FR1235386A - Moteur à réaction - Google Patents

Moteur à réaction

Info

Publication number
FR1235386A
FR1235386A FR795455A FR795455A FR1235386A FR 1235386 A FR1235386 A FR 1235386A FR 795455 A FR795455 A FR 795455A FR 795455 A FR795455 A FR 795455A FR 1235386 A FR1235386 A FR 1235386A
Authority
FR
France
Prior art keywords
jet engine
jet
engine
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
FR795455A
Other languages
English (en)
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.)
General Electric Co
Original Assignee
General Electric Co
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 by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of FR1235386A publication Critical patent/FR1235386A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1215—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, and the downstream series having its flaps hinged at their downstream ends on a fixed structure
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
FR795455A 1958-06-05 1959-05-25 Moteur à réaction Expired FR1235386A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US74011158 US3032977A (en) 1958-06-05 1958-06-05 Correlated bypass inlet and outlet control for a supersonic reaction powerplant

Publications (1)

Publication Number Publication Date
FR1235386A true FR1235386A (fr) 1960-07-08

Family

ID=24975090

Family Applications (1)

Application Number Title Priority Date Filing Date
FR795455A Expired FR1235386A (fr) 1958-06-05 1959-05-25 Moteur à réaction

Country Status (4)

Country Link
US (1) US3032977A (fr)
CH (1) CH373228A (fr)
DE (1) DE1134555B (fr)
FR (1) FR1235386A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5970705A (en) * 1979-08-17 1999-10-26 Rolls Royce, Limited Variable configuration final nozzle assembly for a combined rocket/ramjet engine

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3172253A (en) * 1959-01-02 1965-03-09 Garrett Corp Combination turbo and ramjet propulsion apparatus
GB1040444A (en) * 1962-05-16 1966-08-24 Bristol Siddeley Engines Ltd Improvements in ramjet engines
DE1228859B (de) * 1963-03-29 1966-11-17 Ver Flugtechnische Werke Ges M Von einem Mantelrohr umgebener UEberschalleinlauf fuer Strahltriebwerke von Flugkoerpern
US3316716A (en) * 1964-07-01 1967-05-02 William J D Escher Composite powerplant and shroud therefor
US3772886A (en) * 1970-07-01 1973-11-20 D Cameron Apparatus for water jet propulsion
US4012013A (en) * 1976-02-05 1977-03-15 The Boeing Company Variable camber inlet for supersonic aircraft
US4667900A (en) * 1981-03-05 1987-05-26 Kyusik Kim Ram constriction vane diffuser for jet engine
US5054288A (en) * 1988-10-24 1991-10-08 The Boeing Company Bypass duct for a hypersonic propulsion system
US5317866A (en) * 1992-09-18 1994-06-07 Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government Free-flying tubular vehicle
US5419117A (en) * 1993-07-30 1995-05-30 The Boeing Company Turbo jet/RAM jet propulsion system
US5881758A (en) * 1996-03-28 1999-03-16 The Boeing Company Internal compression supersonic engine inlet
JP4220393B2 (ja) * 2002-01-30 2009-02-04 ガルフストリーム・エアロスペース・コーポレイション ソニック・ブームの制御及び低減のための超音速航空機の胴体成形及びスパイク状組込体
US6948306B1 (en) * 2002-12-24 2005-09-27 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method of using supersonic combustion heater for hypersonic materials and propulsion testing
CA3071172A1 (fr) 2005-12-15 2008-04-17 Gulfstream Aerospace Corporation Entree d'air a compression isentropique pour avion supersonique
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
US20130213481A1 (en) * 2011-10-05 2013-08-22 Gohypersonic, Inc. Self-starting supersonic inlet
US20140208714A1 (en) 2012-12-19 2014-07-31 United Technologies Corporation Thermal Management for Gas Turbine Engine
GB201307004D0 (en) 2013-04-18 2013-05-29 Rolls Royce Plc An air intake and a method of controlling the same
EP3168157B1 (fr) * 2015-11-16 2019-01-02 Airbus Operations S.L. Système d'admission d'air à géométrie variable pour apu
DE102017104043A1 (de) 2017-02-27 2018-08-30 Rolls-Royce Deutschland Ltd & Co Kg Konvergent-divergente Schubdüse für ein Turbofan-Triebwerk eines Überschallflugzeugs und Verfahren zur Reduzierung des Heckwiderstands hinter einer solchen Schubdüse

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2632295A (en) * 1943-06-28 1953-03-24 Lockheed Aircraft Corp Inlet ram for power plants
US2575682A (en) * 1944-02-14 1951-11-20 Lockheed Aircraft Corp Reaction propulsion aircraft power plant having independently rotating compressor and turbine blading stages
DE866145C (de) * 1944-07-21 1953-02-09 Daimler Benz Ag Verfahren und Vorrichtung zum Anlassen von Zweikreis-Strahltriebwerken, insbesonderefuer Luftfahrzeuge
GB592091A (en) * 1944-12-08 1947-09-08 Bristol Aeroplane Co Ltd Improvements in or relating to gas turbine power plants for aircraft
US2610465A (en) * 1945-09-27 1952-09-16 Rateau Soc Auxiliary thrust means for jetpropelled aircraft
US2527732A (en) * 1946-02-07 1950-10-31 Rateau Soc Braking device for aircraft jet turbopropellers
US2612748A (en) * 1946-04-06 1952-10-07 Tenney Pulse jet mount
US2587649A (en) * 1946-10-18 1952-03-04 Pope Francis Selective turbopropeller jet power plant for aircraft
DE858159C (de) * 1947-02-28 1952-12-04 Rene Leduc Rohrkoerper oder Duese fuer den Durchgang eines relativ dazu mit UEberschallgeschwindigkeit bewegten Stroemungsmittels
US2589945A (en) * 1947-02-28 1952-03-18 Leduc Rene Athodyd having air permeable converging intake section for boundary layer controls
US2654215A (en) * 1949-09-27 1953-10-06 United Aircraft Corp Turbine power plant having auxiliary air inlet and thrust augmenter
GB713783A (en) * 1952-01-02 1954-08-18 Armstrong Siddeley Motors Ltd Gas turbine propulsion units
US2770944A (en) * 1952-04-26 1956-11-20 United Aircraft Corp Variable area reaction nozzle movable from convergent to convergent-di-vergent form
US2861419A (en) * 1953-02-13 1958-11-25 United Aircraft Corp Variable bleed diffuser
GB761235A (en) * 1953-02-24 1956-11-14 Rolls Royce Improvements in or relating to air intakes for jet-propulsion power plants
FR1086315A (fr) * 1953-07-06 1955-02-11 Perfectionnements apportés aux réacteurs combinés
FR1006139A (fr) * 1954-11-25 1952-04-21 Cem Comp Electro Mec Procédé et dispositif de réglage des turbo-réacteurs
FR1139775A (fr) * 1954-11-26 1957-07-04 Power Jets Res & Dev Ltd Tuyère de décharge pour un jet propulseur
US2841955A (en) * 1956-02-14 1958-07-08 United Aircraft Corp Directional control for jets
US2853854A (en) * 1957-02-04 1958-09-30 Orenda Engines Ltd Shroud assembly for gas turbine engines
US2920446A (en) * 1957-04-23 1960-01-12 United Aircraft Corp Shock positioning means
US2850873A (en) * 1957-08-16 1958-09-09 United Aircraft Corp By-pass ramjet
FR1150986A (fr) * 1958-03-24 1958-01-22 Serrure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5970705A (en) * 1979-08-17 1999-10-26 Rolls Royce, Limited Variable configuration final nozzle assembly for a combined rocket/ramjet engine

Also Published As

Publication number Publication date
US3032977A (en) 1962-05-08
DE1134555B (de) 1962-08-09
CH373228A (de) 1963-11-15

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