FR1111569A - Installation de turbine à gaz - Google Patents
Installation de turbine à gazInfo
- Publication number
- FR1111569A FR1111569A FR1111569DA FR1111569A FR 1111569 A FR1111569 A FR 1111569A FR 1111569D A FR1111569D A FR 1111569DA FR 1111569 A FR1111569 A FR 1111569A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- turbine installation
- installation
- gas
- turbine
- 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
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
- F02C3/05—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
-
- 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
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (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 |
---|---|---|---|
GB24219/54A GB791232A (en) | 1954-08-19 | 1954-08-19 | Improvements in or relating to gas turbine power plants |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1111569A true FR1111569A (fr) | 1956-03-01 |
Family
ID=10208261
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1111569D Expired FR1111569A (fr) | 1954-08-19 | 1954-08-28 | Installation de turbine à gaz |
Country Status (4)
Country | Link |
---|---|
US (1) | US2709893A (fr) |
DE (1) | DE1130646B (fr) |
FR (1) | FR1111569A (fr) |
GB (1) | GB791232A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1092730B (de) * | 1959-02-11 | 1960-11-10 | Daimler Benz Ag | Gehaeuseausbildung fuer Gasturbinentriebwerke |
EP0206683A2 (fr) * | 1985-06-17 | 1986-12-30 | The University Of Dayton | Turbine à gaz avec un conduit de dérivation interne pour le refroidissement des aubes |
Families Citing this family (57)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2925714A (en) * | 1954-10-11 | 1960-02-23 | Thompson Ramo Wooldridge Inc | Diffuser-regenerator gas turbine engine |
GB805195A (en) * | 1955-12-08 | 1958-12-03 | Rolls Royce | Improvements in or relating to gas turbine power plant |
US2971339A (en) * | 1956-08-23 | 1961-02-14 | Gold Harold | Gas turbine control system |
US2904307A (en) * | 1956-10-01 | 1959-09-15 | Crane Co | Cooling turbine |
DE1033966B (de) * | 1956-11-21 | 1958-07-10 | Kloeckner Humboldt Deutz Ag | Einspritzbrennkraftmaschine |
US3010281A (en) * | 1957-12-24 | 1961-11-28 | Adolph J Cervenka | Toroidal combustion chamber |
US2939626A (en) * | 1957-12-27 | 1960-06-07 | Laval Steam Turbine Co | Turbo-compressor |
US3030005A (en) * | 1958-01-21 | 1962-04-17 | Bertin & Cie | Ejectors or jet apparatus |
US2975959A (en) * | 1958-09-30 | 1961-03-21 | Berry W Foster | Back-to-back centrifugal compressor and centripetal turbine having an integral rotordisc |
DE1278794B (de) * | 1960-11-04 | 1968-09-26 | Rudolph Birmann | Verpuffungsgasturbinenanlage |
DE1218800B (de) * | 1961-04-25 | 1966-06-08 | M A N Turbo Ges Mit Beschraenk | Gasturbine, insbesondere Kleingasturbine |
GB970189A (en) * | 1963-01-31 | 1964-09-16 | Rolls Royce | Combustion equipment for a gas turbine engine |
GB970188A (en) * | 1963-01-31 | 1964-09-16 | Rolls Royce | Gas turbine vertical lift engine |
US3232580A (en) * | 1963-07-18 | 1966-02-01 | Birmann Rudolph | Centripetal turbine |
DE1269418B (de) * | 1964-08-21 | 1968-05-30 | Gen Motors Corp | Gasturbine |
US3309866A (en) * | 1965-03-11 | 1967-03-21 | Gen Electric | Combustion process and apparatus |
US3365892A (en) * | 1965-08-10 | 1968-01-30 | Derderian George | Turbomachine |
DE1301634B (de) * | 1965-09-29 | 1969-08-21 | Curtiss Wright Corp | Gasturbinentriebwerk |
US3493169A (en) * | 1968-06-03 | 1970-02-03 | United Aircraft Corp | Bleed for compressor |
US3994630A (en) * | 1974-08-21 | 1976-11-30 | International Harvester Company | Monorotor turbine and method of cooling |
US3995432A (en) * | 1975-07-28 | 1976-12-07 | United Technologies Corporation | Collector |
US4303377A (en) * | 1978-02-03 | 1981-12-01 | Schwartzman Everett H | Turbine-compressor ejector |
US4357796A (en) * | 1980-09-30 | 1982-11-09 | The United States Of America As Represented By The Secretary Of The Air Force | Small gas turbofan engine with regenerating diffuser |
US4382359A (en) * | 1981-01-27 | 1983-05-10 | Sampayo Eduardo A | Gas turbine engine |
US4502837A (en) * | 1982-09-30 | 1985-03-05 | General Electric Company | Multi stage centrifugal impeller |
DE3339505A1 (de) * | 1983-10-31 | 1985-05-09 | Bernd 6352 Ober-Mörlen Jung | Gasturbine mit einem vorgeschalteten turbokompressor |
EP0148590B1 (fr) * | 1984-01-07 | 1989-04-12 | ROLLS-ROYCE plc | Usines génératrices à turbines à gaz |
JPS6147435U (ja) * | 1984-09-03 | 1986-03-29 | 石川島播磨重工業株式会社 | 過給機の軸受装置 |
US4800717A (en) * | 1986-12-22 | 1989-01-31 | Sundstrand Corporation | Turbine rotor cooling |
DE3815679A1 (de) * | 1988-05-07 | 1989-11-16 | Kuehnle Kopp Kausch Ag | Radialturbine |
US4991390A (en) * | 1988-09-26 | 1991-02-12 | Sundstrand Corporation | Mounting and cooling turbine nozzle vanes |
US5101620A (en) * | 1988-12-28 | 1992-04-07 | Sundstrand Corporation | Annular combustor for a turbine engine without film cooling |
US4932207A (en) * | 1988-12-28 | 1990-06-12 | Sundstrand Corporation | Segmented seal plate for a turbine engine |
US5280703A (en) * | 1989-12-11 | 1994-01-25 | Sundstrand Corporation | Turbine nozzle cooling |
US5111655A (en) * | 1989-12-22 | 1992-05-12 | Sundstrand Corporation | Single wall combustor assembly |
US5253472A (en) * | 1990-02-28 | 1993-10-19 | Dev Sudarshan P | Small gas turbine having enhanced fuel economy |
US5832715A (en) * | 1990-02-28 | 1998-11-10 | Dev; Sudarshan Paul | Small gas turbine engine having enhanced fuel economy |
US5241815A (en) * | 1992-04-22 | 1993-09-07 | Lee Dae S | Heat-recovering-thrust-turbine having rotational flow path |
US5526640A (en) * | 1994-05-16 | 1996-06-18 | Technical Directions, Inc. | Gas turbine engine including a bearing support tube cantilevered from a turbine nozzle wall |
US6585482B1 (en) * | 2000-06-20 | 2003-07-01 | General Electric Co. | Methods and apparatus for delivering cooling air within gas turbines |
US7043811B2 (en) * | 2004-03-22 | 2006-05-16 | General Electric Company | Method of removing studs |
US7251942B2 (en) * | 2004-06-29 | 2007-08-07 | Honeywell International Inc. | Integrated gearless and nonlubricated auxiliary power unit |
US7559745B2 (en) * | 2006-03-21 | 2009-07-14 | United Technologies Corporation | Tip clearance centrifugal compressor impeller |
DE102009014005A1 (de) * | 2009-03-19 | 2010-09-23 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Rotierende Strömungsmaschine |
FR2944060B1 (fr) * | 2009-04-06 | 2013-07-19 | Turbomeca | Systeme d'air secondaire pour compresseur centrifuge ou mixte |
RU2596709C2 (ru) * | 2011-12-18 | 2016-09-10 | РУИС Хонас ВИЙАРРУБИА | Коллектор солнечного излучения с турбиной или с турбокомпрессором |
US10527059B2 (en) | 2013-10-21 | 2020-01-07 | Williams International Co., L.L.C. | Turbomachine diffuser |
GB2536878A (en) * | 2015-03-23 | 2016-10-05 | Aurelia Turbines Oy | Multi-spool gas turbine arrangement |
GB2536876A (en) * | 2015-03-23 | 2016-10-05 | Aurelia Turbines Oy | Two-spool gas turbine arrangement |
US10208628B2 (en) * | 2016-03-30 | 2019-02-19 | Honeywell International Inc. | Turbine engine designs for improved fine particle separation efficiency |
GB201618016D0 (en) * | 2016-10-25 | 2016-12-07 | Jiang Kyle | Gas turbine engine |
US20180135516A1 (en) | 2016-11-16 | 2018-05-17 | Honeywell International Inc. | Scavenge methodologies for turbine engine particle separation concepts |
UA121068C2 (uk) * | 2018-05-16 | 2020-03-25 | Публічне Акціонерне Товариство "Мотор Січ" | Газотурбінна установка |
US11415046B1 (en) * | 2019-06-04 | 2022-08-16 | United States Of America As Represented By The Secretary Of The Air Force | Disk engine with circumferential swirl radial combustor |
RU2730206C1 (ru) * | 2019-08-15 | 2020-08-19 | Александр Тихонович Зыбин | Газотурбинный двигатель внутреннего сгорания с воспламенением от сжатия |
US20220034227A1 (en) * | 2020-08-03 | 2022-02-03 | Rolls-Royce North American Technologies Inc. | Compressor turbine wheel |
US11371434B2 (en) * | 2020-08-19 | 2022-06-28 | Honeywell International Inc. | Compressor particle separator for gas turbine engine |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE137706C (fr) * | ||||
DE346599C (fr) * | ||||
US1926225A (en) * | 1930-09-12 | 1933-09-12 | Birmann Rudolph | Turbo compressor |
US1959703A (en) * | 1932-01-26 | 1934-05-22 | Birmann Rudolph | Blading for centrifugal impellers or turbines |
DE644829C (de) * | 1932-11-19 | 1937-05-14 | Siemens Schuckertwerke Akt Ges | Gasturbine |
US2283176A (en) * | 1937-11-29 | 1942-05-19 | Turbo Engineering Corp | Elastic fluid mechanism |
US2256198A (en) * | 1938-05-27 | 1941-09-16 | Ernst Heinkel | Aircraft power plant |
DE696062C (de) * | 1938-07-10 | 1940-09-10 | Rheinmetall Borsig Akt Ges | Turbinengehaeuse, insbesondere fuer Gasturbinen |
CH225232A (de) * | 1941-02-06 | 1943-01-15 | Bmw Flugmotorenbau Gmbh | Innengekühlte Turbinenschaufel. |
GB587150A (en) * | 1942-04-18 | 1947-04-16 | Turbo Engineering Corp | Turbine unit |
US2473356A (en) * | 1942-04-18 | 1949-06-14 | Turbo Engineering Corp | Combustion gas turbine arrangement |
GB586913A (en) * | 1942-04-18 | 1947-04-08 | Turbo Engineering Corp | Power plant |
US2407531A (en) * | 1942-05-02 | 1946-09-10 | Fed Reserve Bank | Elastic fluid mechanism |
GB586912A (en) * | 1942-05-02 | 1947-04-08 | Turbo Engineering | Turbine system |
CH239435A (de) * | 1942-05-23 | 1945-10-15 | Buechi Alfred | Freifliegend gelagerte Turbine, insbesondere für heisse Gase. |
US2479777A (en) * | 1943-05-22 | 1949-08-23 | Lockheed Aircraft Corp | Fuel injection means for gas turbine power plants for aircraft |
US2489683A (en) * | 1943-11-19 | 1949-11-29 | Edward A Stalker | Turbine |
US2575682A (en) * | 1944-02-14 | 1951-11-20 | Lockheed Aircraft Corp | Reaction propulsion aircraft power plant having independently rotating compressor and turbine blading stages |
US2563270A (en) * | 1944-02-14 | 1951-08-07 | Lockheed Aircraft Corp | Gas reaction power plant with a variable area nozzle |
US2613501A (en) * | 1945-06-02 | 1952-10-14 | Lockheed Aircraft Corp | Internal-combustion turbine power plant |
GB659151A (en) * | 1948-06-02 | 1951-10-17 | Westinghouse Electric Int Co | Improvements in or relating to gas turbine power plants |
US2640319A (en) * | 1949-02-12 | 1953-06-02 | Packard Motor Car Co | Cooling of gas turbines |
GB680581A (en) * | 1949-05-09 | 1952-10-08 | Hermann Oestrich | Means for cooling the blades of gas turbine engines |
BE498667A (fr) * | 1949-08-27 | |||
GB699865A (en) * | 1950-11-06 | 1953-11-18 | W H Allen Sons & Company Ltd | Improvements in or relating to gas turbines |
FR1050722A (fr) * | 1951-02-15 | 1954-01-11 | Power Jets Res & Dev Ltd | Perfectionnements apportés aux rotors pour les machines traversees par un fluide, telles que les turbines |
-
1949
- 1949-08-06 US US108975A patent/US2709893A/en not_active Expired - Lifetime
-
1954
- 1954-08-19 GB GB24219/54A patent/GB791232A/en not_active Expired
- 1954-08-28 FR FR1111569D patent/FR1111569A/fr not_active Expired
- 1954-10-01 DE DEL20057A patent/DE1130646B/de active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1092730B (de) * | 1959-02-11 | 1960-11-10 | Daimler Benz Ag | Gehaeuseausbildung fuer Gasturbinentriebwerke |
EP0206683A2 (fr) * | 1985-06-17 | 1986-12-30 | The University Of Dayton | Turbine à gaz avec un conduit de dérivation interne pour le refroidissement des aubes |
EP0206683A3 (fr) * | 1985-06-17 | 1988-08-03 | The University Of Dayton | Turbine à gaz avec un conduit de dérivation interne pour le refroidissement des aubes |
Also Published As
Publication number | Publication date |
---|---|
GB791232A (en) | 1958-02-26 |
DE1130646B (de) | 1962-05-30 |
US2709893A (en) | 1955-06-07 |
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