FR2412701A1 - Procede d'acceleration d'un turbo-moteur a gaz, turbo-moteur correspondant, et vehicule equipe d'un tel turbo-moteur - Google Patents

Procede d'acceleration d'un turbo-moteur a gaz, turbo-moteur correspondant, et vehicule equipe d'un tel turbo-moteur

Info

Publication number
FR2412701A1
FR2412701A1 FR7835622A FR7835622A FR2412701A1 FR 2412701 A1 FR2412701 A1 FR 2412701A1 FR 7835622 A FR7835622 A FR 7835622A FR 7835622 A FR7835622 A FR 7835622A FR 2412701 A1 FR2412701 A1 FR 2412701A1
Authority
FR
France
Prior art keywords
engine
turbo
gas
idle speed
accelerating
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
Application number
FR7835622A
Other languages
English (en)
Other versions
FR2412701B1 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Garrett Corp
Original Assignee
Garrett Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US05/863,205 external-priority patent/US4266401A/en
Priority claimed from US05/863,365 external-priority patent/US4274253A/en
Priority claimed from US05/863,375 external-priority patent/US4269027A/en
Priority claimed from US05/863,198 external-priority patent/US4244181A/en
Priority claimed from US05/863,495 external-priority patent/US4275558A/en
Application filed by Garrett Corp filed Critical Garrett Corp
Publication of FR2412701A1 publication Critical patent/FR2412701A1/fr
Application granted granted Critical
Publication of FR2412701B1 publication Critical patent/FR2412701B1/fr
Expired legal-status Critical Current

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
    • 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
    • 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)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

L'INVENTION CONCERNE L'INDUSTRIE DES TURBO-MOTEURS. POUR L'ACCELERATION D'UN TURBO-MOTEUR A GAZ COMPORTANT UNE TURBINE LIBRE 54, ON PART D'UNE PREMIERE VITESSE PREDETERMINEE DE RALENTI MINIMUM, ET ON COMMANDE AUTOMATIQUEMENT LE PASSAGE DU MOTEUR A UNE VITESSE DE RALENTI RAPIDE, POUR ANTICIPER UN APPEL DE PUISSANCE. DE PREFERENCE, CE PASSAGE AU REGIME DE RALENTI RAPIDE EST PREVU POUR LE ROTOR DU GENERATEUR DE GAZ 52, DONT ON REGLE EN CONSEQUENCE L'ALIMENTATION EN COMBUSTIBLE PAR LA CANALISATION 64, AU MOYEN D'UN SYSTEME DE REGULATION 6062 ASSERVI A UN BLOC ELECTRONIQUE CENTRAL 68. APPLICATION AUX TURBO-MOTEURS A GAZ, EN PARTICULIER POUR DES VEHICULES TERRESTRES, POUR EN AUGMENTER LA SOUPLESSE DE REPONSE AU MOMENT D'UN APPEL DE PUISSANCE.
FR7835622A 1977-12-22 1978-12-19 Procede d'acceleration d'un turbo-moteur a gaz, turbo-moteur correspondant, et vehicule equipe d'un tel turbo-moteur Expired FR2412701B1 (fr)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US05/863,205 US4266401A (en) 1977-12-22 1977-12-22 Gas turbine engine fuel control
US05/863,365 US4274253A (en) 1977-12-22 1977-12-22 Control for turbine and recuperator inlet temperatures
US05/863,375 US4269027A (en) 1977-12-22 1977-12-22 Gas turbine engine idle control and method
US05/863,198 US4244181A (en) 1977-12-22 1977-12-22 Variable geometry gas turbine engine fuel and guide vane control
US05/863,495 US4275558A (en) 1977-12-22 1977-12-22 Gas turbine engine fuel governor

Publications (2)

Publication Number Publication Date
FR2412701A1 true FR2412701A1 (fr) 1979-07-20
FR2412701B1 FR2412701B1 (fr) 1984-12-21

Family

ID=27542269

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7835622A Expired FR2412701B1 (fr) 1977-12-22 1978-12-19 Procede d'acceleration d'un turbo-moteur a gaz, turbo-moteur correspondant, et vehicule equipe d'un tel turbo-moteur

Country Status (2)

Country Link
FR (1) FR2412701B1 (fr)
GB (2) GB1604518A (fr)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3381470A (en) * 1966-01-17 1968-05-07 Acf Ind Inc Fuel control system for a gas turbine engine
US3529419A (en) * 1968-07-23 1970-09-22 Int Harvester Co Gas turbine engine and control system
FR2040911A5 (fr) * 1969-04-16 1971-01-22 Chandler Evans Inc
US3606754A (en) * 1969-05-19 1971-09-21 Chandler Evans Inc Hybrid fuel control
US3797230A (en) * 1969-09-02 1974-03-19 Gen Motors Corp Control method and apparatus for a single shaft turbine with prewhirl of air entering the compressor
FR2197112A1 (fr) * 1972-08-23 1974-03-22 Mtu Muenchen Gmbh

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3381470A (en) * 1966-01-17 1968-05-07 Acf Ind Inc Fuel control system for a gas turbine engine
US3529419A (en) * 1968-07-23 1970-09-22 Int Harvester Co Gas turbine engine and control system
FR2040911A5 (fr) * 1969-04-16 1971-01-22 Chandler Evans Inc
US3606754A (en) * 1969-05-19 1971-09-21 Chandler Evans Inc Hybrid fuel control
US3797230A (en) * 1969-09-02 1974-03-19 Gen Motors Corp Control method and apparatus for a single shaft turbine with prewhirl of air entering the compressor
FR2197112A1 (fr) * 1972-08-23 1974-03-22 Mtu Muenchen Gmbh

Also Published As

Publication number Publication date
FR2412701B1 (fr) 1984-12-21
GB1604518A (en) 1981-12-09
GB1604511A (en) 1981-12-09

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Legal Events

Date Code Title Description
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