IN2014CN03298A - - Google Patents
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- Publication number
- IN2014CN03298A IN2014CN03298A IN3298CHN2014A IN2014CN03298A IN 2014CN03298 A IN2014CN03298 A IN 2014CN03298A IN 3298CHN2014 A IN3298CHN2014 A IN 3298CHN2014A IN 2014CN03298 A IN2014CN03298 A IN 2014CN03298A
- Authority
- IN
- India
- Prior art keywords
- axial
- radial
- slot
- leg
- received
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
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- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- 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
- F05D2240/00—Components
- F05D2240/55—Seals
- F05D2240/57—Leaf seals
-
- 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
- F05D2240/55—Seals
- F05D2240/59—Lamellar seals
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161556270P | 2011-11-06 | 2011-11-06 | |
US13/443,947 US9810086B2 (en) | 2011-11-06 | 2012-04-11 | Asymmetric radial spline seal for a gas turbine engine |
PCT/US2012/052185 WO2013074165A2 (fr) | 2011-11-06 | 2012-08-24 | Joint cannelé radial asymétrique pour un moteur à turbine à gaz |
Publications (1)
Publication Number | Publication Date |
---|---|
IN2014CN03298A true IN2014CN03298A (fr) | 2015-10-09 |
Family
ID=48223803
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN3298CHN2014 IN2014CN03298A (fr) | 2011-11-06 | 2012-08-24 |
Country Status (8)
Country | Link |
---|---|
US (1) | US9810086B2 (fr) |
EP (1) | EP2776681A2 (fr) |
JP (1) | JP6031116B2 (fr) |
CN (1) | CN103906896B (fr) |
BR (1) | BR112014010747A8 (fr) |
CA (1) | CA2853622C (fr) |
IN (1) | IN2014CN03298A (fr) |
WO (1) | WO2013074165A2 (fr) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9810086B2 (en) * | 2011-11-06 | 2017-11-07 | General Electric Company | Asymmetric radial spline seal for a gas turbine engine |
JP5717904B1 (ja) * | 2014-08-04 | 2015-05-13 | 三菱日立パワーシステムズ株式会社 | 静翼、ガスタービン、分割環、静翼の改造方法、および、分割環の改造方法 |
US9915159B2 (en) | 2014-12-18 | 2018-03-13 | General Electric Company | Ceramic matrix composite nozzle mounted with a strut and concepts thereof |
FR3041993B1 (fr) * | 2015-10-05 | 2019-06-21 | Safran Aircraft Engines | Ensemble d'anneau de turbine avec maintien axial |
US10161257B2 (en) | 2015-10-20 | 2018-12-25 | General Electric Company | Turbine slotted arcuate leaf seal |
US10494943B2 (en) * | 2016-02-03 | 2019-12-03 | General Electric Company | Spline seal for a gas turbine engine |
US10557360B2 (en) * | 2016-10-17 | 2020-02-11 | United Technologies Corporation | Vane intersegment gap sealing arrangement |
US10655495B2 (en) * | 2017-02-24 | 2020-05-19 | General Electric Company | Spline for a turbine engine |
KR101937586B1 (ko) * | 2017-09-12 | 2019-01-10 | 두산중공업 주식회사 | 베인 조립체, 터빈 및 이를 포함하는 가스터빈 |
EP3456927B1 (fr) * | 2017-09-15 | 2021-05-05 | General Electric Company Polska sp. z o.o. | Ensemble d'aube de guidage pour une machine rotative |
US10662794B2 (en) * | 2017-10-19 | 2020-05-26 | Rolls-Royce Corporation | Strip seal axial assembly groove |
EP3486018A1 (fr) | 2017-11-20 | 2019-05-22 | Agie Charmilles SA | Procédé et dispositif d'usinage de formes utilisant un usinage électrique |
US20190309643A1 (en) * | 2018-04-05 | 2019-10-10 | United Technologies Corporation | Axial stiffening ribs/augmentation fins |
US10982559B2 (en) | 2018-08-24 | 2021-04-20 | General Electric Company | Spline seal with cooling features for turbine engines |
US10794206B2 (en) * | 2018-09-05 | 2020-10-06 | Raytheon Technologies Corporation | CMC BOAS intersegment seal |
US20200141276A1 (en) * | 2018-11-07 | 2020-05-07 | General Electric Company | Turbine shroud with lapped seal segments |
US11021990B2 (en) * | 2018-12-19 | 2021-06-01 | General Electric Company | Shroud sealing for a gas turbine engine |
US11326463B2 (en) * | 2019-06-19 | 2022-05-10 | Raytheon Technologies Corporation | BOAS thermal baffle |
US11187094B2 (en) | 2019-08-26 | 2021-11-30 | General Electric Company | Spline for a turbine engine |
US11401830B2 (en) | 2019-09-06 | 2022-08-02 | Raytheon Technologies Corporation | Geometry for a turbine engine blade outer air seal |
US11215063B2 (en) | 2019-10-10 | 2022-01-04 | General Electric Company | Seal assembly for chute gap leakage reduction in a gas turbine |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5074748A (en) | 1990-07-30 | 1991-12-24 | General Electric Company | Seal assembly for segmented turbine engine structures |
US5154577A (en) | 1991-01-17 | 1992-10-13 | General Electric Company | Flexible three-piece seal assembly |
US5641267A (en) * | 1995-06-06 | 1997-06-24 | General Electric Company | Controlled leakage shroud panel |
US5655876A (en) | 1996-01-02 | 1997-08-12 | General Electric Company | Low leakage turbine nozzle |
US5868398A (en) | 1997-05-20 | 1999-02-09 | United Technologies Corporation | Gas turbine stator vane seal |
US6162014A (en) | 1998-09-22 | 2000-12-19 | General Electric Company | Turbine spline seal and turbine assembly containing such spline seal |
FR2786222B1 (fr) * | 1998-11-19 | 2000-12-29 | Snecma | Dispositif d'etancheite a lamelle |
US6503051B2 (en) | 2001-06-06 | 2003-01-07 | General Electric Company | Overlapping interference seal and methods for forming the seal |
US6814538B2 (en) * | 2003-01-22 | 2004-11-09 | General Electric Company | Turbine stage one shroud configuration and method for service enhancement |
FR2869070B1 (fr) * | 2004-04-15 | 2008-10-17 | Snecma Moteurs Sa | Anneau de turbine |
US7063503B2 (en) * | 2004-04-15 | 2006-06-20 | Pratt & Whitney Canada Corp. | Turbine shroud cooling system |
FR2869944B1 (fr) * | 2004-05-04 | 2006-08-11 | Snecma Moteurs Sa | Dispositif de refroidissement pour anneau fixe de turbine a gaz |
FR2869943B1 (fr) * | 2004-05-04 | 2006-07-28 | Snecma Moteurs Sa | Ensemble a anneau fixe d'une turbine a gaz |
US7600967B2 (en) * | 2005-07-30 | 2009-10-13 | United Technologies Corporation | Stator assembly, module and method for forming a rotary machine |
US7625174B2 (en) | 2005-12-16 | 2009-12-01 | General Electric Company | Methods and apparatus for assembling gas turbine engine stator assemblies |
US7316402B2 (en) | 2006-03-09 | 2008-01-08 | United Technologies Corporation | Segmented component seal |
US20070212214A1 (en) | 2006-03-09 | 2007-09-13 | United Technologies Corporation | Segmented component seal |
US7631879B2 (en) | 2006-06-21 | 2009-12-15 | General Electric Company | “L” butt gap seal between segments in seal assemblies |
EP2213841B1 (fr) * | 2009-01-28 | 2011-12-14 | Alstom Technology Ltd | Languette d'étanchéité et son procédé de conception |
US8360716B2 (en) * | 2010-03-23 | 2013-01-29 | United Technologies Corporation | Nozzle segment with reduced weight flange |
FR2968350B1 (fr) * | 2010-12-06 | 2016-01-29 | Snecma | Anneau sectorise de turbine pour turbomachine, et turbomachine equipee d'un tel anneau |
US9810086B2 (en) * | 2011-11-06 | 2017-11-07 | General Electric Company | Asymmetric radial spline seal for a gas turbine engine |
-
2012
- 2012-04-11 US US13/443,947 patent/US9810086B2/en active Active
- 2012-08-24 BR BR112014010747A patent/BR112014010747A8/pt not_active IP Right Cessation
- 2012-08-24 EP EP12832724.4A patent/EP2776681A2/fr not_active Withdrawn
- 2012-08-24 CA CA2853622A patent/CA2853622C/fr not_active Expired - Fee Related
- 2012-08-24 JP JP2014539946A patent/JP6031116B2/ja not_active Expired - Fee Related
- 2012-08-24 CN CN201280054278.6A patent/CN103906896B/zh active Active
- 2012-08-24 IN IN3298CHN2014 patent/IN2014CN03298A/en unknown
- 2012-08-24 WO PCT/US2012/052185 patent/WO2013074165A2/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2013074165A3 (fr) | 2013-08-15 |
EP2776681A2 (fr) | 2014-09-17 |
CN103906896A (zh) | 2014-07-02 |
US9810086B2 (en) | 2017-11-07 |
WO2013074165A8 (fr) | 2013-06-27 |
BR112014010747A2 (pt) | 2017-06-13 |
CA2853622A1 (fr) | 2013-05-23 |
CA2853622C (fr) | 2016-12-13 |
CN103906896B (zh) | 2016-08-31 |
BR112014010747A8 (pt) | 2017-06-20 |
WO2013074165A2 (fr) | 2013-05-23 |
JP6031116B2 (ja) | 2016-11-24 |
JP2014532831A (ja) | 2014-12-08 |
US20130115065A1 (en) | 2013-05-09 |
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