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FR3109570A1 - Computer Assisted Motorized Air Vehicle - Google Patents

Computer Assisted Motorized Air Vehicle Download PDF

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Publication number
FR3109570A1
FR3109570A1 FR2002711A FR2002711A FR3109570A1 FR 3109570 A1 FR3109570 A1 FR 3109570A1 FR 2002711 A FR2002711 A FR 2002711A FR 2002711 A FR2002711 A FR 2002711A FR 3109570 A1 FR3109570 A1 FR 3109570A1
Authority
FR
France
Prior art keywords
computer
vehicle
propulsion system
aerial vehicle
assisted
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.)
Withdrawn
Application number
FR2002711A
Other languages
French (fr)
Inventor
Nicolas BANCE
Xavier François-Emmanuel Rosan André BEAUNOL
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR2002711A priority Critical patent/FR3109570A1/en
Publication of FR3109570A1 publication Critical patent/FR3109570A1/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/026Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
    • 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

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

Vamao est un véhicule aérien motorisé assisté d’un ordinateur destiné au transport de personnes et de marchandises. L’invention concerne un véhicule pouvant évoluer sur les voies terrestres en les survolant à une altitude inférieure à 10 mètres grâce à un système de propulsion composé de 4 hélices. Ainsi il peut éviter divers aléas des voies terrestres tel que les embouteillages, les routes fermées ce qui le rend plus pratique et efficace qu’une voiture. Il est constitué d’un système de propulsion avant (16) composé de deux hélices ; une supérieure et une inférieure et d’un système de propulsion arrière (18) similaire ; il est également constitué d’un habitacle (1) composé d’un siège pour l’utilisateur, d’un guidon (3), d’une tablette de contrôle (5). L’ordinateur central (4) contrôle le véhicule en totalité et il veille grâce au capteur de distance (14) situé en dessous de l’appareil que le véhicule ne dépasse pas l’altitude de 10 mètres. Le véhicule selon l’invention est particulièrement destiné au transport de personne et de marchandise mais peut également être utilisé à des fins militaires et de secours et autres.Vamao is a computer-assisted motorized aerial vehicle intended for the transport of people and goods. The invention concerns a vehicle that can operate on land routes by flying over them at an altitude of less than 10 meters thanks to a propulsion system composed of 4 propellers. Thus it can avoid various hazards of land routes such as traffic jams and closed roads, which makes it more practical and efficient than a car. It consists of a front propulsion system (16) composed of two propellers; an upper and a lower and a similar rear propulsion system (18); it also consists of a passenger compartment (1) composed of a seat for the user, a handlebar (3), a control tablet (5). The central computer (4) controls the entire vehicle and ensures, thanks to the distance sensor (14) located below the device, that the vehicle does not exceed an altitude of 10 meters. The vehicle according to the invention is particularly intended for the transport of people and goods but can also be used for military and emergency and other purposes.

Description

Véhicule aérien motorisé assisté par ordinateurComputer-aided motorized aerial vehicle

La présente invention concerne un véhicule aérien motorisé assisté par ordinateur de transport de personnes et marchandises par voie terrestre.The present invention relates to a computer-assisted motorized aerial vehicle for transporting people and goods by land.

Traditionnellement ce transport est assuré par les véhicules terrestres tel que les voitures, motocycles, camions mais ces déplacements peuvent être retardés ou compromis par des aléas tel que des embouteillages, des routes barrées.Traditionally, this transport is provided by land vehicles such as cars, motorcycles, trucks, but these trips can be delayed or compromised by hazards such as traffic jams, blocked roads.

Le véhicule selon l’invention permet de palier à ces aléas. Il se compose de trois parties : le système de propulsion avant se composant de deux hélices dont une sur rotor ainsi que leur support de protection dans lesquels sont placés les câbles ainsi que les divers capteurs, le support de protection supérieur contient deux rétroviseurs ; l’habitacle sur lequel est placé un siège, la tablette de commande centrale et un guidon. A l’intérieur de l’habitacle se trouve l’ordinateur central, le moteur, les batteries ainsi que toute la transmission. L’habitacle repose sur un châssis en métal, en dessous de l’habitacle se trouve un capteur de distance ; le système de propulsion arrière se composant de deux hélices, une supérieure et une inférieure dont une sur rotor ainsi que leur support de protection. Ainsi l’utilisateur à partir du guidon pourra contrôler l’altitude, le déplacement du véhicule en avant, en arrière, en rotation. L’ordinateur central permet à l’utilisateur de contrôler sa vitesse, son altitude, les éventuels dysfonctionnements, les informations utiles et affiche ces informations sur la tablette de commande. L’ordinateur s’occupe de faire le lien entre le rotor et le guidon. Aussi l’ordinateur central veille à corriger automatiquement l’altitude lorsque le capteur de distance indique une altitude supérieure à 10 mètres afin que l’utilisateur se trouve à moins de 10 mètres du sol.The vehicle according to the invention makes it possible to overcome these hazards. It consists of three parts: the front propulsion system consisting of two propellers, one of which is on a rotor, as well as their protective support in which the cables and the various sensors are placed, the upper protective support contains two mirrors; the passenger compartment on which is placed a seat, the central control tablet and a handlebar. Inside the cabin is the central computer, the engine, the batteries and the entire transmission. The passenger compartment rests on a metal frame, below the passenger compartment is a distance sensor; the rear propulsion system consisting of two propellers, one upper and one lower, one of which is on a rotor, as well as their protective support. Thus the user from the handlebars will be able to control the altitude, the movement of the vehicle forwards, backwards, in rotation. The central computer allows the user to control his speed, altitude, possible malfunctions, useful information and displays this information on the control tablet. The computer takes care of making the connection between the rotor and the handlebars. Also the central computer takes care to automatically correct the altitude when the distance sensor indicates an altitude higher than 10 meters so that the user is less than 10 meters from the ground.

Les dessins annexés illustrent l’invention :The accompanying drawings illustrate the invention:

La figure 1 est une représentation en coupe du véhicule. Figure 1 is a sectional representation of the vehicle.

La figure 2 est une représentation en coupe du véhicule sans le support de protection. Figure 2 is a sectional representation of the vehicle without the protective support.

La figure 3 est une représentation en coupe du véhicule séparée en partie. Figure 3 is a sectional representation of the vehicle separated in part.

La figure 4 est une représentation vue de côté d’une variante du véhicule. Figure 4 is a side view representation of a variant of the vehicle.

En référence à ces dessins, le véhicule comporte un habitacle (1) où l’utilisateur pourra s’asseoir à son siège (2). Ainsi depuis son siège il utilise le guidon (3) afin de contrôler l’altitude, la vitesse et la direction du véhicule. Les actions que l’utilisateur réalise sur le guidon est envoyé à l’ordinateur central (4). Aussi l’ordinateur central à en charge d’envoyer les informations utiles à la tablette de contrôle (5) qui affiche les informations à l’utilisateur. Lors de l’utilisation de l’appareil, les mouvements du véhicule demandées par l’utilisateur sont envoyé depuis le guidon vers l’ordinateur central qui lui envoie l’information au rotor (6) par des câbles se trouvant dans protection de l’arbre de rotation du moteur (7). Toute l’alimentation en énergie de l’appareil est fournie par le moteur électrique (8) qui fonctionne grâce à sa batterie principale (9) et sa batterie auxiliaire (10). Ainsi le moteur assure la rotation des quatre hélices grâce à l’arbre de rotation protégé dans sa protection (7) et le système de transmission (11).Afin d’éviter les risques de blessures les hélices sont entourées de supports de protection (12) qui eux contiennent des câbles, divers lumières ainsi que des capteurs d’obstacles; le support de protection avant supérieur a deux rétroviseurs (13).Les supports de protection inférieurs sont reliés à l’habitacle par les pièces du châssis (14) et les supports de protection arrières sont soutenus par des piliers (15) à l’intérieur desquels passeront les câbles d’alimentation et de connections aux capteurs. En dessous de l’habitacle se trouve le capteur de distance (16) qui permet de contrôler l’altitude par rapport au sol. De ce fait dès que l’altitude est supérieure à 10 mètres, le capteur envoie l’information à l’ordinateur central qui corrigera automatiquement l’inclinaison des pales (17) afin de réduire l’altitude. Ainsi il est possible de séparer l’invention en trois parties, le système de propulsion avant (18), l’habitacle (1) et le système de propulsion arrière (19). L’utilisateur bénéficie d’un espace de rangement à l’arrière du siège (20).With reference to these drawings, the vehicle comprises a passenger compartment (1) where the user can sit in his seat (2). So from his seat he uses the handlebars (3) to control the altitude, speed and direction of the vehicle. The actions that the user performs on the handlebars are sent to the central computer (4). Also the central computer in charge of sending useful information to the control tablet (5) which displays the information to the user. When using the device, the movements of the vehicle requested by the user are sent from the handlebars to the central computer which sends the information to the rotor (6) by cables located in the protection of the motor rotation shaft (7). All the power supply of the device is provided by the electric motor (8) which works thanks to its main battery (9) and its auxiliary battery (10). Thus the engine ensures the rotation of the four propellers thanks to the rotation shaft protected in its protection (7) and the transmission system (11). In order to avoid the risk of injury, the propellers are surrounded by protective supports (12 ) which contain cables, various lights and obstacle sensors; the upper front guard bracket has two mirrors (13). The lower guard brackets are connected to the passenger compartment by the chassis parts (14) and the rear guard brackets are supported by pillars (15) inside from which the power cables and connection cables to the sensors will pass. Below the passenger compartment is the distance sensor (16) which allows the altitude in relation to the ground to be checked. Therefore, as soon as the altitude is higher than 10 meters, the sensor sends the information to the central computer which will automatically correct the inclination of the blades (17) in order to reduce the altitude. Thus it is possible to separate the invention into three parts, the front propulsion system (18), the passenger compartment (1) and the rear propulsion system (19). The user has a storage space at the back of the seat (20).

Selon une variante non illustrée l’invention peut être dépourvue de capteur de distance.According to a variant not illustrated, the invention may be devoid of a distance sensor.

Le véhicule selon l’invention est particulièrement destiné au transport de personne et de marchandise.The vehicle according to the invention is particularly intended for the transport of people and goods.

Claims (6)

Un véhicule aérien motorisé assisté par ordinateur caractérisé en ce qu’il se compose d’un système de propulsion avant (18), arrière (19) et d’un habitacle (1).A motorized computer-assisted aerial vehicle characterized by comprising a front (18), rear (19) propulsion system and a cockpit (1). Un véhicule aérien motorisé assisté par ordinateur selon la revendication 1 caractérisé en ce que le système de propulsion avant se compose de deux hélices dont une sur rotor et le système de propulsion arrière se compose de deux hélices dont une sur rotor (6) qui sont pour les quatre rotors alimentés par un moteur (8) du véhicule.A computer-aided motorized aerial vehicle according to claim 1 characterized in that the forward propulsion system consists of two propellers, one of which is on a rotor, and the rear propulsion system consists of two propellers, one of which is on a rotor (6) which are for the four rotors powered by a motor (8) of the vehicle. Un véhicule aérien motorisé assisté par ordinateur selon la revendication 1 caractérisé en ce qu’un ordinateur central (4) contrôle l’ensemble des actions du véhicule et envoie les informations utiles à une tablette de commande (5).A computer-assisted motorized aerial vehicle according to claim 1 characterized in that a central computer (4) controls all the actions of the vehicle and sends useful information to a control tablet (5). Un véhicule aérien motorisé assisté par ordinateur selon la revendication précédente caractérisé en ce qu’un capteur de distance (16) est placé sous l’habitacle et qu’il empêche le véhicule d’atteindre une altitude supérieure à 10 mètres en envoyant l’information à l’ordinateur central.A computer-assisted motorized aerial vehicle according to the preceding claim, characterized in that a distance sensor (16) is placed under the passenger compartment and that it prevents the vehicle from reaching an altitude greater than 10 meters by sending the information to the central computer. Un véhicule aérien motorisé assisté par ordinateur selon la revendication 3 caractérisé en ce que les informations nécessaires à la conduite ainsi que les informations utiles à l’utilisateur sont affichés sur la tablette de commande (5).A motorized aerial vehicle assisted by computer according to claim 3 characterized in that the information necessary for driving as well as the information useful to the user are displayed on the control tablet (5). Un véhicule aérien motorisé assisté par ordinateur selon la revendication 2 précédentes caractérisé en ce que le moteur est alimenté par une batterie principale (9) ainsi que d’une batterie auxiliaire (10) pour l’alimenter en cas de déchargement de la batterie principale.A computer-assisted motorized aerial vehicle according to the preceding claim 2 characterized in that the motor is powered by a main battery (9) as well as an auxiliary battery (10) to power it in the event of discharge of the main battery.
FR2002711A 2020-04-27 2020-04-27 Computer Assisted Motorized Air Vehicle Withdrawn FR3109570A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2002711A FR3109570A1 (en) 2020-04-27 2020-04-27 Computer Assisted Motorized Air Vehicle

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2002711A FR3109570A1 (en) 2020-04-27 2020-04-27 Computer Assisted Motorized Air Vehicle
FR2002711 2020-04-27

Publications (1)

Publication Number Publication Date
FR3109570A1 true FR3109570A1 (en) 2021-10-29

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FR2002711A Withdrawn FR3109570A1 (en) 2020-04-27 2020-04-27 Computer Assisted Motorized Air Vehicle

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FR (1) FR3109570A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12168510B2 (en) 2023-02-07 2024-12-17 Hunter William KOWALD Compact personal flight vehicle

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050230524A1 (en) * 2003-10-24 2005-10-20 Toyota Jidosha Kabushiki Kaisha Vertical take-off and landing aircraft
US20070034738A1 (en) * 2002-01-07 2007-02-15 Sanders John K Jr Aerodynamically stable, vtol aircraft
US20140158816A1 (en) * 2012-12-07 2014-06-12 Delorean Aerospace, Llc Vertical Takeoff and Landing Aircraft
CA2844721A1 (en) * 2014-03-05 2015-09-05 Catalin Alexandru Duru Un aeronef en forme de plateforme capable de transporter un pilote, procedes de fabrication et utilisations associes
WO2016142555A1 (en) * 2015-03-12 2016-09-15 Martinez Gil Francisco Flying motorcycle
US20170174335A1 (en) * 2014-03-27 2017-06-22 Malloy Aeronautics, Ltd. Rotor-lift aircraft

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070034738A1 (en) * 2002-01-07 2007-02-15 Sanders John K Jr Aerodynamically stable, vtol aircraft
US20050230524A1 (en) * 2003-10-24 2005-10-20 Toyota Jidosha Kabushiki Kaisha Vertical take-off and landing aircraft
US20140158816A1 (en) * 2012-12-07 2014-06-12 Delorean Aerospace, Llc Vertical Takeoff and Landing Aircraft
CA2844721A1 (en) * 2014-03-05 2015-09-05 Catalin Alexandru Duru Un aeronef en forme de plateforme capable de transporter un pilote, procedes de fabrication et utilisations associes
US20170174335A1 (en) * 2014-03-27 2017-06-22 Malloy Aeronautics, Ltd. Rotor-lift aircraft
WO2016142555A1 (en) * 2015-03-12 2016-09-15 Martinez Gil Francisco Flying motorcycle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12168510B2 (en) 2023-02-07 2024-12-17 Hunter William KOWALD Compact personal flight vehicle

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