FR64773E - Perfectionnements aux tuyères et propulseurs à réaction - Google Patents

Perfectionnements aux tuyères et propulseurs à réaction

Info

Publication number
FR64773E
FR64773E FR64773DA FR64773E FR 64773 E FR64773 E FR 64773E FR 64773D A FR64773D A FR 64773DA FR 64773 E FR64773 E FR 64773E
Authority
FR
France
Prior art keywords
jet
thrusters
nozzles
jet nozzles
jet thrusters
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
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR64773E publication Critical patent/FR64773E/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/32—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for reversing thrust
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
FR64773D 1951-05-10 1953-11-02 Perfectionnements aux tuyères et propulseurs à réaction Expired FR64773E (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DES23082A DE867497C (de) 1951-05-10 1951-05-10 Reaktionsantriebsvorrichtung
FR62474T 1952-02-16
FR64773T 1953-11-02

Publications (1)

Publication Number Publication Date
FR64773E true FR64773E (fr) 1955-12-02

Family

ID=62235375

Family Applications (3)

Application Number Title Priority Date Filing Date
FR1020287D Expired FR1020287A (fr) 1951-05-10 1950-06-16 Perfectionnements aux tuyères et propulseurs à réaction
FR62474D Expired FR62474E (fr) 1951-05-10 1952-02-16 Perfectionnements aux tuyères et propulseurs à réaction
FR64773D Expired FR64773E (fr) 1951-05-10 1953-11-02 Perfectionnements aux tuyères et propulseurs à réaction

Family Applications Before (2)

Application Number Title Priority Date Filing Date
FR1020287D Expired FR1020287A (fr) 1951-05-10 1950-06-16 Perfectionnements aux tuyères et propulseurs à réaction
FR62474D Expired FR62474E (fr) 1951-05-10 1952-02-16 Perfectionnements aux tuyères et propulseurs à réaction

Country Status (4)

Country Link
BE (2) BE517529A (fr)
DE (1) DE867497C (fr)
FR (3) FR1020287A (fr)
NL (1) NL161099C (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1048092B (de) * 1956-07-03 1958-12-31 Snecma Verfahren und Vorrichtung zur Regelung des Querschnittes einer Ausstossduese von Strahltriebwerken
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
US3069850A (en) * 1959-05-18 1962-12-25 United Aircraft Corp Rocket nozzle with directional control
US3132476A (en) * 1961-04-27 1964-05-12 Earl W Conrad Thrust vector control apparatus
US3144752A (en) * 1961-10-02 1964-08-18 United Aircraft Corp Injection thrust vectoring
US3318532A (en) * 1964-04-29 1967-05-09 Gen Motors Corp Gas injection thrust vector control system for rocket engines
US3438384A (en) * 1960-07-15 1969-04-15 Hyman Hurvitz Electro-fluid systems

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1030483A (fr) * 1951-01-04 1953-06-15 Snecma Procédé et dispositifs de réglage d'un écoulement et leurs diverses applications
US2834534A (en) * 1951-09-27 1958-05-13 Snecma Centrifugal air compressor control device
US2797548A (en) * 1952-02-16 1957-07-02 Snecma Thrust spoiler for propelling nozzles
US3024602A (en) * 1952-04-22 1962-03-13 Snecma Arrangements for deflecting the jet expelled from a discharge nozzle or from a reaction-propulsion unit
US3048974A (en) * 1952-04-23 1962-08-14 Snecma Jet deflecting device for jet propulsion units
GB724011A (en) * 1952-05-30 1955-02-16 Power Jets Res & Dev Ltd Jet deflectors for aircraft
US2838909A (en) * 1952-07-17 1958-06-17 Snecma Means for the deflection of fluid jets
US3016699A (en) * 1952-10-10 1962-01-16 Snecma Aerodynamically acting jet deflecting device
DE1017474B (de) * 1952-12-12 1957-10-10 Snecma Vorrichtung zum Ablenken des Arbeitsgasstromes eines Strahltriebwerkes
US3020713A (en) * 1952-12-12 1962-02-13 Snecma Thrust spoiling device for jet propulsion units
FR1072523A (fr) * 1952-12-12 1954-09-14 Snecma Dispositif de contrôle d'un écoulement de fluide par un éeoulement auxiliaire
US2807137A (en) * 1953-07-15 1957-09-24 Snecma Jet deflecting device for jet propulsion units
US3002342A (en) * 1953-08-12 1961-10-03 Schatzki Erich Mechanism for controlling relatively high velocity flow of fluids longitudinally through and laterally from ambulant conduit means
US2960822A (en) * 1953-09-21 1960-11-22 Snecma Arrangement for deflecting the jets of reaction propulsion units
US3013386A (en) * 1954-06-01 1961-12-19 United Aircraft Corp Reverse thrust device
BE537645A (fr) * 1954-06-10
US2949734A (en) * 1954-07-27 1960-08-23 Snecma Removable grate for jet deflection
US2929204A (en) * 1954-10-01 1960-03-22 Gen Electric Jet spoiler and reverser
US2950595A (en) * 1954-11-01 1960-08-30 Marquardt Corp Thrust reverser
DE1027521B (de) * 1954-12-23 1958-04-03 Armstrong Siddeley Motors Ltd Strahltriebwerk mit Mitteln zur Schubumkehr
US2933890A (en) * 1955-01-20 1960-04-26 Boeing Co Nozzle closing jet deflectors
US2791088A (en) * 1955-03-02 1957-05-07 Gen Electric Device for thrust spoiling and thrust reversal
US2886946A (en) * 1955-04-14 1959-05-19 Canadair Ltd Thrust reversing device for turbojet engines
US2957306A (en) * 1955-06-16 1960-10-25 John S Attinello Gas jets for controlling entrance and/or exit flow effective diameter
US2952123A (en) * 1956-05-25 1960-09-13 Lockheed Aircraft Corp Directional controls for propulsive jets
CH351801A (fr) * 1956-07-03 1961-01-31 Snecma Propulseur à réaction
GB852829A (en) * 1957-04-03 1960-11-02 Rolls Royce Improvements in or relating to gas-turbine jet propulsion engines
US2968149A (en) * 1957-04-26 1961-01-17 Chance Vought Aircraft Inc Flight control means
DE1123919B (de) * 1957-08-14 1962-02-15 Snecma Vorrichtung zur Stabilisierung und Steuerung von lotrecht startenden und landenden Luftfahrzeugen
DE1147122B (de) * 1959-06-30 1963-04-11 Rolls Royce Strahlduese mit Strahlumlenkeinrichtungen
DE1207216B (de) * 1959-09-07 1965-12-16 Short Brothers & Harland Ltd Flugregelanlage fuer lotrecht startende und landende Luftfahrzeuge
DE1187491B (de) * 1960-03-07 1965-02-18 Moteuers D Aviat Soc Nat D Etu Stroemungskanal mit ringfoermigem Querschnitt und seitlichen Strahlumlenkungsoeffnungen
GB918189A (en) * 1960-07-01 1963-02-13 Rolls Royce Jet propulsion nozzle
DE1277679B (de) * 1967-04-28 1968-09-12 Entwicklungsring Sued G M B H Strahltriebwerk, insbesondere fuer senkrecht startende und landende Flugzeuge, mit schwenkbarer Primaerduese und Zusatzluft ansaugender Sekundaerduese
US4074568A (en) * 1976-05-07 1978-02-21 The United States Of America As Represented By The Secretary Of The Air Force Fluidic oscillating jet for high frequency gust tunnel

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1048092B (de) * 1956-07-03 1958-12-31 Snecma Verfahren und Vorrichtung zur Regelung des Querschnittes einer Ausstossduese von Strahltriebwerken
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
US3069850A (en) * 1959-05-18 1962-12-25 United Aircraft Corp Rocket nozzle with directional control
US3438384A (en) * 1960-07-15 1969-04-15 Hyman Hurvitz Electro-fluid systems
US3132476A (en) * 1961-04-27 1964-05-12 Earl W Conrad Thrust vector control apparatus
US3144752A (en) * 1961-10-02 1964-08-18 United Aircraft Corp Injection thrust vectoring
US3318532A (en) * 1964-04-29 1967-05-09 Gen Motors Corp Gas injection thrust vector control system for rocket engines

Also Published As

Publication number Publication date
BE503064A (fr) 1900-01-01
DE867497C (de) 1953-02-19
NL161099C (nl) 1900-01-01
BE517529A (fr) 1953-02-28
FR1020287A (fr) 1953-02-04
FR62474E (fr) 1955-06-14

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