NO752535L - - Google Patents
Info
- Publication number
- NO752535L NO752535L NO752535A NO752535A NO752535L NO 752535 L NO752535 L NO 752535L NO 752535 A NO752535 A NO 752535A NO 752535 A NO752535 A NO 752535A NO 752535 L NO752535 L NO 752535L
- Authority
- NO
- Norway
- Prior art keywords
- blade
- cooling air
- height
- bucket
- shovel
- Prior art date
Links
- 238000001816 cooling Methods 0.000 claims description 26
- 238000005266 casting Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000011515 electrochemical drilling Methods 0.000 description 1
- 238000005495 investment casting Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
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
- 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
- F05D2260/221—Improvement of heat transfer
- F05D2260/2212—Improvement of heat transfer by creating turbulence
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH982474A CH580750A5 (zh) | 1974-07-17 | 1974-07-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
NO752535L true NO752535L (zh) | 1976-01-20 |
Family
ID=4356031
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO752535A NO752535L (zh) | 1974-07-17 | 1975-07-16 |
Country Status (8)
Country | Link |
---|---|
US (1) | US3989412A (zh) |
JP (1) | JPS5134316A (zh) |
CH (1) | CH580750A5 (zh) |
FR (1) | FR2278925A1 (zh) |
GB (1) | GB1467197A (zh) |
IT (1) | IT1041775B (zh) |
NO (1) | NO752535L (zh) |
SE (1) | SE395505B (zh) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5638161Y2 (zh) * | 1977-04-22 | 1981-09-07 | ||
JPS5638162Y2 (zh) * | 1977-06-15 | 1981-09-07 | ||
US4224011A (en) * | 1977-10-08 | 1980-09-23 | Rolls-Royce Limited | Cooled rotor blade for a gas turbine engine |
US4589824A (en) * | 1977-10-21 | 1986-05-20 | United Technologies Corporation | Rotor blade having a tip cap end closure |
US4236870A (en) * | 1977-12-27 | 1980-12-02 | United Technologies Corporation | Turbine blade |
JPS6172668U (zh) * | 1984-10-18 | 1986-05-17 | ||
GB2260166B (en) * | 1985-10-18 | 1993-06-30 | Rolls Royce | Cooled aerofoil blade or vane for a gas turbine engine |
US4830575A (en) * | 1988-02-08 | 1989-05-16 | Dresser-Rand Company | Spiral grooves in a turbine rotor |
US4820123A (en) * | 1988-04-25 | 1989-04-11 | United Technologies Corporation | Dirt removal means for air cooled blades |
US4820122A (en) * | 1988-04-25 | 1989-04-11 | United Technologies Corporation | Dirt removal means for air cooled blades |
US5813835A (en) * | 1991-08-19 | 1998-09-29 | The United States Of America As Represented By The Secretary Of The Air Force | Air-cooled turbine blade |
US5279111A (en) * | 1992-08-27 | 1994-01-18 | Inco Limited | Gas turbine cooling |
GB9901218D0 (en) | 1999-01-21 | 1999-03-10 | Rolls Royce Plc | Cooled aerofoil for a gas turbine engine |
EP1128023A1 (de) * | 2000-02-25 | 2001-08-29 | Siemens Aktiengesellschaft | Turbinenlaufschaufel |
US6478535B1 (en) * | 2001-05-04 | 2002-11-12 | Honeywell International, Inc. | Thin wall cooling system |
EP1730389B1 (de) * | 2004-03-30 | 2009-12-09 | Alstom Technology Ltd | Vorrichtung zur kühlluftbeaufschlagung einer laufschaufel |
US7144215B2 (en) * | 2004-07-30 | 2006-12-05 | General Electric Company | Method and apparatus for cooling gas turbine engine rotor blades |
US7210906B2 (en) * | 2004-08-10 | 2007-05-01 | Pratt & Whitney Canada Corp. | Internally cooled gas turbine airfoil and method |
US7956486B2 (en) * | 2009-05-23 | 2011-06-07 | Abel Echemendia | Windmill electric generator for hydroelectric power system |
EP2520764A1 (de) * | 2011-05-02 | 2012-11-07 | MTU Aero Engines GmbH | Schaufel mit gekühltem Schaufelfuss |
JP5881369B2 (ja) | 2011-10-27 | 2016-03-09 | 三菱重工業株式会社 | タービン動翼及びこれを備えたガスタービン |
EP2832953A1 (de) * | 2013-07-29 | 2015-02-04 | Siemens Aktiengesellschaft | Turbinenschaufel |
US9771816B2 (en) | 2014-05-07 | 2017-09-26 | General Electric Company | Blade cooling circuit feed duct, exhaust duct, and related cooling structure |
US9638045B2 (en) | 2014-05-28 | 2017-05-02 | General Electric Company | Cooling structure for stationary blade |
US9822653B2 (en) | 2015-07-16 | 2017-11-21 | General Electric Company | Cooling structure for stationary blade |
US9909436B2 (en) | 2015-07-16 | 2018-03-06 | General Electric Company | Cooling structure for stationary blade |
GB201820669D0 (en) * | 2018-12-19 | 2019-01-30 | Rolls Royce Plc | Turbine blade |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL104493C (zh) * | 1957-06-07 | |||
GB893706A (en) * | 1960-01-05 | 1962-04-11 | Rolls Royce | Blades for fluid flow machines |
US3420502A (en) * | 1962-09-04 | 1969-01-07 | Gen Electric | Fluid-cooled airfoil |
US3171631A (en) * | 1962-12-05 | 1965-03-02 | Gen Motors Corp | Turbine blade |
US3533711A (en) * | 1966-02-26 | 1970-10-13 | Gen Electric | Cooled vane structure for high temperature turbines |
US3623825A (en) * | 1969-11-13 | 1971-11-30 | Avco Corp | Liquid-metal-filled rotor blade |
GB1355558A (en) * | 1971-07-02 | 1974-06-05 | Rolls Royce | Cooled vane or blade for a gas turbine engine |
BE794194A (fr) * | 1972-01-18 | 1973-07-18 | Bbc Sulzer Turbomaschinen | Aube mobile refroidie pour des turbines a gaz |
BE794195A (fr) * | 1972-01-18 | 1973-07-18 | Bbc Sulzer Turbomaschinen | Aube directrice refroidie pour des turbines a gaz |
US3902819A (en) * | 1973-06-04 | 1975-09-02 | United Aircraft Corp | Method and apparatus for cooling a turbomachinery blade |
-
1974
- 1974-07-17 CH CH982474A patent/CH580750A5/xx not_active IP Right Cessation
-
1975
- 1975-06-17 US US05/587,668 patent/US3989412A/en not_active Expired - Lifetime
- 1975-06-20 GB GB2638775A patent/GB1467197A/en not_active Expired
- 1975-07-08 JP JP50083897A patent/JPS5134316A/ja active Granted
- 1975-07-14 IT IT25366/75A patent/IT1041775B/it active
- 1975-07-15 SE SE7508095A patent/SE395505B/xx unknown
- 1975-07-16 FR FR7522202A patent/FR2278925A1/fr active Granted
- 1975-07-16 NO NO752535A patent/NO752535L/no unknown
Also Published As
Publication number | Publication date |
---|---|
DE2434989A1 (zh) | 1975-10-30 |
CH580750A5 (zh) | 1976-10-15 |
DE2434989B1 (de) | 1975-10-30 |
US3989412A (en) | 1976-11-02 |
SE395505B (sv) | 1977-08-15 |
JPS5134316A (en) | 1976-03-24 |
JPS5414245B2 (zh) | 1979-06-06 |
FR2278925B1 (zh) | 1979-05-04 |
FR2278925A1 (fr) | 1976-02-13 |
GB1467197A (en) | 1977-03-16 |
SE7508095L (sv) | 1976-01-19 |
IT1041775B (it) | 1980-01-10 |
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