FR1330633A - Turbo-reactor with bypass - Google Patents

Turbo-reactor with bypass

Info

Publication number
FR1330633A
FR1330633A FR906363A FR906363A FR1330633A FR 1330633 A FR1330633 A FR 1330633A FR 906363 A FR906363 A FR 906363A FR 906363 A FR906363 A FR 906363A FR 1330633 A FR1330633 A FR 1330633A
Authority
FR
France
Prior art keywords
turbo
bypass
reactor
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
FR906363A
Other languages
French (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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 GB29960/61A external-priority patent/GB945862A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR906363A priority Critical patent/FR1330633A/en
Application granted granted Critical
Publication of FR1330633A publication Critical patent/FR1330633A/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
    • 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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
FR906363A 1961-08-18 1962-08-07 Turbo-reactor with bypass Expired FR1330633A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR906363A FR1330633A (en) 1961-08-18 1962-08-07 Turbo-reactor with bypass

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB29960/61A GB945862A (en) 1961-08-18 1961-08-18 Gas turbine by-pass engines
FR906363A FR1330633A (en) 1961-08-18 1962-08-07 Turbo-reactor with bypass

Publications (1)

Publication Number Publication Date
FR1330633A true FR1330633A (en) 1963-06-21

Family

ID=26197003

Family Applications (1)

Application Number Title Priority Date Filing Date
FR906363A Expired FR1330633A (en) 1961-08-18 1962-08-07 Turbo-reactor with bypass

Country Status (1)

Country Link
FR (1) FR1330633A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2550821A1 (en) * 1983-08-18 1985-02-22 Snecma DEVICE FOR VARIATING THE SECONDARY FLOW OF A MULTIFLUX TURBOREACTOR
FR2551132A1 (en) * 1983-05-27 1985-03-01 Astech Twin-flow gas turbine engine
FR2602550A1 (en) * 1986-08-11 1988-02-12 Fage Etienne DOUBLE FLOW TURBOMOTEUR WITH VARIABLE CONFLUENT TUBE
FR2755729A1 (en) * 1996-11-12 1998-05-15 Fage Etienne Twin flow gas turbine engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2551132A1 (en) * 1983-05-27 1985-03-01 Astech Twin-flow gas turbine engine
FR2550821A1 (en) * 1983-08-18 1985-02-22 Snecma DEVICE FOR VARIATING THE SECONDARY FLOW OF A MULTIFLUX TURBOREACTOR
US4638631A (en) * 1983-08-18 1987-01-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Multiflow turbo jet engine secondary flow adjusting device
FR2602550A1 (en) * 1986-08-11 1988-02-12 Fage Etienne DOUBLE FLOW TURBOMOTEUR WITH VARIABLE CONFLUENT TUBE
FR2755729A1 (en) * 1996-11-12 1998-05-15 Fage Etienne Twin flow gas turbine engine
US5956939A (en) * 1996-11-12 1999-09-28 Fage; Etienne Bypass jet engine with confluent nozzle, rotating members which control the bypass air flow and a thrust reverser which controls the variable exhaust area

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