FR2596810B1 - Aeronef a tuyere orientable retractable, avec augmentation de la poussee d'ejection - Google Patents

Aeronef a tuyere orientable retractable, avec augmentation de la poussee d'ejection

Info

Publication number
FR2596810B1
FR2596810B1 FR8704834A FR8704834A FR2596810B1 FR 2596810 B1 FR2596810 B1 FR 2596810B1 FR 8704834 A FR8704834 A FR 8704834A FR 8704834 A FR8704834 A FR 8704834A FR 2596810 B1 FR2596810 B1 FR 2596810B1
Authority
FR
France
Prior art keywords
aircraft
adjustable nozzle
ejection push
increased ejection
retractable adjustable
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 - Fee Related
Application number
FR8704834A
Other languages
English (en)
Other versions
FR2596810A1 (fr
Inventor
Gary Frank Szuminski
Benjamin Dixon Ward
Douglas John Nightingale
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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
Priority claimed from US06/849,492 external-priority patent/US4713935A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2596810A1 publication Critical patent/FR2596810A1/fr
Application granted granted Critical
Publication of FR2596810B1 publication Critical patent/FR2596810B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • F02K1/004—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 by using one or more swivable nozzles rotating about their own axis
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
FR8704834A 1986-04-08 1987-04-07 Aeronef a tuyere orientable retractable, avec augmentation de la poussee d'ejection Expired - Fee Related FR2596810B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/849,492 US4713935A (en) 1986-04-08 1986-04-08 Vectorable nozzles for aircraft
US93485486A 1986-11-25 1986-11-25

Publications (2)

Publication Number Publication Date
FR2596810A1 FR2596810A1 (fr) 1987-10-09
FR2596810B1 true FR2596810B1 (fr) 1990-07-13

Family

ID=27126849

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8704834A Expired - Fee Related FR2596810B1 (fr) 1986-04-08 1987-04-07 Aeronef a tuyere orientable retractable, avec augmentation de la poussee d'ejection

Country Status (3)

Country Link
DE (1) DE3711159C2 (fr)
FR (1) FR2596810B1 (fr)
GB (1) GB2188887B (fr)

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1252071B (fr) * 1967-10-12
US2912188A (en) * 1955-09-15 1959-11-10 Bell Aircraft Corp Jet propelled aircraft with tiltable combustion chambers
GB881662A (en) * 1957-01-29 1961-11-08 Bristol Siddeley Engines Ltd Improvements in or relating to gas turbine jet propulsion engine units for aircraft and also jet propelled aircraft
GB881663A (en) * 1957-01-29 1961-11-08 Bristol Siddeley Engines Ltd Improvements in or relating to gas turbine propulsion units
FR1318816A (fr) * 1962-01-13 1963-02-22 Aviation Louis Breguet Sa Avion à décollage et atterrissage verticaux ou courts
US3216675A (en) * 1963-02-28 1965-11-09 Bristol Siddeley Engines Ltd Aircraft propulsion power plants
DE1254474B (de) * 1963-08-23 1967-11-16 Bristol Siddeley Engines Ltd Schwenkbare Strahlduese fuer Flugzeug-Strahltriebwerke
DE1236945C2 (de) * 1964-10-26 1967-09-28 Ver Flugtechnische Werke Ges M Strahlrohr, insbesondere fuer den Antrieb von Flugzeugen, mit schwenkbarem Kruemmer
DE1481554A1 (de) * 1965-04-19 1970-01-22 Gen Electric Bewegliche Duese
GB1178437A (en) * 1966-03-03 1970-01-21 M A N Turbo G M B H Bypass Turbo-Jet Engine for VTOL Aircraft.
US3416754A (en) * 1966-05-19 1968-12-17 Gen Electric Vectorable exhaust nozzle
GB1182417A (en) * 1966-05-21 1970-02-25 Rolls Royce Aircraft with V/STOL Capability
DE1288921B (de) * 1966-07-23 1969-02-06 Boelkow Gmbh Strahlrohr, insbesondere fuer senkrecht startende und landende Flugzeuge
US3357645A (en) * 1966-12-29 1967-12-12 Gen Electric Thrust directing means for aircraft
GB1208806A (en) * 1967-10-06 1970-10-14 Messerschmitt Boelkow Blohm Engine cowling ventral door, for v/stol aircraft
DE1531473B1 (de) * 1967-11-21 1970-04-02 Ver Flugtechnische Werke Strahlablenkeinrichtung fuer ein Schubrohr
GB1370887A (en) * 1970-09-26 1974-10-16 Secr Defence Aircraft and gas turbine engines therefor
DE2233352A1 (de) * 1972-07-07 1974-01-24 Ver Flugtechnische Werke V/stol-flugzeug
DE2430406A1 (de) * 1973-06-28 1975-01-16 Rolls Royce 1971 Ltd Kurz- oder vertikalstartfaehiges flugzeug
IT1101106B (it) * 1977-12-03 1985-09-28 Rolls Royce Impianto generatore di energia a motore a turbina a gas

Also Published As

Publication number Publication date
DE3711159C2 (de) 1994-05-19
FR2596810A1 (fr) 1987-10-09
GB2188887B (en) 1989-11-29
DE3711159A1 (de) 1987-10-15
GB2188887A (en) 1987-10-14
GB8706879D0 (en) 1987-04-29

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Legal Events

Date Code Title Description
ST Notification of lapse