WO2011131733A3 - Engin gyropendulaire à propulsion compensatoire et collimation de gradient fluidique, multi-milieux, multimodal, à décollage et atterrissage vertical - Google Patents

Engin gyropendulaire à propulsion compensatoire et collimation de gradient fluidique, multi-milieux, multimodal, à décollage et atterrissage vertical Download PDF

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Publication number
WO2011131733A3
WO2011131733A3 PCT/EP2011/056356 EP2011056356W WO2011131733A3 WO 2011131733 A3 WO2011131733 A3 WO 2011131733A3 EP 2011056356 W EP2011056356 W EP 2011056356W WO 2011131733 A3 WO2011131733 A3 WO 2011131733A3
Authority
WO
WIPO (PCT)
Prior art keywords
craft
gyropendular
landing
multimodal
vertical take
Prior art date
Application number
PCT/EP2011/056356
Other languages
English (en)
Other versions
WO2011131733A2 (fr
Inventor
Jean-Marc Desaulniers (Joseph)
Original Assignee
Desaulniers Jean-Marc Joseph
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 Desaulniers Jean-Marc Joseph filed Critical Desaulniers Jean-Marc Joseph
Priority to EP11729582.4A priority Critical patent/EP2601100A2/fr
Priority to US13/642,521 priority patent/US20130206915A1/en
Publication of WO2011131733A2 publication Critical patent/WO2011131733A2/fr
Publication of WO2011131733A3 publication Critical patent/WO2011131733A3/fr

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Classifications

    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/024Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/028Micro-sized aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/20Vertical take-off and landing [VTOL] aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/26Ducted or shrouded rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/29Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/293Foldable or collapsible rotors or rotor supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/29Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/296Rotors with variable spatial positions relative to the UAV body
    • B64U30/297Tilting rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/13Propulsion using external fans or propellers
    • B64U50/14Propulsion using external fans or propellers ducted or shrouded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00Undercarriages
    • B64U60/40Undercarriages foldable or retractable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00Undercarriages
    • B64U60/50Undercarriages with landing legs
    • B64U60/55Undercarriages with landing legs the legs being also used as ground propulsion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00Launching, take-off or landing arrangements
    • B64U70/80Vertical take-off or landing, e.g. using rockets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00Launching, take-off or landing arrangements
    • B64U70/80Vertical take-off or landing, e.g. using rockets
    • B64U70/83Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00Launching, take-off or landing arrangements
    • B64U70/80Vertical take-off or landing, e.g. using rockets
    • B64U70/87Vertical take-off or landing, e.g. using rockets using inflatable cushions

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Emergency Lowering Means (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

L'invention concerne un dispositif engin ou drone gyropendulaire pouvant évoluer dans les différents milieux physiques suivants: aérien, terrestre, maritime, sous -marin ou spatial, à décollage et atterrissage vertical, comprenant des groupes de propulsion supérieur et inférieur, muni d'un carénage annulaire accueillant un certain nombre de motorisations ou propulseurs à voilure ou à gaz asservies électroniquement, situées dans le prolongement de l'axe de celui-ci, montées sur rotules 3D à l'extrémité d'un certain nombre de tiges télescopiques, p. ex. réparties à 120° en périphérie du plateau et orientables selon les trois axes en fonction du plan de vol de l'engin multi -milieux multimodal, une structure vertébrale en guise corps central articulé 3D de forme cylindrique plein ou creux réalisant une fonction de stabilisation, de maintien de position et d'orientation, puis d'un plateau à disque rotatif inertiel muni en-dessous d'un habitacle de forme hémisphérique, en prolongement de la structure vertébrale, accueillant une charge utile ou applicative adaptée à différents domaines d'applications, p. ex. au secteur de la défense ou de la sécurité civile, afin de réaliser des fonctions de recherche et de sauvetage, d'exploration, de navigation, de transport, de surveillance de scènes, et de déploiement d'infrastructure de télécommunications en espace libre.
PCT/EP2011/056356 2010-04-22 2011-04-20 Engin gyropendulaire à propulsion compensatoire et collimation de gradient fluidique, multi-milieux, multimodal, à décollage et atterrissage vertical WO2011131733A2 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP11729582.4A EP2601100A2 (fr) 2010-04-22 2011-04-20 Engin gyropendulaire à propulsion compensatoire et collimation de gradient fluidique, multi-milieux, multimodal, à décollage et atterrissage vertical
US13/642,521 US20130206915A1 (en) 2010-04-22 2011-04-20 Vertical take-off and landing multimodal, multienvironment, gyropendular craft with compensatory propulsion and fluidic gradient collimation

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1001719 2010-04-22
FR1001719A FR2959208B1 (fr) 2010-04-22 2010-04-22 Engin gyropendulaire a propulsion compensatoire et collimation de gradient fluidique multi-milieux multimodal a decollage et atterrissage vertical

Publications (2)

Publication Number Publication Date
WO2011131733A2 WO2011131733A2 (fr) 2011-10-27
WO2011131733A3 true WO2011131733A3 (fr) 2011-12-29

Family

ID=43243169

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2011/056356 WO2011131733A2 (fr) 2010-04-22 2011-04-20 Engin gyropendulaire à propulsion compensatoire et collimation de gradient fluidique, multi-milieux, multimodal, à décollage et atterrissage vertical

Country Status (4)

Country Link
US (1) US20130206915A1 (fr)
EP (1) EP2601100A2 (fr)
FR (1) FR2959208B1 (fr)
WO (1) WO2011131733A2 (fr)

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