CA1190480A - Vane structure having improved cooled operation in stationary combustion turbines - Google Patents
Vane structure having improved cooled operation in stationary combustion turbinesInfo
- Publication number
- CA1190480A CA1190480A CA000395998A CA395998A CA1190480A CA 1190480 A CA1190480 A CA 1190480A CA 000395998 A CA000395998 A CA 000395998A CA 395998 A CA395998 A CA 395998A CA 1190480 A CA1190480 A CA 1190480A
- Authority
- CA
- Canada
- Prior art keywords
- vane
- coolant
- hot gas
- shrouds
- gas path
- 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.)
- Expired
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
- 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
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
- F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
-
- 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
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
-
- 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
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US23977781A | 1981-03-02 | 1981-03-02 | |
US239,777 | 1981-03-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1190480A true CA1190480A (en) | 1985-07-16 |
Family
ID=22903695
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA000395998A Expired CA1190480A (en) | 1981-03-02 | 1982-02-10 | Vane structure having improved cooled operation in stationary combustion turbines |
Country Status (8)
Country | Link |
---|---|
JP (1) | JPS57157001A (enrdf_load_stackoverflow) |
AR (1) | AR227226A1 (enrdf_load_stackoverflow) |
BE (1) | BE892325A (enrdf_load_stackoverflow) |
BR (1) | BR8200849A (enrdf_load_stackoverflow) |
CA (1) | CA1190480A (enrdf_load_stackoverflow) |
GB (1) | GB2093923B (enrdf_load_stackoverflow) |
IT (1) | IT1190703B (enrdf_load_stackoverflow) |
MX (1) | MX155528A (enrdf_load_stackoverflow) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2723144B1 (fr) * | 1984-11-29 | 1996-12-13 | Snecma | Distributeur de turbine |
US5720431A (en) * | 1988-08-24 | 1998-02-24 | United Technologies Corporation | Cooled blades for a gas turbine engine |
JP3142850B2 (ja) * | 1989-03-13 | 2001-03-07 | 株式会社東芝 | タービンの冷却翼および複合発電プラント |
US5344283A (en) | 1993-01-21 | 1994-09-06 | United Technologies Corporation | Turbine vane having dedicated inner platform cooling |
US5498126A (en) * | 1994-04-28 | 1996-03-12 | United Technologies Corporation | Airfoil with dual source cooling |
DE69515502T2 (de) * | 1994-11-10 | 2000-08-03 | Siemens Westinghouse Power Corp., Orlando | Gasturbinenschaufel mit einer gekühlten plattform |
JP3426902B2 (ja) | 1997-03-11 | 2003-07-14 | 三菱重工業株式会社 | ガスタービン冷却静翼 |
JP3495579B2 (ja) * | 1997-10-28 | 2004-02-09 | 三菱重工業株式会社 | ガスタービン静翼 |
DE19939179B4 (de) * | 1999-08-20 | 2007-08-02 | Alstom | Kühlbare Schaufel für eine Gasturbine |
US6439837B1 (en) * | 2000-06-27 | 2002-08-27 | General Electric Company | Nozzle braze backside cooling |
US6923623B2 (en) * | 2003-08-07 | 2005-08-02 | General Electric Company | Perimeter-cooled turbine bucket airfoil cooling hole location, style and configuration |
US7070386B2 (en) * | 2004-06-25 | 2006-07-04 | United Technologies Corporation | Airfoil insert with castellated end |
US7140835B2 (en) * | 2004-10-01 | 2006-11-28 | General Electric Company | Corner cooled turbine nozzle |
US9249673B2 (en) * | 2011-12-30 | 2016-02-02 | General Electric Company | Turbine rotor blade platform cooling |
US9297267B2 (en) * | 2012-12-10 | 2016-03-29 | General Electric Company | System and method for removing heat from a turbine |
CA151710S (en) | 2012-12-19 | 2014-12-29 | Brita Gmbh | Carafe |
CA207297S (en) * | 2021-06-14 | 2023-07-04 | Pi Design Ag | Water bottle |
-
1982
- 1982-02-10 CA CA000395998A patent/CA1190480A/en not_active Expired
- 1982-02-12 GB GB8204139A patent/GB2093923B/en not_active Expired
- 1982-02-12 MX MX191381A patent/MX155528A/es unknown
- 1982-02-17 BR BR8200849A patent/BR8200849A/pt unknown
- 1982-02-23 AR AR288529A patent/AR227226A1/es active
- 1982-02-26 IT IT19861/82A patent/IT1190703B/it active
- 1982-03-01 BE BE0/207445A patent/BE892325A/fr not_active IP Right Cessation
- 1982-03-02 JP JP57031873A patent/JPS57157001A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
GB2093923B (en) | 1984-06-27 |
AR227226A1 (es) | 1982-09-30 |
BE892325A (fr) | 1982-09-01 |
BR8200849A (pt) | 1982-12-28 |
IT8219861A0 (it) | 1982-02-26 |
IT1190703B (it) | 1988-02-24 |
JPS57157001A (en) | 1982-09-28 |
MX155528A (es) | 1988-03-24 |
JPS6148610B2 (enrdf_load_stackoverflow) | 1986-10-24 |
GB2093923A (en) | 1982-09-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA1190480A (en) | Vane structure having improved cooled operation in stationary combustion turbines | |
JP2668207B2 (ja) | ガスタービンエンジンのタービンのエーロフオイルセクシヨン | |
US5975850A (en) | Turbulated cooling passages for turbine blades | |
EP2055898B1 (en) | Gas turbine engine with circumferential array of airfoils with platform cooling | |
EP1182339B1 (en) | Clocked turbine airfoil cooling | |
US6283708B1 (en) | Coolable vane or blade for a turbomachine | |
US6607355B2 (en) | Turbine airfoil with enhanced heat transfer | |
US7147432B2 (en) | Turbine shroud asymmetrical cooling elements | |
EP1039096B1 (en) | Turbine nozzle | |
EP1445424B1 (en) | Hollow airfoil provided with an embedded microcircuit for tip cooling | |
US7097425B2 (en) | Microcircuit cooling for a turbine airfoil | |
US4180373A (en) | Turbine blade | |
US4127358A (en) | Blade or vane for a gas turbine engine | |
EP1452693B1 (en) | Turbine nozzle segment cantilevered mount | |
CA2398515C (en) | Turbine airfoil for gas turbine engine | |
US7296972B2 (en) | Turbine airfoil with counter-flow serpentine channels | |
US20050031451A1 (en) | Microcircuit cooling for a turbine blade | |
US20050031450A1 (en) | Microcircuit airfoil mainbody | |
JP2005127314A (ja) | 収束ピン冷却式翼形部 | |
EP3290639B1 (en) | Impingement cooling with increased cross-flow area | |
EP3453831A2 (en) | Airfoil having end wall contoured pedestals | |
US11781434B2 (en) | Components for gas turbine engines | |
EP3578759A1 (en) | Airfoil and corresponding method of directing a cooling flow | |
US12228049B2 (en) | Components for gas turbine engines | |
WO2019245546A1 (en) | Cooled turbine blade assembly, corresponding methods for cooling and manufacturing |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
MKEX | Expiry |