SE420635B - GAS TURBIN INSTALLATION WITH COOLING TOUR BINDERS - Google Patents
GAS TURBIN INSTALLATION WITH COOLING TOUR BINDERSInfo
- Publication number
- SE420635B SE420635B SE7707890A SE7707890A SE420635B SE 420635 B SE420635 B SE 420635B SE 7707890 A SE7707890 A SE 7707890A SE 7707890 A SE7707890 A SE 7707890A SE 420635 B SE420635 B SE 420635B
- Authority
- SE
- Sweden
- Prior art keywords
- tour
- binders
- cooling
- installation
- gas turbin
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19762633222 DE2633222A1 (en) | 1976-07-23 | 1976-07-23 | GAS TURBINE SYSTEM WITH COOLING OF TURBINE PARTS |
Publications (2)
Publication Number | Publication Date |
---|---|
SE7707890L SE7707890L (en) | 1978-01-24 |
SE420635B true SE420635B (en) | 1981-10-19 |
Family
ID=5983795
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7707890A SE420635B (en) | 1976-07-23 | 1977-07-06 | GAS TURBIN INSTALLATION WITH COOLING TOUR BINDERS |
Country Status (5)
Country | Link |
---|---|
CH (1) | CH621387A5 (en) |
DE (1) | DE2633222A1 (en) |
GB (1) | GB1541533A (en) |
IT (1) | IT1085836B (en) |
SE (1) | SE420635B (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4008977A (en) * | 1975-09-19 | 1977-02-22 | United Technologies Corporation | Compressor bleed system |
GB2075123B (en) * | 1980-05-01 | 1983-11-16 | Gen Electric | Turbine cooling air deswirler |
DE3037020C2 (en) * | 1980-10-01 | 1983-11-03 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Gas turbine jet engine in multi-shaft design with compressor high-pressure air extraction and guide devices for turbine cooling |
FR2491549B1 (en) * | 1980-10-08 | 1985-07-05 | Snecma | DEVICE FOR COOLING A GAS TURBINE, BY TAKING AIR FROM THE COMPRESSOR |
GB2118629B (en) * | 1982-04-21 | 1985-07-17 | Rolls Royce | Device for passing a fluid flow eg. cooling air through a barrier eg. bolted joint |
US4674955A (en) * | 1984-12-21 | 1987-06-23 | The Garrett Corporation | Radial inboard preswirl system |
DE4324034A1 (en) * | 1993-07-17 | 1995-01-19 | Abb Management Ag | Gas turbine with a cooled rotor |
DE19852604A1 (en) | 1998-11-14 | 2000-05-18 | Abb Research Ltd | Rotor for gas turbine, with first cooling air diverting device having several radial borings running inwards through first rotor disk |
DE10159670A1 (en) | 2001-12-05 | 2003-06-18 | Rolls Royce Deutschland | Vortex rectifier in the high pressure compressor of a gas turbine |
GB2420155B (en) | 2004-11-12 | 2008-08-27 | Rolls Royce Plc | Turbine blade cooling system |
EP2551453A1 (en) | 2011-07-26 | 2013-01-30 | Alstom Technology Ltd | Cooling device of a gas turbine compressor |
CH705840A1 (en) | 2011-12-06 | 2013-06-14 | Alstom Technology Ltd | High-pressure compressor, in particular in a gas turbine. |
US9085983B2 (en) * | 2012-03-29 | 2015-07-21 | General Electric Company | Apparatus and method for purging a gas turbine rotor |
EP3056666A1 (en) * | 2015-02-13 | 2016-08-17 | Siemens Aktiengesellschaft | Wheel disc element for two blade rows, compressor impeller, turbo engine and method for regulating the temperature of such a double wheel disc element |
-
1976
- 1976-07-23 DE DE19762633222 patent/DE2633222A1/en not_active Ceased
-
1977
- 1977-05-31 CH CH662377A patent/CH621387A5/en not_active IP Right Cessation
- 1977-07-06 SE SE7707890A patent/SE420635B/en unknown
- 1977-07-21 IT IT25944/77A patent/IT1085836B/en active
- 1977-07-22 GB GB30984/77A patent/GB1541533A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2633222A1 (en) | 1978-01-26 |
SE7707890L (en) | 1978-01-24 |
CH621387A5 (en) | 1981-01-30 |
IT1085836B (en) | 1985-05-28 |
GB1541533A (en) | 1979-03-07 |
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