FR2412703A1 - Procede de regulation pour un turbo-moteur a gaz, et turbo-moteur correspondant - Google Patents
Procede de regulation pour un turbo-moteur a gaz, et turbo-moteur correspondantInfo
- Publication number
- FR2412703A1 FR2412703A1 FR7835624A FR7835624A FR2412703A1 FR 2412703 A1 FR2412703 A1 FR 2412703A1 FR 7835624 A FR7835624 A FR 7835624A FR 7835624 A FR7835624 A FR 7835624A FR 2412703 A1 FR2412703 A1 FR 2412703A1
- Authority
- FR
- France
- Prior art keywords
- gas
- turbo
- engine
- turbine
- generator
- 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.)
- Granted
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 abstract 4
- 239000000446 fuel 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
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
-
- 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
- F02C9/48—Control of fuel supply conjointly with another control of the plant
- F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
- F02C9/54—Control of fuel supply conjointly with another control of the plant with control of working fluid flow by throttling the working fluid, by adjusting vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B1/00—Engines characterised by fuel-air mixture compression
- F02B1/02—Engines characterised by fuel-air mixture compression with positive ignition
- F02B1/04—Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Supercharger (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Control Of Turbines (AREA)
Abstract
L'INVENTION CONCERNE LES TURBO-MOTEURS A GAZ. TURBO-MOTEUR A GAZ COMPORTANT UNE TURBINE LIBRE 54 ENTRAINEE PAR LES GAZ PRODUITS PAR UN GENERATEUR DE GAZ 92, DES MOYENS 442444 POUR MESURER LA VITESSE DU GENERATEUR DE GAZ 92, ET DES MOYENS POUR ALIMENTER EN COMBUSTIBLE LE GENERATEUR A GAZ A UN DEBIT VARIABLE, EN FONCTION INVERSE DE LA VITESSE DU GENERATEUR. ON MESURE LA TEMPERATURE DES GAZ A L'ENTREE ET A LA SORTIE DE LA TURBINE DE PUISSANCE 54. ON ASSURE LE GUIDAGE DU COURANT DES GAZ ENTRAINANT LA TURBINE, ET ON EN FAIT VARIER L'INCIDENCE, AU MOYEN D'UNE SERIE D'AUBES DIRECTRICES 120 COMMANDEES PAR UN MECANISME 132130 ASSERVI A UN REGULATEUR 66 SUIVANT LES VALEURS MESUREES DES TEMPERATURES D'ENTREE ET DE SORTIE DE LA TURBINE. APPLICATION A L'AMELIORATION DU RENDEMENT DES TURBO-MOTEURS A GAZ, NOTAMMENT POUR VEHICULES.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/863,365 US4274253A (en) | 1977-12-22 | 1977-12-22 | Control for turbine and recuperator inlet temperatures |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2412703A1 true FR2412703A1 (fr) | 1979-07-20 |
FR2412703B1 FR2412703B1 (fr) | 1984-12-28 |
Family
ID=25340984
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7835624A Granted FR2412703A1 (fr) | 1977-12-22 | 1978-12-19 | Procede de regulation pour un turbo-moteur a gaz, et turbo-moteur correspondant |
Country Status (4)
Country | Link |
---|---|
US (1) | US4274253A (fr) |
CA (1) | CA1121165A (fr) |
FR (1) | FR2412703A1 (fr) |
GB (1) | GB1604516A (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4688663A (en) * | 1982-05-10 | 1987-08-25 | Marchand William C | Motor and brake control for a multi-stage turbine engine |
US5497615A (en) * | 1994-03-21 | 1996-03-12 | Noe; James C. | Gas turbine generator set |
US5819524A (en) * | 1996-10-16 | 1998-10-13 | Capstone Turbine Corporation | Gaseous fuel compression and control system and method |
GB2374904A (en) * | 2001-04-26 | 2002-10-30 | Bowman Power Systems Ltd | Controlling temperature in gas turbine apparatus during startup or shutdown |
US8235150B2 (en) * | 2008-06-24 | 2012-08-07 | Rez Mustafa | Pneumatic hybrid turbo transmission |
WO2009158184A1 (fr) * | 2008-06-24 | 2009-12-30 | Mustafa Rez | Turbotransmission hybride pneumatique |
US8336304B2 (en) * | 2008-06-24 | 2012-12-25 | Rez Mustafa | Hydraulic hybrid turbo-transmission |
US8090456B2 (en) * | 2008-11-03 | 2012-01-03 | United Technologies Corporation | System and method for design and control of engineering systems utilizing component-level dynamic mathematical model |
US8315741B2 (en) * | 2009-09-02 | 2012-11-20 | United Technologies Corporation | High fidelity integrated heat transfer and clearance in component-level dynamic turbine system control |
US8668434B2 (en) * | 2009-09-02 | 2014-03-11 | United Technologies Corporation | Robust flow parameter model for component-level dynamic turbine system control |
NL2005381C2 (en) * | 2010-09-21 | 2012-03-28 | Micro Turbine Technology B V | Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine. |
US9803560B2 (en) * | 2013-03-15 | 2017-10-31 | Ansaldo Energia Ip Uk Limited | Dynamic tuning of a gas turbine engine to detect and prevent lean blowout |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3508395A (en) * | 1968-04-01 | 1970-04-28 | Ford Motor Co | Control system for motor vehicle type gas turbine engine |
US3529419A (en) * | 1968-07-23 | 1970-09-22 | Int Harvester Co | Gas turbine engine and control system |
FR2030930A5 (fr) * | 1969-09-04 | 1970-11-13 | Motoren Turbinen Union | |
US3606754A (en) * | 1969-05-19 | 1971-09-21 | Chandler Evans Inc | Hybrid fuel control |
DE2109215A1 (de) * | 1971-02-26 | 1972-09-07 | Daimler Benz Ag | Regelanlage eines Gasturbinentrieb werkes |
FR2197112A1 (fr) * | 1972-08-23 | 1974-03-22 | Mtu Muenchen Gmbh | |
US3814537A (en) * | 1972-09-22 | 1974-06-04 | Gen Motors Corp | Turbine nozzle control |
US3938321A (en) * | 1974-03-04 | 1976-02-17 | General Motors Corporation | Gas turbine control |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3199293A (en) * | 1963-08-15 | 1965-08-10 | Gen Electric | Two shaft gas turbine control system |
US3383090A (en) * | 1966-12-30 | 1968-05-14 | Ford Motor Co | Fluid pressure control for a turbine nozzle actuator |
US3521446A (en) * | 1968-04-16 | 1970-07-21 | Chandler Evans Inc | Fuel control having pressure referenced turbine overspeed device |
US3952502A (en) * | 1974-03-04 | 1976-04-27 | General Motors Corporation | Gas turbine control |
US3999374A (en) * | 1975-07-11 | 1976-12-28 | General Motors Corporation | Automotive gas turbine control |
-
1977
- 1977-12-22 US US05/863,365 patent/US4274253A/en not_active Expired - Lifetime
-
1978
- 1978-05-23 GB GB21347/78A patent/GB1604516A/en not_active Expired
- 1978-10-24 CA CA000314161A patent/CA1121165A/fr not_active Expired
- 1978-12-19 FR FR7835624A patent/FR2412703A1/fr active Granted
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3508395A (en) * | 1968-04-01 | 1970-04-28 | Ford Motor Co | Control system for motor vehicle type gas turbine engine |
US3529419A (en) * | 1968-07-23 | 1970-09-22 | Int Harvester Co | Gas turbine engine and control system |
US3606754A (en) * | 1969-05-19 | 1971-09-21 | Chandler Evans Inc | Hybrid fuel control |
FR2030930A5 (fr) * | 1969-09-04 | 1970-11-13 | Motoren Turbinen Union | |
DE2109215A1 (de) * | 1971-02-26 | 1972-09-07 | Daimler Benz Ag | Regelanlage eines Gasturbinentrieb werkes |
FR2197112A1 (fr) * | 1972-08-23 | 1974-03-22 | Mtu Muenchen Gmbh | |
US3814537A (en) * | 1972-09-22 | 1974-06-04 | Gen Motors Corp | Turbine nozzle control |
US3938321A (en) * | 1974-03-04 | 1976-02-17 | General Motors Corporation | Gas turbine control |
Also Published As
Publication number | Publication date |
---|---|
FR2412703B1 (fr) | 1984-12-28 |
CA1121165A (fr) | 1982-04-06 |
US4274253A (en) | 1981-06-23 |
GB1604516A (en) | 1981-12-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |