Raytheon Technologies Corporation | Rotor overspeed protection assembly |
US10934878B2 (en) * | 2018-12-05 | 2021-03-02 | Raytheon Technologies Corporation | CMC loop boas |
US10914186B2 (en) * | 2018-12-05 | 2021-02-09 | Raytheon Technologies Corporation | BOAS control structure with center support hook |
US11724969B2 (en) * | 2018-12-14 | 2023-08-15 | General Electric Company | Coating for improved surface finish |
US10927694B2 (en) | 2019-03-13 | 2021-02-23 | Raytheon Technologies Corporation | BOAS carrier with cooling supply |
FR3095668B1 (fr) * | 2019-05-03 | 2021-04-09 | Safran Aircraft Engines | Ensemble d’anneau de turbine monté sur entretoise |
US11365644B2 (en) * | 2019-07-01 | 2022-06-21 | Raytheon Technologies Corporation | Double box boas and carrier system |
CN113062781B (zh) * | 2021-05-06 | 2022-07-08 | 中国航发湖南动力机械研究所 | 一种用于cmc燃气涡轮外环的定心定位结构 |
Family Cites Families (15)
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 |
FR2580033A1 (en) * | 1985-04-03 | 1986-10-10 | Snecma | Elastically suspended turbine ring for a turbine machine |
JPH10103014A (ja) * | 1996-09-30 | 1998-04-21 | Toshiba Corp | ガスタービンシュラウド構造 |
US6340285B1 (en) * | 2000-06-08 | 2002-01-22 | General Electric Company | End rail cooling for combined high and low pressure turbine shroud |
US6478545B2 (en) * | 2001-03-07 | 2002-11-12 | General Electric Company | Fluted blisk |
US6733233B2 (en) * | 2002-04-26 | 2004-05-11 | Pratt & Whitney Canada Corp. | Attachment of a ceramic shroud in a metal housing |
JP2004036443A (ja) * | 2002-07-02 | 2004-02-05 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービンシュラウド構造 |
US7270518B2 (en) * | 2005-05-19 | 2007-09-18 | General Electric Company | Steep angle turbine cover buckets having relief grooves |
US7563071B2 (en) * | 2005-08-04 | 2009-07-21 | Siemens Energy, Inc. | Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine |
US7648336B2 (en) * | 2006-01-03 | 2010-01-19 | General Electric Company | Apparatus and method for assembling a gas turbine stator |
US7749565B2 (en) | 2006-09-29 | 2010-07-06 | General Electric Company | Method for applying and dimensioning an abradable coating |
GB0703827D0 (en) * | 2007-02-28 | 2007-04-11 | Rolls Royce Plc | Rotor seal segment |
JP5490736B2 (ja) * | 2010-01-25 | 2014-05-14 | 株式会社日立製作所 | セラミックアブレーダブルコーテイングを有するガスタービン用シュラウド |
US8740552B2 (en) * | 2010-05-28 | 2014-06-03 | General Electric Company | Low-ductility turbine shroud and mounting apparatus |
US8753073B2 (en) * | 2010-06-23 | 2014-06-17 | General Electric Company | Turbine shroud sealing apparatus |
-
2013
- 2013-02-14 CA CA2806401A patent/CA2806401A1/fr not_active Abandoned
- 2013-02-15 JP JP2013027200A patent/JP6063285B2/ja not_active Expired - Fee Related
- 2013-02-22 CN CN201310056712.0A patent/CN103291387B/zh active Active
- 2013-02-22 EP EP13156445.2A patent/EP2631434A3/fr not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP2631434A3 (fr) | 2017-07-26 |
JP6063285B2 (ja) | 2017-01-18 |
CN103291387B (zh) | 2017-04-26 |
CN103291387A (zh) | 2013-09-11 |
JP2013170578A (ja) | 2013-09-02 |
EP2631434A2 (fr) | 2013-08-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Dead |
Effective date: 20190214 |