FR2432093A1 - Turbosoufflante perfectionnee pour avion adav - Google Patents

Turbosoufflante perfectionnee pour avion adav

Info

Publication number
FR2432093A1
FR2432093A1 FR7915505A FR7915505A FR2432093A1 FR 2432093 A1 FR2432093 A1 FR 2432093A1 FR 7915505 A FR7915505 A FR 7915505A FR 7915505 A FR7915505 A FR 7915505A FR 2432093 A1 FR2432093 A1 FR 2432093A1
Authority
FR
France
Prior art keywords
adav
improved
turbosoufflante
airplanes
blocking device
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Withdrawn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
FR7915505A
Other languages
English (en)
Inventor
Robert Clayton Evans
Robert Charles Ammer
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2432093A1 publication Critical patent/FR2432093A1/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Withdrawn legal-status Critical Current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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/025—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)

Abstract

Turbosoufflante à mécanisme perfectionné d'orientation de la poussée. Elle comprend un dispositif 32 qui bloque à volonté une partie inférieure du canal de dilution 24 tout en laissant ouverte une partie supérieure de celui-ci; un dispositif à grille 27 placée dans cette nacelle 19 en avant du dispositif de blocage pour dévier à volonté le flux provenant de ce dispositif de blocage; et un agencement qui dirige vers le bas le flux détourné, pour produire de la portance Applications aux avions ADAV.
FR7915505A 1978-06-19 1979-06-18 Turbosoufflante perfectionnee pour avion adav Withdrawn FR2432093A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/916,627 US4205813A (en) 1978-06-19 1978-06-19 Thrust vectoring apparatus for a VTOL aircraft

Publications (1)

Publication Number Publication Date
FR2432093A1 true FR2432093A1 (fr) 1980-02-22

Family

ID=25437586

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7915505A Withdrawn FR2432093A1 (fr) 1978-06-19 1979-06-18 Turbosoufflante perfectionnee pour avion adav

Country Status (7)

Country Link
US (1) US4205813A (fr)
JP (1) JPS557991A (fr)
AU (1) AU4731979A (fr)
DE (1) DE2924504A1 (fr)
FR (1) FR2432093A1 (fr)
GB (1) GB2023075A (fr)
IT (1) IT1121812B (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4358074A (en) * 1979-05-24 1982-11-09 The Boeing Company Propulsion system for V/STOL aircraft
US4326686A (en) * 1980-02-15 1982-04-27 Runge Thomas M Fan jet engine bypass air delivery system for blown wing aircraft lift augmentation device
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US4799633A (en) * 1982-10-29 1989-01-24 General Electric Company Laminar flow necelle
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
US6182440B1 (en) * 1986-01-14 2001-02-06 Northrop Grumman Corporation Infrared radiation coanda suppressor
DE3735918A1 (de) * 1987-10-23 1988-09-15 Harry Sindermann Klappen-system
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
GB2231622B (en) * 1989-03-16 1993-10-27 Harold Birkett Engine for V.T.O.L. Aircraft
JPH0382699A (ja) * 1989-08-28 1991-04-08 Aretsukusu Denshi Kogyo Kk 小形垂直離着陸航空機
US5098022A (en) * 1991-01-07 1992-03-24 United Technologies Corporation Flow diverting nozzle for a gas turbine engine
US6318668B1 (en) 1996-08-02 2001-11-20 Allison Advanced Development Company Thrust vectoring techniques
US6105901A (en) * 1996-08-02 2000-08-22 Allison Engine Co., Inc. Thrust vectoring system
US6382559B1 (en) 1999-08-13 2002-05-07 Rolls-Royce Corporation Thrust vectoring mechanism
US6918244B2 (en) * 2001-08-17 2005-07-19 John Eugene Dickau Vertical takeoff and landing aircraft propulsion systems
US6648268B2 (en) * 2002-02-13 2003-11-18 Dupont Anthony A. Control system for vertical take off and land (VTOL) aircraft
GB2431626A (en) * 2005-10-26 2007-05-02 Avcen Ltd Bypass turbofan engine
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
US8935073B2 (en) 2006-10-12 2015-01-13 United Technologies Corporation Reduced take-off field length using variable nozzle
US7966827B2 (en) * 2007-05-31 2011-06-28 United Technologies Corporation Gas turbine engine with fan variable area nozzle having a rotational valve system
US8360356B2 (en) * 2008-07-17 2013-01-29 W. Eric Moore Flying apparatus
US20100170221A1 (en) * 2009-01-08 2010-07-08 Toyota Jidosha Kabushiki Kaisha Turbo fan engine
BRPI1001223A2 (pt) * 2010-04-27 2014-03-25 Marcio Carmo Lopes Pontes Conjunto de aerofólio para turbo ventilador de avião
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
GB201508138D0 (en) 2015-05-13 2015-06-24 Rolls Royce Plc Aircraft
US10563613B2 (en) 2015-08-31 2020-02-18 Rolls-Royce North American Technologies Inc. Coanda device for a round exhaust nozzle
DE102020200741A1 (de) 2020-01-22 2021-07-22 Volkswagen Aktiengesellschaft Tragflächen-Rotor-Anordnung, Luftfahrzeug und Verfahren zum Betreiben eines Luftfahrzeuges
US12559227B1 (en) * 2024-05-31 2026-02-24 Whisper Aero Inc. Uniform exhaust sheet and flow turning control

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126171A (en) * 1964-03-24 Integrated lift and propulsive system for aircraft
FR1155971A (fr) * 1956-07-11 1958-05-12 Snecma Perfectionnement aux propulseurs à réaction à plusieurs flux
US3248878A (en) * 1963-09-18 1966-05-03 Gen Electric Thrust deflector and reverser
GB1103571A (en) * 1963-10-28 1968-02-14 Bristol Siddeley Engines Ltd Aircraft jet propulsion engines
US3262268A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
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
US3797785A (en) * 1972-08-31 1974-03-19 Rohr Industries Inc Thrust modulating apparatus
US4030291A (en) * 1976-01-02 1977-06-21 General Electric Company Thrust reverser for a gas turbofan engine

Also Published As

Publication number Publication date
DE2924504A1 (de) 1980-01-03
AU4731979A (en) 1980-01-03
GB2023075A (en) 1979-12-28
US4205813A (en) 1980-06-03
IT7923666A0 (it) 1979-06-18
JPS557991A (en) 1980-01-21
IT1121812B (it) 1986-04-23

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Legal Events

Date Code Title Description
ST Notification of lapse