NL110872C - - Google Patents

Info

Publication number
NL110872C
NL110872C NL110872DA NL110872C NL 110872 C NL110872 C NL 110872C NL 110872D A NL110872D A NL 110872DA NL 110872 C NL110872 C NL 110872C
Authority
NL
Netherlands
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.)
Publication of NL110872C publication Critical patent/NL110872C/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • F02K1/386Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
NL110872D 1959-03-13 NL110872C (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8814/59A GB871842A (en) 1959-03-13 1959-03-13 Improvements in or relating to gas turbine engines

Publications (1)

Publication Number Publication Date
NL110872C true NL110872C (ja)

Family

ID=9859738

Family Applications (2)

Application Number Title Priority Date Filing Date
NL249340D NL249340A (ja) 1959-03-13
NL110872D NL110872C (ja) 1959-03-13

Family Applications Before (1)

Application Number Title Priority Date Filing Date
NL249340D NL249340A (ja) 1959-03-13

Country Status (3)

Country Link
US (1) US3043101A (ja)
GB (1) GB871842A (ja)
NL (2) NL110872C (ja)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3118276A (en) * 1964-01-21 Gas turbine engines
DE1209808B (de) * 1961-12-27 1966-01-27 Rolls Royce Zweistromgasturbinenstrahltriebwerk mit einer Nachbrenner-Brennstoffeinspritzvorrichtung im Schubrohr
US3149463A (en) * 1963-01-04 1964-09-22 Bristol Siddeley Engines Ltd Variable spread fuel dispersal system
US3750402A (en) * 1963-08-07 1973-08-07 Gen Electric Mixed flow augmentation system
US3330117A (en) * 1964-11-27 1967-07-11 Rolls Royce By-pass gas turbine jet engine
US3343629A (en) * 1965-01-11 1967-09-26 Koppers Co Inc Sound suppressor for reaction engines
US3295325A (en) * 1965-04-29 1967-01-03 United Aircraft Corp Jet engine afterburner flameholder
DE1923150A1 (de) * 1968-05-08 1970-01-15 Man Turbo Gmbh Zweistromturbinenstrahltriebwerk
GB1242066A (en) * 1968-05-16 1971-08-11 Rolls Royce Improvements in reheat combustion apparatus for by-pass gas turbine engines
FR2188060B1 (ja) * 1972-06-01 1976-06-11 Snecma
GB2123486B (en) * 1982-07-12 1986-01-02 Gen Electric Turbofan mixed flow exhaust system
US4490973A (en) * 1983-04-12 1985-01-01 The United States Of America As Represented By The Secretary Of The Air Force Flameholder with integrated air mixer
US4817378A (en) * 1987-02-13 1989-04-04 General Electric Company Gas turbine engine with augmentor and variable area bypass injector
US5076062A (en) * 1987-11-05 1991-12-31 General Electric Company Gas-cooled flameholder assembly
US10935245B2 (en) * 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2308059A (en) * 1941-04-03 1943-01-12 Ammiel F Decker Exhaust device for internal combustion engines
US2588532A (en) * 1943-05-12 1952-03-11 Allis Chalmers Mfg Co Jet propulsion unit
US2501633A (en) * 1943-06-28 1950-03-21 Lockheed Aircraft Corp Gas turbine aircraft power plant having ducted propulsive compressor means
US2523654A (en) * 1948-01-02 1950-09-26 Daniel And Florence Guggenheim Feeding and cooling wall structure for combustion chambers using liquid combustion elements
GB749009A (en) * 1953-04-24 1956-05-16 Power Jets Res & Dev Ltd An improved jet propulsion plant
US2978865A (en) * 1956-02-06 1961-04-11 Curtiss Wright Corp Turbo fan exhaust mixing device
US2929203A (en) * 1956-08-31 1960-03-22 Westinghouse Electric Corp Afterburning bypass aviation turbojet engine
US2921434A (en) * 1957-05-21 1960-01-19 Spadaro Peter Ralph Variable thrust gas turbine engine
US2979900A (en) * 1957-11-12 1961-04-18 United Aircraft Corp Ducted fan flameholder
US2934895A (en) * 1958-09-15 1960-05-03 Curtiss Wright Corp Dual cycle engine distributor construction

Also Published As

Publication number Publication date
NL249340A (ja)
GB871842A (en) 1961-07-05
US3043101A (en) 1962-07-10

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