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FR2457982A1 - Turboreacteur pour aeronef a decollage vertical - Google Patents

Turboreacteur pour aeronef a decollage vertical

Info

Publication number
FR2457982A1
FR2457982A1 FR7832326A FR7832326A FR2457982A1 FR 2457982 A1 FR2457982 A1 FR 2457982A1 FR 7832326 A FR7832326 A FR 7832326A FR 7832326 A FR7832326 A FR 7832326A FR 2457982 A1 FR2457982 A1 FR 2457982A1
Authority
FR
France
Prior art keywords
aircraft
turboreactor
vertical take
landing
blower
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.)
Withdrawn
Application number
FR7832326A
Other languages
English (en)
Inventor
Geoffrey Light Wilde
Maurice Ian Taylor
Geoffrey Patrick Medland
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
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2457982A1 publication Critical patent/FR2457982A1/fr
Withdrawn legal-status Critical Current

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
    • B64C29/0008—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
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

L'INVENTION CONCERNE UN GROUPE MOTEUR A TURBINE A GAZ POUR AERONEF A DECOLLAGE ET ATTERRISSAGE VERTICAL OU SUR DISTANCE REDUITE COMPRENANT UN MOTEUR PRINCIPAL 13 A 20 DONT LE CANAL DE SOUFFLANTE 13A COMPORTE DEUX TUYERES D'ECHAPPEMENT 23, 24 SELECTIVEMENT OBTURABLES PAR UN VOLET 25, ET ABRITE EN OUTRE AU MOINS UN MOTEUR AUXILIAIRE 27 ALIMENTE EN AIR PAR LA SOUFFLANTE ET SE TERMINANT PAR UNE TUYERE D'ECHAPPEMENT 28 ORIENTABLE EN FONCTION DU MODE DE FONCTIONNEMENT DE L'AERONEF, CONJOINTEMENT OU INDEPENDAMMENT DE LA SELECTION DES TUYERES 23 ET 24.
FR7832326A 1977-12-03 1978-11-16 Turboreacteur pour aeronef a decollage vertical Withdrawn FR2457982A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5045777 1977-12-03

Publications (1)

Publication Number Publication Date
FR2457982A1 true FR2457982A1 (fr) 1980-12-26

Family

ID=10455961

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7832326A Withdrawn FR2457982A1 (fr) 1977-12-03 1978-11-16 Turboreacteur pour aeronef a decollage vertical

Country Status (4)

Country Link
US (1) US4248041A (fr)
DE (1) DE2848240A1 (fr)
FR (1) FR2457982A1 (fr)
IT (1) IT1101050B (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4519543A (en) * 1982-04-07 1985-05-28 Rolls-Royce Inc. Vectorable nozzles for turbomachines
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
US4979363A (en) * 1984-11-17 1990-12-25 Rolls-Royce Plc Diverter valve with bypass duct obturator
US4713935A (en) * 1986-04-08 1987-12-22 Rolls-Royce Inc. Vectorable nozzles for aircraft
US5076512A (en) * 1989-02-08 1991-12-31 Boeing Canada Ltd. Ventral segmented nozzles for promoting rapid temperature and pressure decay
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
US4901947A (en) * 1989-02-27 1990-02-20 Lockheed Corporation Reverse engine VSTOL
US5031859A (en) * 1989-07-26 1991-07-16 Cunningham John T Lift-producing machine or device
US5897078A (en) * 1995-12-15 1999-04-27 The Boeing Company Multi-service common airframe-based aircraft
GB2353983B (en) * 2000-07-04 2003-10-15 Adrian Alexander Hubbard Variable mode jet engine-suitable for STOVL
CA2329555A1 (fr) * 2000-12-22 2002-06-22 Jose Albero Systeme principal de moteur a propulsion integre a une unite d'alimentation auxiliaire
CN100390397C (zh) * 2005-04-30 2008-05-28 张鸿元 空气压缩航空发动机
EP3181455B1 (fr) 2015-12-16 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Avion avec une sortie d'air chaud qui comprend deux sections d'échappement montées de manière pivotante
KR20210093264A (ko) * 2018-11-09 2021-07-27 제톱테라 잉크. 조정식 수직 이륙 및 착륙 추진 시스템

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR1304093A (fr) * 1961-08-04 1962-09-21 Snecma Dispositif de gouverne destiné notamment aux aérodynes à décollage et atterrissage court ou à la verticale
GB960398A (en) * 1963-02-13 1964-06-10 Rolls Royce Gas turbine engine and aircraft provided therewith
GB1182417A (en) * 1966-05-21 1970-02-25 Rolls Royce Aircraft with V/STOL Capability
US3517509A (en) * 1968-08-26 1970-06-30 North American Rockwell Integrated aircraft propulsion control system
US3577736A (en) * 1969-08-21 1971-05-04 Us Air Force Thrust diverter valve
US3769797A (en) * 1971-10-28 1973-11-06 Us Air Force By-pass engine having a single, thrust diverter valve mechanism for a v/stol aircraft

Also Published As

Publication number Publication date
US4248041A (en) 1981-02-03
IT7829660A0 (it) 1978-11-09
DE2848240A1 (de) 1981-03-19
IT1101050B (it) 1985-09-28

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Legal Events

Date Code Title Description
ST Notification of lapse