BE755260A - Systeme de commande du dispositif d'augmentation dans une turbine a ga - Google Patents

Systeme de commande du dispositif d'augmentation dans une turbine a ga

Info

Publication number
BE755260A
BE755260A BE755260DA BE755260A BE 755260 A BE755260 A BE 755260A BE 755260D A BE755260D A BE 755260DA BE 755260 A BE755260 A BE 755260A
Authority
BE
Belgium
Prior art keywords
turbine
control system
increasing device
increasing
control
Prior art date
Application number
Other languages
English (en)
Inventor
H Hatz
Original Assignee
Gen Electric
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.)
Publication date
Publication of BE755260A publication Critical patent/BE755260A/fr

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
    • F02K1/17—Control or regulation conjointly with another control with control of fuel supply

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
BE755260D 1969-11-25 Systeme de commande du dispositif d'augmentation dans une turbine a ga BE755260A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US87979469A 1969-11-25 1969-11-25

Publications (1)

Publication Number Publication Date
BE755260A true BE755260A (fr) 1971-02-01

Family

ID=25374903

Family Applications (1)

Application Number Title Priority Date Filing Date
BE755260D BE755260A (fr) 1969-11-25 Systeme de commande du dispositif d'augmentation dans une turbine a ga

Country Status (5)

Country Link
US (1) US3656301A (fr)
BE (1) BE755260A (fr)
DE (1) DE2041782A1 (fr)
FR (1) FR2071660A5 (fr)
GB (1) GB1322356A (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3908363A (en) * 1970-04-11 1975-09-30 Mtu Muenchen Gmbh Aero gas turbine afterburner control
GB1310784A (en) * 1970-09-17 1973-03-21 Nissan Motor Control system for gas turbine engine
DE2930956C2 (de) * 1979-07-31 1985-07-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Regelungsverfahren für eine flächenverstellbare Schubdüse eines Mantelstrom-Gasturbinenstrahltriebwerks mit Nachbrenner
US4809500A (en) * 1987-02-03 1989-03-07 United Technologies Corporation Transient control system for gas turbine engine
US4947643A (en) * 1988-09-20 1990-08-14 United Technologies Corporation Active geometry control system for gas turbine engines
GB2240858B (en) * 1990-02-09 1993-08-04 Secr Defence Engine controller for reheated turbofans
US5394689A (en) * 1993-09-22 1995-03-07 General Electric Company Gas turbine engine control system having integral flight Mach number synthesis method
US5463458A (en) * 1993-12-16 1995-10-31 General Electric Company Optical sensor for duct fan discharge mach numbers
US8209987B2 (en) * 2008-11-26 2012-07-03 United Technologies Corporation Augmentor pilot
FR3004759B1 (fr) * 2013-04-23 2015-05-15 Snecma Procede et dispositif de generation d'une commande de debit de carburant destine a etre injecte dans une chambre de combustion d'une turbomachine
CN110657044B (zh) * 2019-08-30 2020-09-25 中国科学院工程热物理研究所 一种电驱式加力燃烧室与可调面积尾喷管一体化结构

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3014676A (en) * 1956-03-26 1961-12-26 Bendix Corp Power control apparatus
US2987877A (en) * 1956-12-12 1961-06-13 United Aircraft Corp Coordinated control of afterburner fuel supply and exhaust nozzle area in a multispool gas turbine power plant
US3019604A (en) * 1959-01-19 1962-02-06 Gen Motors Corp Turbojet thrust computer
US3186165A (en) * 1961-11-29 1965-06-01 Gen Electric Turbofan engine speed synchronizing arrangement
US3232053A (en) * 1963-09-13 1966-02-01 Bendix Corp Fuel feed and power control apparatus for combustion engines
US3395538A (en) * 1966-12-22 1968-08-06 Gen Electric Company A Corp Of Gas turbine engine afterburner fuel control and ignition
US3472027A (en) * 1966-12-22 1969-10-14 Gen Electric Control systems for axial flow compressors particularly adapted for use in gas turbine engines
US3517509A (en) * 1968-08-26 1970-06-30 North American Rockwell Integrated aircraft propulsion control system

Also Published As

Publication number Publication date
GB1322356A (en) 1973-07-04
US3656301A (en) 1972-04-18
FR2071660A5 (fr) 1971-09-17
DE2041782A1 (de) 1971-05-27

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