CA919091A - Cooling system for a gas turbine - Google Patents
Cooling system for a gas turbineInfo
- Publication number
- CA919091A CA919091A CA087737A CA87737A CA919091A CA 919091 A CA919091 A CA 919091A CA 087737 A CA087737 A CA 087737A CA 87737 A CA87737 A CA 87737A CA 919091 A CA919091 A CA 919091A
- Authority
- CA
- Canada
- Prior art keywords
- gas turbine
- cooling system
- cooling
- turbine
- gas
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Motor Or Generator Cooling System (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US86197769A | 1969-09-29 | 1969-09-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA919091A true CA919091A (en) | 1973-01-16 |
Family
ID=25337275
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA087737A Expired CA919091A (en) | 1969-09-29 | 1970-07-09 | Cooling system for a gas turbine |
Country Status (7)
Country | Link |
---|---|
US (1) | US3602605A (en) |
AT (1) | AT301273B (en) |
CA (1) | CA919091A (en) |
CH (1) | CH519096A (en) |
DE (2) | DE2043480A1 (en) |
FR (1) | FR2062769A5 (en) |
GB (1) | GB1270905A (en) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3750398A (en) * | 1971-05-17 | 1973-08-07 | Westinghouse Electric Corp | Static seal structure |
US3842595A (en) * | 1972-12-26 | 1974-10-22 | Gen Electric | Modular gas turbine engine |
US3945758A (en) * | 1974-02-28 | 1976-03-23 | Westinghouse Electric Corporation | Cooling system for a gas turbine |
US3904307A (en) * | 1974-04-10 | 1975-09-09 | United Technologies Corp | Gas generator turbine cooling scheme |
US3990812A (en) * | 1975-03-03 | 1976-11-09 | United Technologies Corporation | Radial inflow blade cooling system |
GB1501916A (en) * | 1975-06-20 | 1978-02-22 | Rolls Royce | Matching thermal expansions of components of turbo-machines |
US4113406A (en) * | 1976-11-17 | 1978-09-12 | Westinghouse Electric Corp. | Cooling system for a gas turbine engine |
US4184797A (en) * | 1977-10-17 | 1980-01-22 | General Electric Company | Liquid-cooled turbine rotor |
US4306834A (en) * | 1979-06-25 | 1981-12-22 | Westinghouse Electric Corp. | Balance piston and seal for gas turbine engine |
DE3014279A1 (en) * | 1980-04-15 | 1981-10-22 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen | DEVICE FOR COOLING THE INSIDE OF A GAS TURBINE |
FR2484574A1 (en) * | 1980-06-13 | 1981-12-18 | Snecma | MULTI-BODY TURBOMACHINE INTER-SHAFT BEARING WITH OIL-DAMPING DAMPING |
DE3310396A1 (en) * | 1983-03-18 | 1984-09-20 | Kraftwerk Union AG, 4330 Mülheim | MD STEAM TURBINE IN SINGLE-FLOW CONSTRUCTION FOR A HIGH-TEMPERATURE STEAM TURBINE SYSTEM WITH INTERMEDIATE HEATING |
EP0144842B1 (en) * | 1983-12-05 | 1988-07-27 | Westinghouse Electric Corporation | Cascaded air supply for gas turbine cooling |
DE3424139C2 (en) * | 1984-06-30 | 1996-02-22 | Bbc Brown Boveri & Cie | Gas turbine rotor |
US4674955A (en) * | 1984-12-21 | 1987-06-23 | The Garrett Corporation | Radial inboard preswirl system |
US4759688A (en) * | 1986-12-16 | 1988-07-26 | Allied-Signal Inc. | Cooling flow side entry for cooled turbine blading |
US5340271A (en) * | 1990-08-18 | 1994-08-23 | Rolls-Royce Plc | Flow control method and means |
DE4337281A1 (en) * | 1993-11-02 | 1995-05-04 | Abb Management Ag | compressor |
DE4433289A1 (en) * | 1994-09-19 | 1996-03-21 | Abb Management Ag | Axial gas turbine |
DE4435322B4 (en) * | 1994-10-01 | 2005-05-04 | Alstom | Method and device for shaft seal and for cooling on the exhaust side of an axial flowed gas turbine |
JP3652780B2 (en) * | 1996-04-08 | 2005-05-25 | 三菱重工業株式会社 | Turbine cooling system |
SE508085C2 (en) * | 1996-12-12 | 1998-08-24 | Abb Carbon Ab | Method for air flow control of combustion air and barrier air device |
WO1998059156A1 (en) * | 1997-06-20 | 1998-12-30 | Mitsubishi Heavy Industries, Ltd. | Air separator for gas turbines |
US6234746B1 (en) * | 1999-08-04 | 2001-05-22 | General Electric Co. | Apparatus and methods for cooling rotary components in a turbine |
JP4067709B2 (en) * | 1999-08-23 | 2008-03-26 | 三菱重工業株式会社 | Rotor cooling air supply device |
DE102004016244B4 (en) * | 2004-04-02 | 2007-08-23 | Mtu Aero Engines Gmbh | Rotor for a turbomachine |
GB2424927A (en) * | 2005-04-06 | 2006-10-11 | Rolls Royce Plc | A pre-swirl nozzle ring and a method of manufacturing a pre-swirl nozzle ring |
US7189055B2 (en) * | 2005-05-31 | 2007-03-13 | Pratt & Whitney Canada Corp. | Coverplate deflectors for redirecting a fluid flow |
US7189056B2 (en) * | 2005-05-31 | 2007-03-13 | Pratt & Whitney Canada Corp. | Blade and disk radial pre-swirlers |
US7244104B2 (en) * | 2005-05-31 | 2007-07-17 | Pratt & Whitney Canada Corp. | Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine |
US8192151B2 (en) | 2009-04-29 | 2012-06-05 | General Electric Company | Turbine engine having cooling gland |
US8529195B2 (en) | 2010-10-12 | 2013-09-10 | General Electric Company | Inducer for gas turbine system |
US9435206B2 (en) * | 2012-09-11 | 2016-09-06 | General Electric Company | Flow inducer for a gas turbine system |
US9441540B2 (en) * | 2012-11-05 | 2016-09-13 | General Electric Company | Inducer guide vanes |
US9039357B2 (en) * | 2013-01-23 | 2015-05-26 | Siemens Aktiengesellschaft | Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engine |
US9556737B2 (en) | 2013-11-18 | 2017-01-31 | Siemens Energy, Inc. | Air separator for gas turbine engine |
CA2964126C (en) * | 2016-04-12 | 2019-01-08 | Airtek Systems Inc. | System and method for generating rotational power |
US11242804B2 (en) * | 2017-06-14 | 2022-02-08 | General Electric Company | Inleakage management apparatus |
-
1969
- 1969-09-29 US US861977A patent/US3602605A/en not_active Expired - Lifetime
-
1970
- 1970-07-09 CA CA087737A patent/CA919091A/en not_active Expired
- 1970-08-20 GB GB40125/70A patent/GB1270905A/en not_active Expired
- 1970-09-02 DE DE19702043480 patent/DE2043480A1/en active Pending
- 1970-09-28 CH CH1430470A patent/CH519096A/en not_active IP Right Cessation
- 1970-09-28 DE DE19702047648 patent/DE2047648A1/en active Pending
- 1970-09-29 AT AT878570A patent/AT301273B/en not_active IP Right Cessation
- 1970-09-29 FR FR7035126A patent/FR2062769A5/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
CH519096A (en) | 1972-02-15 |
AT301273B (en) | 1972-08-25 |
US3602605A (en) | 1971-08-31 |
DE2043480A1 (en) | 1971-04-01 |
FR2062769A5 (en) | 1971-06-25 |
GB1270905A (en) | 1972-04-19 |
DE2047648A1 (en) | 1971-05-19 |
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