BE532916A - - Google Patents
Info
- Publication number
- BE532916A BE532916A BE532916DA BE532916A BE 532916 A BE532916 A BE 532916A BE 532916D A BE532916D A BE 532916DA BE 532916 A BE532916 A BE 532916A
- Authority
- BE
- Belgium
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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
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- 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
- F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
- F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between rotors
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- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
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- 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
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
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- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
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- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/324—Application in turbines in gas turbines to drive unshrouded, low solidity propeller
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US184543A US2693080A (en) | 1950-09-13 | 1950-09-13 | Differential gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE532916A true BE532916A (US20110009641A1-20110113-C00256.png) | 1956-03-14 |
Family
ID=22677335
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE532916D BE532916A (US20110009641A1-20110113-C00256.png) | 1950-09-13 | 1954-10-28 |
Country Status (4)
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB817591A (en) * | 1954-11-08 | 1959-08-06 | Parsons C A & Co Ltd | Improvements in and relating to gas turbine plants |
| US2960825A (en) * | 1955-10-19 | 1960-11-22 | Thompson Ramo Wooldridge Inc | Reexpansion gas turbine engine with differential compressor drive |
| US3056256A (en) * | 1956-05-07 | 1962-10-02 | United Aircraft Corp | Afterburner control for a multispool gas turbine power plant |
| DE1127150B (de) * | 1957-05-24 | 1962-04-05 | Kronogard Sven Olof | Gasturbinenanlage |
| US2908189A (en) * | 1957-06-12 | 1959-10-13 | Garrett Corp | Combination engine starter and constant speed drive |
| US3280554A (en) * | 1964-09-30 | 1966-10-25 | Ford Motor Co | Motor vehicle gas turbine drive |
| US3632222A (en) * | 1970-10-21 | 1972-01-04 | Avco Corp | Damping means for differential gas turbine engine |
| US3848482A (en) * | 1973-08-03 | 1974-11-19 | Avco Corp | Differential gearing for gas turbine engine |
| DE2525950A1 (de) * | 1975-06-11 | 1976-12-16 | Motoren Turbinen Union | Gasturbinentriebwerk in baukastenbauweise |
| US4132064A (en) * | 1977-05-26 | 1979-01-02 | The Garrett Corporation | Turbine engine with differential gearing between high pressure turbine and compressor |
| US4251987A (en) * | 1979-08-22 | 1981-02-24 | General Electric Company | Differential geared engine |
| US20040159089A1 (en) * | 1999-05-18 | 2004-08-19 | Arthur Vanmoor | Combined input and output system for a combustion engine and turbine power plant |
| US6725644B2 (en) * | 1999-05-18 | 2004-04-27 | Arthur Vanmoor | Combined input and output system for an internal combustion engine and turbine power plant |
| EP1199445A1 (de) * | 2000-10-17 | 2002-04-24 | Siemens Aktiengesellschaft | Vorrichtung und Verfahren zur Brennstoffvorwärmung in kombinierten Gas- und Dampfturbinenanlagen |
| US6895741B2 (en) * | 2003-06-23 | 2005-05-24 | Pratt & Whitney Canada Corp. | Differential geared turbine engine with torque modulation capability |
| KR101603218B1 (ko) * | 2010-03-16 | 2016-03-15 | 한화테크윈 주식회사 | 터빈 시스템 |
| US9347373B2 (en) | 2013-12-19 | 2016-05-24 | Pratt & Whitney Canada Corp. | Gas turbine engine with transmission |
| US11041444B2 (en) * | 2018-11-02 | 2021-06-22 | Pratt & Whitney Canada Corp. | Gas turbine engine with differential gearbox |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB595357A (en) * | 1944-04-08 | 1947-12-03 | Power Jets Res & Dev Ltd | Improvements in or relating to power plants |
| FR418794A (fr) * | 1909-10-08 | 1910-12-19 | Henri Royer | Turbo-moteur pour torpilles automobiles |
| US2358815A (en) * | 1935-03-28 | 1944-09-26 | Jarvis C Marble | Compressor apparatus |
| US2514513A (en) * | 1942-03-06 | 1950-07-11 | Lockheed Aircraft Corp | Jet power plant with boundary layer control for aircraft |
| US2423183A (en) * | 1944-07-13 | 1947-07-01 | Fairey Aviat Co Ltd | Turbine type jet propulsion |
| US2575683A (en) * | 1947-01-13 | 1951-11-20 | Lockheed Aircraft Corp | Intercooler and control system for turbo power plants |
-
1950
- 1950-09-13 US US184543A patent/US2693080A/en not_active Expired - Lifetime
-
1954
- 1954-10-28 BE BE532916D patent/BE532916A/xx unknown
- 1954-10-29 FR FR1113920D patent/FR1113920A/fr not_active Expired
- 1954-10-29 CH CH336645D patent/CH336645A/de unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US2693080A (en) | 1954-11-02 |
| FR1113920A (fr) | 1956-04-05 |
| CH336645A (de) | 1959-02-28 |
