WO2015034150A3 - Aube pour turbine à gaz - Google Patents
Aube pour turbine à gaz Download PDFInfo
- Publication number
- WO2015034150A3 WO2015034150A3 PCT/KR2014/002210 KR2014002210W WO2015034150A3 WO 2015034150 A3 WO2015034150 A3 WO 2015034150A3 KR 2014002210 W KR2014002210 W KR 2014002210W WO 2015034150 A3 WO2015034150 A3 WO 2015034150A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- blade
- gas turbine
- inlet
- compressed air
- supporting
- 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
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- 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
- F05D2250/18—Two-dimensional patterned
- F05D2250/185—Two-dimensional patterned serpentine-like
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
L'invention concerne une aube pour une turbine à gaz comprenant: une partie aube comprenant une partie de bord avant et une partie de bord arrière et comprenant une section transversale fuselée; une partie de support comprenant des admissions dans lesquelles de l'air comprimé s'écoule depuis l'extérieur et supportant une extrémité de la partie aube; et une pluralité de canaux en serpentin dont une extrémité est raccordée à chaque admission et qui s'étendent en parallèle à l'intérieur de la partie aube de manière à permettre à l'air comprimé reçu par le biais de chaque admission de passer à travers ceux-ci.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR10-2013-0106295 | 2013-09-04 | ||
KR20130106295A KR20150027630A (ko) | 2013-09-04 | 2013-09-04 | 가스 터빈용 블레이드 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2015034150A2 WO2015034150A2 (fr) | 2015-03-12 |
WO2015034150A3 true WO2015034150A3 (fr) | 2015-11-12 |
Family
ID=52629062
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/KR2014/002210 WO2015034150A2 (fr) | 2013-09-04 | 2014-03-17 | Aube pour turbine à gaz |
Country Status (2)
Country | Link |
---|---|
KR (1) | KR20150027630A (fr) |
WO (1) | WO2015034150A2 (fr) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030133795A1 (en) * | 2002-01-11 | 2003-07-17 | Manning Robert Francis | Crossover cooled airfoil trailing edge |
JP2003322002A (ja) * | 2002-05-02 | 2003-11-14 | General Electric Co <Ge> | リフレッシュ用孔のメータリング板を備えるタービン翼形部 |
US20060034690A1 (en) * | 2004-08-10 | 2006-02-16 | Papple Michael Leslie C | Internally cooled gas turbine airfoil and method |
US20070128028A1 (en) * | 2005-12-02 | 2007-06-07 | Siemens Westinghouse Power Corporation | Turbine airfoil with counter-flow serpentine channels |
US7645122B1 (en) * | 2006-12-01 | 2010-01-12 | Florida Turbine Technologies, Inc. | Turbine rotor blade with a nested parallel serpentine flow cooling circuit |
-
2013
- 2013-09-04 KR KR20130106295A patent/KR20150027630A/ko not_active Application Discontinuation
-
2014
- 2014-03-17 WO PCT/KR2014/002210 patent/WO2015034150A2/fr active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030133795A1 (en) * | 2002-01-11 | 2003-07-17 | Manning Robert Francis | Crossover cooled airfoil trailing edge |
JP2003322002A (ja) * | 2002-05-02 | 2003-11-14 | General Electric Co <Ge> | リフレッシュ用孔のメータリング板を備えるタービン翼形部 |
US20060034690A1 (en) * | 2004-08-10 | 2006-02-16 | Papple Michael Leslie C | Internally cooled gas turbine airfoil and method |
US20070128028A1 (en) * | 2005-12-02 | 2007-06-07 | Siemens Westinghouse Power Corporation | Turbine airfoil with counter-flow serpentine channels |
US7645122B1 (en) * | 2006-12-01 | 2010-01-12 | Florida Turbine Technologies, Inc. | Turbine rotor blade with a nested parallel serpentine flow cooling circuit |
Also Published As
Publication number | Publication date |
---|---|
KR20150027630A (ko) | 2015-03-12 |
WO2015034150A2 (fr) | 2015-03-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2784267A3 (fr) | Moteur de turbine à gaz avec dispositif de refroidissement | |
GB2493506B (en) | A fan assembly | |
EP2776318A4 (fr) | Moteur à turbine à gaz comportant une turbine à basse pression à faible nombre d'étages | |
EP2831394B8 (fr) | Turbine à gaz avec système d'air de refroidissement réglable | |
IL229089A0 (en) | Adjustable supersonic air intake | |
DK201300502A (en) | Wind turbine blades with air pressure sensors | |
WO2014077922A3 (fr) | Admission de déflecteur de nacelle | |
EP2613036A3 (fr) | Système d'admission de turbine à gaz | |
WO2013002862A3 (fr) | Système générateur à turbine à air dynamique submergé | |
WO2012149347A3 (fr) | Système de récupération d'énergie d'échappement | |
SG11201403587SA (en) | Gas turbine engine with fan variable area nozzle for low fan pressure ratio | |
GB2480199A (en) | Reversible oil pan with integrated oil suction tube | |
EP2612990A3 (fr) | Aube de turbine à gaz avec une barrière d'écoulement | |
GB201421714D0 (en) | Gas turbine engine comprising an exhaust cone attached to the exhaust casing | |
EP2798183B8 (fr) | Turbomoteur à faible rapport de pression de soufflante | |
EP2610179A3 (fr) | Ensembles de déviation d'admission d'air d'aéronef présentant de meilleures caractéristiques aérodynamiques | |
WO2017007809A3 (fr) | Système de conditionnement d'air moteur pour turbines à gaz | |
IN2012DE00274A (fr) | ||
EP2682701A4 (fr) | Condenseur à pression à étages multiples et installation de turbine à vapeur équipée de ce condenseur | |
WO2013158176A3 (fr) | Fixation de pale de ventilateur de moteur à turbine à gaz | |
ZA201502190B (en) | Turbine with radial inlet and outlet and multi-element guide vanes for oscillating flows | |
WO2015034150A3 (fr) | Aube pour turbine à gaz | |
SG11201403544TA (en) | Gas turbine engine with fan variable area nozzle for low fan pressure ratio | |
SG11201403545SA (en) | Gas turbine engine with fan variable area nozzle | |
MY184256A (en) | Centrifugal compressor and water chilling unit having the same |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 14842772 Country of ref document: EP Kind code of ref document: A2 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 14842772 Country of ref document: EP Kind code of ref document: A2 |