BE517529A - Perfectionnements aux tuyeres et propulseurs a reaction - Google Patents

Perfectionnements aux tuyeres et propulseurs a reaction

Info

Publication number
BE517529A
BE517529A BE517529DA BE517529A BE 517529 A BE517529 A BE 517529A BE 517529D A BE517529D A BE 517529DA BE 517529 A BE517529 A BE 517529A
Authority
BE
Belgium
Prior art keywords
vanes
blades
nozzle
jet
grid
Prior art date
Application number
Other languages
English (en)
French (fr)
Inventor
R.H. Marchal
F.M.L. Maunoury
H. Turinetti
M. Kadosch
J. Bertin
Original Assignee
Soc. Nationale D'etude Et De Construction De Moteurs D'aviation
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 Soc. Nationale D'etude Et De Construction De Moteurs D'aviation filed Critical Soc. Nationale D'etude Et De Construction De Moteurs D'aviation
Publication of BE517529A publication Critical patent/BE517529A/fr

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/38Jet flaps
    • 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
    • F02K1/28Plants 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
    • F02K1/32Plants 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
    • 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
    • F02K1/58Reversers mounted on the inner cone or the nozzle housing or the fuselage
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
BE517529D 1951-05-10 1953-02-09 Perfectionnements aux tuyeres et propulseurs a reaction BE517529A (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
BE517529A true BE517529A (fr) 1953-02-28

Family

ID=62235375

Family Applications (2)

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

Family Applications Before (1)

Application Number Title Priority Date Filing Date
BE503064D BE503064A (de) 1951-05-10

Country Status (4)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2949734A (en) * 1954-07-27 1960-08-23 Snecma Removable grate for jet deflection

Families Citing this family (41)

* 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
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 (de) * 1954-06-10
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
DE1048092B (de) * 1956-07-03 1958-12-31 Snecma Verfahren und Vorrichtung zur Regelung des Querschnittes einer Ausstossduese von Strahltriebwerken
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
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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2949734A (en) * 1954-07-27 1960-08-23 Snecma Removable grate for jet deflection

Also Published As

Publication number Publication date
FR64773E (fr) 1955-12-02
BE503064A (de) 1900-01-01
FR62474E (fr) 1955-06-14
DE867497C (de) 1953-02-19
FR1020287A (fr) 1953-02-04
NL161099C (nl) 1900-01-01

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