FR1025827A - Further development of jet aircraft - Google Patents

Further development of jet aircraft

Info

Publication number
FR1025827A
FR1025827A FR1025827DA FR1025827A FR 1025827 A FR1025827 A FR 1025827A FR 1025827D A FR1025827D A FR 1025827DA FR 1025827 A FR1025827 A FR 1025827A
Authority
FR
France
Prior art keywords
further development
jet aircraft
aircraft
jet
development
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
Georges-Francois Culica
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 FR1025827A publication Critical patent/FR1025827A/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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants 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
    • F02K1/008—Plants 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 in any rearward direction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
FR1025827D 1950-10-11 1950-10-11 Further development of jet aircraft Expired FR1025827A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1025827T 1950-10-11

Publications (1)

Publication Number Publication Date
FR1025827A true FR1025827A (en) 1953-04-20

Family

ID=9579698

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1025827D Expired FR1025827A (en) 1950-10-11 1950-10-11 Further development of jet aircraft

Country Status (1)

Country Link
FR (1) FR1025827A (en)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1016505B (en) * 1954-04-21 1957-09-26 Florencio Bienvenido Casale Continuously working jet engine, especially for motor vehicle propulsion
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
DE1100385B (en) * 1958-12-10 1961-02-23 Entwicklungsbau Pirna Veb Device for noise control of the exhaust jet of a jet engine by adding fresh air and for changing the direction of the exhaust jet by means of adjustable deflection plates
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US3039264A (en) * 1959-09-22 1962-06-19 Dale S Ernest Shrouded nozzle
US3142153A (en) * 1961-06-09 1964-07-28 Pneumo Dynamics Corp Solid propellant rocket thrust vectoring system
US3165889A (en) * 1958-11-24 1965-01-19 Richard B Kershner Jet control by rotatable offset nozzle
US3167912A (en) * 1960-01-04 1965-02-02 United Aircraft Corp Thrust control for solid rocket
US3811713A (en) * 1958-11-28 1974-05-21 Us Army Fluid-tight high temperature flexible joint
FR2418873A1 (en) * 1978-03-03 1979-09-28 Mtu Muenchen Gmbh REACTOR TUBE FOR AIRPLANE PROPULSION AND CONTROL
FR2439304A1 (en) * 1978-10-17 1980-05-16 Mtu Muenchen Gmbh END PART OF A REACTOR PROVIDED IN PARTICULAR ON AN AIRCRAFT
FR2501786A1 (en) * 1981-03-13 1982-09-17 Snecma DEVICE FOR BEARING AND GUIDING AN ORIENTABLE NOZZLE OF A REACTION PROPELLER
US4836451A (en) * 1987-09-10 1989-06-06 United Technologies Corporation Yaw and pitch convergent-divergent thrust vectoring nozzle
EP1035316A1 (en) * 1999-03-10 2000-09-13 Snecma Moteurs Vectoriable jet nozzle
EP1045129A1 (en) * 1999-04-15 2000-10-18 Snecma Moteurs Axisymmetric vectoriable convergent - divergent nozzle
EP1045130A1 (en) * 1999-04-15 2000-10-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Axisymmetric vectoriable convergent - divergent nozzle actuated by a unison ring

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1016505B (en) * 1954-04-21 1957-09-26 Florencio Bienvenido Casale Continuously working jet engine, especially for motor vehicle propulsion
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US3165889A (en) * 1958-11-24 1965-01-19 Richard B Kershner Jet control by rotatable offset nozzle
US3811713A (en) * 1958-11-28 1974-05-21 Us Army Fluid-tight high temperature flexible joint
DE1100385B (en) * 1958-12-10 1961-02-23 Entwicklungsbau Pirna Veb Device for noise control of the exhaust jet of a jet engine by adding fresh air and for changing the direction of the exhaust jet by means of adjustable deflection plates
US3039264A (en) * 1959-09-22 1962-06-19 Dale S Ernest Shrouded nozzle
US3167912A (en) * 1960-01-04 1965-02-02 United Aircraft Corp Thrust control for solid rocket
US3142153A (en) * 1961-06-09 1964-07-28 Pneumo Dynamics Corp Solid propellant rocket thrust vectoring system
FR2418873A1 (en) * 1978-03-03 1979-09-28 Mtu Muenchen Gmbh REACTOR TUBE FOR AIRPLANE PROPULSION AND CONTROL
FR2439304A1 (en) * 1978-10-17 1980-05-16 Mtu Muenchen Gmbh END PART OF A REACTOR PROVIDED IN PARTICULAR ON AN AIRCRAFT
EP0060763A1 (en) * 1981-03-13 1982-09-22 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Bearing and guiding device for a movable jet propulsion nozzle
FR2501786A1 (en) * 1981-03-13 1982-09-17 Snecma DEVICE FOR BEARING AND GUIDING AN ORIENTABLE NOZZLE OF A REACTION PROPELLER
US4508270A (en) * 1981-03-13 1985-04-02 S.N.E.C.M.A. Apparatus for rolling and guiding a directable jet nozzle
US4836451A (en) * 1987-09-10 1989-06-06 United Technologies Corporation Yaw and pitch convergent-divergent thrust vectoring nozzle
EP1035316A1 (en) * 1999-03-10 2000-09-13 Snecma Moteurs Vectoriable jet nozzle
FR2790791A1 (en) * 1999-03-10 2000-09-15 Snecma EJECTION NOZZLE OF AXISYMMETRIC TURBOREACTOR WITH GLOBAL ORIENTATION
US6276126B1 (en) 1999-03-10 2001-08-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle
EP1045129A1 (en) * 1999-04-15 2000-10-18 Snecma Moteurs Axisymmetric vectoriable convergent - divergent nozzle
EP1045130A1 (en) * 1999-04-15 2000-10-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Axisymmetric vectoriable convergent - divergent nozzle actuated by a unison ring
FR2792367A1 (en) * 1999-04-15 2000-10-20 Snecma AXISYMMETRIC EJECTION NOZZLE, DIVERSE CONVERGENT, ORIENTED BY A GUIDED RING
FR2792366A1 (en) * 1999-04-15 2000-10-20 Snecma AXISYMMETRIC EJECTION NOZZLE, CONVERGENT DIVERGENT AND ADJUSTABLE
US6360527B1 (en) 1999-04-15 2002-03-26 Snecma Moteurs Axisymmetric, converging-diverging exhaust nozzle swiveled by a guided ring
US6375095B1 (en) 1999-04-15 2002-04-23 Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Swiveling, converging-diverging, axisymmetric exhaust nozzle

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