BE520316A - Perfectionnements apportes aux tuyeres deflectrices du jet propulseur des avions a reaction - Google Patents

Perfectionnements apportes aux tuyeres deflectrices du jet propulseur des avions a reaction

Info

Publication number
BE520316A
BE520316A BE520316A BE520316A BE520316A BE 520316 A BE520316 A BE 520316A BE 520316 A BE520316 A BE 520316A BE 520316 A BE520316 A BE 520316A BE 520316 A BE520316 A BE 520316A
Authority
BE
Belgium
Prior art keywords
jet
nozzles
curvilinear
nozzle
wall
Prior art date
Application number
BE520316A
Other languages
English (en)
French (fr)
Inventor
Frederick Ashwood Peter
John Fletcher Philip
Original Assignee
Power Jets Res & Dev Ltd
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 Power Jets Res & Dev Ltd filed Critical Power Jets Res & Dev Ltd
Publication of BE520316A publication Critical patent/BE520316A/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0091—Accessories not provided for elsewhere
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
    • 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
    • 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
    • F02K1/006—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 within one plane only

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Jet Pumps And Other Pumps (AREA)
BE520316A 1952-05-30 1953-05-29 Perfectionnements apportes aux tuyeres deflectrices du jet propulseur des avions a reaction BE520316A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13775/52A GB724011A (en) 1952-05-30 1952-05-30 Jet deflectors for aircraft

Publications (1)

Publication Number Publication Date
BE520316A true BE520316A (fr) 1955-06-10

Family

ID=10029133

Family Applications (1)

Application Number Title Priority Date Filing Date
BE520316A BE520316A (fr) 1952-05-30 1953-05-29 Perfectionnements apportes aux tuyeres deflectrices du jet propulseur des avions a reaction

Country Status (6)

Country Link
US (1) US2770095A (de)
BE (1) BE520316A (de)
CH (1) CH317635A (de)
DE (1) DE1043824B (de)
GB (1) GB724011A (de)
NL (1) NL94757C (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2986877A (en) * 1957-03-07 1961-06-06 Paul C Emmons Rotatable afterburners for jet aircraft
US2968149A (en) * 1957-04-26 1961-01-17 Chance Vought Aircraft Inc Flight control means
US3048011A (en) * 1960-04-22 1962-08-07 United Aircraft Corp Dirigible reaction motor
DE1216705B (de) * 1962-04-11 1966-05-12 Ver Flugtechnische Werke Ges M Im Querschnitt ringfoermiger Stroemungskanal, insbesondere fuer den Mantelstrom von Zweikreisstrahltriebwerken mit im Kanal schwenkbaren Absperrklappen hinter einem zu oeffnenden Durchlass in der Kanalaussenwand

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE657397C (de) * 1938-03-03 Brev Et Procedes Coanda Soc Co Einrichtung zur Ablenkung eines Strahls von Fluessigkeit oder Gas
US2418488A (en) * 1944-07-29 1947-04-08 Westinghouse Electric Corp Power-plant apparatus
BE464035A (de) * 1945-03-22 1900-01-01
CH272464A (de) * 1946-08-27 1950-12-15 Douglas Aubrey Einrichtung zum Absaugen der Grenzschicht an Luftfahrzeugen mit Strahlantrieb.
US2526510A (en) * 1947-11-05 1950-10-17 United Aircraft Corp Directional control of propulsive jets
IT500013A (de) * 1951-04-05 1900-01-01
BE503064A (de) * 1951-05-10 1900-01-01

Also Published As

Publication number Publication date
DE1043824B (de) 1958-11-13
US2770095A (en) 1956-11-13
GB724011A (en) 1955-02-16
NL94757C (nl)
CH317635A (de) 1956-11-30

Similar Documents

Publication Publication Date Title
EP0646525B1 (de) Zweidimensionaler Über- und Hyperschall-Lufteinlauf mit drei bewegbaren Rampen für die Verbrennungsluft eines Flugzeugmotors
EP2271835B1 (de) Vorrichtung mit sekundärdüsen zur minderung des durch ein flugzeugtriebwerk erzeugten lärms
EP2257704B1 (de) Vorrichtung zur reduzierung des durch ein flugzeugdüsentriebwerk erzeugten lärms mit gleich ausgerichteten flüssigkeitsdüsen
EP2279341B1 (de) Vorrichtung zur Minderung des von einem Flugzeugtriebwerk mit gekrümmten Kanälen erzeugten Lärms
FR2483523A1 (fr) Tuyere d'ejection pour moteur a turbine a gaz
FR2929336A1 (fr) Dispositif a jets plans de reduction du bruit genere par un reacteur d'aeronef
BE517529A (fr) Perfectionnements aux tuyeres et propulseurs a reaction
FR2463859A1 (fr) Tuyere d'ejection a flux de gaz ejectes orientable
FR2710691A1 (fr) Procédé d'obtention de poussée par un jet de fluide et tuyère de poussée pour sa mise en Óoeuvre.
WO2006013243A1 (fr) Reacteur d’avion equipe d’un dispositif de reduction de bruit des jets propulsifs
WO2017013362A1 (fr) Ensemble propulsif pour aeronef comportant un inverseur de poussee
EP1020631B1 (de) Strahltriebdüse mit integrierter Schubumkehrvorrichtung
BE520316A (fr) Perfectionnements apportes aux tuyeres deflectrices du jet propulseur des avions a reaction
FR2653177A1 (fr) Turbo-statoreacteur equipant des avions pour vol sub et/ou hypersonique.
CA2198419C (fr) Statoreacteur a geometrie evolutive pour aeronef
WO2021136898A1 (fr) Inverseur de poussée comprenant des portes formant en position ouverte une ouverture de déflexion d'air vers le haut
EP2946101A1 (de) Gondelstrahlrohr mit vorrichtungen zur druckregelung
EP4085190B1 (de) Türschubumkehrvorrichtung mit einer ablenkvorrichtung zum umlenken eines luftstroms in aufwärtsrichtung
CH337688A (fr) Tuyère à réaction
WO2021140053A1 (fr) Tuyère à section de sortie variable pour moteur de fusée et moteur de fusée comportant une telle tuyère
WO2021136899A1 (fr) Inverseur de poussée comprenant des portes formant en position ouverte une ouverture de déflexion asymétrique
FR3105989A1 (fr) Inverseur de poussée à portes comprenant au moins une ouverture de déflexion débouchant sur un logement de vérin
FR2664657A1 (fr) Perfectionnements aux moteurs a turbine a gaz.
BE527857A (de)
FR2721536A1 (fr) Procédé et dispositif de pulvérisation de liquide.