FR2356001A1 - Systeme de commande de circuit de carburant pour turboreacteur d'avion - Google Patents
Systeme de commande de circuit de carburant pour turboreacteur d'avionInfo
- Publication number
- FR2356001A1 FR2356001A1 FR7719296A FR7719296A FR2356001A1 FR 2356001 A1 FR2356001 A1 FR 2356001A1 FR 7719296 A FR7719296 A FR 7719296A FR 7719296 A FR7719296 A FR 7719296A FR 2356001 A1 FR2356001 A1 FR 2356001A1
- Authority
- FR
- France
- Prior art keywords
- control system
- turboreactor
- airplane
- circuit control
- fuel circuit
- 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.)
- Withdrawn
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
- F02C9/32—Control of fuel supply characterised by throttling of fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
L'invention concerne un système de commande de circuit de carburant pour turboréacteur d'avion comportant un mode de fonctionnement où la poussée nette du moteur augmente quand la vitesse de l'avion croît et un mode de fonctionnement où cette poussée diminue dans le même cas, la sélection de l'un ou l'autre de ces modes étant assurée par un distributeur 44, à commande manuelle ou automatique, piloté par un stabilisateur de nombre de Mach 46, et commandant un régulateur de débit de carburant 42 en fonction des conditions de vol.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB26317/76A GB1530693A (en) | 1976-06-24 | 1976-06-24 | Fuel control systems for gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2356001A1 true FR2356001A1 (fr) | 1978-01-20 |
Family
ID=10241741
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7719296A Withdrawn FR2356001A1 (fr) | 1976-06-24 | 1977-06-23 | Systeme de commande de circuit de carburant pour turboreacteur d'avion |
Country Status (6)
Country | Link |
---|---|
US (1) | US4270346A (fr) |
JP (1) | JPS53309A (fr) |
DE (1) | DE2725748C2 (fr) |
FR (1) | FR2356001A1 (fr) |
GB (1) | GB1530693A (fr) |
IT (1) | IT1092454B (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4212161A (en) * | 1978-05-01 | 1980-07-15 | United Technologies Corporation | Simulated parameter control for gas turbine engine |
MX18620A (es) | 1988-12-19 | 1993-10-01 | American Cyanamid Co | Floculante polimerico de alto desempeño, proceso para su preparacion, metodo para la liberacion de agua de un dispersion de solidos suspendidos y metodo de floculacion de una dispersion de solidos suspendidos |
GB2238356B (en) * | 1989-11-25 | 1994-04-13 | Rolls Royce Plc | Engine fuel control system |
US8290683B2 (en) * | 2010-02-16 | 2012-10-16 | Telectro-Mek, Inc. | Apparatus and method for reducing aircraft fuel consumption |
FR2992354B1 (fr) * | 2012-06-20 | 2015-09-18 | Snecma | Procede et dispositif d'ajustement d'une valeur de consigne d'un parametre influencant une poussee d'un moteur a turbine a gaz |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1054323A (fr) * | 1951-01-17 | 1954-02-09 | Napier & Son Ltd | Dispositif d'alimentation en combustible pour installations motrices d'avions, en particulier pour stato-réacteurs |
GB729077A (en) * | 1953-01-05 | 1955-05-04 | Hobson Ltd H M | Improvements in fuel supply systems for airborne vehicles |
GB734580A (en) * | 1952-01-23 | 1955-08-03 | Lucas Industries Ltd | Liquid fuel control means for jet-propelled aerial bodies |
GB759787A (en) * | 1954-03-10 | 1956-10-24 | Hobson Ltd H M | Improvements in pressure sensitive devices |
FR1157997A (fr) * | 1955-09-22 | 1958-06-05 | Bendix Aviat Corp | Dispositif de commande de la poussée propulsive et de la vitesse de vol d'un engin volant |
US2850871A (en) * | 1954-01-11 | 1958-09-09 | Marquardt Aircraft Co | Automatic constant mach number control system |
US2974479A (en) * | 1954-07-01 | 1961-03-14 | Curtiss Wright Corp | Manual or air speed fuel control for a jet engine |
US3129563A (en) * | 1955-02-02 | 1964-04-21 | Marquardt Corp | Pressure ratio sensing device |
FR1375826A (fr) * | 1963-08-13 | 1964-10-23 | Snecma | Dispositif de régulation du nombre de mach de vol |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2693081A (en) * | 1951-04-04 | 1954-11-02 | Allen S Atkinson | Apparatus for controlling gas turbine engines during transient operation |
GB1173841A (en) * | 1967-01-13 | 1969-12-10 | Rolls Royce | Aircraft Gas Turbine Engine Fuel System |
GB1141113A (en) * | 1967-02-21 | 1969-01-29 | Hobson Ltd H M | Improvements in fuel supply systems for aircraft jet engines |
US3713290A (en) * | 1971-05-28 | 1973-01-30 | Nasa | Gas turbine engine fuel control |
US3898796A (en) * | 1971-12-13 | 1975-08-12 | Colt Ind Operating Corp | Ambient compensating means |
US3813063A (en) * | 1972-07-21 | 1974-05-28 | United Aircraft Corp | Automatic aircraft engine pressure ratio control system |
-
1976
- 1976-06-24 GB GB26317/76A patent/GB1530693A/en not_active Expired
-
1977
- 1977-06-07 DE DE2725748A patent/DE2725748C2/de not_active Expired
- 1977-06-22 IT IT24948/77A patent/IT1092454B/it active
- 1977-06-23 FR FR7719296A patent/FR2356001A1/fr not_active Withdrawn
- 1977-06-24 JP JP7539977A patent/JPS53309A/ja active Granted
-
1979
- 1979-06-27 US US06/052,661 patent/US4270346A/en not_active Expired - Lifetime
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1054323A (fr) * | 1951-01-17 | 1954-02-09 | Napier & Son Ltd | Dispositif d'alimentation en combustible pour installations motrices d'avions, en particulier pour stato-réacteurs |
GB734580A (en) * | 1952-01-23 | 1955-08-03 | Lucas Industries Ltd | Liquid fuel control means for jet-propelled aerial bodies |
GB729077A (en) * | 1953-01-05 | 1955-05-04 | Hobson Ltd H M | Improvements in fuel supply systems for airborne vehicles |
US2850871A (en) * | 1954-01-11 | 1958-09-09 | Marquardt Aircraft Co | Automatic constant mach number control system |
GB759787A (en) * | 1954-03-10 | 1956-10-24 | Hobson Ltd H M | Improvements in pressure sensitive devices |
US2974479A (en) * | 1954-07-01 | 1961-03-14 | Curtiss Wright Corp | Manual or air speed fuel control for a jet engine |
US3129563A (en) * | 1955-02-02 | 1964-04-21 | Marquardt Corp | Pressure ratio sensing device |
FR1157997A (fr) * | 1955-09-22 | 1958-06-05 | Bendix Aviat Corp | Dispositif de commande de la poussée propulsive et de la vitesse de vol d'un engin volant |
FR1375826A (fr) * | 1963-08-13 | 1964-10-23 | Snecma | Dispositif de régulation du nombre de mach de vol |
Also Published As
Publication number | Publication date |
---|---|
DE2725748C2 (de) | 1982-02-25 |
GB1530693A (en) | 1978-11-01 |
JPS5636291B2 (fr) | 1981-08-22 |
JPS53309A (en) | 1978-01-05 |
DE2725748A1 (de) | 1977-12-29 |
IT1092454B (it) | 1985-07-12 |
US4270346A (en) | 1981-06-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |