WO2017136906A1 - Sac à dos à ailes dirigeables pour vol individuel - Google Patents

Sac à dos à ailes dirigeables pour vol individuel Download PDF

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Publication number
WO2017136906A1
WO2017136906A1 PCT/BR2016/000047 BR2016000047W WO2017136906A1 WO 2017136906 A1 WO2017136906 A1 WO 2017136906A1 BR 2016000047 W BR2016000047 W BR 2016000047W WO 2017136906 A1 WO2017136906 A1 WO 2017136906A1
Authority
WO
WIPO (PCT)
Prior art keywords
flight
backpack
envelope
new
innovating
Prior art date
Application number
PCT/BR2016/000047
Other languages
English (en)
Portuguese (pt)
Inventor
Gilberto DE ALMEIDA FREITAS FILHO
Original Assignee
De Almeida Freitas Filho Gilberto
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 De Almeida Freitas Filho Gilberto filed Critical De Almeida Freitas Filho Gilberto
Publication of WO2017136906A1 publication Critical patent/WO2017136906A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • 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
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes

Definitions

  • This patent application aims to innovate people's means of transport and air travel by means of a one-way backpack! with centralized vertical frame and horizontally sized wings measured to the weight of the passenger.
  • the aerodynamically shaped envelope filled with helium gas that is coupled to the container along with its clean energy propulsion engine and engine makes it a new way to get around with total control and safety.
  • the state of the art comprises an aerodynamically shaped backpack formed of special fabrics (textiles) already used in the aeronautics sector for cargo airships, which are filled with helium gas, and has a temperature control system (balloon). ) automatic, electric control valves, so that the traveler can control from two electric buttons their altitude accurately, safely and easily, ejecting or storing (compressing) the gas in the reservoir cylinder that is in the container connected between the backpack and the Helium gas envelope, the function of which is to store and protect apparatus and the engine with clean energy.
  • This engine is essentially a hybrid propeller paramotor engine adapted to the Hydrogen Kit, compressed air or rechargeable lithium-ion batteries, which are the new renewable forms of energy, where it can be adapted and chosen by each person according to their own needs. need and weight.
  • Helium gas being a noble and non-flammable gas, has qualities to be used safely and successfully and can be stored and reused.
  • the object of the present patent is a backpack with vertical extension separated by 3 main layers, which are:
  • the (3rd) third-layer envelope is that stores helium gas, divided by cells that form its aerodynamic design with wings and cuff coupled internally to control its temperature and altitude.
  • Fig. 2 shows in side perspective aiming at its working parts.
  • Fig. 3 shows in front perspective aiming at the continuation of the operating parts.
  • Fig. 4 shows in top perspective (top to bottom) showing inner layers and the last two operating parts.
  • Fig. 5 shows Bottom-up (bottom-up) perspective showing the ratio of frame size to pilot as weight and proportional size calculations for each traveler.
  • Its yellow construction (1) represents the carbon fiber nozzle and rods which serve to shape and stiffen the strategic points of the envelope and also indicated on the wings as anchor points.
  • Figure (2) indicating the side air intakes, one on each side, where they join at the tail end directing the relative wind that decreases the drag of the aerodynamic structure, in Figure (3) are the aerodynamic lateral wings, which serve for maneuvers. , flight and landing curves, as shown in the sectional side drawing with spherical hollow internal cells for the division of helium gas between the wings.
  • Indication (4) shows the two main areas of the largest space filled with helium gas that divides between the wings; Indication (5) represents the internal space that the relative wind travels through the air inlet; (6) indicates the central air flow outlet at the tail end of the airship structure to reduce envelope drag and improve center of vertical trunk balance and wing turn maneuvers;
  • the call sign (7) represents the rear center carbon fiber rod with rubberized cover for protection and envelope support; (8) indicates the engine protection cage and propellers that will generate horizontal propulsion with minor angle adjustments assisting flight and landing displacement;
  • Indication (9) represents the hydrogen cell powered electric motor or hydrogen kit adaptable to conventional engines, and the lithium battery electric or compressed air motor which can be mounted according to the calculations. of the total weight of the equipment and the pilot, thus determining its power to propel the structure.
  • Indicative (10) are the suspension arms to support the weight of the container; the (11) indicates that the reserve parachute is stored and coupled to the backpack (I layer) in cases of loss of control of the container or envelope, which may be ejected from it and thus be triggered automatically reserves the parachute; indication (12) refers to knee support with adjustment and positioning lock; (13) represented in the green part is the Air-Bag for different cases of accidents, which has the speed and approach sensor that triggers if the spare parachute is not activated or in situations of frontal, lateral and vertical collision; Indicative (14) are the high-range headlights to assist in night flights or in times of low visibility; (15) represents the instrument holder on which the smartphone is coupled (where it will have access to flight aid applications) and other instruments for measuring and locating this flight practice; (16) indicates the side padding with seat belts where the container is attached to the rucksack for support of the rider and is also the same point where it ejects and separates the envelope next to the container from the backpack,
  • the indications (17) are representative figures of seat belt inserts; (18) represents the hydrogen kit where the generator hydrolyses the water next to the soluble thus transforming the fossil combustion of gasoline into a clean energy combustion, besides generating more autonomy and power to the engine that represents in this design model; (19) represents the electric valves, connected to the compressor and the battery that divide the gas transportation, one valve transfers helium gas from the cylinder to the envelope and vice versa, and the second valve drives the cuff by injecting hot air or air. cold to control the internal temperature of the envelope together; Figure 20 shows the internal cuff connected to the sensor that measures the internal temperature of the Helium gas, which in turn triggers the device that releases hot or cold air inside the cuff for envelope and gas temperature control.
  • the indicative (21) represents the high strength anchor lines of the central envelope structure; the lines that anchor the wings on the support arm (24) so that maneuvers and turns can be performed, and with positioning locks, where the pilot can adjust wing angles for safe landing in smaller spaces, is represented by the indicative (22);
  • Figure (23) refers to the two altitude control knobs either injecting with the (yellow) button or pressing with the (green) button to control the rise and fall of the entire structure;
  • (24) represents the support arms that serve to maneuver the wings for positioning and locking, and rest for the pilot's arms;
  • reference (25) indicates the airbag sensor that determines its activation from the speed and approach of some object;
  • (26) are the two buttons, indicated by the colors red and blue, where the red button turns the engine on and off, and the blue button accelerates the engine, generating horizontal propulsion;
  • (27) indicated by the yellow color in the figure represents the carbon fiber keels, which cut the wind, giving better grip to the wings, where the final lines that produce the directional curve of the pilot are

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

Le présent brevet d'invention vise à innover la locomotion des personnes au moyen du vol libre unidirigeable avec les nouvelles technologies, en utilisant des énergies propres pour la propulsion. Un nouveau concept de locomotion aérienne individuelle permet d'innover non seulement le moyen de transport, mais aussi le tourisme, et d'aider divers secteurs dans la société, tels que le domaine de la santé, l'environnement, l'agriculture et la sécurité, outre le fait de générer de nouveaux emplois et d'innover divers commerces nationaux et internationaux. La technologie utilisée nous permet d'utiliser un moyen de transport durable et accessible. La disposition de cette demande consiste en un projet visant à proposer un concept différencié de locomotion durable, offrant une excellente expérience de bien-être aux personnes, améliorant leur qualité de vie et l'interaction avec l'environnement, changeant leur quotidien vers une nouvelle perception, avec sensation de liberté dans leur transport et avec une totale sécurité en termes d'équipement.
PCT/BR2016/000047 2016-02-12 2016-04-22 Sac à dos à ailes dirigeables pour vol individuel WO2017136906A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BR102016003046 2016-02-12
BRBR102016003046 2016-02-12

Publications (1)

Publication Number Publication Date
WO2017136906A1 true WO2017136906A1 (fr) 2017-08-17

Family

ID=59562845

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/BR2016/000047 WO2017136906A1 (fr) 2016-02-12 2016-04-22 Sac à dos à ailes dirigeables pour vol individuel

Country Status (1)

Country Link
WO (1) WO2017136906A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11155350B2 (en) 2019-08-20 2021-10-26 Carl Kuntz Personal flight vehicle having a helium backpack
WO2023023828A1 (fr) * 2021-08-24 2023-03-02 De Almeida Freitas Filho Gilberto Drone planeur pourvu d'un ballon dirigeable pour vol personnel, doté de modes automatique et manuel

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04254296A (ja) * 1991-02-01 1992-09-09 Takashi Ikeda パラグライダー
JPH07285497A (ja) * 1994-04-18 1995-10-31 Kunihide Miyake モーターバルーングライダー
US20020134890A1 (en) * 2001-03-26 2002-09-26 Leonid Berzin Parachute with a controlled active lift
WO2011002517A2 (fr) * 2009-07-03 2011-01-06 Jon Kunowski Système de vol individuel à turbine
US20110198437A1 (en) * 2010-02-12 2011-08-18 Lyle Marvin Tweet Helium rocket aerochute

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04254296A (ja) * 1991-02-01 1992-09-09 Takashi Ikeda パラグライダー
JPH07285497A (ja) * 1994-04-18 1995-10-31 Kunihide Miyake モーターバルーングライダー
US20020134890A1 (en) * 2001-03-26 2002-09-26 Leonid Berzin Parachute with a controlled active lift
WO2011002517A2 (fr) * 2009-07-03 2011-01-06 Jon Kunowski Système de vol individuel à turbine
US20110198437A1 (en) * 2010-02-12 2011-08-18 Lyle Marvin Tweet Helium rocket aerochute

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11155350B2 (en) 2019-08-20 2021-10-26 Carl Kuntz Personal flight vehicle having a helium backpack
WO2023023828A1 (fr) * 2021-08-24 2023-03-02 De Almeida Freitas Filho Gilberto Drone planeur pourvu d'un ballon dirigeable pour vol personnel, doté de modes automatique et manuel

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