GB201223193D0 - Turbine blade - Google Patents
Turbine bladeInfo
- Publication number
- GB201223193D0 GB201223193D0 GBGB1223193.2A GB201223193A GB201223193D0 GB 201223193 D0 GB201223193 D0 GB 201223193D0 GB 201223193 A GB201223193 A GB 201223193A GB 201223193 D0 GB201223193 D0 GB 201223193D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine blade
- turbine
- blade
- 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.)
- Ceased
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/13—Two-dimensional trapezoidal
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1223193.2A GB201223193D0 (en) | 2012-12-21 | 2012-12-21 | Turbine blade |
US14/100,784 US20140178207A1 (en) | 2012-12-21 | 2013-12-09 | Turbine blade |
EP13196186.4A EP2746536A1 (en) | 2012-12-21 | 2013-12-09 | Rotor stage of a turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1223193.2A GB201223193D0 (en) | 2012-12-21 | 2012-12-21 | Turbine blade |
Publications (1)
Publication Number | Publication Date |
---|---|
GB201223193D0 true GB201223193D0 (en) | 2013-02-06 |
Family
ID=47682419
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB1223193.2A Ceased GB201223193D0 (en) | 2012-12-21 | 2012-12-21 | Turbine blade |
Country Status (3)
Country | Link |
---|---|
US (1) | US20140178207A1 (en) |
EP (1) | EP2746536A1 (en) |
GB (1) | GB201223193D0 (en) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9850762B2 (en) | 2013-03-13 | 2017-12-26 | General Electric Company | Dust mitigation for turbine blade tip turns |
JP6462332B2 (en) * | 2014-11-20 | 2019-01-30 | 三菱重工業株式会社 | Turbine blade and gas turbine |
US20160245095A1 (en) * | 2015-02-25 | 2016-08-25 | General Electric Company | Turbine rotor blade |
CN104775854A (en) * | 2015-04-23 | 2015-07-15 | 华能国际电力股份有限公司 | Movable vane top structure capable of restraining tip leakage and reducing tip temperature |
US10107108B2 (en) | 2015-04-29 | 2018-10-23 | General Electric Company | Rotor blade having a flared tip |
JP6565105B2 (en) * | 2015-09-29 | 2019-08-28 | 三菱日立パワーシステムズ株式会社 | Rotor blade and gas turbine provided with the same |
CN105179022B (en) * | 2015-09-30 | 2017-06-27 | 北京大学 | A kind of turbo blade of use leaf top rib wing structure |
US10006294B2 (en) * | 2015-10-19 | 2018-06-26 | General Electric Company | Article and method of cooling an article |
US10260355B2 (en) | 2016-03-07 | 2019-04-16 | Honeywell International Inc. | Diverging-converging cooling passage for a turbine blade |
US10227878B2 (en) * | 2016-03-10 | 2019-03-12 | General Electric Company | Article and method of forming an article |
US10519861B2 (en) * | 2016-11-04 | 2019-12-31 | General Electric Company | Transition manifolds for cooling channel connections in cooled structures |
US11434770B2 (en) | 2017-03-28 | 2022-09-06 | Raytheon Technologies Corporation | Tip cooling design |
US11021967B2 (en) * | 2017-04-03 | 2021-06-01 | General Electric Company | Turbine engine component with a core tie hole |
US10605675B2 (en) | 2017-06-22 | 2020-03-31 | Unison Industries, Llc | Air temperature sensor |
US10545057B2 (en) | 2017-06-22 | 2020-01-28 | Unison Industries, Llc | Air temperature sensor and method of reducing error |
US10578498B2 (en) | 2017-06-22 | 2020-03-03 | Unison Industries, Llc | Air temperature sensor |
US10585007B2 (en) | 2017-06-22 | 2020-03-10 | Unison Industries, Llc | Air temperature sensor |
USD844466S1 (en) | 2017-06-22 | 2019-04-02 | Unison Industries, Llc | Temperature sensor |
US10753207B2 (en) * | 2017-07-13 | 2020-08-25 | General Electric Company | Airfoil with tip rail cooling |
US10605098B2 (en) | 2017-07-13 | 2020-03-31 | General Electric Company | Blade with tip rail cooling |
KR101937588B1 (en) * | 2017-09-13 | 2019-01-10 | 두산중공업 주식회사 | Cooling blade of turbine and turbine and gas turbine comprising the same |
US10408065B2 (en) | 2017-12-06 | 2019-09-10 | General Electric Company | Turbine component with rail coolant directing chamber |
US10570750B2 (en) | 2017-12-06 | 2020-02-25 | General Electric Company | Turbine component with tip rail cooling passage |
US11512598B2 (en) | 2018-03-14 | 2022-11-29 | General Electric Company | Cooling assembly for a turbine assembly |
CN108506047A (en) * | 2018-03-15 | 2018-09-07 | 哈尔滨工业大学 | Axial-flow turbine leaf grating with three-dimension curved surface leaf top |
WO2019212478A1 (en) * | 2018-04-30 | 2019-11-07 | Siemens Aktiengesellschaft | Turbine blade tip with multi-outlet cooling channels |
US20190338650A1 (en) * | 2018-05-07 | 2019-11-07 | Rolls-Royce Corporation | Turbine blade squealer tip including internal squealer tip cooling channel |
US10801334B2 (en) | 2018-09-12 | 2020-10-13 | Raytheon Technologies Corporation | Cooling arrangement with purge partition |
US10934852B2 (en) | 2018-12-03 | 2021-03-02 | General Electric Company | Turbine blade tip cooling system including tip rail cooling insert |
US11352889B2 (en) * | 2018-12-18 | 2022-06-07 | General Electric Company | Airfoil tip rail and method of cooling |
KR102162969B1 (en) * | 2019-02-26 | 2020-10-07 | 두산중공업 주식회사 | Turbine blade and gas turbine comprising the same |
US11299991B2 (en) * | 2020-04-16 | 2022-04-12 | General Electric Company | Tip squealer configurations |
EP4234885A3 (en) * | 2021-02-04 | 2023-09-06 | Doosan Enerbility Co., Ltd. | Airfoil with a squealer tip cooling system for a turbine blade, corresponding turbine blade, turbine blade assembly, gas turbine and manufacturing method of an airfoil |
US11840940B2 (en) | 2021-03-09 | 2023-12-12 | Mechanical Dynamics And Analysis Llc | Turbine blade tip cooling hole supply plenum |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5660523A (en) * | 1992-02-03 | 1997-08-26 | General Electric Company | Turbine blade squealer tip peripheral end wall with cooling passage arrangement |
US5738491A (en) * | 1997-01-03 | 1998-04-14 | General Electric Company | Conduction blade tip |
DE19944923B4 (en) * | 1999-09-20 | 2007-07-19 | Alstom | Turbine blade for the rotor of a gas turbine |
US6602052B2 (en) * | 2001-06-20 | 2003-08-05 | Alstom (Switzerland) Ltd | Airfoil tip squealer cooling construction |
US6971851B2 (en) * | 2003-03-12 | 2005-12-06 | Florida Turbine Technologies, Inc. | Multi-metered film cooled blade tip |
US6916150B2 (en) * | 2003-11-26 | 2005-07-12 | Siemens Westinghouse Power Corporation | Cooling system for a tip of a turbine blade |
FR2887581A1 (en) * | 2005-06-24 | 2006-12-29 | Snecma Moteurs Sa | TURBOMACHINE HOLLOW AUBE |
GB2461502B (en) * | 2008-06-30 | 2010-05-19 | Rolls Royce Plc | An aerofoil |
US7997865B1 (en) * | 2008-09-18 | 2011-08-16 | Florida Turbine Technologies, Inc. | Turbine blade with tip rail cooling and sealing |
US8366394B1 (en) * | 2010-10-21 | 2013-02-05 | Florida Turbine Technologies, Inc. | Turbine blade with tip rail cooling channel |
KR20120048439A (en) * | 2010-11-05 | 2012-05-15 | 한국항공대학교산학협력단 | Gas turbine blade having squealer tip |
-
2012
- 2012-12-21 GB GBGB1223193.2A patent/GB201223193D0/en not_active Ceased
-
2013
- 2013-12-09 US US14/100,784 patent/US20140178207A1/en not_active Abandoned
- 2013-12-09 EP EP13196186.4A patent/EP2746536A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP2746536A1 (en) | 2014-06-25 |
US20140178207A1 (en) | 2014-06-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |