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

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/20—Vertical take-off and landing [VTOL] aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/55—UAVs specially adapted for particular uses or applications for life-saving or rescue operations; for medical use
    • B64U2101/58—UAVs specially adapted for particular uses or applications for life-saving or rescue operations; for medical use for medical evacuation, i.e. the transportation of persons or animals to a place where they can receive medical care
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
    • B64U2101/61—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for transporting passengers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/26—Ducted or shrouded rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/293—Foldable or collapsible rotors or rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/296—Rotors with variable spatial positions relative to the UAV body
    • B64U30/297—Tilting rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00—Undercarriages
    • B64U60/40—Undercarriages foldable or retractable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00—Undercarriages
    • B64U60/50—Undercarriages with landing legs
    • B64U60/55—Undercarriages with landing legs the legs being also used as ground propulsion
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/80—Vertical take-off or landing, e.g. using rockets
    • B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/80—Vertical take-off or landing, e.g. using rockets
    • B64U70/87—Vertical take-off or landing, e.g. using rockets using inflatable cushions

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Emergency Lowering Means (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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US20130206915A1 (en) 2013-08-15

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