WO2020116925A1 - Appareil de charge de batterie pour moyen mobile - Google Patents

Appareil de charge de batterie pour moyen mobile Download PDF

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Publication number
WO2020116925A1
WO2020116925A1 PCT/KR2019/016995 KR2019016995W WO2020116925A1 WO 2020116925 A1 WO2020116925 A1 WO 2020116925A1 KR 2019016995 W KR2019016995 W KR 2019016995W WO 2020116925 A1 WO2020116925 A1 WO 2020116925A1
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WIPO (PCT)
Prior art keywords
solar panel
wing
folded
propeller
folding
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PCT/KR2019/016995
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English (en)
Korean (ko)
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이정용
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이정용
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Publication date
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Publication of WO2020116925A1 publication Critical patent/WO2020116925A1/fr

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/31—Supply or distribution of electrical power generated by photovoltaics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K16/00—Arrangements in connection with power supply of propulsion units in vehicles from forces of nature, e.g. sun or wind
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L50/00—Electric propulsion with power supplied within the vehicle
    • B60L50/50—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells
    • B60L50/60—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L8/00—Electric propulsion with power supply from forces of nature, e.g. sun or wind
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L8/00—Electric propulsion with power supply from forces of nature, e.g. sun or wind
    • B60L8/003—Converting light into electric energy, e.g. by using photo-voltaic systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62M—RIDER PROPULSION OF WHEELED VEHICLES OR SLEDGES; POWERED PROPULSION OF SLEDGES OR SINGLE-TRACK CYCLES; TRANSMISSIONS SPECIALLY ADAPTED FOR SUCH VEHICLES
    • B62M6/00—Rider propulsion of wheeled vehicles with additional source of power, e.g. combustion engine or electric motor
    • B62M6/40—Rider propelled cycles with auxiliary electric motor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62M—RIDER PROPULSION OF WHEELED VEHICLES OR SLEDGES; POWERED PROPULSION OF SLEDGES OR SINGLE-TRACK CYCLES; TRANSMISSIONS SPECIALLY ADAPTED FOR SUCH VEHICLES
    • B62M6/00—Rider propulsion of wheeled vehicles with additional source of power, e.g. combustion engine or electric motor
    • B62M6/80—Accessories, e.g. power sources; Arrangements thereof
    • B62M6/90—Batteries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/40—Balloons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C33/00—Ornithopters
    • B64C33/02—Wings; Actuating mechanisms therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/30—Aircraft characterised by electric power plants
    • B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
    • B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S20/00—Supporting structures for PV modules
    • H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S30/00—Structural details of PV modules other than those related to light conversion
    • H02S30/20—Collapsible or foldable PV modules
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
    • H02S40/20—Optical components
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
    • H02S40/30—Electrical components
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60Y—INDEXING SCHEME RELATING TO ASPECTS CROSS-CUTTING VEHICLE TECHNOLOGY
    • B60Y2200/00—Type of vehicle
    • B60Y2200/50—Aeroplanes, Helicopters
    • B60Y2200/51—Aeroplanes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/50—Photovoltaic [PV] energy
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/80—Technologies aiming to reduce greenhouse gasses emissions common to all road transportation technologies
    • Y02T10/90—Energy harvesting concepts as power supply for auxiliaries' energy consumption, e.g. photovoltaic sun-roof
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Definitions

  • the present invention relates to a battery charging device for a moving vehicle, and more specifically, a solar panel is formed on one side of a wing that is folded and unfolded by a hinge coupling, and is installed on a drone, a ship, an electric bicycle, an electric kickboard, and a vehicle, and photovoltaic. It relates to a battery charging device for a vehicle that can be used by converting energy into electrical energy.
  • the background technology of the present invention is a folding solar cell and a wing to which Bernoulli's theorem is applied.
  • a solar cell is a device that converts solar light into electrical energy. It is already an old technology for cars to run on the road and boats to cross the sea using these devices.
  • the airplane developed by Kuwano was designed on the basis of a man-powered airplane (a light aircraft that flies on the pedals with the power of a person), so it has a light weight.
  • the total length of the body of the airplane was 7m and the width of the main wing was 17.5m.
  • Most of the cockpits were made of hard and light carbon fiber, except for using glass fibers in a part of the cockpit. Here, only 1.5 kg of flexible amorphous silicon solar cells are attached.
  • the plane was named Dandelion Lake (Sun Seeker in English).
  • the battery had a capacity capable of supplying a current of 20A to the motor for about 10 minutes.
  • the Dandelion Lake takes off and rises from an altitude of 100 m to 300 m, then slowly rotates using the energy produced by the solar cell and rises from 600 m to 4,000 m in an ascending air stream. After that, you go straight down the altitude and fly in the sky again.
  • the Dandelion flight also departed from Wilcox, Arizona, on August 4, and successfully arrived in Kitty Hawk, North Carolina, on September 3, making its second flight.
  • the total flight distance was 4,000 km.
  • the highest altitude of the solar cell airplane was 3,900 m, and the flight time was 7 hours and 35 minutes, which was a new world record.
  • Paraline C is a material used to coat electronic products or machinery, and serves to prevent moisture and dust from the outside.
  • the research team observed that the surface of Paralin C was smoother than other plastics using a microscope, and used it to make a solar cell with a thickness of 2 ⁇ m (micrometer. 1 ⁇ m is 1 millionth of a meter). As a result of actual experiments, this solar cell showed almost the same performance as a conventional solar cell made of glass.
  • the SRB separates from 47,000 meters and the spacecraft flies on its own power.
  • a spectacular moment for rocket scientists the spacecraft now flies into orbit and SRB reenters the Earth's atmosphere. Diving from space to Earth at a high altitude of 400 kilometers per hour, free fall for 153 seconds. At such speeds, the sea level will feel as hard as concrete. Therefore, the parachute is unfolded to reduce the rocket's falling speed to 80 kilometers per hour. Captains and crews who will pull them out of the sea for recycling wait while tracking the rocket. SRB's re-entry into the atmosphere is as exciting as launch for them. With a tumultuous landing, a diving team is dispatched to SRB 1, which has been acquired at sea at high speed, and the status of the SRB soaring above the water surface, such as an iceberg, is checked.
  • the present invention functions as a transportation means in which a drone carries or moves a courier or a person as a transportation means. Since there are problems and difficulties in long-distance transportation, it is intended to provide sufficient electric charging devices and methods for long-distance movement of drones, ships, electric bicycles, electric kickboards, and automobiles.
  • the wings are formed to be very long, which can cause the aircraft to weigh too much.
  • the challenge is to popularize airplanes flying with solar cells.
  • the present invention to solve the above problems
  • the wings attached to the solar panel can be folded or folded by hinges to take off and land vertically.
  • the solar panel is unfolded as the wing is unfolded
  • the solar panel supplies electricity to the sub-motor while charging the secondary battery provided on one side of the sub-motor, so that the propeller connected to the sub-motor rotates to fly,
  • the propeller is to provide a battery charging device for a moving means, characterized in that it rotates 90 degrees using a servo motor as a driving means to become a forward type.
  • the folding that connects the node of the solar panel to the hinge, or the node is sequentially opened at the beginning of the wing, and the opened wing is folded back to the beginning of the wing.
  • a solar panel is attached to the wing and is formed on one side of the ship,
  • the solar panel is opened and folded on one side of the ship so that it folds and folds, and when entering, the solar panel is folded, and when charging is required in a large space after departure, the solar panel is unfolded.
  • the battery charging device for a vehicle to enable In the battery charging device for a vehicle to enable,
  • the sub-motor which is a driving means disposed on one side of the wing, expands the solar panel according to the unfolding of the wing, and the secondary battery provided on one side of the sub-motor is charged to supply electricity to the ship,
  • a buoyancy means toward the water surface may be formed to support the weight of the solar cell.
  • a drone formed inside the rocket booster is provided when it is formed and recovered inside the rocket booster, and one or more joints or arms formed by folding are extended, and the arm A propeller is formed on one side so that the cover is formed so as not to receive air resistance on the outside of the drone.
  • the rocket booster is formed inside the rocket booster and when recovered, it is formed inside the rocket booster.
  • the beginning of the original wing is formed and the nodes are sequentially from the beginning.
  • a servo motor as a driving means, expand the solar panel and charge the secondary battery by the solar cell, supply electricity to the motor, rotate the propeller to fly,
  • the propeller is rotated 90 degrees using a servo motor to form a forward type or a propeller in which a motor and a propeller are integrated on one side of the solar panel, and the folding plate on which the solar panel is formed is convex, and lift is generated by Bernoulli's principle. It can be characterized by.
  • one or more folding arms are formed on one or more sides of an electric bicycle, an electric kickboard, an electric wheel, or a bicycle, and a propeller is formed at the ends thereof, so that the folding arms are lifted during takeoff and flight.
  • a propeller is formed at the ends thereof, so that the folding arms are lifted during takeoff and flight.
  • the nodes are sequentially opened, and the wings are folded back to the beginning of the wings, where a solar panel is attached to the wing or a folding solar panel is formed, such as an electric bicycle, an electric kickboard, an electric wheel, or one side of a bicycle. It is formed above, and when it reaches a certain altitude by taking off, it can be characterized by spreading the wings formed with the solar panel or the solar panel and charging the secondary battery by the solar cell to supply electricity to the motor and rotate the propeller to fly. .
  • the portion where sunlight enters the upper portion of the hot air balloon is formed of a transparent material, and the lower portion is formed of a material such as black that can absorb and radiate sunlight well.
  • One or more vents are formed to discharge the electricity.
  • electricity is charged to the secondary battery by a solar cell or a control back element, and heating means such as a Peltier element at a time when sunlight is not emitted by the secondary battery.
  • Hot air balloon using the greenhouse effect characterized in that is operated by the radio control
  • a foldable solar panel or a foldable solar panel wing is formed, and when taking off, it takes off only by the greenhouse effect, or by a motor and a propeller, or by a greenhouse effect and a motor and a propeller. It is a fold that is connected by
  • Folded solar panel or foldable solar panel is formed by folding the folding solar panel or the folded solar panel to open the solar cell. It can be characterized by supplying electricity to a thermoelectric element or a propeller to a hot air balloon using the greenhouse effect while charging the secondary battery.
  • the wing portion to which the solar panel is attached is formed to be foldable, and the folding and unfolding expression in which the nodes of the solar panel are connected by hinges or the node to the beginning of the wings are sequentially
  • the solar cell formed at the end of the fan spreads out in a circular shape and the center of the fan that is folded moves from the center of the air vehicle, and the fan is exposed to the outside.
  • the center of the fan moves to the center of the air vehicle and the fan expands, and when folded, the solar panel is unfolded. It can be characterized in that the fan shape is not exposed.
  • a foldable solar panel rotating part is formed on a roof panel of a vehicle, the solar panel is folded in response to one-way rotation of the rotating part, and when folded forward, the folded part faces the front side, and is parked.
  • the rotating part rotates in the other direction so that the folded part is stretched toward the side to charge, and is formed to cover the window of the car.
  • the rotating part may be characterized in that the fixing part is formed such that the folding solar panel faces the front or side of the vehicle.
  • the folding that connects the node of the solar panel to the hinge, or the node is sequentially opened at the beginning of the wing, and the opened wing is folded back to the beginning of the wing.
  • a solar panel is attached to the wing and is formed on one side of the ship,
  • the solar panel is opened and folded on one side of the ship so that it folds and folds, and when entering, the solar panel is folded, and when charging is required in a large space after departure, the solar panel is unfolded.
  • the battery charging device for a vehicle to enable In the battery charging device for a vehicle to enable,
  • At least one support of one or more solar panels is formed at the bottom of the solar panel, and at the end of the support, wheels are formed or wheels are formed integrally with an electric motor to form a number of solar panels with support, which are opened and closed by opening and closing. It can be characterized by being closed.
  • a rail may be formed on one side of a hull such as a deck at the bottom of the wheel.
  • the submarine or drone submarine is connected by a connecting means with a submarine when it is submerged or not, and is driven by a submotor driving means that floats on the surface by buoyancy means. It may be characterized in that a folding and unfolding foldable solar panel is formed.
  • the folding solar panel that is folded and unfolded by the driving means of the sub-motor connected by the connecting means with the submarine and floated on the surface by the buoyancy means has one or more motors. It can be characterized in that the thrust generating device is formed.
  • the drive is folded and unfolded by a driving means such as a sub-motor that floats on the surface by buoyancy means, such as when a submarine or a drone submarine dives or does not dive.
  • a driving means such as a sub-motor that floats on the surface by buoyancy means, such as when a submarine or a drone submarine dives or does not dive.
  • the foldable solar panel is formed by thrust generating device by one or more motors, and is characterized in that the secondary battery of the submarine is wirelessly charged to the submarine by the foldable solar panel and the ultrasonic wireless power transmitting and receiving device formed in the submarine. can do.
  • a folding blade is formed, a hole is formed on one side of the folding blade, a motor and a propeller are formed inside the hole, and the portion outside the hole is a solar cell It may be characterized in that to be attached.
  • a folding blade is formed instead of a propeller integrated with a drone arm and a motor on one side of an electric bicycle, an electric kickboard, an electric wheel, or a bicycle, and a hole is formed on one side of the folding blade.
  • a motor and a propeller are formed inside the hole, and a portion of the outside of the hole may be characterized in that a solar cell is attached.
  • the buoyancy means is formed with a support for the solar cell so as to be positioned at an appropriate height above the water surface at the end of the solar cell, and at the bottom of the support so as to be positioned at an appropriate height above the water surface. It can be characterized in that the buoyancy means is formed.
  • a hydrofoil-type plate is formed at the lower portion of the buoyancy means so that the end of the solar panel rises to a certain height when the ship speeds integrally with the support, regardless of the waves below the water surface. It may be characterized in that the angle adjustment means is formed to adjust the angle of the hydrofoil-type plate so that the end of the solar cell is maintained at a constant height.
  • the buoyancy means is formed with a support for the solar cell so as to be positioned at an appropriate height above the water surface at the end of the solar cell, and at the bottom of the support so as to be positioned at an appropriate height above the water surface. It can be characterized in that the buoyancy means is formed.
  • the battery charging device for a vehicle it may be characterized in that at least one support is formed on one side of a deck of an LNG carrier to form a roof panel of a solar panel on the support, thereby forming a solar panel on top of the roof panel.
  • the propeller may include a charging means on one side, and may store energy obtained by rotation of the propeller in the charging means.
  • the wings are formed to be extremely long, which causes the weight of the aircraft to go out excessively. Since a light solar cell is commercially available, it is a function for charging separately from the function of the wing. If a thin and light material plate is formed and attached separately, the airplane flying with the solar cell can be popularized.
  • the battery charging device for the moving means is installed on the moving means desired by the user to prevent discharge during long-distance movement, so that it can move for a long time.
  • FIG. 1 is a perspective view of the present invention.
  • FIG. 2 is a perspective view of a battery charging method in a ship.
  • FIG 3 is another perspective view of the present invention.
  • FIG 4 is another perspective view of the present invention.
  • FIG 5 is another perspective view of the present invention.
  • FIG 6 is another perspective view of the present invention.
  • FIG 7 is another perspective view of the present invention.
  • FIG 8 is another perspective view of the present invention.
  • FIG 9 is another perspective view of the present invention.
  • FIG. 10 is a perspective view of a foldable solar panel with wings attached to a hot air balloon using the greenhouse effect.
  • FIG. 11 is a perspective view of a foldable solar panel with wings attached to a hot air balloon using the greenhouse effect.
  • FIG. 12 is a plan view seen from above of a robot bird on which a collapsible solar cell is formed.
  • FIG. 13 is a cross-sectional view of a robot bird in which a collapsible solar cell is formed.
  • FIG. 14 is a perspective view of a fan with a fan-shaped folding solar panel formed on a hot air balloon using the greenhouse effect.
  • 15 is a perspective view of a fan with a fan-folded solar panel formed on a hot air balloon using the greenhouse effect.
  • 16 is a perspective view of a foldable charging device for a vehicle in a folded state.
  • 17 is a perspective view of a foldable charging device for a vehicle in an unfolded state.
  • FIG. 18 is a perspective view of a folded state of the battery charging device of the submarine of the present invention.
  • 19 is a perspective view of an unfolded state of the battery charging device of the submarine of the present invention.
  • 20 is a perspective view of a folded state of the battery charging device of the ship of the present invention.
  • 21 is a perspective view of an unfolded state of a battery charging device for a ship of the present invention.
  • 22 is another embodiment of the folded state of the battery charging device of the ship of the present invention.
  • FIG 23 is another perspective view of the unfolded state of the battery charging device of the ship of the present invention.
  • 24 is another embodiment of the folded state of the battery charging device of the ship of the present invention.
  • 25 is another perspective view of the unfolded state in which the hydrofoil of the battery charging device of the ship of the present invention is formed.
  • 26 is another embodiment in which a solar cell is formed on a roof panel of a battery charging device of a ship of the present invention.
  • the solar panel is formed by folding and formed on one side of the ship.
  • the folding solar cell When entering, the folding solar cell is folded, and after departure, the folding solar cell is unfolded in a certain large space. At this time, the solar panel is unfolded using the servo motor as the driving means, and the secondary battery is charged by the solar cell to supply electricity to the ship.
  • a support is formed at the end of the unfolded solar cell, and a buoyancy means is formed at the end of the support so that it can support the weight of the solar cell.
  • the buoyancy means is that the support of the solar cell is formed to be positioned at an appropriate height above the water surface at the end of the solar cell, and the buoyancy means is formed at the bottom of the support so that it can be positioned at an appropriate height above the water surface.
  • a hydrofoil-type plate is formed so that the end of the solar panel rises to a certain height when the ship speeds integrally with the support, but the end of the solar cell is maintained at a constant height regardless of the waves below the water surface.
  • the angle adjustment means is formed so that the angle of the hydrofoil type plate is adjusted as much as possible.
  • the buoyancy means is that the support of the solar cell is formed to be positioned at an appropriate height above the water surface at the end of the solar cell, and the buoyancy means is formed at the bottom of the support so that it can be positioned at an appropriate height above the water surface.
  • the solar panel may be attached to one side of the hull, and the portion where the unfolding starts to rise and fall.
  • a support for one or more folding solar panels is formed under the solar panels.
  • a wheel is formed at the end of the support or a wheel is formed in which the electric motor is integrally formed to move.
  • a rail is formed on one side of a hull such as a deck at the bottom of the wheel.
  • An electric ship operated by such a solar cell can enable long-distance operation with only a solar cell without a single drop of fuel.
  • the battery charging device for a vehicle forms one or more supports on one side of the deck of an LNG carrier to form a roof panel of a solar panel on the support, thereby forming a solar panel on top of the roof panel. It can be characterized by forming.
  • the battery charging device for a vehicle is attached to the solar panel to take off and land vertically among the take-off and landing method of the drone or drone-type aircraft that can be boarded It is a fold that is connected by hinges to the wings.
  • the solar panel is unfolded as the wing is unfolded
  • the solar panel supplies electricity to the sub-motor while charging the secondary battery provided on one side of the sub-motor, so that the propeller connected to the sub-motor rotates to fly,
  • the propeller may be characterized in that it rotates 90 degrees by using a servo motor as a driving means to become a forward type.
  • the propeller is formed on the top of the wing using Bernoulli's theorem, and rotated 90 degrees using a driving means to become an advanced wing, and a solar cell is formed on the top of the advanced wing.
  • FIG. 2 is a perspective view of a battery charging method for a ship in a battery charging device for a vehicle according to another preferred embodiment of the present invention.
  • the solar panel is formed by folding and formed on one side of the ship.
  • the folding solar cell When entering, the folding solar cell is folded, and after departure, the folding solar cell is unfolded in a certain large space. At this time, the solar panel is unfolded using the servo motor as the driving means, and the secondary battery is charged by the solar cell to supply electricity to the ship.
  • a support is formed at the end of the unfolded solar cell, and a buoyancy means is formed at the end of the support so that it can support the weight of the solar cell.
  • the buoyancy means is that the support of the solar cell is formed to be positioned at an appropriate height above the water surface at the end of the solar cell, and the buoyancy means is formed at the bottom of the support so that it can be positioned at an appropriate height above the water surface.
  • a hydrofoil-type plate is formed so that the end of the solar panel rises to a certain height when the ship speeds integrally with the support, but the end of the solar cell is maintained at a constant height regardless of the waves below the water surface.
  • the angle adjusting means is formed so that the angle of the hydrofoil type plate is adjusted as much as possible.
  • the buoyancy means is that the support of the solar cell is formed to be positioned at an appropriate height above the water surface at the end of the solar cell, and the buoyancy means is formed at the bottom of the support so that it can be positioned at an appropriate height above the water surface.
  • the solar panel may be attached to one side of the hull, and the portion where the unfolding starts to rise and fall.
  • a support for one or more folding solar panels is formed under the solar panels.
  • a wheel is formed at the end of the support or a wheel is formed in which the electric motor is integrally formed to move.
  • a rail is formed on one side of a hull such as a deck at the bottom of the wheel.
  • An electric ship operated by such a solar cell can enable long-distance operation with only a solar cell without a single drop of fuel.
  • the battery charging device for a vehicle forms one or more supports on one side of the deck of an LNG carrier to form a roof panel of a solar panel on the support, thereby forming a solar panel on top of the roof panel. It can be characterized by forming.
  • 3 to 5 are perspective views showing still another embodiment of the present invention.
  • the rocket booster When it is formed inside the rocket booster and is recovered, a drone formed inside the rocket booster is provided, and one or more joints or arms formed by folding are unfolded, and a propeller is formed on one side of the arm.
  • the rocket booster In the battery charging device for a vehicle characterized in that the cover is formed so as not to receive air resistance on the outside of the drone formed in, the rocket booster is formed inside the rocket booster and is formed inside the rocket booster when it is recovered, so as to take off and land In the city, it takes off and lands vertically using the conventional drone take-off and landing method, and is formed by folding inside the rocket booster and attaching the solar panel to the node by the hinge, or the beginning of the original wing is formed.
  • Nodes are formed by folding, such as folding, where the nodes are stretched sequentially at the beginning and folded to the original beginning of the wings to expand the solar panel using the servo motor as the driving means and charge the secondary battery by the solar cell. While supplying electricity to the motor, rotate the propeller to fly, form a propeller in which the motor and the propeller are integrated on one side of the solar panel, and the folding plate on which the solar panel is formed is convex so that lift is generated by Bernoulli's principle. In this case, the foldable plate convexly formed by the driving means rotates 90 degrees to become an advanced propeller and fly with the lift by Bernoulli's theorem.
  • FIG 6 and 7 are perspective views showing still another embodiment of the present invention.
  • One or more folding arms are formed on one or more sides of an electric bicycle, electric kickboard, electric wheel, or bicycle, and a propeller is formed at the end thereof. During takeoff and flight, the folding arms are extended and the propeller is rotated to take off and fly.
  • the battery charging device for a vehicle In the battery charging device for a vehicle,
  • the nodes are sequentially opened, and the wings are folded back to the beginning of the wings, where a solar panel is attached to the wing or a folding solar panel is formed, such as an electric bicycle, an electric kickboard, an electric wheel, or one side of a bicycle. It is formed above, and when it reaches a certain altitude by taking off, it can be characterized by spreading the wings formed with the solar panel or the solar panel and charging the secondary battery by the solar cell to supply electricity to the motor and rotate the propeller to fly. .
  • a folding blade is formed instead of a propeller integrated with a drone's arm and a motor on one or more sides of an electric bicycle, electric kickboard, electric wheel, or bicycle, a hole is formed on one side of the folding blade, and a motor and propeller are formed inside the hole.
  • the portion outside the hole may be characterized in that the solar cell is attached.
  • FIG 8 and 9 are perspective views showing still another embodiment of the present invention.
  • Drones are attached to the body of a person or a companion animal by forming a harness that is attached to the body of the person or a companion animal, and a drone is formed with a propeller at the end of the arm, but the arm is folded and formed inside the body.
  • One side of the body of the aircraft having a harness which is characterized in that it is folded or unfolded inward or outward after being sent in and out, is a folding solar panel or a folding solar panel wing other than a folding propeller type.
  • the main body itself is formed with a servo motor 15 and an arm type panel 32 capable of rotating the main body up and down around the upper part, and also a servo motor 15 and an arm type panel ( The servo motor 15 and the arm type panel 32 which can rotate the servo motor 15 and the arm type panel 32 up and down are also formed on the lower part of the lower part 32. Allow the drone to be vertical or horizontal to the ground, or to adjust the rotary vane at different angles for flight
  • the main body itself is formed with a servo motor 15 and an arm type panel 32 capable of rotating the main body up and down around the lower part, and also a servo motor 15 and an arm type panel.
  • Servo motor 15 and arm type panel 32 that can rotate the servo motor 15 and the arm type panel 32 up and down are also formed at the upper part of the upper part of the 32.
  • a folding solar panel or a folding solar panel wing other than a folding propeller type is formed on one side of the body.
  • FIGS. 10 and 11 are perspective views of a wing with a collapsible solar panel formed on a hot air balloon using a greenhouse effect.
  • a portion in which sunlight enters an upper portion of a heating device is formed of a transparent material, and a lower portion is a black light that can absorb and radiate sunlight well. It is formed of a material, and at the bottom of the hot air balloon, at least one exhaust port capable of discharging heated air is formed, and while sunlight is shining, electricity is charged to the secondary battery by a solar cell or a control back element.
  • a heating means such as a Peltier element
  • hot air is supplied into the hot air balloon, and on one side of the hot air balloon, a motor 30 and a propeller, or a cylinder (25) containing a motor, a propeller, a motor, and a propeller
  • the motor 30 is capable of rotating 360 degrees by a servo motor 15 or a step motor, etc., in which a motor 30 and a propeller or a cylinder in which a motor and a propeller and a motor and a propeller enter are formed.
  • a foldable solar panel or a foldable solar panel wing is formed, and when taking off, it takes off only by the greenhouse effect, or by a motor and a propeller, or by a greenhouse effect and a motor and a propeller. It is a fold that is connected by
  • Folded solar panel or foldable solar panel is formed by folding the folding solar panel or the folded solar panel to open the solar cell. It can be characterized by supplying electricity to a thermoelectric element or a propeller to a hot air balloon using the greenhouse effect while charging the secondary battery.
  • the battery charging device for a vehicle applies the principle and structure of the robot bird as it is to a robot bird that can be burned, but makes the size large enough to be rideable by a person, and its size is large.
  • An air bag is formed in the frame of the robot bird, and the helium or hydrogen gas is filled in the air bag.
  • ballast tank to improve the resilience of robot birds that store helium gas separately, and helium gas is filled inside the ballast tank, and helium gas is injected through the valve of the ballast tank to fill the air bag or It includes a gas intake compression injection part and an air bag part that can adjust the buoyancy by itself, even without loading cargo by inhaling and compressing the helium gas of the robotic air bag.
  • the collapsible wing of the robot bird is straightened so that it can be lifted by Bernoulli's theorem, and on one side or more of the robot bird, a cylinder and a motor and a propeller or a motor and a propeller are integrally formed.
  • the cylinder and the motor and the propeller formed on one or more sides of the robot bird or the motor and the propeller can be rotated vertically or horizontally with respect to the wing by a servo motor or the like.
  • FIG. 14 is a perspective view showing a state in which a fan-folded solar panel is formed on a hot air balloon using the greenhouse effect
  • FIG. 15 is a perspective view of a state in which a fan-folded solar panel is formed on a hot-air balloon using the greenhouse effect.
  • the wing part to which the solar panel is attached is formed by folding, and the folding and unfolding expression in which the node nodes of the solar panel are connected by a hinge or the node nodes are sequentially opened at the beginning of the wing and folded to the original starting part of the wing
  • the solar cell formed at the end of the fan fan expands in a circular shape and the center of the fan fan that is folded moves from the center of the air vehicle so that the fan is not exposed to the outside and then the fan is unfolded.
  • the center of the vehicle moves to the center of the aircraft, the fan is flat, the solar panel is unfolded in a circular shape, and when folded, the fan is folded into a fan and the center of the folded fan is moved from the center of the aircraft so that the fan is not exposed to the outside. have.
  • FIG. 16 is a perspective view of the folded device of the foldable solar cell of the present invention
  • FIG. 17 is a perspective view of the unfolded charging device of the foldable solar cell of the car.
  • a foldable solar panel rotating part is formed on the roof panel of the vehicle, and the solar panel is folded in response to one-way rotation of the rotating part, so that when folded forward, the folded part faces the front side. It is stretched toward and is charged so that it is formed to cover the window of the car, and the rotating part may be characterized in that a fixed part is formed such that the foldable solar panel faces the front or side of the car.
  • a fixed portion is formed on the rotating part so that the foldable solar panel faces the front or side in the case of folding and unfolding.
  • FIG. 18 is a perspective view of a folded state of the battery charging device of a submarine of the present invention
  • FIG. 19 is a perspective view of a folded state of the battery charging device of a submarine of the present invention.
  • a submarine or a drone submarine When a submarine or a drone submarine is submerged or not submerged, it is connected by a connection means with a submarine, and a folding solar panel that is folded and unfolded by a submotor driving means that floats on the surface by buoyancy means is formed. It can be characterized by.
  • a thrust generating device by one or more motors may be formed on a folding solar panel that is folded and unfolded by a drive means of a servo motor that is connected by a connection means with a submarine and is floated on the surface by a buoyancy means. .
  • a submarine or a drone submarine dives or does not dive
  • one or more motors are operated on a folding solar panel that is folded and unfolded by a driving means such as a servo motor that floats on the surface by buoyancy means.
  • the thrust generating device by the back may be characterized in that the secondary battery of the submarine is wirelessly charged to the submarine by means of a folding solar panel and an ultrasonic wireless power transmitting and receiving device formed in the submarine.
  • the submarine with a foldable solar cell according to the present invention can be supplied with electricity even when diving, and expands and folds the foldable solar cell with buoyancy means on the sea to produce electricity, and then folds the foldable solar cell with buoyancy means in the sea. It is fixed to a fixture fixed to one side of a submarine by means of a thrust generator by a motor and a propeller formed in the battery itself, or by means of connecting and pulling and unwinding.
  • one or more cameras are formed toward the underwater air in front, back, left, and right, or are formed as a whole, and one or more are formed as well as periscopes. This operation can be seen through the camera facing from the surface of the water, and if there are other submarines, the submarines on board and other submarines can be simultaneously viewed through the camera on the surface.
  • FIG. 20 is a perspective view of a folded state of the battery charging device of the ship of the present invention
  • FIG. 21 is a perspective view of an expanded state of the battery charging device of the ship of the present invention.
  • the solar panel is attached to the side of the ship by attaching the solar panel to the wing of the folding type that connects the node of the solar panel to the hinge, or the node is sequentially expanded at the beginning of the wing, and the expanded wing is folded back to the beginning of the wing. Is formed,
  • the solar panel is opened and folded on one side of the ship so that it folds and folds, and when entering, the solar panel is folded, and when charging is required in a large space after departure, the solar panel is unfolded.
  • the battery charging device for a vehicle to enable In the battery charging device for a vehicle to enable,
  • At least one support of one or more solar panels is formed at the bottom of the solar panel, and at the end of the support, wheels are formed or wheels are formed integrally with an electric motor to form a number of solar panels with support, which are opened and closed by opening and closing. It can be characterized by being closed.
  • a rail is formed on one side of the hull such as a deck at the bottom of the wheel.
  • FIG. 22 is a perspective view showing another embodiment of the folded state of the battery charging device of the ship of the present invention
  • FIG. 23 is another perspective view of the opened state of the battery charging device of the ship of the present invention
  • FIG. 24 is the present invention Another embodiment of the folded state of the battery charging device of the ship
  • FIG. 25 is another perspective view of the expanded state in which the hydrofoil of the battery charging device of the present invention is formed
  • FIG. 26 is a battery charging device of the ship of the present invention Another embodiment of the solar cell is formed on the roof panel.
  • the battery charging device for a vehicle is a solar cell impulse to fly by charging the secondary battery with a solar cell has a long wing. This can cause the aircraft to weigh too much. Therefore, the wings can be made separately and the solar panel can be formed as a ready-made product with a thickness of about 3 mm.
  • the battery charging device for a vehicle can form a propeller in which a motor and a propeller are integrated on one side of a solar panel of an aircraft that can be drone or drone-type or on one side of the aircraft body. have. And it is preferable that the foldable plate on which the solar cell panel is formed is convexly formed upward so that lift is generated by Bernoulli's law.
  • the battery charging device for a vehicle is formed with a folding wing instead of a propeller integrated with a drone's arm and a motor, a hole is formed on one side of the folding wing, and a motor and a propeller are formed inside the hole. It is preferable that a solar cell is attached to the portion outside the hole.
  • a folding wing may be formed in place of a propeller integrated with an arm and a motor of a drone on one side or more of an electric bicycle, an electric kickboard, an electric wheel, or a bicycle.
  • a hole is formed on one side of the folding wing, a motor and a propeller are formed inside the hole, and a solar cell is attached to the portion outside the hole.
  • the propeller of the drone or the drone-type aircraft can be advanced by rotating 90 degrees using a servo motor as a driving means from the existing propeller.
  • the aircraft that is flying with lift by Bernoulli's theorem with wings will expand and charge the folding solar panel in addition to the propellers or airplane wings.
  • the battery charging device for a moving means may further include a charging means.
  • the propeller is provided with a charging means on one side, and may be characterized in that the energy obtained by the rotation of the propeller is stored in the charging means.
  • ballast tank (helium tank)
  • valve 62 air bag stretching direction
  • the industrial applicability of the present invention is significant if the fuel cost can be significantly reduced or if no fuel cost is required.

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  • Chemical & Material Sciences (AREA)
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Abstract

Un drone décolle et atterrit verticalement de la même manière qu'un drone existant décolle et atterrit. Le drone a une partie d'aile pliable à laquelle un panneau de cellule solaire est fixé, et lorsqu'il atteint une hauteur prédéterminée, le drone déplie le panneau de cellule solaire, à l'aide d'un servomoteur ou similaire en tant que moyen d'entraînement. Le drone est amené à voler en fournissant de l'électricité au moteur pour faire tourner une hélice pendant le chargement d'une batterie secondaire par la cellule solaire. L'hélice du drone est tournée de 90 degrés, à l'aide du servomoteur ou analogue qui est un moyen d'entraînement de l'hélice existante, de façon à faire avancer le drone. En variante, le moteur et l'hélice sont intégrés l'un à l'autre sur un côté du panneau de cellules solaires. Une plaque pliable, sur laquelle est disposé le panneau de cellules solaires, a une section transversale convexe vers le haut pour générer une force de sustentation selon la loi de Bernoulli.
PCT/KR2019/016995 2018-12-04 2019-12-04 Appareil de charge de batterie pour moyen mobile WO2020116925A1 (fr)

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KR20-2018-0005884 2018-12-17
KR20180006028 2018-12-21
KR20-2018-0006028 2018-12-21
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CN114919702A (zh) * 2022-04-21 2022-08-19 上海海洋大学 一种高效利用太阳能和波浪力驱动的无人艇

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