BE503064A - - Google Patents

Info

Publication number
BE503064A
BE503064A BE503064DA BE503064A BE 503064 A BE503064 A BE 503064A BE 503064D A BE503064D A BE 503064DA BE 503064 A BE503064 A BE 503064A
Authority
BE
Belgium
Application number
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.)
Publication date
Publication of BE503064A publication Critical patent/BE503064A/xx

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)
BE503064D 1951-05-10 BE503064A (enrdf_load_stackoverflow)

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
BE503064A true BE503064A (enrdf_load_stackoverflow) 1900-01-01

Family

ID=62235375

Family Applications (2)

Application Number Title Priority Date Filing Date
BE503064D BE503064A (enrdf_load_stackoverflow) 1951-05-10
BE517529D BE517529A (fr) 1951-05-10 1953-02-09 Perfectionnements aux tuyeres et propulseurs a reaction

Family Applications After (1)

Application Number Title Priority Date Filing Date
BE517529D BE517529A (fr) 1951-05-10 1953-02-09 Perfectionnements aux tuyeres et propulseurs a reaction

Country Status (4)

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

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1017474B (de) * 1952-12-12 1957-10-10 Snecma Vorrichtung zum Ablenken des Arbeitsgasstromes eines Strahltriebwerkes
US2834534A (en) * 1951-09-27 1958-05-13 Snecma Centrifugal air compressor control device
US2838909A (en) * 1952-07-17 1958-06-17 Snecma Means for the deflection of fluid jets
US2886946A (en) * 1955-04-14 1959-05-19 Canadair Ltd Thrust reversing device for turbojet engines
US2906089A (en) * 1951-01-04 1959-09-29 Snecma Air intake control for jet propulsion units
US2952123A (en) * 1956-05-25 1960-09-13 Lockheed Aircraft Corp Directional controls for propulsive jets
US3016699A (en) * 1952-10-10 1962-01-16 Snecma Aerodynamically acting jet deflecting device
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

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2797548A (en) * 1952-02-16 1957-07-02 Snecma Thrust spoiler for propelling nozzles
GB724011A (en) * 1952-05-30 1955-02-16 Power Jets Res & Dev Ltd Jet deflectors for aircraft
FR1072523A (fr) * 1952-12-12 1954-09-14 Snecma Dispositif de contrôle d'un écoulement de fluide par un éeoulement auxiliaire
US3020713A (en) * 1952-12-12 1962-02-13 Snecma Thrust spoiling device for jet propulsion units
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 (enrdf_load_stackoverflow) * 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
US2957306A (en) * 1955-06-16 1960-10-25 John S Attinello Gas jets for controlling entrance and/or exit flow effective diameter
CH351801A (fr) * 1956-07-03 1961-01-31 Snecma Propulseur à réaction
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
DE1048092B (de) * 1956-07-03 1958-12-31 Snecma Verfahren und Vorrichtung zur Regelung des Querschnittes einer Ausstossduese von Strahltriebwerken
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
US3069850A (en) * 1959-05-18 1962-12-25 United Aircraft Corp Rocket nozzle with directional control
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
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
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 (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2906089A (en) * 1951-01-04 1959-09-29 Snecma Air intake control for jet propulsion units
US2834534A (en) * 1951-09-27 1958-05-13 Snecma Centrifugal air compressor control device
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
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
US2886946A (en) * 1955-04-14 1959-05-19 Canadair Ltd Thrust reversing device for turbojet engines
US2952123A (en) * 1956-05-25 1960-09-13 Lockheed Aircraft Corp Directional controls for propulsive jets

Also Published As

Publication number Publication date
FR62474E (fr) 1955-06-14
BE517529A (fr) 1953-02-28
FR1020287A (fr) 1953-02-04
FR64773E (fr) 1955-12-02
NL161099C (nl) 1900-01-01
DE867497C (de) 1953-02-19

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