CA2544070C - Vehicules a decollage et atterrissage verticaux a soufflantes carenees - Google Patents
Vehicules a decollage et atterrissage verticaux a soufflantes carenees Download PDFInfo
- Publication number
- CA2544070C CA2544070C CA2544070A CA2544070A CA2544070C CA 2544070 C CA2544070 C CA 2544070C CA 2544070 A CA2544070 A CA 2544070A CA 2544070 A CA2544070 A CA 2544070A CA 2544070 C CA2544070 C CA 2544070C
- Authority
- CA
- Canada
- Prior art keywords
- vehicle
- duct
- fuselage
- vanes
- air flow
- 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
Links
- 230000033001 locomotion Effects 0.000 claims description 11
- 230000008859 change Effects 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 239000003570 air Substances 0.000 claims 34
- 230000002093 peripheral effect Effects 0.000 claims 10
- 239000013598 vector Substances 0.000 claims 3
- 239000012530 fluid Substances 0.000 claims 2
- 239000012080 ambient air Substances 0.000 claims 1
- 230000005465 channeling Effects 0.000 claims 1
- 239000003381 stabilizer Substances 0.000 description 19
- 238000010276 construction Methods 0.000 description 15
- 230000005540 biological transmission Effects 0.000 description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 238000013461 design Methods 0.000 description 5
- 230000001965 increasing effect Effects 0.000 description 5
- 238000009434 installation Methods 0.000 description 5
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000000087 stabilizing effect Effects 0.000 description 3
- 238000013519 translation Methods 0.000 description 3
- 230000014616 translation Effects 0.000 description 3
- 210000001015 abdomen Anatomy 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 230000003416 augmentation Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 230000000284 resting effect Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- IBSREHMXUMOFBB-JFUDTMANSA-N 5u8924t11h Chemical compound O1[C@@H](C)[C@H](O)[C@@H](OC)C[C@@H]1O[C@@H]1[C@@H](OC)C[C@H](O[C@@H]2C(=C/C[C@@H]3C[C@@H](C[C@@]4(O3)C=C[C@H](C)[C@@H](C(C)C)O4)OC(=O)[C@@H]3C=C(C)[C@@H](O)[C@H]4OC\C([C@@]34O)=C/C=C/[C@@H]2C)/C)O[C@H]1C.C1=C[C@H](C)[C@@H]([C@@H](C)CC)O[C@]11O[C@H](C\C=C(C)\[C@@H](O[C@@H]2O[C@@H](C)[C@H](O[C@@H]3O[C@@H](C)[C@H](O)[C@@H](OC)C3)[C@@H](OC)C2)[C@@H](C)\C=C\C=C/2[C@]3([C@H](C(=O)O4)C=C(C)[C@@H](O)[C@H]3OC\2)O)C[C@H]4C1 IBSREHMXUMOFBB-JFUDTMANSA-N 0.000 description 1
- 208000032370 Secondary transmission Diseases 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/04—Air-cushion wherein the cushion is contained at least in part by walls
- B60V1/043—Air-cushion wherein the cushion is contained at least in part by walls the walls being flexible
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; 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
- B64C1/1407—Doors; surrounding frames
- B64C1/1415—Cargo doors, e.g. incorporating ramps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/22—Other structures integral with fuselages to facilitate loading, e.g. cargo bays, cranes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- 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
- B64C29/0025—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 fixed relative to the fuselage
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/40—Varying angle of sweep
-
- 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
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
-
- 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
- B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
-
- 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
- Y02T50/10—Drag 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)
Abstract
L'invention concerne un véhicule qui comprend un fuselage présentant un axe longitudinal et un axe transversal, deux hélices génératrices de portance carénées, portées par le fuselage de chaque côté de l'axe transversal ; un compartiment de pilote formé dans le fuselage, entre les hélices, et qui est sensiblement aligné sur un côté du fuselage ; une soute formée dans le fuselage, entre les hélices, à l'opposé du compartiment de pilote ; et deux soufflantes propulsives placées à l'arrière du véhicule. Dans diverses variantes décrites, le véhicule peut être utilisé non seulement comme véhicule à décollage et atterrissage verticaux, mais aussi comme véhicule utilitaire multifonction pour mettre en oeuvre de nombreuses fonctions variées telles que des fonctions d'aéroglisseur et de véhicule tout-terrain. L'invention concerne également une version sans pilote du véhicule. Des caractéristiques uniques, qui peuvent être appliquées à des soufflantes carénées uniques ou multiples ou à des véhicules à décollage et atterrissage verticaux, sont également décrites.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2718309A CA2718309A1 (fr) | 2003-10-27 | 2004-10-27 | Vehicules a decollage et atterrissage verticaux a soufflantes carenees |
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US51455503P | 2003-10-27 | 2003-10-27 | |
| US60/514,555 | 2003-10-27 | ||
| US60327404P | 2004-08-23 | 2004-08-23 | |
| US60/603,274 | 2004-08-23 | ||
| PCT/IL2004/000984 WO2005039972A2 (fr) | 2003-10-27 | 2004-10-27 | Vehicules a decollage et atterrissage verticaux a soufflantes carenees |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2718309A Division CA2718309A1 (fr) | 2003-10-27 | 2004-10-27 | Vehicules a decollage et atterrissage verticaux a soufflantes carenees |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2544070A1 CA2544070A1 (fr) | 2005-05-06 |
| CA2544070C true CA2544070C (fr) | 2010-12-21 |
Family
ID=34527010
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2718309A Abandoned CA2718309A1 (fr) | 2003-10-27 | 2004-10-27 | Vehicules a decollage et atterrissage verticaux a soufflantes carenees |
| CA2544070A Expired - Fee Related CA2544070C (fr) | 2003-10-27 | 2004-10-27 | Vehicules a decollage et atterrissage verticaux a soufflantes carenees |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2718309A Abandoned CA2718309A1 (fr) | 2003-10-27 | 2004-10-27 | Vehicules a decollage et atterrissage verticaux a soufflantes carenees |
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)
| 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)
| 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 |
-
2004
- 2004-10-27 WO PCT/IL2004/000984 patent/WO2005039972A2/fr not_active Ceased
- 2004-10-27 BR BRPI0415955-1A patent/BRPI0415955A/pt not_active Application Discontinuation
- 2004-10-27 EP EP04791846A patent/EP1711399A4/fr not_active Withdrawn
- 2004-10-27 CA CA2718309A patent/CA2718309A1/fr not_active Abandoned
- 2004-10-27 CA CA2544070A patent/CA2544070C/fr not_active Expired - Fee Related
- 2004-10-27 JP JP2006536260A patent/JP4612636B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2544070A1 (fr) | 2005-05-06 |
| JP4612636B2 (ja) | 2011-01-12 |
| JP2007509790A (ja) | 2007-04-19 |
| BRPI0415955A (pt) | 2007-07-24 |
| 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 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2544070C (fr) | Vehicules a decollage et atterrissage verticaux a soufflantes carenees | |
| US7806362B2 (en) | Ducted fan VTOL vehicles | |
| US7857253B2 (en) | Ducted fan VTOL vehicles | |
| US8833692B2 (en) | Wall effects on VTOL vehicles | |
| US20090159757A1 (en) | Ducted Fan Vtol Vehicles | |
| US20080054121A1 (en) | Ducted fan VTOL vehicles | |
| WO2007052271A2 (fr) | Flux par rapport au toit et au plancher | |
| US6883748B2 (en) | Vehicles particularly useful as VTOL vehicles | |
| US20060113426A1 (en) | Vtol vehicles | |
| US8857755B2 (en) | Vertical/short take-off and landing passenger aircraft | |
| EP2928772B1 (fr) | Aéronef à décollage et atterrissage verticaux | |
| US20140151494A1 (en) | Vertical take-off and landing (vtol) aerial vehicle and method of operating such a vtol aerial vehicle | |
| WO2004031876A1 (fr) | Systeme de commande de vol pour aeronef a decollage et atterrissage verticaux (vtol) | |
| IL184520A (en) | Ducted fan vtol vehicles | |
| IL175265A (en) | Ducted fan vtol vehicles | |
| IL194985A (en) | Ducted fan vtol vehicles |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |
Effective date: 20221027 |