FR1086315A - Improvements to combined reactors - Google Patents

Improvements to combined reactors

Info

Publication number
FR1086315A
FR1086315A FR1086315DA FR1086315A FR 1086315 A FR1086315 A FR 1086315A FR 1086315D A FR1086315D A FR 1086315DA FR 1086315 A FR1086315 A FR 1086315A
Authority
FR
France
Prior art keywords
combined reactors
reactors
combined
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.)
Expired
Application number
Other languages
French (fr)
Inventor
Louis Breguet
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
Application granted granted Critical
Publication of FR1086315A publication Critical patent/FR1086315A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • 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
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1086315D 1953-07-06 1953-07-06 Improvements to combined reactors Expired FR1086315A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1086315T 1953-07-06

Publications (1)

Publication Number Publication Date
FR1086315A true FR1086315A (en) 1955-02-11

Family

ID=9612739

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1086315D Expired FR1086315A (en) 1953-07-06 1953-07-06 Improvements to combined reactors

Country Status (1)

Country Link
FR (1) FR1086315A (en)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2984068A (en) * 1958-06-30 1961-05-16 Orenda Engines Ltd Propulsive nozzle system for reaction propulsion units
US2986002A (en) * 1957-06-05 1961-05-30 Curtiss Wright Corp Leaky-type exhaust nozzle for jet propulsion devices
US3032977A (en) * 1958-06-05 1962-05-08 Gen Electric Correlated bypass inlet and outlet control for a supersonic reaction powerplant
DE1137606B (en) * 1960-03-01 1962-10-04 Entwicklungsbau Pirna Veb Arrangement of a lubricant cooler for a stationary gas flow machine
US3069848A (en) * 1959-02-23 1962-12-25 Rolls Royce Jet lift gas turbine engines having thrust augmenting and silencing means
DE1153215B (en) * 1959-03-13 1963-08-22 Rolls Royce Twin-flow gas turbine jet engine
US3150484A (en) * 1960-08-02 1964-09-29 Rolls Royce Gas turbine by-pass engine
US3161018A (en) * 1960-07-11 1964-12-15 Nord Aviation Combined turbojet-ramjet engine
US3167911A (en) * 1961-01-27 1965-02-02 Nord Aviation Thrust-reversing device for combined turbojet-ramjet units
DE1193734B (en) * 1960-07-13 1965-05-26 United Aircraft Corp Fuel injector for gas turbine jet engines
DE1209807B (en) * 1959-02-23 1966-01-27 Rolls Royce Gas turbine jet engine with a jet device that accelerates the ambient air in an outer ring duct
US3269114A (en) * 1966-08-30 Marchant etal j et propulsion engines
US3340689A (en) * 1967-09-12 Turbojet bypass engine
DE1276969B (en) * 1962-10-30 1968-09-05 Bristol Siddeley Engines Ltd Gas turbine jet engine
US3540216A (en) * 1967-01-23 1970-11-17 Snecma Two-flow gas turbine jet engine
FR2626044A1 (en) * 1988-01-14 1989-07-21 Snecma VARIABLE SECTION FLUX MIXER WITH INTEGRATED HEATING STABILIZER FOR DOUBLE FLOW TURBOJETACTOR
WO1990008255A1 (en) * 1989-01-10 1990-07-26 Alfred Cowie Craig Controlling the flow ratio in a multiflow jet engine
FR2672641A1 (en) * 1991-02-13 1992-08-14 Snecma POST-COMBUSTION DEVICE WITH PIVOTING SHUTTERS.
WO2003025378A2 (en) * 2001-09-14 2003-03-27 Mtu Aero Engines Gmbh Device for mixing two flows of fluid, which are initially guided separate from one another, in a two-circuit reaction engine

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3340689A (en) * 1967-09-12 Turbojet bypass engine
US3269114A (en) * 1966-08-30 Marchant etal j et propulsion engines
US2986002A (en) * 1957-06-05 1961-05-30 Curtiss Wright Corp Leaky-type exhaust nozzle for jet propulsion devices
US3032977A (en) * 1958-06-05 1962-05-08 Gen Electric Correlated bypass inlet and outlet control for a supersonic reaction powerplant
US2984068A (en) * 1958-06-30 1961-05-16 Orenda Engines Ltd Propulsive nozzle system for reaction propulsion units
DE1209807B (en) * 1959-02-23 1966-01-27 Rolls Royce Gas turbine jet engine with a jet device that accelerates the ambient air in an outer ring duct
US3069848A (en) * 1959-02-23 1962-12-25 Rolls Royce Jet lift gas turbine engines having thrust augmenting and silencing means
DE1153215B (en) * 1959-03-13 1963-08-22 Rolls Royce Twin-flow gas turbine jet engine
DE1137606B (en) * 1960-03-01 1962-10-04 Entwicklungsbau Pirna Veb Arrangement of a lubricant cooler for a stationary gas flow machine
US3161018A (en) * 1960-07-11 1964-12-15 Nord Aviation Combined turbojet-ramjet engine
DE1193734B (en) * 1960-07-13 1965-05-26 United Aircraft Corp Fuel injector for gas turbine jet engines
US3150484A (en) * 1960-08-02 1964-09-29 Rolls Royce Gas turbine by-pass engine
DE1184562B (en) * 1960-08-02 1964-12-31 Rolls Royce Twin-flow gas turbine jet engine
US3167911A (en) * 1961-01-27 1965-02-02 Nord Aviation Thrust-reversing device for combined turbojet-ramjet units
DE1276969B (en) * 1962-10-30 1968-09-05 Bristol Siddeley Engines Ltd Gas turbine jet engine
US3540216A (en) * 1967-01-23 1970-11-17 Snecma Two-flow gas turbine jet engine
US4899539A (en) * 1988-01-14 1990-02-13 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Flow mixer and flame stabilizer for a turbofan engine
EP0326448A1 (en) * 1988-01-14 1989-08-02 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Mixing device with a variable section for the different jets of a jet engine
FR2626044A1 (en) * 1988-01-14 1989-07-21 Snecma VARIABLE SECTION FLUX MIXER WITH INTEGRATED HEATING STABILIZER FOR DOUBLE FLOW TURBOJETACTOR
WO1990008255A1 (en) * 1989-01-10 1990-07-26 Alfred Cowie Craig Controlling the flow ratio in a multiflow jet engine
FR2672641A1 (en) * 1991-02-13 1992-08-14 Snecma POST-COMBUSTION DEVICE WITH PIVOTING SHUTTERS.
US5212945A (en) * 1991-02-13 1993-05-25 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Post-combustion device with pivoting flaps
WO2003025378A2 (en) * 2001-09-14 2003-03-27 Mtu Aero Engines Gmbh Device for mixing two flows of fluid, which are initially guided separate from one another, in a two-circuit reaction engine
WO2003025378A3 (en) * 2001-09-14 2003-05-30 Mtu Aero Engines Gmbh Device for mixing two flows of fluid, which are initially guided separate from one another, in a two-circuit reaction engine
US7299635B2 (en) 2001-09-14 2007-11-27 Mtu Aero Engines Gmbh Device for mixing two flows of fluid which are initially guided separate from one another in a bypass jet engine

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