ES239387A1 - Un sistema de control para un motro de turbina de gas - Google Patents
Un sistema de control para un motro de turbina de gasInfo
- Publication number
- ES239387A1 ES239387A1 ES0239387A ES239387A ES239387A1 ES 239387 A1 ES239387 A1 ES 239387A1 ES 0239387 A ES0239387 A ES 0239387A ES 239387 A ES239387 A ES 239387A ES 239387 A1 ES239387 A1 ES 239387A1
- Authority
- ES
- Spain
- Prior art keywords
- control
- compressor
- control mechanism
- air
- nozzle
- 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
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/16—Control or regulation conjointly with another control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Abstract
Un sistema de control para un motor de turbina de gas que tiene un compresor de aire, una toma de aire para suministrar air al compresor, una tobera de escape y una palanca de mando accionable entre posiciones correspondientes a un mínimo y a un máximo de potencia de salida de motor que tiene unos medios de mando para modificar el área de la tobera, un mecanismo de mando para gobernar el funcionamiento de dichos medios de mando, pudiendo ponerse en acción dicho mecanismo de mando en función de dicha posición de la palanca de mando para establecer un área predeterminada de tobera, medios para percibir la temperatura de toma de aire, unidos funcionalmente a dicho mecanismo de mando y unos medios correspondientes a la velocidad de dicho compresor de aire, conectados funcionalmente a dicho mecanismo de mando en función de la temperatura de toma de aire y de la velocidad de compresor citadas, para producir una variación de dicha área de tobera con objeto de regular dicho motor a una velocidad esencialmente constante conforme a una potencia de salida elegida.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US633659A US3021668A (en) | 1957-01-11 | 1957-01-11 | Nozzle area control for turbojet engines |
Publications (1)
Publication Number | Publication Date |
---|---|
ES239387A1 true ES239387A1 (es) | 1958-06-16 |
Family
ID=24540582
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES0239387A Expired ES239387A1 (es) | 1957-01-11 | 1957-12-31 | Un sistema de control para un motro de turbina de gas |
Country Status (2)
Country | Link |
---|---|
US (1) | US3021668A (es) |
ES (1) | ES239387A1 (es) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3186165A (en) * | 1961-11-29 | 1965-06-01 | Gen Electric | Turbofan engine speed synchronizing arrangement |
FR1379642A (fr) * | 1963-06-04 | 1964-11-27 | Snecma | Dispositif de régulation à commande unique pour turboréacteurs multiflux à postcombustion |
GB998341A (en) * | 1963-07-02 | 1965-07-14 | Rolls Royce | Improvements in or relating to vertical lift jet engines |
GB1215931A (en) * | 1967-03-11 | 1970-12-16 | Rolls Royce | Improvements in or relating to gas turbine engines |
GB1126809A (en) * | 1967-07-04 | 1968-09-11 | Rolls Royce | Gas turbine engine |
US5301500A (en) * | 1990-07-09 | 1994-04-12 | General Electric Company | Gas turbine engine for controlling stall margin |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE517469A (es) * | ||||
US2736166A (en) * | 1956-02-28 | Afterburning and exhaust nozzle | ||
US2563745A (en) * | 1942-03-06 | 1951-08-07 | Lockheed Aircraft Corp | Variable area nozzle for power plants |
US2514248A (en) * | 1945-03-09 | 1950-07-04 | Margaret Virginia Grimwood | Device for automatically adjusting a variable jet nozzle for a jet propulsion unit with variations in the temperature prevailing in the jet pipe |
US2529973A (en) * | 1946-05-29 | 1950-11-14 | Rateau Soc | Arrangement for the starting of two shaft gas turbine propelling means chiefly on board of aircraft |
US2545703A (en) * | 1947-03-17 | 1951-03-20 | George M Holley | Gas turbine temperature control responsive to air and fuel flow, compressor intake and discharge temperature and speed |
US2739441A (en) * | 1949-11-23 | 1956-03-27 | Gen Electric | Temperature responsive control system for gas turbine power plant having exhaust reheating |
US2750734A (en) * | 1950-01-26 | 1956-06-19 | Rateau Soc | Motive fluid flow control device for turbine compressor units used for aircraft propulsion |
US2857739A (en) * | 1951-04-06 | 1958-10-28 | Pratt & Whitney Co Inc | Control system for turbo-jet engine |
US2726507A (en) * | 1952-01-14 | 1955-12-13 | Solar Aircraft Co | Jet power plant controls |
US2807138A (en) * | 1952-07-05 | 1957-09-24 | United Aircraft Corp | Fuel control for a split-turbine type of power plant |
FR1108176A (fr) * | 1953-07-16 | 1956-01-10 | Rolls Royce | Perfectionnements aux moteurs à turbine à gaz |
GB760806A (en) * | 1953-07-16 | 1956-11-07 | Rolls Royce | Improvements in or relating to gas-turbine engines |
US2785848A (en) * | 1953-08-28 | 1957-03-19 | Rolls Royce | Gas turbine engines with speed control mechanism |
US2844936A (en) * | 1955-07-15 | 1958-07-29 | Ca Nat Research Council | Control of reheat in turbojet engines |
US2921433A (en) * | 1956-01-20 | 1960-01-19 | United Aircraft Corp | Afterburner control for a multispool gas turbine power plant |
US2955416A (en) * | 1958-10-06 | 1960-10-11 | Bendix Corp | Coordinated fuel feed and exhaust jet area control for gas turbine engines |
-
1957
- 1957-01-11 US US633659A patent/US3021668A/en not_active Expired - Lifetime
- 1957-12-31 ES ES0239387A patent/ES239387A1/es not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3021668A (en) | 1962-02-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB909511A (en) | Improvements relating to gas turbine engines having a compressor bleed valve | |
SE7606086L (sv) | Regleringsorgan for dieselmotorer | |
ES275951A1 (es) | Aparato de control de combustible para un motor de combustión | |
GB1179994A (en) | Electronic Fuel Control System for Gas Turbine Engines. | |
SE7909855L (sv) | Brenslereglerapparat for en turbinmotor | |
ES239387A1 (es) | Un sistema de control para un motro de turbina de gas | |
GB642229A (en) | Improvements in or relating to gas-turbine or jet-engines | |
SE7511937L (sv) | Anordning for reglering av sammansettningen av gaser for en forbrenningsmotor | |
SE7610723L (sv) | Forbrenningsmotor med avgasturbokompression | |
ES304004A1 (es) | Aparato regulador de la circulacion de combustible en un turbomotor de gas. | |
ES257490A1 (es) | Perfeccionamientos en los reguladores de divisiën de corriente en motores de turbina de gas | |
GB946111A (en) | Fuel supply control for gas turbine engines | |
GB538229A (en) | Improvements in or relating to automatic control devices, suitable for use with internal combustion engines | |
GB1422969A (en) | Arrangement and method for controlling the supply of fuel to a gas turbine engine | |
GB727201A (en) | Improvements in fuel supply systems for gas turbine engines | |
GB742270A (en) | Improvements relating to gas-turbine engine fuel systems | |
ES234991A1 (es) | UN MOTOR DE COMBUSTIoN INTERNA CON REGULADOR AUTOMáTICO | |
GB866461A (en) | A turbo-unit for supplying charging and cooling air for an internal-combustion engine | |
ES251362A1 (es) | Sistema perfeccionado de suministro y control de combustible para motores de gas | |
GB1084957A (en) | Improvements in or relating to turbojets with afterburner and variable area nozzle means | |
GB812557A (en) | Improvements in or relating to gas turbine power plants | |
GB781962A (en) | Fuel controls for turbo power plants | |
ES2025947A6 (es) | Regulador variable para arrancadores neumaticos de avion. | |
GB656888A (en) | Improvements in hot-gas engines and gas turbines of the closed cycle type | |
GB729300A (en) | Fuel control system for gas turbines |