WO2017112983A1 - Dispositif de déplacement aérien - Google Patents

Dispositif de déplacement aérien Download PDF

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Publication number
WO2017112983A1
WO2017112983A1 PCT/BR2015/050275 BR2015050275W WO2017112983A1 WO 2017112983 A1 WO2017112983 A1 WO 2017112983A1 BR 2015050275 W BR2015050275 W BR 2015050275W WO 2017112983 A1 WO2017112983 A1 WO 2017112983A1
Authority
WO
WIPO (PCT)
Prior art keywords
displacement
propellers
turbines
air
lifting
Prior art date
Application number
PCT/BR2015/050275
Other languages
English (en)
Portuguese (pt)
Inventor
Danilo Azanha QUINONEZ
Original Assignee
Quinonez Danilo Azanha
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 Quinonez Danilo Azanha filed Critical Quinonez Danilo Azanha
Priority to PCT/BR2015/050275 priority Critical patent/WO2017112983A1/fr
Publication of WO2017112983A1 publication Critical patent/WO2017112983A1/fr

Links

Classifications

    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63C—SKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00—Roller skates; Skate-boards
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
    • B64C29/04—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded characterised by jet-reaction propulsion

Definitions

  • the present invention belongs to the field of electro-electronic entertainment devices, having as main advantage over the devices known in the state of the art, the fact that it travels over any terrain, with total flight control performed by the user, not needing a specific or pre-prepared contact surface, as well as not employing high quantity of semiconductor or chemical products.
  • the present invention belongs to the field of displacement devices for entertainment purposes, which include skateboards and boards of various shapes.
  • Various forms of entertainment displacement are known in the art, the simplest being skateboarding, as already mentioned, and the most sophisticated are levitation systems on a specially prepared surface.
  • an air displacement device consisting of a body, solid or not, which has the shape of a board or other known and suitable geometry, said board having near its marginal portions two holes that receive a means of lifting and propulsion through a system of propellers or turbines, which in a first cycle of work raise the device from the ground to a predetermined distance, continuously to obtain displacement. in linear trajectory, providing the fluctuation of the board and consequently of its user.
  • turbines or propellers receive mechanical transmission from a power transmission tree.
  • Said tree obtains a transmission flow through a motor source, which may be one or more battery or combustion engines, branching said force flow so as to imprint movement on the propellers or turbines and provide thrust and propulsion of the device.
  • a motor source which may be one or more battery or combustion engines
  • the device further counts, as will be better described in the preferred embodiment with self-balancing and steerability control means through height sensors and other forms of device monitoring.
  • Figure 01 is a perspective view of the air displacement device object of the present invention.
  • Figure 02 is a perspective view with details of the propeller or turbine propelling the air displacement device object of the present invention
  • Figure 03 is a perspective view of the air displacement device object of the present invention with turbine blades or propellers arranged at different angles.
  • Figure 04 is a perspective view of the air displacement device object of the present invention illustrating its internal components including its transmission system illustrating the flow of mechanical force.
  • the present invention essentially comprises a board-shaped body (01) or other suitable geometry, said body being constructed of high strength polymers and good weight bearing or other known material and suitable for this purpose, so that at work stage there is a medium adult.
  • a power source preferably a battery, also driving one or more electric motors or combustion engines and driving a transmission shaft of a mechanical or electrical force flow.
  • Said tree is composed of a drive shaft that is engaged, either through a cardan or flexible shafts to a power flow transmission box, consisting of a single or multiple input reducer (03A) installed in the middle portion of the device and two moved axes (03B-03C) arranged respectively to the right and left of the same gearbox.
  • Joining shafts to receive the flow of mechanical force can be by means of crown and pinion or other form known and suitable for this purpose, such as contact gears or couplings.
  • the shafts engage the propellers or turbines (04) installed at the perimeter of the holes (02A-02B).
  • the displacement by positioning the propeller or turbine blades (04) at an angle relative to the direction the user wants to travel.
  • Elevation and displacement take place through the constant impellers of the propellers or turbines (4).
  • Said impellers at work stage admit the air of the atmosphere through the holes (02A-02B) and provide the elevation and displacement of the device, and the elevation occurs by the displacement of air generated by the propellers or turbines (04).
  • the position of the propellers or turbines (04) is adjusted by a stepper motor (not shown), said stepper motor or servo motors is associated with electronic controls that allow fine adjustment of the position of the propeller or turbine shaft in the angular plane. .
  • Stepper or servo motor rotation is controlled by an algorithm associated with a control interface that can be a button, pedal or any form of wired or wireless remote control, including joysticks, so that When it is activated, the direction of travel of the device is altered by the air intake to the propeller or turbine blades (04).
  • a control interface can be a button, pedal or any form of wired or wireless remote control, including joysticks, so that When it is activated, the direction of travel of the device is altered by the air intake to the propeller or turbine blades (04).
  • the algorithm described above also has information obtained through sensors or electronic transducers in order to sensing parameters such as: height of the device in relation to the ground, cruising speed, displacement of the user's body, autonomy among others that provide the user. better device handling and faster response to commands.
  • This information is obtained by the sensors, sent to a data processor or microcontroller, which provides its management. Since in some cases the algorithm can manage them in an automated manner, for example, information obtained by means of distance sensors can be managed by the data processor, so that the device's cruising speed at shock imminence is reduced. with some obstacle.

Landscapes

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

Abstract

La présente invention relève du domaine des dispositifs électriques/électroniques de loisir, mis au point pour se caractériser avantageusement par rapport aux dispositifs connus dans l'état de la technique, par le fait de se déplacer sur n'importe quel terrain, sans qu'il soit nécessaire de disposer d'une surface de contact spécifique ou préalablement préparée, le déplacement s'opérant à l'aide de moyens de propulsion faisant intervenir des hélices et des turbines assurant sa sustentation par déplacement d'air.
PCT/BR2015/050275 2015-12-30 2015-12-30 Dispositif de déplacement aérien WO2017112983A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/BR2015/050275 WO2017112983A1 (fr) 2015-12-30 2015-12-30 Dispositif de déplacement aérien

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/BR2015/050275 WO2017112983A1 (fr) 2015-12-30 2015-12-30 Dispositif de déplacement aérien

Publications (1)

Publication Number Publication Date
WO2017112983A1 true WO2017112983A1 (fr) 2017-07-06

Family

ID=59224068

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/BR2015/050275 WO2017112983A1 (fr) 2015-12-30 2015-12-30 Dispositif de déplacement aérien

Country Status (1)

Country Link
WO (1) WO2017112983A1 (fr)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417896A (en) * 1943-08-10 1947-03-25 Charles H Zimmerman Helicopter flying apparatus
US20070034738A1 (en) * 2002-01-07 2007-02-15 Sanders John K Jr Aerodynamically stable, vtol aircraft
WO2015103700A1 (fr) * 2014-01-07 2015-07-16 4525612 Canada Inc. Dba Maginaire Véhicule volant personnel

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417896A (en) * 1943-08-10 1947-03-25 Charles H Zimmerman Helicopter flying apparatus
US20070034738A1 (en) * 2002-01-07 2007-02-15 Sanders John K Jr Aerodynamically stable, vtol aircraft
WO2015103700A1 (fr) * 2014-01-07 2015-07-16 4525612 Canada Inc. Dba Maginaire Véhicule volant personnel

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