BE689296A - - Google Patents

Info

Publication number
BE689296A
BE689296A BE689296DA BE689296A BE 689296 A BE689296 A BE 689296A BE 689296D A BE689296D A BE 689296DA BE 689296 A BE689296 A BE 689296A
Authority
BE
Belgium
Application number
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
Application filed filed Critical
Publication of BE689296A publication Critical patent/BE689296A/xx

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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners

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)
BE689296D 1966-02-07 1966-11-04 BE689296A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US525639A US3331204A (en) 1966-02-07 1966-02-07 Standby afterburner operation system

Publications (1)

Publication Number Publication Date
BE689296A true BE689296A (ja) 1967-05-05

Family

ID=24094049

Family Applications (1)

Application Number Title Priority Date Filing Date
BE689296D BE689296A (ja) 1966-02-07 1966-11-04

Country Status (4)

Country Link
US (1) US3331204A (ja)
BE (1) BE689296A (ja)
DE (1) DE1526824A1 (ja)
GB (1) GB1122290A (ja)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1126809A (en) * 1967-07-04 1968-09-11 Rolls Royce Gas turbine engine
US3747344A (en) * 1970-07-20 1973-07-24 Gen Electric Variable nozzle area control system
US4095420A (en) * 1977-04-26 1978-06-20 The United States Of America As Represented By The Secretary Of The Air Force Augmentor outer segment lockout and fan upmatch
US4134259A (en) * 1977-05-20 1979-01-16 United Technologies Corporation Fuel manifold prefill
US4242865A (en) * 1978-01-25 1981-01-06 Curtiss-Wright Corporation Turbojet afterburner engine with two-position exhaust nozzle
US4244183A (en) * 1978-04-27 1981-01-13 United Technologies Corporation Control means for an augmentor for a gas turbine engine
US7762078B2 (en) * 2006-09-13 2010-07-27 Aerojet-General Corporation Nozzle with temperature-responsive throat diameter
US20120174559A1 (en) * 2011-01-07 2012-07-12 Honeywell International Inc. System and method for controlling a gas turbine engine afterburner
CN102878130A (zh) * 2011-07-11 2013-01-16 上海立新液压有限公司 电调制比例节流控制阀
GB201819748D0 (en) 2018-10-12 2019-01-16 Rolls Royce Plc Afterburner system
CN113864067B (zh) * 2020-06-30 2022-08-02 中国航发商用航空发动机有限责任公司 一种滚动优化预测闭环控制器及系统
CN114136628B (zh) * 2021-10-20 2023-06-30 中国航发四川燃气涡轮研究院 一种航空发动机试验角度可调的油门杆限位装置

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2774215A (en) * 1949-04-22 1956-12-18 Bendix Aviat Corp Tailpipe or afterburning control for turbojet engines
US2737775A (en) * 1950-09-15 1956-03-13 Solar Aircraft Co Afterburner electric controls
US2737016A (en) * 1950-09-15 1956-03-06 Solar Aircraft Co Afterburner controls
US2958186A (en) * 1955-05-25 1960-11-01 Bendix Corp Fuel feed and exhaust nozzle control for gas turbine engines
US3243955A (en) * 1960-09-13 1966-04-05 Gen Electric Afterburner fuel control mechanism
US3060683A (en) * 1960-10-26 1962-10-30 Gen Electric Afterburner fuel and nozzle area control

Also Published As

Publication number Publication date
DE1526824A1 (de) 1970-02-12
GB1122290A (en) 1968-08-07
US3331204A (en) 1967-07-18

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