WO2017112983A1 - Aerial transportation device - Google Patents
Aerial transportation device Download PDFInfo
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- 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
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- WO
- WIPO (PCT)
- Prior art keywords
- displacement
- propellers
- turbines
- air
- lifting
- Prior art date
Links
- 238000006073 displacement reaction Methods 0.000 claims description 27
- 230000005540 biological transmission Effects 0.000 claims description 8
- 238000002485 combustion reaction Methods 0.000 claims description 3
- 230000009347 mechanical transmission Effects 0.000 claims description 2
- 239000007787 solid Substances 0.000 claims description 2
- 230000008901 benefit Effects 0.000 abstract description 4
- 238000010276 construction Methods 0.000 description 4
- 239000004065 semiconductor Substances 0.000 description 3
- 238000005339 levitation Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 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 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 238000001816 cooling 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
- 230000003028 elevating effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
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- 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
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- 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
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- 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.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Motorcycle And Bicycle Frame (AREA)
Abstract
The present invention belongs to the field of electric-eletronic entertainment devices, and was designed to achieve as its main advantage in comparison with the known prior art devices the possibility to move over any ground, dispensing with a specific or previously prepared contact surface, since the movement is obtained by propulsion means comprising propellers and turbines that lift the device on an air stream.
Description
DISPOSITIVO DE DESLOCAMENTO AÉREO AIR DISPLACEMENT DEVICE
CAMPO DA INVENÇÃO FIELD OF INVENTION
[0001 ]O presente invento pertence ao campo dos dispositivos eletro-eletrônicos para entretenimento, trazendo como principal vantagem em relação aos dispositivos conhecidos no estado da técnica, o fato de se deslocar sobre qualquer terreno, com controle total de voo executado pelo usuário, não precisando de uma superfície de contato específica ou previamente preparada, bem como não emprega alta quantidade de produtos semicondutores ou químicos. 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.
SUMÁRIO DO INVENTO SUMMARY OF THE INVENTION
[0002]O presente invento pertence ao campo dos dispositivos de deslocamento para fins de entretenimento, que incluem skates e pranchas das mais diversas conformações. São conhecidas no estado da técnica diversas formas de deslocamento para fins de entretenimento, sendo as mais simples o skate, como já mencionado, e as mais sofisticadas são sistemas de levitação em uma superfície especialmente preparada para este fim. 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.
[0003]Estes sistemas de levitação em uma superfície preparada para este fim compreende uma prancha capaz de se elevar por meio de um campo magnético e se deslocar linearmente através de uma fonte propulsora externa. No entanto, essa construção apresenta uma série de inconvenientes e desvantagens, sendo o maior dele o fato de demandar um terreno previamente preparado com ligas que geram campos magnéticos, como por exemplo, imãs. Em outras formas construtivas, há necessidade que a prancha que se elevará contenha materiais semicondutores que dependem de sistemas de refrigeração para que em combinação com a superfície previamente preparada seja elevado. These levitation systems on a surface prepared for this purpose comprise a board capable of elevating by means of a magnetic field and moving linearly through an external propelling source. However, this construction has a number of drawbacks and drawbacks, the biggest one being that it requires previously prepared terrain with alloys that generate magnetic fields, such as magnets. In other constructive forms, the rising board needs to contain semiconductor materials that depend on cooling systems so that in combination with the previously prepared surface it is raised.
[0004]Nesta última forma de construção mencionada, os semicondutores empregados são muito caros e seus recipientes devem ser blindados, o que gera um alto custo e complexibilidade tanto para a construção como na manutenção do referido dispositivo. In the latter mentioned construction, the semiconductors employed are very expensive and their containers must be shielded, which generates a high cost and complexity for both the construction and maintenance of said device.
[0005]Assim, é objetivo do presente invento a provisão de um dispositivo de deslocamento aéreo auto propelido que tenha sua propulsão por meio de fontes mecânicas que garantam maior segurança e um menor custo, tanto de fabricação como de manutenção.
[0006]É ainda objetivo do presente invento a provisão de um dispositivo para deslocamento aéreo de autoequilíbrio que se adapte a qualquer superfície, independente de preparação prévia. [0005] Thus, it is an object of the present invention to provide a self-propelled air displacement device which is propelled by mechanical sources to ensure greater safety and lower manufacturing and maintenance costs. It is a further object of the present invention to provide a self-balancing air displacement device that fits any surface, regardless of prior preparation.
[0007]É finalmente, objetivo do presente invento a provisão de um dispositivo de deslocamento aéreo que seja de fácil operação, manutenção e custos competitivos. It is finally an object of the present invention to provide an air displacement device which is easy to operate, maintain and cost competitive.
[0008]Estas e outras vantagens e benefícios acima citados são alcançados pela provisão de um dispositivo de deslocamento aéreo, composto por um corpo, maciço ou não, o qual tem formato de uma prancha ou outra geometria conhecida e adequada, sendo que dita prancha comporta próximo as suas porções marginal dois orifícios que recebem um meio de elevação e propulsão através de um sistema de hélices ou turbinas, que em um primeiro ciclo de trabalho elevam o dispositivo em relação ao solo a uma distância preestabelecida, em ato contínuo para obter o deslocamento em trajetória linear, provendo a flutuação da prancha e consequentemente de seu usuário. These and other advantages and benefits mentioned above are attained by the provision of 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.
[0009]De acordo com a invenção ora proposta, as turbinas ou hélices recebem transmissão mecânica de uma árvore de transmissão de força. Dita árvore obtém um fluxo de transmissão através de uma fonte motora, que pode ser um ou mais motores a bateria ou a combustão, ramificando dito fluxo de força de modo a imprimir movimento nas hélices ou turbinas e prover o empuxo e a propulsão do dispositivo. According to the proposed invention, 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.
[0010]O dispositivo conta ainda, como será melhor descrito na configuração preferencial com meios de controle de auto equilíbrio e dirigibilidade através de sensores de altura e outras forma de monitoramento do dispositivo. 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.
BREVE DESCRIÇÃO DAS FIGURAS BRIEF DESCRIPTION OF THE FIGURES
[001 1 ]O invento será melhor descrito com base nos desenhos anexos, dados a título exemplificativo nos quais: The invention will be further described based on the accompanying drawings, given by way of example in which:
A figura 01 representa uma vista em perspectiva do dispositivo de deslocamento aéreo, objeto do presente invento; Figure 01 is a perspective view of the air displacement device object of the present invention;
A figura 02 representa uma vista em perspectiva com detalhes da hélice ou turbina que propulsiona o dispositivo de deslocamento aéreo, objeto do presente invento;
A figura 03 representa uma vista em perspectiva do dispositivo de deslocamento aéreo, objeto do presente invento com as pás das turbinas ou hélices dispostas em diferentes ângulos. 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.
A figura 04 representa uma vista em perspectiva do dispositivo de deslocamento aéreo, objeto do presente invento ilustrando seus componentes internos incluindo seu sistema de transmissão ilustrando o fluxo de força mecânica. 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.
CONFIGURAÇÃO PREFERENCIAL PREFERRED CONFIGURATION
[0012]Com base nos desenhos acima descritos o presente invento compreende essencialmente um corpo (01 ) em formato de uma prancha ou outra geometria adequada, sendo que dito corpo é construído em polímeros de alta resistência e boa sustentação de peso ou outro material conhecido e adequado a este fim, de modo que em estágio de trabalho comporte um adulto mediano. Based on the drawings described above 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.
[0013]Estendendo-se longitudinalmente ao centro do corpo (01 ) estão dispostos pelo menos dois orifícios (02A-02B), sendo que ditos orifícios abrigam os dispositivos de elevação e deslocamento que serão melhor descritos mais a frente. Uma fonte de energia, preferencialmente uma bateria acionando também um ou mais motores elétricos ou motores a combustão e acionam uma árvore de transmissão de um fluxo de força mecânica ou elétrica. Dita árvore é composta por um eixo motor que está engrenado, seja através de um cardã ou de eixos flexíveis a uma caixa de transmissão de fluxo de força, composta por um redutor simples ou de múltiplas entradas (03A) instalado na porção mediana do dispositivo e dois eixos movidos (03B-03C) dispostos respectivamente à direita e a esquerda da mesma caixa de transmissão. Extending longitudinally to the center of the body (01) are arranged at least two holes (02A-02B), said holes housing the lifting and displacement devices that will be further described later. 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.
[0014]A união dos eixos para que recebam o fluxo de força mecânica pode se dar através de coroa e pinhão ou outra forma conhecida e adequada a este fim, como engrenagens de contato ou acoplamentos. Uma vez ramificado o fluxo de transmissão de força mecânica, os eixos se acoplam as hélices ou turbinas (04) instaladas no perímetro dos orifícios (02A-02B). Os eixos movidos (03B-03C) operativamente associados às hélices ou turbinas (04), em estágio de trabalho passam a imprimir movimento às mesmas, de forma que em um primeiro ciclo de trabalho as hélices ou turbinas (04) elevam o dispositivo sobre o solo em uma distância pré-determinada pelo usuário. Em ato contínuo passa a ocorrer o
deslocamento através do posicionamento das pás das hélices ou turbinas (04) em ângulo relativo a direção que o usuário quer se deslocar. 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. Once the mechanical force transmission flow is branched, the shafts engage the propellers or turbines (04) installed at the perimeter of the holes (02A-02B). The driven shafts (03B-03C) operatively associated with the propellers or turbines (04), in working stage, start to move them, so that in a first working cycle the propellers or turbines (04) lift the device over the ground at a distance predetermined by the user. In a continuous act, the displacement by positioning the propeller or turbine blades (04) at an angle relative to the direction the user wants to travel.
[0015]A elevação e o deslocamento se dá através dos impelidores constantes das hélices ou turbinas (4). Ditos impelidores em estágio de trabalho admitem o ar da atmosfera através dos orifícios (02A-02B) e provê a elevação e o deslocamento do dispositivo, sendo que a elevação se dá pelo deslocamento de ar gerado pelas hélices ou turbinas (04). A posição das hélices ou turbinas (04) é ajustada através de um motor de passo (não representado), dito motor de passo ou servos motores está associado a controles eletronicos que permitem o ajuste fino da posição do eixo das hélices ou turbinas no plano angular. [0015] 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. .
[0016]O controle da rotação dos motores de passo ou servo motores se dá através de um algoritmo associado a uma interface de controle que pode ser um botão, pedal ou qualquer forma de controle remoto com ou sem fios, inclusive joysticks, de forma que ao acioná-lo a direção de curso do dispositivo é alterada pela forma de admissão do ar nas pás das hélices ou turbinas (04). 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).
[0017]O algoritmo acima descrito conta ainda com informações obtidas através de sensores ou transdutores eletronicos de modo à sensorizar parâmetros como: altura do dispositivo em relação ao solo, velocidade de cruzeiro, deslocamento do corpo do usuário, autonomia entre outras que provêm ao usuário melhor dirigibilidade ao dispositivo e respostas mais rápidas aos comandos. 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.
[0018]Estas informações são obtidas pelos sensores, enviadas a um processador de dados ou microcontrolador, que provê sua gestão. Sendo que em alguns casos o algoritmo pode gerencia-las de maneira automatizadas, como por exemplo, informações obtidas por meio sensores de distância podem ser geridas pelo processador de dados, de modo a que se reduza a velocidade de cruzeiro do dispositivo na eminência de choque com algum obstáculo. 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.
[0019]Tendo descrita a configuração preferencial, fica claro que eventuais mudanças podem ocorrer como, por exemplo, nos componentes empregados em sua construção e nas formas de interface com o usuário sem que, contudo fuja do escopo das reivindicações que acompanham o presente relatório descritivo.
Having described the preferred embodiment, it is clear that any changes may occur such as, for example, the components employed in its construction and user interface forms without, however, departing from the scope of the claims accompanying this specification. .
Claims
1 . DISPOSITIVO DE DESLOCAMENTO AÉREO compreendendo um corpo em formato de uma prancha (01 ) de corpo maciço ou não sendo caracterizada por dito corpo (01 ) possuir pelo menos um orifício (02A) no qual está instalado um meio de elevação e deslocamento do corpo em formato de prancha (01 ), que pode ser uma turbina, hélice ou múltiplas pás (04), ou outro meio conhecido e adequado. 1 . AIR SHIFTING DEVICE comprising a body shaped like a solid body board (01) or not characterized in that said body (01) has at least one hole (02A) in which a body shaped lifting and displacement means is installed (01), which may be a turbine, propeller or multiple blades (04), or other known and suitable means.
2. DISPOSITIVO DE DESLOCAMENTO AÉREO de acordo com a reivindicação 01 é caracterizado pelo fato do meio de elevação e deslocamento através dos impelidores constantes das hélices ou turbinas (4), receber um fluxo de transmissão mecânica a partir de um ou mais motores elétricos ou a combustão (não representado), por meio de uma árvore de transmissão de fluxo de força mecânica um eixo cardã, sistemas de eixos flexíveis formados por um eixo motor (03), o qual ramifica o fluxo de transmissão por meio de pelo menos dois eixos movidos (03B-03C). Air displacement device according to claim 01, characterized in that the lifting and displacement means through the constant impellers of the propellers or turbines (4) receive a mechanical transmission flow from one or more electric motors or the combustion (not shown), by means of a mechanical force flow transmission spindle a cardan shaft, flexible shaft systems formed by a drive shaft (03), which branches the transmission flow by at least two driven shafts (03B-03C).
3. DISPOSITIVO DE DESLOCAMENTO AÉREO de acordo com a reivindicação 03 é caracterizado pelo fato dos meios de elevação e deslocamento, possuírem sistemas de ajustes do ângulo de ataque das pás das hélices ou turbinas (4) através de motores de passo ou servo-motores (não representado), e ou deslocamento do eixo de rotação das hélices ou turbinas (4) produzindo um empuxo direcionado de modo a ajustar o deslocamento do corpo (01 ) durante o estágio de trabalho. Air displacement device according to claim 03, characterized in that the lifting and displacement means have propeller or turbine blade (4) angle adjustment systems by means of stepping motors or servo motors ( not shown), and or displacement of the axis of rotation of the propellers or turbines (4) producing a thrust directed to adjust the displacement of the body (01) during the working stage.
4. DISPOSITIVO DE DESLOCAMENTO AÉREO de acordo com qualquer uma das reivindicações anteriores é caracterizado pelo fato do dispositivo possuir uma interface de controle através de um algoritmo, sendo que dito algoritmo dotado de um sistema de autoequilíbrio recebe através de um microcontrolador ou processador de dados às informações sensorizadas por sensores de altura, direção e deslocamento de modo que estas informações possam ser geridas alteradas através de meios como pedais, botões ou controles remotos com ou sem fios.
Air displacement device according to any one of the preceding claims, characterized in that the device has a control interface via an algorithm, said algorithm having a self-balancing system receiving via a microcontroller or data processor at the same time. information sensed by height, direction and displacement sensors so that this information can be managed changed through means such as pedals, buttons or wired or wireless remote controls.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/BR2015/050275 WO2017112983A1 (en) | 2015-12-30 | 2015-12-30 | Aerial transportation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/BR2015/050275 WO2017112983A1 (en) | 2015-12-30 | 2015-12-30 | Aerial transportation device |
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| Publication Number | Publication Date |
|---|---|
| WO2017112983A1 true WO2017112983A1 (en) | 2017-07-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/BR2015/050275 WO2017112983A1 (en) | 2015-12-30 | 2015-12-30 | Aerial transportation device |
Country Status (1)
| Country | Link |
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| WO (1) | WO2017112983A1 (en) |
Cited By (1)
| 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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| 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 (en) * | 2014-01-07 | 2015-07-16 | 4525612 Canada Inc. Dba Maginaire | Personal flight vehicle |
-
2015
- 2015-12-30 WO PCT/BR2015/050275 patent/WO2017112983A1/en active Application Filing
Patent Citations (3)
| 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 (en) * | 2014-01-07 | 2015-07-16 | 4525612 Canada Inc. Dba Maginaire | Personal flight vehicle |
Cited By (1)
| 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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