WO2018188028A1 - 充电器及无人机便携装置 - Google Patents

充电器及无人机便携装置 Download PDF

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Publication number
WO2018188028A1
WO2018188028A1 PCT/CN2017/080475 CN2017080475W WO2018188028A1 WO 2018188028 A1 WO2018188028 A1 WO 2018188028A1 CN 2017080475 W CN2017080475 W CN 2017080475W WO 2018188028 A1 WO2018188028 A1 WO 2018188028A1
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WIPO (PCT)
Prior art keywords
charger
charging
drone
battery
portable device
Prior art date
Application number
PCT/CN2017/080475
Other languages
English (en)
French (fr)
Inventor
郭晓凯
渠鸿翔
彭涛
Original Assignee
深圳市大疆创新科技有限公司
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Filing date
Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to PCT/CN2017/080475 priority Critical patent/WO2018188028A1/zh
Priority to CN201780004515.0A priority patent/CN108495767B/zh
Publication of WO2018188028A1 publication Critical patent/WO2018188028A1/zh
Priority to US16/595,078 priority patent/US11332265B2/en

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F3/00—Ground installations specially adapted for captive aircraft
    • 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
    • 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
    • B60L50/66—Arrangements of 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
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14—Conductive energy transfer
    • 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
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14—Conductive energy transfer
    • B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
    • 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
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30—Constructional details of charging stations
    • B60L53/305—Communication interfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • 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
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/50—Charging stations characterised by energy-storage or power-generation means
    • B60L53/51—Photovoltaic means
    • 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
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/50—Charging stations characterised by energy-storage or power-generation means
    • B60L53/57—Charging stations without connection to power networks
    • 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
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/60—Monitoring or controlling charging stations
    • B60L53/62—Monitoring or controlling charging stations in response to charging parameters, e.g. current, voltage or electrical charge
    • 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
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/005—Protective coverings for aircraft not in use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/36—Other airport installations
    • B64F1/362—Installations for supplying conditioned air to parked aircraft
    • B64F1/364—Mobile units
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/70—Transport or storage specially adapted for UAVs in containers
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J13/00—Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network
    • H02J13/00002—Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network characterised by monitoring
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/00032—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by data exchange
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0013—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries acting upon several batteries simultaneously or sequentially
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
    • H02J7/0044—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction specially adapted for holding portable devices containing batteries
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
    • H02J7/0045—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction concerning the insertion or the connection of the batteries
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0047—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with monitoring or indicating devices or circuits
    • H02J7/0048—Detection of remaining charge capacity or state of charge [SOC]
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0047—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with monitoring or indicating devices or circuits
    • H02J7/0048—Detection of remaining charge capacity or state of charge [SOC]
    • H02J7/0049—Detection of fully charged condition
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
    • 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
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    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B60L2260/00—Operating Modes
    • B60L2260/20—Drive modes; Transition between modes
    • B60L2260/32—Auto pilot mode
    • H—ELECTRICITY
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    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
    • 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
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    • 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
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    • 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
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    • 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
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    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/12—Electric charging stations
    • 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
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    • 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
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    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
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    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles

Definitions

  • the present invention relates to the field of charging technologies, and in particular, to a charger and a drone portable device that can be used for charging a drone.
  • the battery is used to power the device and can be applied to various devices in various fields, such as handheld pan/tilt, handheld camera, drone, robot, etc., so as to guarantee the battery life of the device, so that the device can be wirelessly controlled. .
  • a device as a drone. Due to the limitation of the power capacity stored in the battery, the time for the drone to last is limited. If a long-time flight operation is required, multiple batteries are needed for replacement.
  • a battery charging stand is generally used to charge and manage a plurality of batteries. However, the battery charging stand can only charge the battery, has a single function, and is a chicken rib product in outdoor work, which is easily forgotten by the user.
  • the present invention provides a charger and a drone portable device that can be used to charge a drone and a battery to solve the above technical problems.
  • a charger includes: a charger body including a first housing portion for housing an electronic device and matching a shape of the electronic device; and a charging main board disposed on the The at least one first charging portion is disposed in the first accommodating portion and electrically connected to the charging main board for charging the electronic device; at least one second charging portion is disposed at The charger body is electrically connected to the charging motherboard Used to charge a battery of the electronic device.
  • a drone portable device for accommodating and carrying a drone, the drone portable device comprising: a drone portable device body, including for housing no a first receiving portion of the human machine and matching the shape of the drone; a charging main plate disposed in the main body of the drone portable device; at least one first charging portion disposed in the first receiving portion Electrically connected to the charging main board for charging the drone; at least one second charging part is disposed on the main body of the drone portable device, and is electrically connected to the charging main board for Charging batteries.
  • the present invention designs a charger and a drone portable device having the same, the charger having a plurality of charging parts available for the drone and the battery Charging, and providing a first accommodating portion matching the shape of the drone on the main body of the charger to assemble the drone on the charger, thereby bringing greater convenience to the charging and carrying of the drone Sex.
  • FIG. 1 is a schematic perspective view of a charger according to an exemplary embodiment of the present invention.
  • FIG. 2 is a further perspective structural view of a charger according to an exemplary embodiment of the present invention.
  • FIG. 3 is an exploded view of a charger according to an exemplary embodiment of the present invention.
  • FIG. 4 is a schematic structural view of a charger equipped with a drone and a battery according to an exemplary embodiment of the present invention
  • FIG. 5 is a structural diagram of a portable device of a drone according to an exemplary embodiment of the present invention.
  • FIG. 6 is a side view of a drone portable device according to still another exemplary embodiment of the present invention.
  • the charger of the present invention can simultaneously accommodate batteries of electronic devices and electronic devices, such as accommodating drones and drone batteries, accommodating robots, and robot batteries.
  • the electronic device will be described by taking an unmanned aerial vehicle as an example.
  • the charger 100 of the present invention includes a charger body 1, a charging main board 2, at least one first charging portion 4, and at least one second charging portion 5.
  • the charging main board 2 is disposed in the charger main body 1
  • the second charging unit 5 is disposed on the charger main body 1
  • the first charging unit 4 and the second charging unit 5 are electrically connected to the charging main board 2 , respectively.
  • the first charging unit 4 is used to charge the drone 10
  • the second charging unit 5 is used to charge the battery 20, so that the charger 100 can realize the existing function of charging the battery 20.
  • the function of charging the drone 10 expands the function of the charger 100 and provides convenience for the user.
  • the charger body 1 includes a first receiving portion 13 for accommodating the drone 10 and matching the shape of the drone 10, and the first charging portion 4 is located in the first housing portion 13.
  • the first receiving portion 13 is designed to fit the vulnerable portion of the drone 10 into the first receiving portion 13 to protect the drone 10.
  • the charger 100 of the present invention allows the drone 10 to provide a carrier for the storage of the drone 10 during charging, thereby protecting the drone 10 and facilitating the carrying by the user. It can be understood that the shape of the first receiving portion 13 matches the shape of the other electronic device when other electronic devices are accommodated.
  • the first charging portion 4 is disposed in the first receiving portion 13 to facilitate electrical connection between the first charging portion 4 and the drone 10 .
  • the charging contact on the unmanned aerial vehicle 10 is electrically connected to the first charging portion 4.
  • the first charging portion 4 is a charging contact disposed at the bottom of the first receiving portion 13 to be electrically connected to the charging contact of the drone 10 .
  • the position and structure of the first charging portion 4 in other embodiments of the present invention are not limited thereto.
  • the first charging portion 4 may also be located at the first receiving portion. Any position in the portion 13; the structure of the first charging portion 4 may also be a plug or a socket or the like.
  • the charger body 1 further includes a second accommodating portion 14 for accommodating the battery 20, and the second charging portion 5 is disposed in the second accommodating portion 14, such that after the battery 20 is assembled to the second accommodating portion 14, the battery The charging contact of 20 is electrically connected to the second charging portion 5 in the second receiving portion 14.
  • the second charging portion 5 is a charging contact disposed at the bottom of the second receiving portion 14 and adjacent to one of the side walls.
  • the position and structure of the second charging unit 5 are not absolutely limited, and the position and structure of the second charging unit 5 can be matched according to the position and structure of the charging contact provided on the battery 20.
  • the first receiving portion 13 includes a first cavity 131 for housing the drone main body 101 and a second cavity 132 for housing the drone wing 102.
  • the second receiving portion 14 is two, which are respectively disposed on two sides of the first cavity 131 of the first receiving portion 13 , so as to be
  • the idle space on the charger 100 is fully utilized, and the plurality of batteries 20 can be simultaneously charged, so that more power demand of the user can be satisfied.
  • the number of the first accommodating portion 13 and the second accommodating portion 14 is not limited, and the charger 100 may be provided with any number of the first accommodating portions 13 according to the needs of the user.
  • the second housing portion 14 can thereby simultaneously charge a plurality of drones 10 and a plurality of batteries 20.
  • two sides of the first cavity 131 are provided with two second cavities 132, wherein the second accommodating portion 14 is located at the second cavity 132 of the first cavity 131 on the contract side.
  • the arrangement is such that the cooperation of the first receiving portion 13 and the second receiving portion 14 is more compact, which is advantageous for reducing the volume of the charger 100, thereby making it more convenient for the user to carry and transport.
  • the charger body 1 further includes a latching portion 15 respectively disposed at both ends of the first cavity 131.
  • the unmanned vehicle 10 is engaged in the first housing portion 13 by the engagement of the two holding portions 15 .
  • the holding portion 15 may be an elastic plastic member, and the elastic device is elasticized to engage the unmanned aerial vehicle 10; the holding portion 15 may also be an elastic member and a tie rod.
  • the structure utilizes the elastic properties of the resilient member to lock the lever to the drone 10.
  • other manners and structures that simply fit the drone 10 into the first housing portion 13 and are not easily removed are suitable for the latching portion 15.
  • the second cavity 132 may include an arm receiving portion 1321 and a motor receiving portion 1322.
  • the arm receiving portion 1321 is in communication with the second receiving portion 14.
  • the mating receptacles allow positioning and protection of other components outside the drone body 101.
  • the distance from the bottom of the arm receiving portion 1321 to the bottom of the second receiving portion 14 is not less than the thickness of the battery 20, so that the battery 20 is located below the drone wing 102, so that the charger 100 can be further improved.
  • the drone of the upper drone 10 and the battery 20 is compact, making full use of the space on the charger 100; and the battery 20 is prevented from falling out of the second housing portion 14 by the drone wing 102.
  • the depth of the second receiving portion 14 is greater than the depth of the first cavity 131, and the purpose thereof is also to satisfy the position that the battery 20 is located below the drone wing 102, thereby High space utilization on the charger 100.
  • the charger 100 of the present invention further includes a power module 3 disposed in the charger body 1.
  • the power module 3 is electrically connected to the charging motherboard 2 to provide power.
  • the power module 3 is built in the charger 100, so that the user can charge the drone 10 or the battery 20 outdoors, which increases the life time of the drone 10 and improves the outdoor work efficiency of the user.
  • the charger 100 can also connect the power source and the charger 100 through a charging line, thereby enabling the charger 100 to directly charge the drone 10 and the battery 20.
  • the charger 100 of the present invention further includes a charging interface 17 disposed on the charger body 1.
  • the charging interface 17 is electrically connected to the charging motherboard 2, and the charging motherboard 2 is used for controlling charging.
  • the power distribution in the device 100 is connected to the power source and the charging interface 17 through the charging line when the power module 3 is charged to store the power to the power module 3.
  • the charging motherboard 2 plays a vital role.
  • the charging main board 2 includes a control unit and a detecting unit connected to the control unit.
  • the control unit controls the power supply module 3 to charge the drone 10 and/or the battery 20.
  • the control unit controls the power module 3 to simultaneously charge the drone 10 and the battery 20 by obtaining the power and calculation of the power module 3 by the control unit so that the power module 3 can ensure that its own power can fully charge the drone 10 and the battery 20.
  • the detecting unit can detect whether the drone 10 and the battery 20 are assembled to the charger 100 by means of weight sensing, sensor sensing, light sensing, and the like.
  • control unit may be configured to: when the detecting unit detects that the drone 10 and the battery 20 are mounted on the charger 100, the control power module 3 preferentially charges the drone 10; After detecting that the drone 10 is fully charged, the control power module 3 charges the battery 20.
  • the control unit can intelligently select to charge the drone 10 and the battery 20 in the charger 100. Since the drone 10 is an important device for the user to work outdoors, the control unit can be configured to give priority to The drone 10 is charged.
  • the charging main board 2 further includes a first judging unit connected to the control unit and the detecting unit.
  • the first determining unit stores, according to the power storage of the plurality of batteries 20 detected by the detecting unit, determining that the control unit preferentially charges the battery 20 in which the battery is high.
  • the control unit preferably selects the battery 20 with a higher power to be preferentially charged. After the battery 20 is fully charged, the battery 20 that is selected to be the higher battery 20 in the remaining battery 20 is selected.
  • the charging is configured such that the charger 100 is fully charged to fully charge one of the plurality of batteries 20, so that the battery 20 can be replaced for the drone 10 in a timely manner.
  • the charging main board 2 further includes a second judging unit connected to the control unit and the detecting unit; wherein, when the detecting unit detects that the unmanned aerial vehicle 10 and the battery 20 are mounted on the charger 100, The second judging unit stores, according to the electric quantity storage of the unmanned aerial vehicle 10 and the battery 20 detected by the detecting unit, that the control unit preferentially charges the electric power in the unmanned aerial vehicle 10 and the battery 20.
  • the detecting unit further needs to detect the remaining power of the power module 3, and when the remaining power is insufficient to fill a drone 10 or a battery 20, the second judging unit compares to select the drone 10 and The higher the amount of electricity in the battery 20 is preferentially charged, so as to ensure that the storage capacity of the single battery 20 (the battery 20 can be the backup battery 20 or the battery 20 on the drone 10) is as large as possible, thereby ensuring that the single battery 20 is free.
  • the charging main board 2 further includes a wireless communication module disposed thereon, the wireless communication module is configured to communicate with the mobile terminal to remotely monitor the working state of the charger 100 and control the control module to the drone through the mobile terminal. 10 or the charging of the battery 20.
  • the user can communicate with the charger 100 through the wireless communication module by using the mobile terminal, thereby realizing remote monitoring of the working state of the charger 100 and controlling the charging priority of the charger 100.
  • the working state of the charger 100 includes the power storage information of the power module 3, the power storage information of the drone 10 on the charger 100, the battery 20 current storage information on the drone 10, and the charging information of the charger 100.
  • the wireless communication module may be a WiFi (WIreless-Fidelity) module, a Bluetooth module, or a Zigbee module.
  • the charger 100 of the present invention is further provided with a control button (not shown) electrically connected to the charging main board 2, and the triggering of the regulating button can control the priority order of charging the main board 2 to charge the drone 10 and the battery 20.
  • the user selectively triggers the control button through his own demand to select to preferentially charge the drone 10 or the battery 20.
  • the charger 100 is further provided with a switch button 16 to control the charger 100 to perform charging and discharging. Further, an indicator light 18 is further disposed on the charger 100 to indicate the power and/or working state of the charger 100.
  • the power of the charger 100 includes the power storage information of the power module 3, the power storage information of the drone 10, the power storage information of the battery 20, and the like.
  • the operational status includes whether the charger 100 is charging the drone 10 or charging the battery 20, or simultaneously charging the drone 10 and the battery 20.
  • the charger body 1 includes a top case 11 and a bottom case 12 that are fitted together.
  • the charging main board 2 and the power module 3 are located in an accommodating space formed by the upper case 11 and the bottom case 12.
  • the first receiving portion 13 and the second receiving portion 14 are located on the upper casing 11.
  • the charging interface 17 in the embodiment of the present invention may be disposed on the bottom case 12, and the switch button 16 may be disposed on the upper case 11.
  • the charger 100 further includes a protective cover 6 mounted to the charger body 1 for protecting the drone 10 assembled in the charger 100.
  • the charger body 1 is provided with a connection mechanism that is fitted to the protective cover 6.
  • the protective cover 6 can be detachably fitted to the charger body 1 by a connecting mechanism or can be pivotally attached to the charger body 1.
  • the attachment mechanism includes a hinge portion 111 disposed on one side of the charger body 1 and a latch portion 112 disposed on the other side of the charger body 1.
  • the protective cover 6 includes a hinge (not shown) that pivots with the hinge portion 111, and a locking portion (not shown) that cooperates with the locking portion 112; the hinge and the locking portion are provided On both sides of the protective cover 6.
  • the hinge portion 111 is engaged with the hinge member to enable the protective cover 6 to pivot relative to the charger body 1 and to be locked by the locking portion 112 and the locking portion to fix the protective cover 6 to the charger body. 1 on.
  • the locking portion 112 can be a structure with a hook and a spring and a button.
  • the locking portion is a hooking hook for engaging with the hook, and the locking of the locking portion is achieved by the button fitting spring and the hook.
  • the hinge portion and the locking portion may also be disposed on the protective cover 6, and the hinge and the locking portion are disposed on the charger body 1.
  • the protective cover 6 includes a resisting protrusion 61 disposed on one side of the first receiving portion 13 for resisting the drone main body 101 to further ensure that the drone 10 is limited to The charger body 1 is mounted to facilitate carrying and transport of the charger 100.
  • the protective cover 6 can also be provided with a solar panel (not shown), which is electrically connected to the charging main board 2.
  • the solar panel can be used to convert sunlight into electric energy to charge the power module 3 or directly charge the drone 10 and the battery 20, so that the solar battery can be fully utilized. Natural resources, and bring great convenience to the charging of the charger 100.
  • a solar panel may be further disposed on the outer side of the charger 100, and the solar panel is electrically connected to the charging main board 2 to store power for the charger 100 by using sunlight or directly to the drone 10 And the battery 20 is charged.
  • the charger 100 of the present invention achieves a breakthrough on the basis of charging the battery 20, and can simultaneously charge the drone 10, thereby improving the convenience for the user to charge the drone 10; the charger 100 is provided with a drone
  • the first accommodating portion 13 of the shape of 10 can be used to fix the drone 10 to the charger 100 so that the charger 100 can serve as a transport carrier for the drone 10, thereby protecting the drone 10.
  • a drone portable device 100 for housing and carrying a drone 10 is provided.
  • the drone portable device 100 includes a drone portable device main body 1, a charging main board 2, a first charging portion 4, a second charging portion 5, and a first housing portion 13.
  • the first accommodating portion 13 is configured to receive the unmanned aerial vehicle 10 and is matched with the shape of the drone 10;
  • the charging main board 2 is disposed in the main body 1 of the drone portable device;
  • the first charging portion 4 is disposed in the first accommodating portion 13
  • the charging main board 2 is electrically connected for charging the drone 10;
  • the second charging part 5 is disposed on the main body 1 of the drone portable device, and is electrically connected to the charging main board 2 for being used for electricity. Pool 20 is charged.
  • the specific structure of the UAV portable device refers to the above detailed description of the structure of the charger.
  • the UAV portable device main body 1 further includes a second accommodating portion 14 for accommodating the battery 20, and the second charging portion 5 is disposed in the second accommodating portion 14, such that after the battery 20 is assembled to the second accommodating portion 14, the battery 20 The charging contact is electrically connected to the second charging portion 5 in the second receiving portion 14.
  • the second charging portion 5 is a charging contact disposed at the bottom of the second receiving portion 14 and adjacent to one of the side walls.
  • the first receiving portion 13 includes a first cavity 131 for housing the drone main body 101 and a second cavity 132 for housing the drone wing 102.
  • the second accommodating portion 14 is disposed at two sides of the first cavity 131 of the first accommodating portion 13 respectively, so as to fully utilize the idle space on the charger 100, and At the same time, a plurality of batteries 20 are charged, so that more power demand of the user can be satisfied.
  • the number of the first accommodating portion 13 and the second accommodating portion 14 is not limited, and the charger 100 may be provided with any number of the first accommodating portions 13 according to the needs of the user.
  • the second housing portion 14 can thereby simultaneously charge a plurality of drones 10 and a plurality of batteries 20.
  • two sides of the first cavity 131 are provided with two second cavities 132, wherein the second accommodating portion 14 is located at the second cavity 132 of the first cavity 131 on the contract side.
  • the arrangement is such that the cooperation of the first receiving portion 13 and the second receiving portion 14 is more compact, which is advantageous for reducing the volume of the charger 100, thereby making it more convenient for the user to carry and transport.
  • the main body 1 of the drone carrying device further includes a holding portion 15 respectively disposed at two ends of the first cavity 131.
  • the unmanned vehicle 10 is engaged in the first housing portion 13 by the engagement of the two holding portions 15 .
  • the holding portion 15 may be an elastic plastic member, and the elastic device is elasticized to engage the unmanned aerial vehicle 10; the holding portion 15 may also be an elastic member and a tie rod.
  • the structure utilizes the elastic properties of the resilient member to lock the lever to the drone 10.
  • other manners and structures that simply fit the drone 10 into the first housing portion 13 and are not easily removed are suitable for the latching portion 15.
  • the second cavity 132 may include an arm receiving portion 1321 and a motor receiving portion 1322.
  • the arm receiving portion 1321 is in communication with the second receiving portion 14.
  • the mating receptacles allow positioning and protection of other components outside the drone body 101.
  • the distance from the bottom of the arm receiving portion 1321 to the bottom of the second receiving portion 14 is not less than the thickness of the battery 20, so that the battery 20 is located below the drone wing 102, so that the charger 100 can be further improved.
  • the drone of the upper drone 10 and the battery 20 is compact, making full use of the space on the charger 100; and the battery 20 is prevented from falling out of the second housing portion 14 by the drone wing 102.
  • the depth of the second receiving portion 14 is greater than the depth of the first cavity 131, and the purpose thereof is also to satisfy the situation that the battery 20 is located below the drone wing 102, thereby improving the charger 100. Space utilization.
  • the charger 100 of the present invention further includes a power module 3 disposed in the main body 1 of the drone carrier.
  • the power module 3 is electrically connected to the charging main board 2 to provide power.
  • the power module 3 is built in the charger 100, so that the user can charge the drone 10 or the battery 20 outdoors, which increases the life time of the drone 10 and improves the outdoor work efficiency of the user.
  • the charger 100 can also connect the power source and the charger 100 through a charging line, thereby enabling the charger 100 to directly charge the drone 10 and the battery 20.
  • the charger 100 of the present invention further includes a charging interface 17 disposed on the main body 1 of the drone, and the charging interface 17 is electrically connected to the charging main board 2, and the charging main board 2 is used.
  • the power source and the charging interface 17 are connected through a charging line to store the power to the power module 3.
  • the charging motherboard 2 plays a vital role.
  • the charging main board 2 includes a control unit and a detecting unit connected to the control unit.
  • the control unit controls the power supply module 3 to charge the drone 10 and/or the battery 20. Pass
  • the control unit acquires the power and calculation of the power module 3 so that the power module 3 ensures that the power of the power module 3 can be fully charged for the drone 10 and the battery 20, the control unit controls the power module 3 to simultaneously charge the drone 10 and the battery 20.
  • the detecting unit can detect whether the drone 10 and the battery 20 are assembled to the charger 100 by means of weight sensing, sensor sensing, light sensing, and the like.
  • control unit may be configured to: when the detecting unit detects that the drone 10 and the battery 20 are mounted on the charger 100, the control power module 3 preferentially charges the drone 10; After detecting that the drone 10 is fully charged, the control power module 3 charges the battery 20.
  • the control unit can intelligently select to charge the drone 10 and the battery 20 in the charger 100. Since the drone 10 is an important device for the user to work outdoors, the control unit can be configured to give priority to The drone 10 is charged.
  • the charging main board 2 further includes a first judging unit connected to the control unit and the detecting unit.
  • the first determining unit stores, according to the power storage of the plurality of batteries 20 detected by the detecting unit, determining that the control unit preferentially charges the battery 20 in which the battery is high.
  • the control unit preferably selects the battery 20 with a higher power to be preferentially charged. After the battery 20 is fully charged, the battery 20 that is selected to be the higher battery 20 in the remaining battery 20 is selected.
  • the charging is configured such that the charger 100 is fully charged to fully charge one of the plurality of batteries 20, so that the battery 20 can be replaced for the drone 10 in a timely manner.
  • the charging main board 2 further includes a second judging unit connected to the control unit and the detecting unit; wherein, when the detecting unit detects that the unmanned aerial vehicle 10 and the battery 20 are mounted on the charger 100, The second judging unit stores, according to the electric quantity storage of the unmanned aerial vehicle 10 and the battery 20 detected by the detecting unit, that the control unit preferentially charges the electric power in the unmanned aerial vehicle 10 and the battery 20.
  • the detecting unit further needs to detect the remaining power of the power module 3, and when the remaining power is insufficient to fill a drone 10 or a battery 20, the second judging unit compares to select the drone 10 and The battery with a higher battery charge is preferentially charged, so as to ensure a single charge.
  • the storage capacity of the pool 20 (which may be the backup battery 20 or the battery 20 on the drone 10) is as much as possible to ensure the battery life of the drone 10 in the air.
  • the charging main board 2 further includes a wireless communication module disposed thereon, the wireless communication module is configured to communicate with the mobile terminal to remotely monitor the working state of the charger 100 and control the control module to the drone through the mobile terminal. 10 or the charging of the battery 20.
  • the user can communicate with the charger 100 through the wireless communication module by using the mobile terminal, thereby realizing remote monitoring of the working state of the charger 100 and controlling the charging priority of the charger 100.
  • the working state of the charger 100 includes the power storage information of the power module 3, the power storage information of the drone 10 on the charger 100, the battery 20 current storage information on the drone 10, and the charging information of the charger 100.
  • the wireless communication module may be a WiFi (WIreless-Fidelity) module, a Bluetooth module, or a Zigbee module.
  • the charger 100 of the present invention is further provided with a control button (not shown) electrically connected to the charging main board 2, and the triggering of the regulating button can control the priority order of charging the main board 2 to charge the drone 10 and the battery 20.
  • the user selectively triggers the control button through his own demand to select to preferentially charge the drone 10 or the battery 20.
  • the charger 100 is further provided with a switch button 16 to control the charger 100 to perform charging and discharging. Further, an indicator light 18 is further disposed on the charger 100 to indicate the power and/or working state of the charger 100.
  • the power of the charger 100 includes the power storage information of the power module 3, the power storage information of the drone 10, the power storage information of the battery 20, and the like.
  • the operational status includes whether the charger 100 is charging the drone 10 or charging the battery 20, or simultaneously charging the drone 10 and the battery 20.
  • the main body 1 of the drone carrying device 1 includes a top case 11 and a bottom case 12 which are fitted together.
  • the charging main board 2 and the power module 3 are located in the accommodating space formed by the upper case 11 and the bottom case 12.
  • the first receiving portion 13 and the second receiving portion 14 are located on the upper casing 11.
  • the charging interface 17 in the embodiment of the present invention may be disposed on the bottom case 12, and the switch button 16 may be disposed on the upper case 11.
  • the charger 100 further includes a protective cover 6 mounted on the main body 1 of the drone to protect the drone assembled in the charger 100.
  • the main body 1 of the drone carrying device is provided with a connecting mechanism that is assembled with the protective cover 6.
  • the protective cover 6 can be detachably mounted on the drone carrying device main body 1 by a connecting mechanism, or can be pivotally attached to the unmanned portable device main body 1.
  • the attachment mechanism includes a hinge portion 111 disposed on one side of the main body 1 of the drone, and a latch portion 112 disposed on the other side of the main body 1 of the drone.
  • the protective cover 6 includes a hinge (not shown) that pivots with the hinge portion 111, and a locking portion (not shown) that cooperates with the locking portion 112; the hinge and the locking portion are provided On both sides of the protective cover 6.
  • the hinge portion 111 is engaged with the hinge member to enable the protective cover 6 to pivot relative to the UAV carrier body 1 and to be locked by the locking portion 112 and the locking portion to fix the protective cover 6
  • the drone carries the device body 1.
  • the locking portion 112 can be a structure of a hook-fit spring and a button, and the locking portion is a hooking hook matched with the hook, and the locking portion is locked by the button fitting spring and the hook.
  • the hinge portion and the locking portion may also be disposed on the protective cover 6, and the hinge and the locking portion are disposed on the main body 1 of the drone.
  • the protective cover 6 includes a resisting protrusion 61 disposed on one side of the first receiving portion 13 for resisting the drone main body 101 to further ensure that the drone 10 is limited to The drone carries the device body 1 to facilitate carrying and transport of the charger 100.
  • the protective cover 6 can also be provided with a solar panel (not shown), which is electrically connected to the charging main board 2.
  • the solar panel can be used to convert sunlight into electric energy to charge the power module 3 or directly charge the drone 10 and the battery 20, so that the solar battery can be fully utilized. Natural resources, and bring great convenience to the charging of the charger 100.
  • a solar panel may be further disposed on the outer side of the charger 100, and the solar panel is electrically connected to the charging main board 2 to store power for the charger 100 by using sunlight or directly to the drone 10 And electricity Pool 20 is charged.
  • the invention designs a charger and a drone portable device, the charger has a plurality of charging parts for charging the drone and the battery, and the charger main body is provided with a shape matching the shape of the drone A receiving portion is used to assemble the drone on the charger, thereby bringing greater convenience to the charging and carrying of the drone.

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Remote Sensing (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
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  • Manufacturing & Machinery (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

一种充电器（100），该充电器（100）包括：充电器主体（1），包括用于容纳电子设备（10）并与该电子设备（10）的形状相匹配的第一容纳部（13）；充电主板（2），设于该充电器主体（1）内；至少一个第一充电部（4），设于该第一容纳部（13）内，与充电主板（2）电性连接以用于为电子设备（10）充电；至少一个第二充电部（5），设于充电器主体（1）上，与充电主板（2）电性连接以用于为电子设备的电池（20）充电。还包括一种无人机便携装置，包括充电器（100）的结构，且第一容纳部（13）用于容纳无人机。

Description

充电器及无人机便携装置 技术领域
本发明涉及充电技术领域，尤其涉及一种可用于供无人机充电的充电器及无人机便携装置。
背景技术
电池用于为设备供电，可以应用于多个领域的各种设备，例如：手持云台、手持摄像机、无人机、机器人等，从而可以为设备的续航提供保证，以使设备能够进行无线控制。
以下以设备为无人机为例具体说明，由于电池所存储的电能容量的限制导致为无人机续航的时间有限，若需要长时间飞行作业，则需要多块电池以供更换。现有技术中，为了保证闲置电池充满电以待用，通常使用电池充电座对多块电池进行充电和管理。然而，该电池充电座仅能给电池充电，功能单一，为户外作业中的鸡肋产品，容易被用户遗忘。
发明内容
本发明提出一种可用于为无人机及电池充电的充电器及无人机便携装置以解决上述技术问题。
根据本发明实施例的第一方面，提供了一种充电器，包括：充电器主体，包括用于容纳电子设备并与所述电子设备的形状相匹配的第一容纳部；充电主板，设于所述充电器主体内；至少一个第一充电部，设于所述第一容纳部内，与所述充电主板电性连接以用于为所述电子设备充电；至少一个第二充电部，设于所述充电器主体上，与所述充电主板电性连接以 用于为所述电子设备的电池充电。
根据本发明实施例的第二方面，提供了一种无人机便携装置，用于容纳并携带无人机，所述无人机便携装置包括：无人机便携装置主体，包括用于容纳无人机并与所述无人机的形状相匹配的第一容纳部；充电主板，设于所述无人机便携装置主体内；至少一个第一充电部，设于所述第一容纳部内，与所述充电主板电性连接以用于为所述无人机充电；至少一个第二充电部，设于所述无人机便携装置主体上，与所述充电主板电性连接以用于为电池充电。
本发明的实施例提供的技术方案可以包括以下有益效果：本发明设计了一种充电器及具有该充电器的无人机便携式装置，该充电器具有多个充电部可用以为无人机及电池充电，且在充电器主体上设有与无人机的形状相匹配的第一容纳部以将无人机装配在充电器上，从而为无人机的充电及携带均带来较大的便捷性。
应当理解的是，以上的一般描述和后文的细节描述仅是示例性和解释性的，并不能限制本发明。
附图说明
为了更清楚地说明本发明实施例中的技术方案，下面将对实施例描述中所需要使用的附图作简单地介绍，显而易见地，下面描述中的附图仅仅是本发明的一些实施例，对于本领域普通技术人员来讲，在不付出创造性劳动性的前提下，还可以根据这些附图获得其他的附图。
图1是本发明一示例性实施例示出的一种充电器的一角度结构示意图；
图2是本发明一示例性实施例示出的一种充电器的又一角度结构图；
图3是本发明一示例性实施例示出的一种充电器的分解图；
图4是本发明一示例性实施例示出的一种充电器装配有无人机及电池的结构示意图；
图5是本发明一示例性实施例示出的一种无人机便携装置的结构图；
图6是本发明又一示例性实施例示出的一种无人机便携装置的侧视图。
具体实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。
下面结合附图，对本发明的一些实施方式作详细说明，在不冲突的情况下，下述的实施例及实施例中的特征可以相互组合。
本发明的充电器可以同时容纳电子设备和电子设备的电池，如容纳无人机和无人机电池、容纳机器人和机器人电池等。本实施方式中，所述电子设备以无人机为例进行说明。如图1至图3所示，本发明的充电器100包括：充电器主体1、充电主板2、至少一个第一充电部4和至少一个第二充电部5。其中，充电主板2设于充电器主体1内，第二充电部5设于充电器主体1上，第一充电部4和第二充电部5分别于充电主板2电性连接。在本发明中，第一充电部4用以为无人机10充电，第二充电部5用以为电池20充电，以使充电器100在为电池20充电的现有功能下，实现了还可 以为无人机10充电的功能，扩展了充电器100的功能，为用户提供了便捷。
在本发明的一实施例中，充电器主体1包括用于容纳无人机10并与无人机10的形状相匹配的第一容纳部13，第一充电部4位于第一容纳部13内，该第一容纳部13的设计可以满足将无人机10中易损坏的部分置于第一容纳部13内，以实现对无人机10的保护。本发明的充电器100以使无人机10在充电的过程中，还可以为无人机10的存放提供了载体，从而保护无人机10，而且便于用户携带。可以理解，当容纳的是其他电子设备时，所述第一容纳部13的形状与所述其他电子设备的形状相匹配。
在本实施例中，将第一充电部4设于第一容纳部13内，以便于第一充电部4与无人机10电性连接。其中，当将无人机10放置于第一容纳部13内后，该无人机10上的充电触点即与第一充电部4电性连接。在一可选实施例中，第一充电部4为设置于第一容纳部13底部的充电触点，以与无人机10的充电触点配合电性连接。当然，本发明的其他实施例中第一充电部4的位置及结构并不限于此，例如：根据无人机10上的充电触点的布局，该第一充电部4还可以位于第一容纳部13内的任意位置；该第一充电部4的结构还可以为插头或者插座等。
进一步地，该充电器主体1还包括用于收容电池20的第二容纳部14，第二充电部5设于第二容纳部14内，如此在电池20装配于第二容纳部14后，电池20的充电触点即会与第二容纳部14内的第二充电部5电性连接。在一可选实施例中，第二充电部5为设置于第二容纳部14底部并靠近其中一侧壁的充电触点。同样地，该第二充电部5的位置及结构也并不绝对限定，该第二充电部5的位置及结构可以根据电池20上设置充电触点的位置及结构而匹配。
其中，第一容纳部13包括收容无人机主体101的第一腔体131，以及收容无人机机翼102的第二腔体132。在一可选实施例中，第二容纳部14为两个，分别设于第一容纳部13的第一腔体131的两侧，如此设置以 充分利用充电器100上的闲置空间，并且可以同时为多个电池20充电，从而可以满足用户的更多用电需求。当然，在本发明的其他实施例中，对第一容纳部13与第二容纳部14的数量并不限定，该充电器100上可以根据用户的需求，设置任意数量的第一容纳部13和第二容纳部14，从而可以为多个无人机10和多个电池20同时充电。
在本实施例中，该第一腔体131的任一侧设有两个第二腔体132，其中，第二容纳部14位于第一腔体131配合同侧两个第二腔体132所构成的区域内，如此布局以使第一容纳部13与第二容纳部14的配合更加紧凑，有利于减小充电器100的体积，从而更加方便用户携带及运输。
充电器主体1还包括分别设于第一腔体131两端的卡持部15。其中，通过两个卡持部15的配合，以将无人机10卡配于第一容纳部13内。在本发明的实施例中，该卡持部15可以为弹性塑胶件，利用弹性塑胶件弹性的特点，以对无人机10进行卡配；该卡持部15也可以为弹性件配合拉杆的结构，利用弹性件的弹性属性，以使拉杆锁定住无人机10。当然，其他简易将无人机10卡配于第一容纳部13内且不易轻易取出的配合方式及结构均适用于卡持部15。
进一步地，该第二腔体132可以包括机臂容纳部1321及电机容纳部1322，机臂容纳部1321与第二容纳部14连通，本实施例中根据无人机10的各个不同的结构设置匹配的容纳部，从而可以对无人机主体101外的其他部件进行定位及保护。其中，机臂容纳部1321的底部到第二容纳部14的底部的距离不小于电池20的厚度，如此设计以使电池20位于无人机机翼102的下方，从而可以进一步地提高充电器100上无人机10与电池20布局的紧凑性，充分利用充电器100上的空间；且通过无人机机翼102防止电池20从第二容纳部14中脱落。
在本发明的实施例中，该第二容纳部14的深度大于第一腔体131的深度，其目的也是为了满足使电池20位于无人机机翼102的下方，从而提 高充电器100上的空间利用率。
在一可选实施例中，本发明的充电器100还包括设于充电器主体1内的电源模块3，电源模块3与充电主板2电性连接以提供电源。本实施例中，通过充电器100内置该电源模块3，实现用户在户外也可以为无人机10或电池20充电，增加了无人机10的续航时间，提高了用户户外作业效率。在又一实施例中，该充电器100还可以通过充电线连接电源与充电器100，从而实现使充电器100直接为无人机10和电池20充电。
相对应地，为了给电源模块3充电，本发明的充电器100还包括设于充电器主体1上的充电接口17，该充电接口17与充电主板2电性连接，充电主板2用以管控充电器100内的电源分配，在给电源模块3充电时，通过充电线连接于电源与充电接口17，以将电量储存到电源模块3。
在充电器100中的智能电量管理，充电主板2起到至关重要的作用。其中，充电主板2包括控制单元、以及与控制单元连接的检测单元。在本发明的实施例中，当检测单元检测到充电器100上装配有无人机10和/或电池20，控制单元控制电源模块3为无人机10和/或电池20充电。通过控制单元的获取电源模块3的电量及计算以使电源模块3确保自身的电量可以为无人机10及电池20充满电时，控制单元控制电源模块3同时为无人机10及电池20充电。本实施例中，检测单元可以通过重量感应、传感器感应、光线感应等方式来检测无人机10和电池20是否装配到充电器100上。
在一可选实施例中，控制单元可以被配置为：当检测单元检测到充电器100上装配有无人机10和电池20时，控制电源模块3优先为无人机10充电；当检测单元检测到无人机10已充满电后，控制电源模块3为电池20充电。在该实施例中，控制单元可以智能地选择给充电器100中的无人机10和电池20进行充电，由于无人机10为用户户外作业的重要设备，因此控制单元可以被配置为优先为无人机10充电。
在又一可选实施例中，充电主板2还包括与控制单元及检测单元连接的第一判断单元。其中，当检测单元检测到无人机10充满电后，第一判断单元根据检测单元所检测多个电池20的电量存储，判断控制单元优先为其中电量较高的电池20充电。该实施例中，在满足无人机10充电完成后，控制单元优选选择为电量较高的电池20优先充电，待该电池20充满电后，在选择为剩余电池20中电量较高的电池20充电，如此配置以使充电器100达到最快速地为多个电池20中其中一个电池20充满电，从而可以及时为无人机10更换电池20进行续航。
在又一可选实施例中，充电主板2还包括与控制单元及检测单元连接的第二判断单元；其中，当检测单元检测到充电器100上装配有无人机10和电池20时，第二判断单元根据检测单元所检测无人机10及电池20的电量存储，判断控制单元为无人机10和电池20中电量较高者优先充电。该实施例中，检测单元还需要检测电源模块3的剩余电量，在剩余电量不足以充满一个无人机10或一个电池20时，通过第二判断单元的比较，从而选择为无人机10和电池20中电量较高者优先充电，如此以保证单个电池20(该电池20可以为备用电池20或者无人机10上的电池20)的储电量尽可能地多，从而保证单个电池20使无人机10在空中的续航时间。
进一步地，充电主板2还包括设于其上的无线通信模块，该无线通信模块用以与移动终端通信连接，以使通过移动终端远程监测充电器100的工作状态和控制控制模块对无人机10或者电池20的充电。用户可以利用移动终端通过无线通信模块与充电器100通信连接，从而实现对充电器100的工作状态进行远程监控以及控制充电器100的充电优先级。其中，充电器100的工作状态包括电源模块3的电量储存信息、充电器100上无人机10的电量储存信息、无人机10上电池20电流储存信息、以及充电器100充电信息等。该无线通信模块可以为WiFi(WIreless-Fidelity，无线保真)模块、蓝牙模块、或Zigbee模块等。
另外，在本发明的充电器100还设有与充电主板2电性连接的调控按键(未图示)，该调控按键的触发可以控制充电主板2为无人机10和电池20充电的优先顺序级，用户通过自身需求选择地触发调控按键从而选择优先为无人机10或电池20进行充电。
在本发明的实施例中，充电器100上还设置有开关按键16，以控制充电器100进行充放电。进一步地，充电器100上还设置有指示灯18，以指示充电器100的电量和/或工作状态。其中，充电器100的电量包括电源模块3的电量储存信息，无人机10的电量储存信息，电池20的电量储存信息等。该工作状态包括充电器100是为无人机10充电还是为电池20充电，或者同时为无人机10和电池20充电等。
进一步地，充电器主体1包括配合装配的上壳11和底壳12，充电主板2和电源模块3位于上壳11与底壳12所构成的容置空间内。其中，第一容纳部13和第二容纳部14位于上壳11上。本发明实施例中的充电接口17可以设于底壳12上，开关按键16可以设于上壳11上。
如图3至图6所示，在本发明的实施例中，该充电器100还包括装配于充电器主体1的保护罩6，用以保护装配于充电器100中的无人机10。该充电器主体1上设有与保护罩6装配的连接机构。该保护罩6可以通过连接机构可拆卸地装配在充电器主体1上，或者枢轴连接地装配在充电器主体1上。
在一可选实施例中，该连接机构包括设于充电器主体1一侧的铰接部111，以及设于充电器主体1另一侧的锁扣部112。相对应地，保护罩6包括与铰接部111配合枢轴转动的铰接件(未图示)，以及与锁扣部112配合锁定的锁止部(未图示)；铰接件与锁止部分设于保护罩6的两侧。本实施例中，通过铰接部111与铰接件配合以使保护罩6可以相对充电器主体1枢轴转动，并通过锁扣部112与锁止部配合锁定以使保护罩6固定在充电器主体1上。其中，锁扣部112可以为卡勾配合弹簧及按钮的结构， 锁止部为与卡勾配合的卡配勾，通过按钮配合弹簧及卡勾实现对锁止部的锁定。在本发明的其他实施例中，该铰接部和锁扣部也可以设置于保护罩6上，铰接件和锁止部设置于充电器主体1上。
进一步地，保护罩6包括设置于朝向第一容纳部13一面上的抵持凸起61，该抵持凸起61用以抵持无人机主体101，以进一步确保无人机10限位在充电器主体1上，从而便于对该充电器100的携带及运输。
在一可选实施例中，该保护罩6上还可以设有太阳能面板(未图示)，该太阳能面板与充电主板2电性连接。本实施例中，在户外没有电源为充电器100充电的前提下，可以利用太阳能面板将阳光转化为电能以为电源模块3进行充电或者直接为无人机10及电池20充电，从而可以充分合理利用自然资源，且为充电器100的充电带来很大便捷。在又一可选实施例中，该充电器100外侧面上还可以设有太阳能面板，该太阳能面板与充电主板2电性连接，以利用阳光为充电器100蓄电或者直接为无人机10及电池20充电。
本发明的充电器100在为电池20充电的基础上实现突破，可以同时为无人机10进行充电，提高了用户为无人机10充电的便捷性；充电器100上设有与无人机10的形状相匹配的第一容纳部13，可以实现将无人机10固定在充电器100上，以使充电器100可以作为无人机10的运输载体，从而可以保护无人机10。
如图1至图6所示，根据本发明实施例的第二方面，提供了一种无人机便携装置100，用于容纳并携带无人机10。无人机便携装置100包括无人机便携装置主体1、充电主板2、第一充电部4、第二充电部5、以及第一容纳部13。第一容纳部13用于容纳无人机10并与无人机10的形状相匹配；充电主板2设于无人机便携装置主体1内；第一充电部4设于第一容纳部13内，与充电主板2电性连接以用于为无人机10充电；第二充电部5设于无人机便携装置主体1上，与充电主板2电性连接以用于为电 池20充电。在本实施例中，该无人机便携装置的具体结构请参照上述对充电器的结构的具体描述。
无人机便携装置主体1还包括用于收容电池20的第二容纳部14，第二充电部5设于第二容纳部14内，如此在电池20装配于第二容纳部14后，电池20的充电触点即会与第二容纳部14内的第二充电部5电性连接。在一可选实施例中，第二充电部5为设置于第二容纳部14底部并靠近其中一侧壁的充电触点。
其中，第一容纳部13包括收容无人机主体101的第一腔体131，以及收容无人机机翼102的第二腔体132。在一可选实施例中，第二容纳部14为两个，分别设于第一容纳部13的第一腔体131的两侧，如此设置以充分利用充电器100上的闲置空间，并且可以同时为多个电池20充电，从而可以满足用户的更多用电需求。当然，在本发明的其他实施例中，对第一容纳部13与第二容纳部14的数量并不限定，该充电器100上可以根据用户的需求，设置任意数量的第一容纳部13和第二容纳部14，从而可以为多个无人机10和多个电池20同时充电。
在本实施例中，该第一腔体131的任一侧设有两个第二腔体132，其中，第二容纳部14位于第一腔体131配合同侧两个第二腔体132所构成的区域内，如此布局以使第一容纳部13与第二容纳部14的配合更加紧凑，有利于减小充电器100的体积，从而更加方便用户携带及运输。
无人机携带装置主体1还包括分别设于第一腔体131两端的卡持部15。其中，通过两个卡持部15的配合，以将无人机10卡配于第一容纳部13内。在本发明的实施例中，该卡持部15可以为弹性塑胶件，利用弹性塑胶件弹性的特点，以对无人机10进行卡配；该卡持部15也可以为弹性件配合拉杆的结构，利用弹性件的弹性属性，以使拉杆锁定住无人机10。当然，其他简易将无人机10卡配于第一容纳部13内且不易轻易取出的配合方式及结构均适用于卡持部15。
进一步地，该第二腔体132可以包括机臂容纳部1321及电机容纳部1322，机臂容纳部1321与第二容纳部14连通，本实施例中根据无人机10的各个不同的结构设置匹配的容纳部，从而可以对无人机主体101外的其他部件进行定位及保护。其中，机臂容纳部1321的底部到第二容纳部14的底部的距离不小于电池20的厚度，如此设计以使电池20位于无人机机翼102的下方，从而可以进一步地提高充电器100上无人机10与电池20布局的紧凑性，充分利用充电器100上的空间；且通过无人机机翼102防止电池20从第二容纳部14中脱落。
在本发明的实施例中，该第二容纳部14的深度大于第一腔体131的深度，其目的也是为了满足使电池20位于无人机机翼102的下方，从而提高充电器100上的空间利用率。
在一可选实施例中，本发明的充电器100还包括设于无人机携带装置主体1内的电源模块3，电源模块3与充电主板2电性连接以提供电源。本实施例中，通过充电器100内置该电源模块3，实现用户在户外也可以为无人机10或电池20充电，增加了无人机10的续航时间，提高了用户户外作业效率。在又一实施例中，该充电器100还可以通过充电线连接电源与充电器100，从而实现使充电器100直接为无人机10和电池20充电。
相对应地，为了给电源模块3充电，本发明的充电器100还包括设于无人机携带装置主体1上的充电接口17，该充电接口17与充电主板2电性连接，充电主板2用以管控充电器100内的电源分配，在给电源模块3充电时，通过充电线连接于电源与充电接口17，以将电量储存到电源模块3。
在充电器100中的智能电量管理，充电主板2起到至关重要的作用。其中，充电主板2包括控制单元、以及与控制单元连接的检测单元。在本发明的实施例中，当检测单元检测到充电器100上装配有无人机10和/或电池20，控制单元控制电源模块3为无人机10和/或电池20充电。通过 控制单元的获取电源模块3的电量及计算以使电源模块3确保自身的电量可以为无人机10及电池20充满电时，控制单元控制电源模块3同时为无人机10及电池20充电。本实施例中，检测单元可以通过重量感应、传感器感应、光线感应等方式来检测无人机10和电池20是否装配到充电器100上。
在一可选实施例中，控制单元可以被配置为：当检测单元检测到充电器100上装配有无人机10和电池20时，控制电源模块3优先为无人机10充电；当检测单元检测到无人机10已充满电后，控制电源模块3为电池20充电。在该实施例中，控制单元可以智能地选择给充电器100中的无人机10和电池20进行充电，由于无人机10为用户户外作业的重要设备，因此控制单元可以被配置为优先为无人机10充电。
在又一可选实施例中，充电主板2还包括与控制单元及检测单元连接的第一判断单元。其中，当检测单元检测到无人机10充满电后，第一判断单元根据检测单元所检测多个电池20的电量存储，判断控制单元优先为其中电量较高的电池20充电。该实施例中，在满足无人机10充电完成后，控制单元优选选择为电量较高的电池20优先充电，待该电池20充满电后，在选择为剩余电池20中电量较高的电池20充电，如此配置以使充电器100达到最快速地为多个电池20中其中一个电池20充满电，从而可以及时为无人机10更换电池20进行续航。
在又一可选实施例中，充电主板2还包括与控制单元及检测单元连接的第二判断单元；其中，当检测单元检测到充电器100上装配有无人机10和电池20时，第二判断单元根据检测单元所检测无人机10及电池20的电量存储，判断控制单元为无人机10和电池20中电量较高者优先充电。该实施例中，检测单元还需要检测电源模块3的剩余电量，在剩余电量不足以充满一个无人机10或一个电池20时，通过第二判断单元的比较，从而选择为无人机10和电池20中电量较高者优先充电，如此以保证单个电 池20(该电池20可以为备用电池20或者无人机10上的电池20)的储电量尽可能地多，从而保证单个电池20使无人机10在空中的续航时间。
进一步地，充电主板2还包括设于其上的无线通信模块，该无线通信模块用以与移动终端通信连接，以使通过移动终端远程监测充电器100的工作状态和控制控制模块对无人机10或者电池20的充电。用户可以利用移动终端通过无线通信模块与充电器100通信连接，从而实现对充电器100的工作状态进行远程监控以及控制充电器100的充电优先级。其中，充电器100的工作状态包括电源模块3的电量储存信息、充电器100上无人机10的电量储存信息、无人机10上电池20电流储存信息、以及充电器100充电信息等。该无线通信模块可以为WiFi(WIreless-Fidelity，无线保真)模块、蓝牙模块、或Zigbee模块等。
另外，在本发明的充电器100还设有与充电主板2电性连接的调控按键(未图示)，该调控按键的触发可以控制充电主板2为无人机10和电池20充电的优先顺序级，用户通过自身需求选择地触发调控按键从而选择优先为无人机10或电池20进行充电。
在本发明的实施例中，充电器100上还设置有开关按键16，以控制充电器100进行充放电。进一步地，充电器100上还设置有指示灯18，以指示充电器100的电量和/或工作状态。其中，充电器100的电量包括电源模块3的电量储存信息，无人机10的电量储存信息，电池20的电量储存信息等。该工作状态包括充电器100是为无人机10充电还是为电池20充电，或者同时为无人机10和电池20充电等。
进一步地，无人机携带装置主体1包括配合装配的上壳11和底壳12，充电主板2和电源模块3位于上壳11与底壳12所构成的容置空间内。其中，第一容纳部13和第二容纳部14位于上壳11上。本发明实施例中的充电接口17可以设于底壳12上，开关按键16可以设于上壳11上。
如图3至图6所示，在本发明的实施例中，该充电器100还包括装配于无人机携带装置主体1的保护罩6，用以保护装配于充电器100中的无人机10。该无人机携带装置主体1上设有与保护罩6装配的连接机构。该保护罩6可以通过连接机构可拆卸地装配在无人机携带装置主体1上，或者枢轴连接地装配在无人机携带装置主体1上。
在一可选实施例中，该连接机构包括设于无人机携带装置主体1一侧的铰接部111，以及设于无人机携带装置主体1另一侧的锁扣部112。相对应地，保护罩6包括与铰接部111配合枢轴转动的铰接件(未图示)，以及与锁扣部112配合锁定的锁止部(未图示)；铰接件与锁止部分设于保护罩6的两侧。本实施例中，通过铰接部111与铰接件配合以使保护罩6可以相对无人机携带装置主体1枢轴转动，并通过锁扣部112与锁止部配合锁定以使保护罩6固定在无人机携带装置主体1上。其中，锁扣部112可以为卡勾配合弹簧及按钮的结构，锁止部为与卡勾配合的卡配勾，通过按钮配合弹簧及卡勾实现对锁止部的锁定。在本发明的其他实施例中，该铰接部和锁扣部也可以设置于保护罩6上，铰接件和锁止部设置于无人机携带装置主体1上。
进一步地，保护罩6包括设置于朝向第一容纳部13一面上的抵持凸起61，该抵持凸起61用以抵持无人机主体101，以进一步确保无人机10限位在无人机携带装置主体1上，从而便于对该充电器100的携带及运输。
在一可选实施例中，该保护罩6上还可以设有太阳能面板(未图示)，该太阳能面板与充电主板2电性连接。本实施例中，在户外没有电源为充电器100充电的前提下，可以利用太阳能面板将阳光转化为电能以为电源模块3进行充电或者直接为无人机10及电池20充电，从而可以充分合理利用自然资源，且为充电器100的充电带来很大便捷。在又一可选实施例中，该充电器100外侧面上还可以设有太阳能面板，该太阳能面板与充电主板2电性连接，以利用阳光为充电器100蓄电或者直接为无人机10及电 池20充电。
本发明设计了一种充电器及无人机便携式装置，该充电器具有多个充电部用以为无人机及电池充电，且在充电器主体上设有与无人机的形状相匹配的第一容纳部以将无人机装配在充电器上，从而为无人机的充电及携带均带来较大的便捷性。
需要说明的是，在本文中，诸如第一和第二等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来，而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含，从而使得包括一系列要素的过程、方法、物品或者设备不仅包括那些要素，而且还包括没有明确列出的其他要素，或者是还包括为这种过程、方法、物品或者设备所固有的要素。在没有更多限制的情况下，由语句“包括一个……”限定的要素，并不排除在包括所述要素的过程、方法、物品或者设备中还存在另外的相同要素。
以上对本发明实施例所提供的方法和装置进行了详细介绍，本文中应用了具体个例对本发明的原理及实施方式进行了阐述，以上实施例的说明只是用于帮助理解本发明的方法及其核心思想；同时，对于本领域的一般技术人员，依据本发明的思想，在具体实施方式及应用范围上均会有改变之处，综上所述，本说明书内容不应理解为对本发明的限制。

Claims (48)

  1. 一种充电器，其特征在于，包括：
    充电器主体，包括用于容纳电子设备并与所述电子设备的形状相匹配的第一容纳部；
    充电主板，设于所述充电器主体内；
    至少一个第一充电部，设于所述第一容纳部内，与所述充电主板电性连接以用于为所述电子设备充电；
    至少一个第二充电部，设于所述充电器主体上，与所述充电主板电性连接以用于为所述电子设备的电池充电。
  2. 根据权利要求1所述的充电器，其特征在于，所述充电器主体还包括用于收容所述电池并与所述电池的形状相匹配的第二容纳部，所述第二充电部设于所述第二容纳部内。
  3. 根据权利要求2所述的充电器，其特征在于，所述第一容纳部用于容纳无人机并与无人机的形状相匹配。
  4. 根据权利要求3所述的充电器，其特征在于，所述第一容纳部包括收容所述无人机主体的第一腔体，以及收容所述无人机机翼的第二腔体。
  5. 根据权利要求4所述的充电器，其特征在于，所述第二容纳部为两个，分别设于所述第一容纳部的第一腔体的两侧。
  6. 根据权利要求4所述的充电器，其特征在于，所述第一腔体的任一侧设有两个所述第二腔体，其中，所述第二容纳部位于所述第一腔体配合同侧两个所述第二腔体所构成的区域内。
  7. 根据权利要求6所述的充电器，其特征在于，所述第二腔体包括机臂容纳部及电机容纳部，所述机臂容纳部与所述第二容纳部连通，其中，所述机臂容纳部的底部到所述第二容纳部的底部的距离不小于电池的厚度。
  8. 根据权利要求2至7中任一项所述的充电器，其特征在于，所述第二容纳部的深度大于所述第一腔体的深度。
  9. 根据权利要求2所述的充电器，其特征在于，所述充电器还包括设于所述充电器主体内的电源模块，所述电源模块与所述充电主板电性连接以提供电源。
  10. 根据权利要求9所述的充电器，其特征在于，所述充电器主体包括配合装配的上壳和底壳，所述充电主板和所述电源模块位于所述上壳与所述底壳所构成的容置空间内；其中，所述第一容纳部和所述第二容纳部位于所述上壳上。
  11. 根据权利要求4所述的充电器，其特征在于，所述充电器主体还包括分别设于所述第一腔体两端的卡持部；其中，通过两个所述卡持部的配合，以将所述无人机卡配于所述第一容纳部内。
  12. 根据权利要求1所述的充电器，其特征在于，所述第一充电部为设置于所述第一容纳部底部的充电触点。
  13. 根据权利要求2所述的充电器，其特征在于，所述第二充电部为设置于所述第二容纳部底部并靠近其中一侧壁的充电触点。
  14. 根据权利要求1所述的充电器，其特征在于，所述充电器还包括装配于所述充电器主体的保护罩，所述充电器主体上设有与所述保护罩装配的连接机构。
  15. 根据权利要求14所述的充电器，其特征在于，所述连接机构包括设于所述充电器主体一侧的铰接部，以及设于所述充电器主体另一侧的锁扣部；所述保护罩包括与所述铰接部配合枢轴转动的铰接件，以及与所述锁扣部配合锁定的锁止部。
  16. 根据权利要求14所述的充电器，其特征在于，所述保护罩包括设置于朝向第一容纳部一面上的抵持凸起，以抵持电子设备的主体。
  17. 根据权利要求14所述的充电器，其特征在于，所述保护罩上设有太阳能面板。
  18. 根据权利要求1或17所述的充电器，其特征在于，所述充电器外侧面上设有太阳能面板。
  19. 根据权利要求9所述的充电器，其特征在于，所述充电主板包括控制单元、以及与所述控制单元连接的检测单元；其中，当所述检测单元检测到所述充电器上装配有所述电子设备和/或所述电子设备的电池，所述控制单元控制所述电源模块为所述电子设备和/或所述电池充电。
  20. 根据权利要求19所述的充电器，其特征在于，所述控制单元被配置为：
    当所述检测单元检测到所述充电器上装配有所述电子设备和所述电池时，控制所述电源模块优先为所述电子设备充电；
    当所述检测单元检测到所述电子设备已充满电后，控制所述电源模块为所述电池充电。
  21. 根据权利要求20所述的充电器，其特征在于，所述充电主板还包括与所述控制单元及所述检测单元连接的第一判断单元；其中，
    当所述检测单元检测到所述电子设备充满电后，所述第一判断单元根据所述检测单元所检测多个所述电池的电量存储，判断所述控制单元优先为其中电量较高的电池充电。
  22. 根据权利要求19所述的充电器，其特征在于，所述充电主板还包括与所述控制单元及所述检测单元连接的第二判断单元；其中，
    当所述检测单元检测到所述充电器上装配有所述电子设备和所述电池时，所述第二判断单元根据所述检测单元所检测电子设备及电池的电量存储，判断所述控制单元为所述电子设备和所述电池中电量较高者优先充电。
  23. 根据权利要求1所述的充电器，其特征在于，所述充电主板包括无线通信模块，用以与移动终端通信连接，以使通过所述移动终端远程监测所述充电器的工作状态和控制所述控制模块对所述电子设备或者所述电池的充电。
  24. 根据权利要求1所述的充电器，其特征在于，所述充电器上还设置有开关按键，以控制所述充电器进行充放电；和/或所述充电器上还设置有指示灯，以显示所述充电器的电量和/或工作状态。
  25. 一种无人机便携装置，用于容纳并携带无人机，其特征在于，所述无人机便携装置包括：
    无人机便携装置主体，包括用于容纳无人机并与所述无人机的形状相匹配的第一容纳部；
    充电主板，设于所述无人机便携装置主体内；
    至少一个第一充电部，设于所述第一容纳部内，与所述充电主板电性连接以用于为所述无人机充电；
    至少一个第二充电部，设于所述无人机便携装置主体上，与所述充电主板电性连接以用于为电池充电。
  26. 根据权利要求25所述的无人机便携装置，其特征在于，所述无人机便携装置主体还包括用于收容所述电池的第二容纳部，所述第二充电部设于所述第二容纳部内。
  27. 根据权利要求26所述的无人机便携装置，其特征在于，所述第一容纳部包括收容所述无人机主体的第一腔体，以及收容所述无人机机翼的第二腔体。
  28. 根据权利要求27所述的无人机便携装置，其特征在于，所述第二容纳部为两个，分别设于所述第一容纳部的第一腔体的两侧。
  29. 根据权利要求27所述的无人机便携装置，其特征在于，所述第一腔体的任一侧设有两个所述第二腔体，其中，所述第二容纳部位于所述第一腔体配合同侧两个所述第二腔体所构成的区域内。
  30. 根据权利要求29所述的无人机便携装置，其特征在于，所述第二腔体包括机臂容纳部及电机容纳部，所述机臂容纳部与所述第二容纳部连通，其中，所述机臂容纳部的底部到所述第二容纳部的底部的距离不小于电池的厚度。
  31. 根据权利要求26至30中任一项所述的无人机便携装置，其特征在于，所述第二容纳部的深度大于所述第一腔体的深度。
  32. 根据权利要求26所述的无人机便携装置，其特征在于，所述充电器 还包括设于所述无人机便携装置主体内的电源模块，所述电源模块与所述充电主板电性连接以提供电源。
  33. 根据权利要求26所述的无人机便携装置，其特征在于，所述无人机便携装置主体包括配合装配的上壳和底壳，所述充电主板和所述电源模块位于所述上壳与所述底壳所构成的容置空间内；其中，所述第一容纳部和所述第二容纳部位于所述上壳上。
  34. 根据权利要求27所述的无人机便携装置，其特征在于，所述无人机便携装置主体还包括分别设于所述第一腔体两端的卡持部；其中，通过两个所述卡持部的配合，以将所述无人机卡配于所述第一容纳部内。
  35. 根据权利要求25所述的无人机便携装置，其特征在于，所述第一充电部为设置于所述第一容纳部底部的充电触点。
  36. 根据权利要求25所述的无人机便携装置，其特征在于，所述第二充电部为设置于所述第二容纳部底部并靠近其中一侧壁的充电触点。
  37. 根据权利要求25所述的无人机便携装置，其特征在于，所述充电器还包括装配于所述无人机便携装置主体的保护罩，所述无人机便携装置主体上设有与所述保护罩装配的连接机构。
  38. 根据权利要求37所述的无人机便携装置，其特征在于，所述连接机构包括设于所述无人机便携装置主体一侧的铰接部，以及设于所述无人机便携装置主体另一侧的锁扣部；所述保护罩包括与所述铰接部配合枢轴转动的铰接件，以及与所述锁扣部配合锁定的锁止部。
  39. 根据权利要求37所述的无人机便携装置，其特征在于，所述保护罩包括设置于朝向第一容纳部一面上的抵持凸起，以抵持无人机主体。
  40. 根据权利要求37所述的无人机便携装置，其特征在于，所述保护罩上设有太阳能面板。
  41. 根据权利要求25或39所述的无人机便携装置，其特征在于，所述充电器外侧面上设有太阳能面板。
  42. 根据权利要求32所述的无人机便携装置，其特征在于，所述充电主 板包括控制单元、以及与所述控制单元连接的检测单元；其中，当所述检测单元检测到所述充电器上装配有所述无人机和/或所述电池，所述控制单元控制所述电源模块为所述无人机和/或所述电池充电。
  43. 根据权利要求42所述的无人机便携装置，其特征在于，所述控制单元被配置为：
    当所述检测单元检测到所述充电器上装配有所述无人机和所述电池时，控制所述电源模块优先为所述无人机充电；
    当所述检测单元检测到所述无人机已充满电后，控制所述电源模块为所述电池充电。
  44. 根据权利要求42所述的无人机便携装置，其特征在于，所述充电主板还包括与所述控制单元及所述检测单元连接的第一判断单元；其中，
    当所述检测单元检测到所述无人机充满电后，所述第一判断单元根据所述检测单元所检测多个所述电池的电量存储，判断所述控制单元优先为其中电量较高的电池充电。
  45. 根据权利要求42所述的无人机便携装置，其特征在于，所述充电主板还包括与所述控制单元及所述检测单元连接的第二判断单元；其中，
    当所述检测单元检测到所述充电器上装配有所述无人机和所述电池时，所述第二判断单元根据所述检测单元所检测无人机及电池的电量存储，判断所述控制单元为所述无人机和所述电池中电量较高者优先充电。
  46. 根据权利要求25所述的无人机便携装置，其特征在于，所述充电主板包括无线通信模块，用以与移动终端通信连接，以使通过所述移动终端远程监测所述充电器的工作状态和控制所述控制模块对所述无人机或者所述电池的充电。
  47. 根据权利要求25所述的无人机便携装置，其特征在于，所述充电器上还设置有开关按键，以控制所述充电器进行充放电。
  48. 根据权利要求25或47所述的无人机便携装置，其特征在于，所述充电器上还设置有指示灯，以显示所述充电器的电量和/或工作状态。
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