BRPI0415955A - veìculos vtol com hélice fechada em duto - Google Patents

veìculos vtol com hélice fechada em duto

Info

Publication number
BRPI0415955A
BRPI0415955A BRPI0415955-1A BRPI0415955A BRPI0415955A BR PI0415955 A BRPI0415955 A BR PI0415955A BR PI0415955 A BRPI0415955 A BR PI0415955A BR PI0415955 A BRPI0415955 A BR PI0415955A
Authority
BR
Brazil
Prior art keywords
vehicle
propellers
fuselage
vtol
geometry axis
Prior art date
Application number
BRPI0415955-1A
Other languages
English (en)
Portuguese (pt)
Inventor
Raphael Yoeli
Original Assignee
Urban Aeronautics 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 Urban Aeronautics Ltd filed Critical Urban Aeronautics Ltd
Publication of BRPI0415955A publication Critical patent/BRPI0415955A/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V1/00Air-cushion
    • B60V1/04Air-cushion wherein the cushion is contained at least in part by walls
    • B60V1/043Air-cushion wherein the cushion is contained at least in part by walls the walls being flexible
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407Doors; surrounding frames
    • B64C1/1415Cargo doors, e.g. incorporating ramps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/22Other structures integral with fuselages to facilitate loading, e.g. cargo bays, cranes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/20Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • B64C29/0025Aircraft 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 fixed relative to the fuselage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • B64C29/0033Aircraft 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/40Varying angle of sweep
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00Parachutes
    • B64D17/80Parachutes in association with aircraft, e.g. for braking thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Handcart (AREA)
BRPI0415955-1A 2003-10-27 2004-10-27 veìculos vtol com hélice fechada em duto BRPI0415955A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US51455503P 2003-10-27 2003-10-27
US60327404P 2004-08-23 2004-08-23
PCT/IL2004/000984 WO2005039972A2 (fr) 2003-10-27 2004-10-27 Vehicules a decollage et atterrissage verticaux a soufflantes carenees

Publications (1)

Publication Number Publication Date
BRPI0415955A true BRPI0415955A (pt) 2007-07-24

Family

ID=34527010

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0415955-1A BRPI0415955A (pt) 2003-10-27 2004-10-27 veìculos vtol com hélice fechada em duto

Country Status (5)

Country Link
EP (1) EP1711399A4 (fr)
JP (1) JP4612636B2 (fr)
BR (1) BRPI0415955A (fr)
CA (2) CA2718309A1 (fr)
WO (1) WO2005039972A2 (fr)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6464166B1 (en) 2001-05-29 2002-10-15 Romeo Yankee Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US7275712B2 (en) 2002-05-28 2007-10-02 Urban Aeronautics, Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US6883748B2 (en) 2001-06-04 2005-04-26 Rafi Yoeli Vehicles particularly useful as VTOL vehicles
US7857253B2 (en) 2003-10-27 2010-12-28 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
EP1855942A2 (fr) 2005-01-10 2007-11-21 Urban Aeronautics Ltd. Vehicules adav a soufflantes canalisees
US7267300B2 (en) * 2005-02-25 2007-09-11 The Boeing Company Aircraft capable of vertical and short take-off and landing
US7946528B2 (en) 2005-04-15 2011-05-24 Urban Aeronautics, Ltd. Flight control system especially suited for VTOL vehicles
US7717368B2 (en) 2005-06-07 2010-05-18 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
BRPI0708425A2 (pt) 2006-03-01 2011-05-31 Urban Aeronautics Ltd disposição de palhetas em efeito solo
WO2008065654A2 (fr) * 2006-11-27 2008-06-05 Urban Aeronautics Ltd. Effets de paroi sur des véhicules à décollage et atterrissage verticaux
EP2152576A2 (fr) 2007-05-02 2010-02-17 Urban Aeronautics Ltd. Commande d'écoulements et de forces dans des véhicules à décollage et atterrissage verticaux
WO2010026517A2 (fr) 2008-09-02 2010-03-11 Urban Aeronautics Ltd. Véhicule vtol à rotors coaxialement basculés ou basculants
US8876038B2 (en) 2010-10-05 2014-11-04 Urban Aeronautics Ltd. Ducted fan for VTOL vehicles with system and method to reduce roll moments
EP2921400A1 (fr) * 2014-03-20 2015-09-23 BAE Systems PLC Portières de véhicule reconfigurables
EP3057865B1 (fr) 2013-10-18 2020-08-05 BAE Systems PLC Portes reconfigurables pour véhicule
WO2015103700A1 (fr) 2014-01-07 2015-07-16 4525612 Canada Inc. Dba Maginaire Véhicule volant personnel
CN105856995B (zh) * 2016-04-08 2019-05-07 吉林大学 涵道式低潜飞行器
RU178183U1 (ru) * 2017-10-05 2018-03-26 Закрытое акционерное общество "Газовая нанотехнологическая компания" Гироплан медицинского назначения
JP7025937B2 (ja) * 2018-01-18 2022-02-25 本田技研工業株式会社 マルチコプタ
JP6669916B2 (ja) * 2019-04-01 2020-03-18 株式会社フジタ 無線操縦式の回転翼機
JP7374828B2 (ja) * 2020-03-23 2023-11-07 三菱重工業株式会社 ダクテッドファン装置及び航空機
ES1266365Y (es) * 2021-03-09 2021-08-03 Pinilla Enrique Jose Rivas Vehiculo aerodeslizador con alas retractiles de efecto suelo
US11383831B1 (en) * 2021-06-01 2022-07-12 Hoversurf, Inc. Methods of vertical take-off/landing and horizontal straight flight of aircraft and aircraft for implementation
US11541999B2 (en) 2021-06-01 2023-01-03 Hoversurf, Inc. Methods of vertical take-off/landing and horizontal straight flight of aircraft and aircraft for implementation
US11377220B1 (en) 2021-09-27 2022-07-05 Hoversurf, Inc. Methods of increasing flight safety, controllability and maneuverability of aircraft and aircraft for implementation thereof
CN115520172A (zh) * 2022-10-24 2022-12-27 江苏优利先进科技有限公司 一种具有飞行模式的气垫船及气垫船的控制方法
EP4495003A1 (fr) 2023-07-20 2025-01-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Adaptateur de chargement externe destiné à être utilisé avec un giravion

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955780A (en) * 1958-08-11 1960-10-11 Fluid sustained and fluid propelled flying vehicle
US3116898A (en) * 1962-03-23 1964-01-07 Gen Electric Vto inlet
US3262511A (en) * 1962-09-06 1966-07-26 Douglas Aircraft Co Inc Jet thrust controller for ground effect machine
US3335977A (en) * 1965-06-16 1967-08-15 Ludwig F Meditz Convertiplane
US3606208A (en) * 1968-12-11 1971-09-20 Steven Postelson Apostolescu Flying platform-automobile boat and air suspension car combination
US4171784A (en) * 1971-03-08 1979-10-23 Karl Eickmann Combination road and air vehicle having a lowerable chassis
US3752417A (en) * 1972-06-23 1973-08-14 P Lagace Aircraft using lifting fans
CH685692A5 (de) * 1992-01-29 1995-09-15 Sky Disc Holding Sa C O Norasi Fluggerät.
US5890441A (en) * 1995-09-07 1999-04-06 Swinson Johnny Horizontal and vertical take off and landing unmanned aerial vehicle
US6464166B1 (en) * 2001-05-29 2002-10-15 Romeo Yankee Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US6883748B2 (en) * 2001-06-04 2005-04-26 Rafi Yoeli Vehicles particularly useful as VTOL vehicles
USD543928S1 (en) * 2003-01-23 2007-06-05 Ufoz, Llc Hovercraft with stacked rotor thruster and winglets
US6892979B2 (en) * 2002-09-11 2005-05-17 Karl F. Milde, Jr. VTOL personal aircraft

Also Published As

Publication number Publication date
CA2544070A1 (fr) 2005-05-06
JP4612636B2 (ja) 2011-01-12
JP2007509790A (ja) 2007-04-19
CA2544070C (fr) 2010-12-21
CA2718309A1 (fr) 2005-05-06
EP1711399A4 (fr) 2012-08-08
EP1711399A2 (fr) 2006-10-18
WO2005039972A3 (fr) 2006-01-26
WO2005039972A2 (fr) 2005-05-06

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements