BE616503A - Système de ventilateur de croisière par appareil VTOL. - Google Patents

Système de ventilateur de croisière par appareil VTOL.

Info

Publication number
BE616503A
BE616503A BE616503A BE616503A BE616503A BE 616503 A BE616503 A BE 616503A BE 616503 A BE616503 A BE 616503A BE 616503 A BE616503 A BE 616503A BE 616503 A BE616503 A BE 616503A
Authority
BE
Belgium
Prior art keywords
fan system
vtol device
cruise fan
cruise
vtol
Prior art date
Application number
BE616503A
Other languages
English (en)
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BE616503A publication Critical patent/BE616503A/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
    • B64C29/0008—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
    • B64C29/0016—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 free or ducted propellers or by blowers
    • B64C29/0033—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 free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • 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
    • 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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
BE616503A 1961-04-20 1962-04-16 Système de ventilateur de croisière par appareil VTOL. BE616503A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US104327A US3033492A (en) 1961-04-20 1961-04-20 Cruise lift-fan system

Publications (1)

Publication Number Publication Date
BE616503A true BE616503A (fr) 1962-08-16

Family

ID=22299902

Family Applications (1)

Application Number Title Priority Date Filing Date
BE616503A BE616503A (fr) 1961-04-20 1962-04-16 Système de ventilateur de croisière par appareil VTOL.

Country Status (5)

Country Link
US (1) US3033492A (fr)
BE (1) BE616503A (fr)
CH (1) CH391471A (fr)
DE (1) DE1238340C2 (fr)
GB (1) GB970082A (fr)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3289414A (en) * 1966-12-06 Cruise fan powerplant
US3138350A (en) * 1963-04-04 1964-06-23 Jr William L Lovett Ducted fan aircraft and engine
US3154917A (en) * 1963-04-15 1964-11-03 Ryan Aeronautical Co Diverter for ducted fan aircraft
US3215369A (en) * 1963-05-09 1965-11-02 Boeing Co Dual mission propulsion system
US3265329A (en) * 1963-08-27 1966-08-09 Postelson Steven Flying platform-automobile-boat and air suspension car combination
US3212731A (en) * 1963-09-09 1965-10-19 Gen Electric Fan powered aircraft
US3318095A (en) * 1964-05-14 1967-05-09 Bristol Siddeley Engines Ltd Jet propulsion plant for aircraft with gas turbine engine and with fan driven by exhaust of such engine
US3212733A (en) * 1964-07-30 1965-10-19 Gen Electric Cruise fan coupling system
DE1270888B (de) * 1964-07-30 1968-06-20 Gen Electric Reisefluggeblaesetriebwerk
US3388878A (en) * 1965-06-01 1968-06-18 Ryan Aeronautical Co Vtol aircraft with balanced power, retractible lift fan system
US3355890A (en) * 1965-06-09 1967-12-05 Gen Electric Cruise fan powerplant
GB1089549A (en) * 1965-06-14 1967-11-01 Rolls Royce Aircraft
DE1301637B (de) * 1965-10-27 1969-08-21 Daimler Benz Ag Turboantrieb fuer Hochgeschwindigkeits-Hubschrauber
US3494575A (en) * 1966-04-25 1970-02-10 David Budworth Ltd Ground and air vehicles
US3528631A (en) * 1968-11-07 1970-09-15 Us Army Lift fan scroll area control
SE450480B (sv) * 1982-08-30 1987-06-29 Tech Gerete Und Entwicklungsge Styvvingad flygkropp
US4828203A (en) * 1986-12-16 1989-05-09 Vulcan Aircraft Corporation Vertical/short take-off and landing aircraft
US4886224A (en) * 1988-09-15 1989-12-12 Joy Mario G Aircraft lift mechanism
US5275356A (en) * 1992-07-15 1994-01-04 Lockheed Corporation Propulsion system for a V/STOL aircraft
US5312069A (en) * 1992-07-15 1994-05-17 Lockheed Corporation Propulsion system for an aircraft providing V/STOL capability
GB2313580B (en) * 1996-05-31 2000-02-23 Astovl Limited An aircraft power plant
FR2864029B1 (fr) * 2003-12-23 2006-04-07 Eurocopter France Aeronef convertible pourvu de deux "tilt fan" de part et d'autre du fuselage et d'un "fan" fixe insere dans le fuselage
US7540450B2 (en) * 2004-07-16 2009-06-02 Pratt & Whitney Canada Corp. Aircraft propulsion system
US7677502B2 (en) * 2005-09-29 2010-03-16 The Boeing Company Method and apparatus for generating lift
US20100281874A1 (en) * 2007-01-09 2010-11-11 Rolls-Royce Corporation Airflow vectoring member
FR2921043B1 (fr) * 2007-09-18 2010-04-02 Gfic Methode pour faire decoller et atterrir, a faible niveau de bruit, un avion de transport, ainsi que pour ameliorer son rendement, et avion permettant la mise en oeuvre de cette methode
US20100001121A1 (en) * 2008-05-30 2010-01-07 Airbus Espana, S.L.. System for tilting a power unit
ITPD20080244A1 (it) * 2008-08-07 2008-11-06 Pompeo Bertolin Diluitori a vortice di getti di gas
US8708274B2 (en) 2011-09-09 2014-04-29 United Technologies Corporation Transverse mounted gas turbine engine
US20140117152A1 (en) * 2012-10-29 2014-05-01 United Technologies Corporation Twin Tip Turbine Propulsors Powered by a Single Gas Turbine Generator
DE102014213215A1 (de) * 2014-07-08 2016-01-14 Lilium GmbH Senkrechtstarter
FR3039133B1 (fr) * 2015-07-22 2020-01-17 Safran Aircraft Engines Aeronef avec un ensemble propulsif comprenant une soufflante a l'arriere du fuselage
JP2022523652A (ja) 2019-01-20 2022-04-26 エアーボーン モーターズ，エルエルシー 医療用スタビライザハーネスの方法および装置
US20210222649A1 (en) * 2019-11-21 2021-07-22 Garett Williams Annular exhaust nozzle
US20220106033A1 (en) * 2020-10-07 2022-04-07 Airborne Motor Works Inc. Thrust producing gyroscope autorotation safety system method and apparatus

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2863620A (en) * 1952-10-04 1958-12-09 Sud Aviation Jet-propelled aircraft
GB811840A (en) * 1954-09-14 1959-04-15 Mini Of Supply Improvements in or relating to aircraft
FR1187201A (fr) * 1957-11-19 1959-09-08 Perfectionnements apportés aux aérodynes à rotor sustentateur intégré dans la voilure, notamment à ceux à décollage vertical
DE1053321B (de) * 1957-11-20 1959-03-19 Ernst Heinkel Fahrzeugbau G M Strahlangetriebenes Schnellflugzeug
GB862032A (en) * 1958-10-03 1961-03-01 Power Jets Res & Dev Ltd Aircraft
FR1212967A (fr) * 1958-10-18 1960-03-28 Doak Aircraft Co Système de contrôle de vol
US2961189A (en) * 1958-12-12 1960-11-22 Edmond R Doak Vertical take-off aircraft construction
US2974900A (en) * 1959-03-11 1961-03-14 Doak Aircraft Co Inc Aircraft flight control system

Also Published As

Publication number Publication date
GB970082A (en) 1964-09-16
CH391471A (de) 1965-04-30
US3033492A (en) 1962-05-08
DE1238340C2 (de) 1967-10-19
DE1238340B (de) 1967-04-06

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