FR1153561A - New jet propulsion mode for marine vehicles and new jet diverter - Google Patents

New jet propulsion mode for marine vehicles and new jet diverter

Info

Publication number
FR1153561A
FR1153561A FR1153561DA FR1153561A FR 1153561 A FR1153561 A FR 1153561A FR 1153561D A FR1153561D A FR 1153561DA FR 1153561 A FR1153561 A FR 1153561A
Authority
FR
France
Prior art keywords
new jet
diverter
propulsion mode
marine vehicles
new
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
Alexandre Korganoff
Hans Hermann Schluenz
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 FR1153561A publication Critical patent/FR1153561A/en
Expired legal-status Critical Current

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
    • F02K1/002Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • 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
    • F02K1/06Varying effective area of jet pipe or nozzle
    • 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
    • F02K1/36Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/56Reversing jet main flow
FR1153561D 1956-06-01 1956-06-01 New jet propulsion mode for marine vehicles and new jet diverter Expired FR1153561A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1153561T 1956-06-01

Publications (1)

Publication Number Publication Date
FR1153561A true FR1153561A (en) 1958-03-12

Family

ID=9648946

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1153561D Expired FR1153561A (en) 1956-06-01 1956-06-01 New jet propulsion mode for marine vehicles and new jet diverter

Country Status (1)

Country Link
FR (1) FR1153561A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2369428A1 (en) * 1976-10-29 1978-05-26 Messerschmitt Boelkow Blohm Rocket outlet nozzle with spoilers - has deflectors with air stream separating jet from one deflector wall
FR2557925A1 (en) * 1984-01-05 1985-07-12 Hurel Dubois Avions IMPROVEMENT TO DOUBLE FLOW REACTION ENGINES EQUIPPED WITH A THRUST INVERTER.
EP0385834A1 (en) * 1989-03-01 1990-09-05 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Variable and vectorable nozzle unit for a jet engine
FR2736390A1 (en) * 1995-07-05 1997-01-10 Hispano Suiza Sa PUSH INVERTER OF A SHELL TURBOREACTOR

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2369428A1 (en) * 1976-10-29 1978-05-26 Messerschmitt Boelkow Blohm Rocket outlet nozzle with spoilers - has deflectors with air stream separating jet from one deflector wall
FR2557925A1 (en) * 1984-01-05 1985-07-12 Hurel Dubois Avions IMPROVEMENT TO DOUBLE FLOW REACTION ENGINES EQUIPPED WITH A THRUST INVERTER.
EP0150649A1 (en) * 1984-01-05 1985-08-07 Societe De Construction Des Avions Hurel-Dubois Dual flux jet engines having a thrust reverser
EP0385834A1 (en) * 1989-03-01 1990-09-05 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Variable and vectorable nozzle unit for a jet engine
FR2643947A1 (en) * 1989-03-01 1990-09-07 Snecma AXISYMMETRICAL NOZZLE TURBOREACTOR EJECTION ASSEMBLY WITH VARIABLE SECTION AND PUSH-THROUGH
US4993638A (en) * 1989-03-01 1991-02-19 Societe Nationale D'etude Et De Construction De Mateurs D'aviation "S.N.E.C.M.A." Thrust vectoring nozzle assembly
FR2736390A1 (en) * 1995-07-05 1997-01-10 Hispano Suiza Sa PUSH INVERTER OF A SHELL TURBOREACTOR
WO1997002419A1 (en) * 1995-07-05 1997-01-23 Societe Hispano-Suiza Single-clamshell turbojet thrust reverser
EP0757170A1 (en) * 1995-07-05 1997-02-05 Hispano Suiza Jet engine thrust reverser with a single door
US5785249A (en) * 1995-07-05 1998-07-28 Societe Hispano Suiza Single baffle turbojet engine thrust reverser

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