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- Withdrawn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
- 239000000446 fuel Substances 0.000 title abstract 3
- 230000007423 decrease Effects 0.000 abstract 1
- 239000003381 stabilizer Substances 0.000 abstract 1
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)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
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| FR7719296A Withdrawn FR2356001A1 (fr) | 1976-06-24 | 1977-06-23 | Systeme de commande de circuit de carburant pour turboreacteur d'avion |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 (OSRAM) |
| JP (1) | JPS53309A (OSRAM) |
| DE (1) | DE2725748C2 (OSRAM) |
| FR (1) | FR2356001A1 (OSRAM) |
| GB (1) | GB1530693A (OSRAM) |
| IT (1) | IT1092454B (OSRAM) |
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 |
|---|---|
| GB1530693A (en) | 1978-11-01 |
| DE2725748C2 (de) | 1982-02-25 |
| IT1092454B (it) | 1985-07-12 |
| DE2725748A1 (de) | 1977-12-29 |
| JPS5636291B2 (OSRAM) | 1981-08-22 |
| JPS53309A (en) | 1978-01-05 |
| US4270346A (en) | 1981-06-02 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2438663A (en) | Fuel injection system for internalcombustion engines | |
| US2419171A (en) | Regulating device for controlling the supply of fuel to internal-combustion engines | |
| US2407652A (en) | Detonation responsive means for controlling internal-combustion engines | |
| JPS57140536A (en) | Internal-combustion engine controller | |
| FR2403459A1 (fr) | Dispositif de commande de ralenti pour systeme electronique d'injection de carburant | |
| SE8107800L (sv) | Temperaturregler-/synkroniseringssystem | |
| FR2357739A1 (fr) | Regulateur de poussee pour un moteur a turbine a gaz | |
| FR2431609A1 (fr) | Systeme d'alimentation en air de refroidissement pour moteur a turbine a gaz | |
| FR2356001A1 (fr) | Systeme de commande de circuit de carburant pour turboreacteur d'avion | |
| SE8002018L (sv) | Brenslesystem for gasturbinmotor | |
| FR2398185A1 (fr) | Commande de secours pour systeme de commande de moteur a turbine a gaz | |
| GB1237680A (en) | Flow metering apparatus, particularly for combustion engine fuel control | |
| GB1058927A (en) | Improvements in fuel control devices for gas turbine engines | |
| US2449468A (en) | Fuel injection system for internalcombustion engines | |
| US2661796A (en) | Hydraulic control means for engine fuel systems | |
| GB1256666A (OSRAM) | ||
| GB1238897A (OSRAM) | ||
| GB692666A (en) | Automatic control of gas turbine engines, particularly for aircraft | |
| US2959920A (en) | Speed and temperature responsive fuel control system for combustion engines | |
| GB1445347A (en) | Fuel control apparatus for gas turbine engines | |
| US2960155A (en) | Afterburner fuel metering control | |
| US2972229A (en) | Jet engine fuel control | |
| US2451204A (en) | Engine controller | |
| GB911021A (en) | Improvements relating to turbo-propeller engine fuel control | |
| GB1011055A (en) | Improved engine fuel control system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |