WO2019105412A1 - 电池、无人机、自动终端、转运中心及货物的拆装方法 - Google Patents

电池、无人机、自动终端、转运中心及货物的拆装方法 Download PDF

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Publication number
WO2019105412A1
WO2019105412A1 PCT/CN2018/118166 CN2018118166W WO2019105412A1 WO 2019105412 A1 WO2019105412 A1 WO 2019105412A1 CN 2018118166 W CN2018118166 W CN 2018118166W WO 2019105412 A1 WO2019105412 A1 WO 2019105412A1
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WO
WIPO (PCT)
Prior art keywords
battery
package
cargo
drone
charging
Prior art date
Application number
PCT/CN2018/118166
Other languages
English (en)
French (fr)
Inventor
周鹏跃
Original Assignee
周鹏跃
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 周鹏跃 filed Critical 周鹏跃
Publication of WO2019105412A1 publication Critical patent/WO2019105412A1/zh

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Classifications

    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/202—Casings or frames around the primary casing of a single cell or a single battery
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
    • 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
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10—Energy storage using batteries

Definitions

  • the invention belongs to the technical field of batteries, and particularly relates to a battery, a drone, an automatic terminal, a transfer center and a method for disassembling and loading goods.
  • the object of the present invention is to provide a battery, which aims to solve the technical problem that the structure of the unmanned aerial vehicle in the prior art is complicated and the loading and unloading efficiency of the battery and the package is low.
  • the present invention is achieved by a battery comprising a battery body and a clamping mechanism coupled to the battery body for gripping and releasing the package.
  • the battery body includes a housing and a battery pack disposed within the housing;
  • the clamping mechanism includes a driving assembly disposed within the housing, and is drivingly coupled to the driving assembly and used for The opening and closing movement is performed under the driving of the driving assembly to grip or release the wrapped clamping assembly.
  • the present invention also provides a drone comprising a battery as described above, the bottom of the drone having a battery compartment for accommodating the battery and having an opening downward.
  • the present invention also provides an automatic terminal comprising a storage compartment having a locker having a battery exchange mechanism for replacing the battery and charging the battery.
  • the present invention also provides a transshipment center for coordinating bag retransmission with a drone, the transshipment center including a battery charging cabinet for charging the battery as described above, a battery for transferring the battery and the package And a package transfer device for clamping and releasing the package.
  • the invention also provides a method for disassembling and loading goods, which is disassembled and assembled by using the above-mentioned automatic terminal, the goods comprising the above-mentioned battery and package, comprising the following steps:
  • the battery exchange mechanism splits the battery and the package in the cargo and charges a battery body of the battery
  • the goods are loaded on the external device.
  • the invention also provides a method for disassembling and arranging goods, which is disassembled and assembled by using the above-mentioned transfer center, the goods including the above-mentioned battery and package, comprising the following steps:
  • the battery and package transfer device splits the battery and the package that the cargo has, and transfers the battery to the battery charging cabinet;
  • the battery charging cabinet charges the separated battery
  • the goods are loaded on the external device.
  • a battery embodying the present invention has the following advantages: it is provided by a clamping mechanism connected to the battery body for gripping or releasing the package so that the package can be loaded onto the drone together with the battery. At the same time, it is unloaded from the drone, which saves the loading and unloading time and improves the loading and unloading efficiency.
  • the drone only needs to have a structure for loading the battery, and does not need to have a structure for loading the package, which simplifies the structure of the drone. Reduce the cost of drones.
  • FIG. 1 is a schematic perspective view of a battery according to an embodiment of the present invention (1);
  • FIG. 2 is a schematic perspective view of a battery according to an embodiment of the present invention (2);
  • FIG. 3 is a schematic exploded view of a battery according to an embodiment of the present invention.
  • FIG. 4 is a schematic perspective view of a package provided by an embodiment of the present invention.
  • FIG. 5 is a schematic view showing the assembly of a battery and a package according to an embodiment of the present invention.
  • FIG. 6 is a schematic view showing the assembly of a driving assembly and a clamping assembly according to an embodiment of the present invention
  • FIG. 7 is a schematic perspective structural view of a drone according to an embodiment of the present invention.
  • FIG. 8 is a schematic diagram of a three-dimensional structure of a drone loaded with a package according to an embodiment of the present invention.
  • FIG. 9 is a schematic perspective structural view of an automatic terminal according to an embodiment of the present invention.
  • FIG. 10 is a schematic perspective structural view of a left side storage cabinet according to an embodiment of the present invention.
  • Figure 11 is a perspective view showing the structure of a cargo lifting platform according to an embodiment of the present invention.
  • Figure 12 is a perspective view showing the structure of a transfer center according to an embodiment of the present invention.
  • FIG. 13 is a schematic perspective structural view of a mobile hanger according to an embodiment of the present invention.
  • FIG. 14 is a schematic perspective structural view of a battery charging cabinet according to an embodiment of the present invention.
  • the battery 1 provided by the embodiment of the invention comprises a battery body and a clamping mechanism, which can be applied to a drone in the field of express logistics.
  • the clamping mechanism is coupled to the battery body and the clamping mechanism is adapted to grip the package 2 when the package 2 is loaded onto the battery and to release the package 2 when the package 2 is unloaded from the battery.
  • the embodiment of the invention enables the package 2 to be combined with the battery 1 before loading, and then loaded onto the drone together, or can be unloaded together from the drone as a whole, and then split, thereby improving the drone's stay.
  • the drone realizes the loading and unloading of the package 2 synchronously when the battery 1 is replaced, which saves the loading and unloading time, improves the loading and unloading efficiency, and simplifies the structure of the drone and related supporting devices.
  • the clamping mechanism can be located inside the battery body or outside the battery body. Moreover, the clamping mechanism may be directly connected to the battery body or may be indirectly connected to the battery body through the intermediate connection.
  • the battery 1 and the package 2 can also be connected to the detaching structure through other quick connection, such as electromagnetic adsorption, and other structures, which are not limited herein.
  • the clamping mechanism is located within the battery body.
  • the battery body includes a housing 11 and a battery pack 12, and the clamping mechanism includes a drive assembly 13 and a clamp assembly 14.
  • the battery pack 12 and the driving assembly 13 are both disposed in the outer casing 11.
  • the battery pack 12 can be stacked and connected in series by a plurality of cells.
  • the clamping assembly 14 is drivingly coupled to the driving assembly 13 and is used for gripping and releasing the package 2.
  • the clamp assembly 14 is rotatably coupled to the bottom of the outer casing 11 and partially extends out of the bottom of the outer casing 11, and is driven to open and close under the drive of the drive assembly 13 to grip or release the package 2.
  • the outer casing 11 is substantially rectangular parallelepiped and has a receiving cavity for accommodating the battery pack 12 and the driving assembly 13 in the middle, and the driving assembly 13 is located in the middle of the receiving cavity and is used for driving the clamping assembly 14 to grip or release the package 2,
  • a battery pack 12 is disposed on both sides of the drive unit 13.
  • the clamp assembly 14 is disposed below the drive assembly 13 and is driven to open and close under the drive of the drive assembly 13.
  • the package 2 includes a package body 21 having a closed receiving space therein, and a first groove is symmetrically disposed on the upper end surface of the package body 21. 211 and the second groove 212, and a sealing plate 2111 is disposed on a side opposite to the notch of the first groove 211 and the second groove 212; the end of the clamping assembly 14 extends into the groove and is driven The assembly is driven to close and abut against the inner surface of the sealing plate 2111, thereby enabling the clamping assembly 14 to grip the package 2.
  • the first groove 211 and the second groove 212 also facilitate the user to grasp the package 2.
  • a groove is formed instead of the first groove 211 and the second groove 212, and at the same time
  • the middle portion is provided with a sealing plate instead of the above-mentioned sealing plate 2111 disposed in the first recess 211 and the second recess 212.
  • a communication unit is further included, and a power interface 114 is disposed on an outer surface of the outer casing 11, and the power interface 114 is electrically connected to the battery pack 12 and/or the drive assembly 13, respectively.
  • the power interface 114 can be used to charge the battery pack 12, as well as to power the external device (preferably a drone) using the battery pack 12.
  • the communication unit performs signal transmission with an external device (preferably a drone) by wire or wirelessly, and the external device itself is also provided with a communication unit that cooperates with the communication unit in the battery 1 to implement external device control in the battery 1
  • the drive assembly 13 drives the clamp assembly 14 to complete the gripping and release of the package 2. At the same time, the battery 1 can also feed back information to the external device.
  • a plurality of card slots 113 for detachably connecting the battery 1 to an external device are provided on opposite sides of the casing 11.
  • an external device specifically, a battery compartment of an external device
  • a buckle that cooperates with the card slot is disposed on the inner wall of the battery compartment. It can be understood that, in other embodiments of the present invention, the buckles may be disposed on opposite sides of the outer casing 11, and correspondingly, the inner wall of the battery compartment is provided with a latching groove.
  • a quick release mechanism for quick connection and quick disassembly is provided between the external device and the battery 1, such as electromagnetic adsorption, and is not limited to the snap fit of the buckle and the card slot. This is not a single limitation.
  • the drive assembly 13 includes a first baffle 131, a second baffle 132, a first driver 133, and a gear set 134.
  • the first baffle 131 and the second baffle 132 are both disposed in the outer casing 11 and disposed in parallel with each other.
  • the first driver 133 is disposed on the first shutter 131.
  • the first driver 133 is preferably a steering gear.
  • the gear set 134 is disposed on a side of the first shutter 131 away from the first driver 133 and is coupled to an output shaft of the first driver 133.
  • the gear set 134 acts as a transmission mechanism, and its end gear is connected to the clamping assembly 14 and is used to drive the clamping assembly to perform an opening and closing movement to facilitate the clamping or release of the package 2.
  • the gear set 134 includes a first stage gear 1341, a second stage gear 1342, a third stage gear 1343, a fourth stage gear 1344, and a fifth stage gear 1345.
  • the first stage gear 1341 is coupled to the output shaft of the first driver 133;
  • the second stage gear 1342 is meshed with the first stage gear 1341;
  • the third stage gear 1343 is meshed with the second stage gear 1342;
  • the fourth stage gear 1344 and the The secondary gear 1342 is engaged;
  • the fifth stage gear 1345 is meshed with the fourth stage gear 1344.
  • the third stage gear 1343 and the fifth stage gear 1345 are coupled to the clamp assembly 14.
  • the clamping assembly 14 is driven to perform an opening and closing motion.
  • the clamping assembly 14 includes a first clamping plate 141 and a second clamping plate 142 that are rotatably coupled between the first barrier 131 and the second barrier 132.
  • the first clamping plate 141 and the second clamping plate 142 are oppositely disposed.
  • One end of the first clamping plate 141 is coupled to the third stage gear 1343, and one end of the second clamping plate 142 is coupled to the fifth stage gear 134.
  • the first clamping plate 141 cooperates with the first groove 211, and the second clamping plate 142 cooperates with the second groove 212 to enable the battery 1 to grip and release the package 2.
  • a first opening 111 and a second opening 112 are respectively opened at the bottom of the outer casing 11, and the first opening 111 corresponds to the first clamping plate 141 and is used for the first clamping
  • the holding plate 141 provides a rotatable space
  • the second opening 112 corresponds to the second clamping plate 142 and serves to provide a rotatable space for the second clamping plate 142.
  • the battery 1 further includes a second driver 15 and a locking member 16.
  • the locking member 16 is configured to rotate under the driving of the second driver 15 and abut against the fourth-stage gear 1344 to lock the transmission process of the gear set 13.
  • the transmission process of the gear set 13 is locked by the locking member 16, which can reduce the package 2 from being detached due to the failure of the first driver 133 when the drone is in the air. The risk of battery 1.
  • an embodiment of the present invention further provides a drone 3 including a rack and a battery 1 as described above.
  • a battery compartment 31 is provided at the bottom of the rack of the drone 3, the battery compartment 31 has an opening facing downward, the battery 1 is detachably connected in the battery compartment 31, and the package 2 is loaded with the battery 1 to the unmanned The bottom of the machine 3.
  • an interface matching the power source interface 114 is provided in the battery compartment 31 to facilitate the battery 1 to supply or charge the drone 3.
  • the power supply unit is provided in the drone 3, and the battery 1 can charge the power supply unit to ensure that the drone 3 still has power supply when the battery 1 is not loaded.
  • the drone 3 has a communication unit corresponding to the communication unit on the battery 1, and the communication unit transmits signals by wire or wirelessly to realize the control of the battery 1 by the drone 3 or the battery 1 is not. Man machine 3 feedback information.
  • a first buckle 311 is provided on the inner wall of the battery compartment 31, and a card slot matching the first buckle 311 is provided on opposite sides of the outer casing 11 of the battery 1.
  • an embodiment of the present invention further provides an automatic terminal including a storage platform 41 and a cargo lifting platform 42.
  • the storage table 41 is used for temporarily storing the package 2 and the battery 1, and realizing the replacement and charging function of the unmanned battery 1;
  • the cargo lifting platform 42 is used for transporting the battery 1 and the package 2, and is also used for lifting the battery 1 and
  • the package 2 is such that the battery 1 is docked with the drone 3.
  • a battery exchange mechanism for replacing and charging the battery 1 is provided in the storage table 41.
  • the storage table 41 includes a locker and an access platform 413.
  • the locker includes a left storage cabinet 411 and a right storage cabinet 412 disposed oppositely, and the access platform 413 is disposed on the left storage cabinet 411. And the top of the right side locker 412.
  • a transport passage is formed between the storage cabinet 411 on the left side and the storage cabinet 412 on the right side.
  • the cargo lifting platform 42 is located in the transport passage.
  • An access port 4131 is defined in the access platform 413.
  • the access port 4131 is located in the transport passage. Directly above. When the drone 3 landed on the access platform 413, its battery 1 and package 2 are located directly above the access opening 431.
  • a plurality of partition plates 4111 are disposed in parallel in the left side storage cabinet 411 and the right side storage cabinet 412, and the partition plate 4111 divides the left side storage cabinet 411 and the right side storage cabinet 412 into a plurality of parallel arrangements.
  • the storage location, the opening of each storage location is opposite to the handling channel, the storage location is used to temporarily store the package 2, and in all or part of the storage location, the battery 1 is loaded and unloaded from the package 2 and the battery 1 is charged Battery replacement mechanism.
  • first shifting rollers 4112 and a first driving member drivingly connected to the first shifting roller 4112 and driving the first shifting roller 4112 to rotate are disposed on each of the partition plates 4111, and the package 2 is
  • the first shift roller 4112 can be driven out or stored in the storage bit.
  • the cargo lifting platform 42 includes a lifting plate 421, a second displacement roller 422, a second driving member, and a moving mechanism 423.
  • a plurality of second displacement rollers 422 are arranged in parallel on the lifting plate 421, and the plurality of second displacement rollers 422 are driven to rotate under the driving of the second driving member, the first displacement roller 4112 and the second displacement roller 422 collectively completes the transfer of the package 2 and the battery 1 between the lift plate 421 and the shelf partition 4111.
  • the moving mechanism 423 is connected to the lifting plate 421.
  • the automatic terminal of the embodiment of the present invention may further include a slide rail disposed in the transport passage, and the moving mechanism 423 is slidably coupled to the slide rail to realize the movement of the cargo lift platform 42 in the transport passage.
  • the automatic terminal may further include a third drive member for driving the moving mechanism 423 to slide along the slide rail.
  • the cargo lifting platform 42 further includes a fourth driving member and a link mechanism 424 drivingly connected to the fourth driving member, the linkage mechanism 424 is deployed or contracted by the driving of the fourth driving member, and the moving mechanism 423 and lifting The plates 421 are connected by a link mechanism 424.
  • the fourth driving member driving link mechanism 424 When the fourth driving member driving link mechanism 424 is deployed, the lifting plate 421 moves away from the sliding bar, and when the fourth driving member driving link mechanism 424 is contracted, the lifting plate 421 moves toward the sliding bar, by setting The link mechanism 424 can lift the lift plate 421 to receive the unloaded battery 1 and/or the package 2 during the unloading of the battery 1 and/or the package 2 to the cargo lift 42 by the drone 3 . And during the loading of the battery 1 and/or the package 2 from the cargo lift 42 by the drone 3, the lift plate 421 is lifted to enable the drone 3 to load the battery 1 and/or the package 2.
  • the battery exchange mechanism includes a first vertical rail 4121 disposed in the storage position, a first horizontal rail 4122 slidably coupled to the first vertical rail 4121, and disposed at the first At least one battery holder 4123 under the horizontal rail 4122 and for holding the battery 1 (preferably, a driving guide assembly may also be disposed between the battery holder 4123 and the first horizontal rail 4122, specifically, the battery holder
  • the holder 4123 is slidably coupled to the rail to achieve movement of the opening adjacent to or away from the storage position when the battery holder 4123 moves along the rail, and for driving the first horizontal rail 4122 on the first vertical rail 4121 A sliding vertical drive member and a horizontal drive member for driving the battery holder 4123 to slide over the first horizontal rail 4122.
  • the battery holder 4123 has a downward first opening, and a second buckle 4124 is disposed on the inner wall of the first opening, and the second card is disposed on opposite sides of the outer casing 11 of the battery 1
  • the button 4124 is matched with the card slot 113.
  • the terminal further includes a communication unit interconnected with the communication unit on the battery 1, preferably disposed in the battery holder 4123, and the communication unit performs signal transmission by wire or wireless to realize automatic terminal pair. The control of the battery 1 or the battery 1 feedback information to the terminal.
  • the purpose is to realize that the battery replacement mechanism in a single storage position can replace the plurality of batteries 1 and charge.
  • the holder 4123 moves on the first horizontal rail 4122 to the docking position. Moving upward and along the first vertical rail 4121 until docking with the battery 1 to be charged or the battery 1 held by the holder 4123 is docked with the package 2.
  • the number of battery holders 4123 on the first horizontal rail 4122 should be such that all of the battery holders 4123 can be moved to the designated docking position.
  • the automatic terminal realizes the process of unloading and splitting the battery 1 and the package 2 mounted on the drone 3: the drone 3 landed on the access platform 413, and the cargo lifting platform 42 moves to the access port. And the lifting plate 421 is driven upward by the connecting rod mechanism 424 to receive the battery 1 and the package 2 unloaded by the drone 3, and then the cargo lifting platform 42 drives the lifting plate 421 to descend through the connecting rod mechanism 424 and moves along the carrying path through the moving mechanism 423.
  • the automatic terminal realizes the process of combining and loading the battery 1 and the package 2 to the drone 3: transferring the package 2 to be loaded by the drone 3 to the storage position through the cargo lifting platform 42 or temporarily stored therein
  • the storage position, the holding member 4123 holding the battery 1 to be loaded by the drone 3 is moved to the designated docking position by horizontal and vertical movement, and controls the battery 1 to hold the package 2, completing the new battery 1 and to be loaded.
  • the buckle of the holding member 4123 is separated from the card slot of the new battery 1; the first shifting roller 4112 and the second shifting roller 422 cooperate to transfer the assembled battery 1 and the package 2 to the lifting plate 421, and then the cargo lifting platform 42 rises to the access port, the lifting plate 421 is lifted up until the battery 1 is pushed into the battery compartment 31 of the drone 3, and the drone 3 fixes the battery 1 by the buckle, thereby realizing the unmanned aerial vehicle 3 loading the battery 1 and the package 2.
  • the automatic terminal can also realize the function of replacing only the battery 1 of the drone 3 when the drone 3 does not carry the package 2, and the specific implementation manner is that the battery 1 unloaded by the drone 3 can be received by the cargo lifting platform 42 and Transferring to one of the storage locations, the battery replacement mechanism of the storage location holds and uncharges the unloaded battery 1, and then the battery exchange mechanism releases another battery 1 to be loaded by the drone 3, from which the battery 1 is transferred to the cargo The lifting platform 42 is finally loaded by the cargo lifting platform 42 to the drone 3 .
  • Another implementation is provided by the automatic terminal providing a package 2 or other device that assists in replacing the battery 1 of the drone 3, the device having the same interface as the package 2 that can be gripped by the battery 1 of the drone 3.
  • the specific process is that the package 2 or other device is transferred from the storage terminal of the automatic terminal to the access port through the cargo lifting platform 42 and raised, and the drone 3 controls the battery 1 to clamp the package 2 or other device, and then the drone 3 Unloading the battery 1, the package 2 or other combination of the device and the battery 1 is received by the cargo elevator 42 and transferred to one of the storage locations, the battery replacement mechanism of the storage location being unloaded from the package 2 or other device.
  • the battery 1 is loaded with another battery 1 to the package 2 or other device to be loaded by the drone 3, and then the combination of the package 2 or other device and the battery 1 is transferred from the storage position to the cargo lifting platform 42 and by the cargo lifting platform 42. Loading to the drone 3, the drone 3 controls the battery 1 to release the package 2 or other device, and the automatic terminal recycles the package 2 or other device.
  • an embodiment of the present invention further provides a transshipment center for cooperating with a drone.
  • the transfer center unloads and sorts the package 2 collected by the drone 3, and sorts and loads the package 2 to be delivered by the drone 3, and completes the battery 1 carried by the drone 3 Replacement.
  • the transshipment center includes at least one drone landing platform 51, a battery and package transfer device 52 for transferring the battery 1 and the package 2, and splitting or combining the battery 1 and the package 2, and is disposed at the drone.
  • a cargo transition device 53 between the landing platform 51 and the battery and package transfer device 52, and a battery charging cabinet 54 for charging the battery 1 are provided.
  • the drone landing platform 51 is installed in an outdoor or roof openable compartment to facilitate take-off and landing of the drone 3, and the battery and package transfer device 52 and the battery charging cabinet 54 are installed indoors, and the cargo transition device 53 is installed. Between the drone landing platform 51 and the battery and package transfer device 52, it can extend from the outside to the interior.
  • the battery and package transfer device 52 includes a track 521, a plurality of mobile hangers 522 movably coupled to the track 521, and a mobile hanger drive for driving the mobile hanger 522 to move over the track.
  • the rail 521 is installed indoors and has a certain height from the ground, and the plurality of mobile hangers 522 are vertically extended downward.
  • the mobile hanger 522 is used for receiving the package 2 and the battery 1 unloaded by the drone 3 from the cargo transition device 52.
  • the package 2 and the battery 1 are split and transferred to the collection parcel sorting system and the battery charging system (specifically, the battery charging cabinet 54); the mobile hanger 522 is simultaneously used to receive the battery charging system and the distribution parcel sorting system, respectively.
  • the battery 1 and the package 2 to be loaded by the drone 3, the battery 1 and the package 2 are assembled and transferred to the cargo transition device 53.
  • a vertical rotating shaft is disposed at the top of the rotating shaft.
  • At least one crossbar when the rotating shaft rotates, the crossbar is rotated about the rotating shaft, and the moving hanger 522 is connected to the end of the end of the crossbar away from the rotating shaft, and the crossbar is rotated by the rotating shaft to drive the movable hanger. 522 arrived at each work place.
  • the mobile hanger 522 includes a slider 5221, a telescopic unit 5222, and a gripping member 5223.
  • the slider 5221 is connected to the rail 521 and can slide on the rail 521.
  • the telescopic unit 5222 is fixedly connected to the slider 5221 and extends vertically downward.
  • the telescopic unit 5222 can be changed in length by telescopic to adjust the relative position of the gripping member 5223.
  • the gripping member 5223 is fixedly coupled to one end of the telescopic unit 5222 away from the slider 5221 for gripping and releasing the battery 1.
  • the clamping member 5223 has a second downward opening, a card slot 113 is disposed on opposite sides of the outer casing 11 of the battery 1, and a third card matched with the card slot is disposed on the inner wall of the second opening.
  • Buckle 5224 a communication unit cooperating with the communication unit in the battery 1 is disposed in the gripping member 5223 or other portions of the battery and package transfer device 52, and the communication unit in the battery 1 receives the gripping member 5223 or the battery and the package transfer
  • the control signal sent by the communication unit of the other portion of the device 52 controls the drive assembly 13 to drive the clamp assembly 14 to pick up and release the package 2.
  • the cargo transition device 53 may employ the cargo lifting platform 42 as described in the above automatic terminal (for the simplification of the structure, the second shifting roller 422 in the cargo lifting platform 42 may not be provided), and the horizontal sliding rail 531, the cargo lifting The table 42 is slidable on the horizontal rail 531.
  • One end of the horizontal rail 531 extends to the area of the drone landing platform 51 to enable the cargo lifting platform 42 to move below the drone 3 while the drone 3 is staying, and the other end extends below the rail 521.
  • the cargo transition device 53 is configured to receive the battery 1 and the package 2 unloaded by the drone 3 and transfer it to the lower side of the track 521, so that the mobile hanger 522 picks up the battery 1 and the package 2, or receives no from the mobile hanger 522.
  • the battery 1 and the package 2 to be loaded by the human machine 3 are transferred to the area of the landing platform 51 and loaded to the drone 3 .
  • the transfer center further includes a first conveyor 55 and a second conveyor 56 for transporting only the package 2.
  • first conveyor 55 receives the package 2 unloaded by the drone 3 from the mobile hanger 522, that is, when one of the mobile hangers 522 holds the battery 1 and the package 2 and moves to the upper side of the first conveyor 55 near 522,
  • the telescoping unit 5222 of the mobile hanger 522 is extended downward to bring the package 2 close to the first conveyor 55, and then the clamping assembly 14 of the battery 1 is controlled to release the package 2, and the first conveyor 55 receives the package 2 and then transports the package 2 to Collect cargo sorting systems or other logistics distribution links.
  • the second conveying device 56 transfers the package 2 to be loaded by the drone 3 from the distribution package sorting system or other logistics distribution link to the lower side of the track 521, when the mobile hanger 522 holds the battery 1 to be loaded by the drone 3 and
  • the telescoping unit 5222 of the mobile hanger 522 is extended downward and controls the clamping assembly 14 of the battery 1 to grip the package 2.
  • the first conveyor 55 and the second conveyor 56 are both belt or roller drives.
  • the above-mentioned collection parcel sorting system is configured to classify the collected parcels 2 according to the delivery information, place them in different areas or transfer to different areas; the above-mentioned delivery parcel sorting system assigns parcels 2 to different ones according to the delivery information.
  • Drone 3 It can be understood that the parcel sorting system can also be installed, and the parcel unloaded by the drone 3 can be directly transferred from the first conveying device 55 to other logistics distribution links, such as land transportation. Alternatively, the distribution parcel sorting system may not be provided, and other logistics distribution links, such as land transportation links, may be directly transferred to the second transport device.
  • the battery charging system includes a battery charging cabinet 54 and a battery pick-and-place mechanism 542.
  • the battery charging cabinet 54 is partitioned into a plurality of charging cells 541 arranged in an array, and the charging grid 541 is used for Charge battery 1.
  • a second interface matching the power source interface 114 of the battery 1 is disposed on the inner wall of the charging cell 541, and a buckle for fixing the battery 1 is provided.
  • the battery pick-and-place mechanism 542 is disposed on a side of the charging grid 541 having an opening for receiving the battery 1 on the mobile hanger 522 and placed in the charging grid 541.
  • the charging grid 541 fixes the battery 1 and charges the battery 1;
  • the release mechanism 542 can also be used to remove the battery 1 within the charging grid 541 and receive and secure it by the mobile hanger 522.
  • the same battery charging cabinet 54 may be provided with a plurality of battery pick-and-place mechanisms 542.
  • the battery pick-and-place mechanism 542 includes a second horizontal rail 5421 disposed on one side of the battery charging cabinet 54 and a second vertical rail 5422 slidably coupled to the second horizontal rail 5421.
  • the second vertical rail 5422 is slidably coupled to the second vertical rail 5422.
  • a third horizontal guide rail 5423 thereon a battery receiving bracket 5424 slidably coupled to the third horizontal rail 5423, and a fifth driving member for driving the second vertical rail 5422 to slide on the second horizontal rail 5421 for a sixth driving member that drives the third horizontal rail 5423 to slide on the second vertical rail 5422 and a seventh driving member for driving the battery receiving bracket 5424 to slide on the third horizontal rail 5423 to make the battery receiving bracket 5424
  • Three-degree-of-freedom motion can be performed (the above-described battery pick-and-place mechanism 542 can also be replaced with an industrial robot capable of achieving three-degree-of-freedom motion).
  • the top of the battery receiving bracket 5424 is provided with a battery fixing interface 5425 having the same structure as the first groove 211 and the second groove 212 on the package 2.
  • the second horizontal rail 5421 includes two rails disposed horizontally disposed at the top and bottom of the battery charging cabinet 54
  • the second vertical rail 5422 includes a vertical rail disposed at the second horizontal rail 5421.
  • Two tracks between and parallel to each other the third horizontal rail 5423 includes two rails horizontally disposed between the second vertical rails 5422 and parallel to each other, and the third horizontal rails 5423 are perpendicular to the second horizontal rails 5422 to realize
  • the battery holder 5424 can extend into or out of the charging compartment 541.
  • the battery pick-and-place mechanism 542 receives the battery 1 on the mobile hanger 522 and puts it into the charging grid 541.
  • the charging grid 541 fixes and charges the battery 1 in the process of: when one of the mobile hangers 522 holds the unmanned aerial vehicle 3 and unloads
  • the battery receiving bracket 5424 is moved until the battery fixing interface 5425 on the battery receiving bracket 5424 is located directly under the clamping assembly 14 of the battery 1, at which time the battery receiving The bracket 5424 is moved upward or the moving hanger 522 is extended downward until the clamping assembly 14 of the battery 1 can secure the battery securing interface 5425 of the battery carrier 5424.
  • the mobile hanger 522 releases the battery 1.
  • the battery receiving bracket 5424 moves downward to drive the battery 1 away from the moving hanger 522, and then the battery receiving bracket 5424 moves and puts the battery into the battery.
  • the battery charging cabinet 54 is vacant in a charging compartment 541 until the charging compartment 541 fixes the battery 1 and starts charging. After the battery 1 is fixed in the charging compartment 541, the battery 1 releases the battery fixing interface 5425, and the battery receiving bracket 5424 is separated from the battery 1. Transfer out the charging grid.
  • the battery pick-and-place mechanism 542 takes out the battery 1 in the charging compartment 541 and receives and fixes it by the mobile hanger 522: the charged battery 1 is taken out from the charging grid 541 by the movement of the battery receiving bracket 5424 and transferred. Directly below the gripping member 5223 on the mobile hanger 522, the battery receiving bracket 5424 is moved upward to push the battery 1 into the gripping member 5223, so that the latching groove 113 of the battery 1 and the gripping member 5223 are snap-fitted. The gripping member 5233 is clamped to the battery 1, and then the drive assembly 13 of the battery 1 drives the clamp assembly 14 to release the battery holder 5424, and then the battery holder 5424 is moved to disengage the battery 1.
  • the track 521 is an annular guide rail, and a plurality of drone landing platforms 51 are disposed on one side of the annular guide rail and arranged side by side, and the cargo transition device 53 is disposed at none.
  • the battery charging cabinet 54 is disposed on the other side of the annular rail, and the cargo transition device 53, the first conveying device 55, the battery pick-and-place mechanism 542 and the second conveying device 56 are disposed around Around the annular guide rail, the positional sequence of the cargo transition device 53, the first conveyor 55, the battery pick-and-place mechanism 542, and the second conveyor 56 is arranged in the direction in which the moving hanger 522 moves in the direction of the rail 521.
  • the track 521 is also a linear guide
  • the drone landing platform 51 is respectively disposed at two ends of the track 521
  • the drone 3 respectively unloads and loads the battery 1 and the package 2 at both ends of the track 521, of course.
  • Other structures may be substituted, and are not limited herein.
  • the working principle of the transfer center is as follows: the drone 3 landed on the drone landing platform 51, and the cargo transition device 53 receives the battery 1 and the package 2 unloaded by the drone 3 and the battery 1 and the package 2 is transferred to the lower side of the track 521, the moving hanger 525 lowers the height of the gripping member 5223 to grip the battery 1 and the package 2, and then moves the hanger 525 to raise the height of the gripping member 5223 and transfers to the first conveying device 55 near the moving crane Above the one end of the frame 522, the moving hanger 522 lowers the height of the gripping member 5223, the clamping assembly 14 of the battery 1 releases the package 2, the first conveying device 55 receives the package 2 and transmits it to the collecting package sorting system, and the moving hanger 522 continues.
  • the battery 1 on the mobile hanger 522 is transferred to the charging compartment 541 for charging by the battery pick-and-place mechanism 542, and the battery pick-and-place mechanism 542 loads the battery to be loaded by the drone 3 1 is transferred to the mobile hanger 522, the moving hanger 522 continues to move and is transferred to the second conveyor 56 near the end of the mobile hanger 522, the moving hanger 522 lowers the height of 5223 and the clamping assembly 14 of the battery 1 is gripped.
  • the transfer center is provided with a plurality of mobile hangers 522, and the battery 1 and the package 2 are separated and combined in synchronization, and the cargo transition device 53 transfers the battery 1 and the package 2 unloaded by the drone 3 to the mobile hanger. The battery 1 and the package 2 to be loaded by the drone 3 are then received from another mobile hanger 522.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Battery Mounting, Suspending (AREA)

Abstract

一种电池(1)、无人机(3)、自动终端及转运中心，所述电池(1)包括电池本体，以及与所述电池本体连接且用于夹取和放开包裹(2)的夹持机构。上述技术方案通过设置与电池本体连接且用于夹取或释放包裹(2)的夹持机构，使得包裹(2)可以在装载前先与电池(1)组合，然后一起装载到无人机(3)上，也可作为一个整体从无人机(3)上一起卸载下来，然后再进行拆分，提高了无人机(3)停留期间的装卸效率，也即实现了无人机(3)在更换电池(1)时同步完成包裹(2)的装卸，节省了装卸时间，提高了装卸效率；并使得无人机(3)以及相关配套装置的结构得到了简化。

Description

电池、无人机、自动终端、转运中心及货物的拆装方法
技术领域
本发明属于电池技术领域，特别涉及一种电池、无人机、自动终端、转运中心及货物的拆装方法。
背景技术
目前，无人机已应用于快递物流领域，而多数应用场景下无人机需要连续执行多个运输任务，这就需要经常为无人机装卸包裹以及更换电池。而目前普遍的方法，无论通过人工还是自动化装置，包裹的装卸和电池的更换过程都相互独立，不但在无人机停留期间会增加执行的流程，从而有可能延长无人机停留的时间和增加故障发生的几率，而且也增加了无人机相关结构以及配套装置结构的复杂程度。
发明内容
本发明的目的在于提供一种电池，旨在解决现有技术中的无人机结构复杂且电池和包裹的装卸效率低的技术问题。
本发明是这样实现的，一种电池，包括电池本体，以及与所述电池本体连接且用于夹取和放开包裹的夹持机构。
进一步地，所述电池本体包括外壳以及设置在所述外壳内的电池组；所述夹持机构包括与设置在所述外壳内的驱动组件，以及与所述驱动组件驱动连接且用于在所述驱动组件的驱动下进行开合运动以夹取或放开包裹的夹持组件。
本发明还提供了一种无人机，包括如上述所述的电池，所述无人机的底部具有用于容纳所述电池且开口向下的电池仓。
本发明还提供了一种自动终端，包括具有储物柜的储物台，所述储物柜内设有用于更换上述电池并为所述电池充电的电池更换机构。
本发明还提供了一种转运中心，用于配合无人机快递实现包裹中转，所述转运中心包括用于上述的电池进行充电的电池充电柜、用于转移所述电池和所述包裹的电池及包裹转移装置，所述电池的夹持机构用于夹取和放开所述包裹。
本发明还提供了一种货物的拆装方法，利用上述的自动终端对货物进行拆装，所述货物包括上述的电池和包裹，包括以下步骤：
将所述货物从外部设备卸下；
所述电池更换机构将所述货物中的所述电池和所述包裹拆分，并对所述电池的电池本体充电；
将所述包裹置于收取存储位；
将充电完成的所述电池与配送存储位上的待配送的所述包裹组合形成所述货物；
将所述货物装载于所述外部设备。
本发明还提供了一种货物的拆装方法，利用上述的转运中心对货物进行拆装，所述货物包括上述的电池和包裹，包括以下步骤：
将所述货物从外部设备卸下；
所述电池及包裹转移装置将所述货物具有的所述电池和所述包裹拆分，并将所述电池转移至所述电池充电柜；
将所述包裹转移至物流配送环节；
所述电池充电柜对拆分后的所述电池充电；
将所述电池充电柜内充电完成的所述电池与物流配送环节接收的待配送的所述包裹组合形成所述货物；
将所述货物装载于所述外部设备。
实施本发明的一种电池，具有以下有益效果：其通过设置与电池本体连接的夹持机构，该夹持机构用于夹取或放开包裹，使得包裹可以跟电池一起装载到无人机上，并同时从无人机上一起卸载下来，节省了装卸时间，提高了装卸效率；另外，无人机上只需要有装载电池的结构，而不需要有装载包裹的结构，简化了无人机的结构，降低了无人机的成本。
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是本发明实施例提供的电池的立体结构示意图（一）；
图2是本发明实施例提供的电池的立体结构示意图（二）；
图3是本发明实施例提供的电池的爆炸示意图；
图4是本发明实施例提供的包裹的立体结构示意图；
图5是本发明实施例提供的电池与包裹的装配示意图；
图6是本发明实施例提供的驱动组件与夹持组件的装配示意图；
图7是本发明实施例提供的无人机的立体结构示意图；
图8是本发明实施例提供的无人机装载有包裹的立体结构示意图；
图9是本发明实施例提供的自动终端的立体结构示意图；
图10是本发明实施例提供的左侧储物柜的立体结构示意图；
图11是本发明实施例提供的货物升降台的立体结构示意图；
图12是本发明实施例提供的转运中心的立体结构示意图；
图13是本发明实施例提供的移动吊架的立体结构示意图；
图14是本发明实施例提供的电池充电柜的立体结构示意图。
上述附图所涉及的标号明细如下：
1-电池；11-外壳；111-第一开口；112-第二开口；113-卡槽；114-充电和通讯接口；12-电池组；13-驱动组件；131-第一挡板；132-第二挡板；133-第一驱动器；134-齿轮组；1341-第一级齿轮；1342-第二级齿轮；1343-第三级齿轮；1344-第四级齿轮；1345-第五级齿轮；14-夹持组件；141-第一夹持板；142-第二夹持板；15-第二驱动器；16-锁止件；2-包裹；21-包装箱体；211-第一凹槽；2111-封板；212-第二凹槽；3-无人机；31-电池仓；311-第一卡扣； 41-储物台； 411-左侧储物柜；4111-隔板；4112-第一移位滚轮；412-右侧储物柜；4121-第一竖直导轨；4122-第一水平导轨；4123-电池夹持件；4124-第二卡扣413-存取平台；4131-存取口；42-货物升降台；421-升降板；422-第二移位滚轮；423-移动机构；424-连杆机构；51-无人机起降平台；52-电池及包裹转移装置；521-轨道；522-移动吊架；5221-滑块；5222-伸缩单元；5223-夹取件；5224-第三卡扣；53-货物过渡装置；531-水平滑轨；54-电池充电柜；541-充电格；542-电池取放机构；5421-第二水平导轨；5422-第二竖直导轨；5423-第三水平导轨；5424-电池承托架；5425-电池固定接口；55-第一传送装置；56-第二传送装置。
具体实施方式
为了使本发明的目的、技术方案及优点更加清楚明白，以下结合附图及实施例，对本发明进行进一步详细说明。应当理解，此处所描述的具体实施例仅用以解释本发明，并不用于限定本发明。
需说明的是，当部件被称为“固定于”或“设置于”另一个部件，它可以直接或者间接在该另一个部件上。当一个部件被称为“连接于”另一个部件，它可以是直接或者间接连接至该另一个部件上。
术语“上”、“下”、“左”、“右”等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作，因此不能理解为对本专利的限制。术语“第一”、“第二”仅用于便于描述目的，而不能理解为指示或暗示相对重要性或者隐含指明技术特征的数量。“多个”的含义是两个或两个以上，除非另有明确具体的限定。
如图1至图5所示，本发明实施例提供的电池1包括电池本体和夹持机构，可应用于快递物流领域的无人机。其中，夹持机构与电池本体连接，且夹持机构用于在包裹2装载到电池上时夹取包裹2，并在包裹2从电池上卸载时释放包裹2。本发明实施例使得包裹2可以在装载前先与电池1组合，然后一起装载到无人机上，也可作为一个整体从无人机上一起卸载下来，然后再进行拆分，提高了无人机停留期间的装卸效率，也即实现了无人机在更换电池1时同步完成包裹2的装卸,节省了装卸时间，提高了装卸效率；并使得无人机以及相关配套装置的结构得到了简化。
可以理解的是，夹持机构可以位于电池本体内部，也可以位于电池本体外部。并且，夹持机构可以直接与电池本体连接，也可以通过中间连接件间接连接到电池本体。
可以理解的是，电池1与包裹2之间也可以通过其他快速连接与拆卸结构进行连接，例如电磁吸附，也可为其他结构，此处不作唯一限定。
进一步地，在本发明的一个实施例中，夹持机构位于电池本体内。具体地，电池本体包括外壳11和电池组12，夹持机构包括驱动组件13和夹持组件14。其中，电池组12和驱动组件13均设置在外壳11内，电池组12可以由多节电池堆叠并串联而成，夹持组件14与驱动组件13驱动连接且用于夹取和释放包裹2。在本实施例中，夹持组件14转动连接于外壳11的底部且部分伸出外壳11的底部，并在驱动组件13的驱动下进行开合运动，以夹取或释放包裹2。
进一步地，外壳11大致呈长方体型且内部具有一用于容纳电池组12和驱动组件13的容纳腔，驱动组件13位于容纳腔的中部且用于驱动夹持组件14夹取或释放包裹2，另外，在驱动组件13的两侧均设置有电池组12。在本实施例中，夹持组件14设置在驱动组件13的下方且在驱动组件13的驱动下进行开合运动。
进一步地，在本发明的一个实施例中，包裹2包括包装箱体21，该包装箱体21内具有一封闭的容纳空间，并在包装箱体21的上端面对称设置有第一凹槽211和第二凹槽212，并且在第一凹槽211和第二凹槽212的槽口相对的一侧均设有封板2111；夹持组件14的端部伸入凹槽后，在驱动组件驱动下闭合，并实现抵接于封板2111的内表面上，进而实现夹持组件14夹取住包裹2。另外，该第一凹槽211和第二凹槽212也便于用户抓取包裹2。优选的，在本发明的有些实施例中，对于上盖为一个整体的上述包装箱体21，则开设一个凹槽以替代上述第一凹槽211和第二凹槽212，同时在该凹槽的中部设置封板以替代上述设置在第一凹槽211和第二凹槽212内的封板2111。
进一步地，在本发明的一个实施例中，还包括有通信单元，在外壳11的外表面上设置有电源接口114，该电源接口114与电池组12和/或驱动组件13分别电连接。具体地，该电源接口114可用于为电池组12充电，也可以用于使用电池组12为外部设备（优选为无人机）供电。通信单元通过有线或无线的方式与外部设备（优选为无人机）进行信号传输，且外部设备自身也设有与电池1中的通信单元相配合的通信单元，以实现外部设备控制电池1中的驱动组件13驱动夹持组件14完成夹取和释放包裹2。同时，电池1也可对外部设备反馈信息。
进一步地，在本发明的一个实施例中，在外壳11的两相对侧面上均设有用于将电池1可拆卸连接在外部设备（具体可为外部设备的电池仓内）的多个卡槽113。相应地，在电池仓的内壁上设置有与卡槽配合的卡扣。可以理解的是，在本发明的其它实施例中，也可以在外壳11的两相对侧面上设置有卡扣，相应地，在电池仓的内壁上设置有与卡扣配合的卡槽。
进一步地，于本发明的某些实施例中，外部设备与电池1之间设置有快速连接与快速拆卸的快拆机构，例如电磁吸附，并不限于上述卡扣与卡槽的卡接配合，此处不作唯一限定。
进一步地，结合图6，在本发明的一个实施例中，驱动组件13包括第一挡板131、第二挡板132、第一驱动器133和齿轮组134。其中，第一挡板131和第二挡板132均设置在外壳11内且相互平行设置。第一驱动器133设置在第一挡板131上。该第一驱动器133优选为舵机。齿轮组134设置在第一挡板131远离第一驱动器133的一侧且与第一驱动器133的输出轴连接。该齿轮组134作为传动机构，其末端齿轮与夹持组件14连接且用于带动夹持组件进行开合运动，以便于夹取或释放包裹2。
进一步地，齿轮组134包括第一级齿轮1341、第二级齿轮1342、第三级齿轮1343、第四级齿轮1344和第五级齿轮1345。其中，第一级齿轮1341与第一驱动器133的输出轴连接；第二级齿轮1342与第一级齿轮1341啮合；第三级齿轮1343与第二级齿轮1342啮合；第四级齿轮1344与第二级齿轮1342啮合；第五级齿轮1345与第四级齿轮1344啮合。第三级齿轮1343和第五级齿轮1345与夹持组件14连接。当第一驱动器133工作时，带动夹持组件14进行开合运动。
进一步地，在本发明的一个实施例中，夹持组件14包括转动连接在第一挡板131和第二挡板132之间的第一夹持板141和第二夹持板142。其中，第一夹持板141和第二夹持板142相对设置，第一夹持板141的一端与第三级齿轮1343连接，第二夹持板142的一端与第五级齿轮134连接。该第一夹持板141与第一凹槽211配合，第二夹持板142与第二凹槽212配合，以实现电池1夹取和释放包裹2。
进一步地，在本发明的一个实施例中，在外壳11的底部分别开设有第一开口111和第二开口112，该第一开口111与第一夹持板141对应且用于为第一夹持板141提供可转动的空间，第二开口112与第二夹持板142对应且用于为第二夹持板142提供可转动的空间。
进一步地，在本发明的一个实施例中，电池1还包括第二驱动器15以及锁止件16。该锁止件16用于在第二驱动器15的驱动下转动并抵接在第四级齿轮1344上，以锁止齿轮组13的传动过程。当电池1和包裹2组合后装载在无人机上时，通过锁止件16将齿轮组13的传动过程锁止，可减小无人机在空中时由于第一驱动器133失效而导致包裹2脱离电池1的风险。
进一步地，结合图7图8，本发明实施例还提供了一种无人机3，该无人机3包括机架以及如上述所述的电池1。具体地，在无人机3的机架的底部设有电池仓31，该电池仓31的开口朝下，电池1可拆卸连接在该电池仓31内，包裹2与电池1一起装载到无人机3的底部。另外，在电池仓31内设置有与电源接口114匹配的接口，以便于电池1为无人机3供电或充电。例如无人机3内设置有其他供电单元，电池1可对该供电单元进行充电，以保证无人机3在未装载有电池1时依然具有电能供应。同时无人机3内置有与电池1上的通信单元相对应的通信单元，通信单元之间通过有线或无线的方式进行信号传输，以实现无人机3对电池1的控制或者电池1对无人机3反馈信息。
在本发明的一个实施例中，在电池仓31的内壁上设有第一卡扣311，此时在电池1的外壳11的两相对侧面上设有与第一卡扣311匹配的卡槽。
进一步地，结合图9和图10，本发明实施例还提供了一种自动终端，该自动终端包括储物台41以及货物升降台42。其中，储物台41用于临时存储包裹2和电池1，并且实现对无人机电池1更换及充电功能；货物升降台42用于转运电池1和包裹2，还用于举升电池1和包裹2以使电池1与无人机3对接。另外，在储物台41内设置有用于对电池1进行更换及充电的电池更换机构。
具体地，储物台41包括储物柜和存取平台413，储物柜包括相对设置的左侧储物柜411和右侧储物柜412，存取平台413设置在左侧储物柜411和右侧储物柜412的顶部。左侧储物柜411和右侧储物柜412之间形成搬运通道，货物升降台42位于搬运通道内，在存取平台413上开设有存取口4131，该存取口4131位于搬运通道的正上方。当无人机3降落在存取平台413上时，其电池1和包裹2位于存取口431正上方。
进一步地，左侧储物柜411和右侧储物柜412内均平行设置有多个隔板4111，该隔板4111将左侧储物柜411和右侧储物柜412分成多个平行设置的存储位，每一存储位的开口正对搬运通道，该存储位用于临时存储包裹2，并在其中全部或部分的存储位中设有将电池1从包裹2上装卸并为电池1充电的电池更换机构。另外，在每一隔板4111上均设置有多个第一移位滚轮4112及与第一移位滚轮4112驱动连接且用于驱动第一移位滚轮4112转动的第一驱动件，包裹2在该第一移位滚轮4112的驱动下能够移出或存入存储位。
进一步地，结合图11，货物升降台42包括升降板421、第二移位滚轮422、第二驱动件及移动机构423。其中，在升降板421上平行设置有多个第二移位滚轮422，且多个第二移位滚轮422在第二驱动件的驱动下转动，第一移位滚轮4112与第二移位滚轮422共同完成包裹2和电池1在升降板421及置物板隔板4111之间的转移。移动机构423连接于升降板421。可以理解的是，本发明实施例的自动终端还可包括设置在搬运通道内的滑轨，移动机构423滑动连接在滑轨上以实现货物升降台42在搬运通道内的移动。自动终端还可包括用于驱动移动机构423沿滑轨滑动的第三驱动件。
进一步地，货物升降台42还包括第四驱动件及与第四驱动件驱动连接的连杆机构424，该连杆机构424在第四驱动件的驱动下展开或收缩，上述移动机构423及升降板421通过连杆机构424连接。当第四驱动件驱动连杆机构424展开时，升降板421向远离滑杆的方向运动，当第四驱动件驱动连杆机构424收缩时，升降板421向靠近滑杆的方向运动，通过设置连杆机构424，在无人机3将电池1和/或包裹2卸载至货物升降台42的过程中，可抬升升降板421，以接收卸载的电池1和/或包裹2。以及在无人机3从货物升降台42装载电池1和/或包裹2过程中，抬升升降板421以实现无人机3装载电池1和/或包裹2。
进一步地，在本发明的一个实施例中，电池更换机构包括设置在存储位中的第一竖直导轨4121、滑动连接在第一竖直导轨4121上的第一水平导轨4122、设置在第一水平导轨4122下方且用于夹持电池1的至少一个电池夹持件4123（优选的，也可在电池夹持件4123与第一水平导轨4122之间设置驱动导向组件，具体可为与电池夹持件4123滑动连接的导轨，以实现电池夹持件4123沿着该导轨移动时实现靠近或远离储存位的开口的运动），以及用于驱动第一水平导轨4122在第一竖直导轨4121上滑动的竖直驱动件和用于驱动电池夹持件4123在第一水平导轨4122上滑动的水平驱动件。具体地，电池夹持件4123具有向下的第一开口，在第一开口的内壁上设有第二卡扣4124，此时在电池1的外壳11的两相对侧面上设有与第二卡扣4124匹配的卡槽113。
另外，在电池夹持件4123的底部设置有与电源接口114匹配的第一接口，用于为电池夹持件4123内的电池1充电。同时上述终端还包括有与电池1上的通信单元相互联的通信单元，优选的可设置在电池夹持件4123内，通信单元之间通过有线或无线的方式进行信号传输，以实现自动终端对电池1的控制或者电池1对终端反馈信息。
可以理解的是，当第一水平导轨4122上滑动连接的电池夹持件4123为多个时，其目的是实现单一存储位中的电池更换机构可更换多个电池1并充电。当其中一个电池夹持件4123需要将电池1从包裹2上卸下充电或将充好的电池1装配到包裹2上时，该夹持件4123在第一水平导轨4122上移动至对接位置的上方并沿着第一竖直导轨4121向下移动直至与待充电电池1对接或者该夹持件4123夹持的电池1与包裹2对接。第一水平导轨4122上的电池夹持件4123数量设置应确保所有电池夹持件4123均能移动至指定的对接位置。
具体地，上述自动终端实现将无人机3搭载的电池1和包裹2卸下并拆分的过程为：无人机3降落在存取平台413上，货物升降台42移动至存取口，并通过连杆机构424带动升降板421向上运动并承接无人机3卸载的电池1和包裹2，然后货物升降台42通过连杆机构424带动升降板421下降并通过移动机构423沿搬运通道向下运动直至升降板与其中一存储位的隔板4111等高，再通过第二移位滚轮422和第一移位滚轮4112将包裹2和电池1组合转移至相邻的存储位；电池夹持件4123通过水平和竖直运动以使其中一空置的电池夹持件4123夹持包裹2上的电池1，并且控制电池1释放夹持的包裹2，然后电池夹持件4123上升并开始对取下的电池1进行充电，而包裹2将停留在同一存储位或被转移至其他存储位进行暂存。
自动终端实现将电池1和包裹2组合并装载到无人机3的过程为：将待无人机3装载的包裹2通过货物升降台42转移至其中一存储位或本已暂存于此的存储位，夹持待无人机3装载的电池1的夹持件4123通过水平和竖直运动移动至指定的对接位置，并控制电池1夹持住包裹2，完成新的电池1与待装载包裹2的组合，可以理解的是，电池1与包裹2可以在无人机3降落前进行组合；然后夹持件4123释放电池1，并通过第一竖直导轨4121向上移动，以使电池夹持件4123的卡扣脱离新的电池1的卡槽；第一移位滚轮4112和第二移位滚轮422协同工作将装配好的电池1和包裹2转移至升降板421上，然后货物升降台42上升至存取口，升降板421抬升直至电池1推入无人机3的电池仓31内，无人机3通过卡扣固定住该电池1，进而实现无人机3装载电池1和包裹2。
进一步的，自动终端还能实现在无人机3未携带包裹2时仅更换无人机3的电池1的功能，具体实现方式为，无人机3卸载的电池1可由货物升降台42接收并转移至其中一存储位，该存储位的电池更换机构夹持卸载的电池1并进行充电，然后电池更换机构释放另一待无人机3装载的电池1，电池1由该存储位转移至货物升降台42，并由货物升降台42最终装载至无人机3。另一种实现方式为，由自动终端提供辅助更换无人机3的电池1的包裹2或其它装置，该装置具有和包裹2一样的可被无人机3的电池1夹取的对接口。具体过程为，包裹2或其它装置由自动终端的某一存储位通过货物升降台42转移至存取口并抬升，无人机3控制电池1夹取住包裹2或其它装置，然后无人机3卸载电池1，包裹2或其它装置与电池1的组合由货物升降台42接收并转移至其中一存储位，该存储位的电池更换机构从包裹2或其它装置上拆卸无人机3卸载的电池1并装载另一待无人机3装载的电池1至包裹2或其它装置，然后，包裹2或其它装置与电池1的组合由存储位转移至货物升降台42，并由货物升降台42装载至无人机3，无人机3控制电池1释放包裹2或其它装置，自动终端回收包裹2或其他装置。
进一步地，结合图12至图14，本发明实施例还提供了一种转运中心，用于配合无人机快递。具体地，所述转运中心将无人机3收取的包裹2进行卸载和分拣转运，以及将待无人机3配送的包裹2进行分拣和装载，并完成无人机3搭载的电池1的更换。具体地，所述转运中心包括至少一个无人机起降平台51、用于转移电池1及包裹2以及拆分或组合电池1和包裹2的电池及包裹转移装置52、设置在无人机起降平台51与电池及包裹转移装置52之间的货物过渡装置53，以及用于为电池1进行充电的电池充电柜54。其中，无人机起降平台51安装在室外或屋顶可开合的室内以便于无人机3的起飞和降落，电池及包裹转移装置52和电池充电柜54安装在室内，货物过渡装置53安装在无人机起降平台51与电池及包裹转移装置52之间，其可由室外延伸到室内。
进一步地，电池及包裹转移装置52包括轨道521、活动连接在轨道521上的多个移动吊架522，以及用于驱动移动吊架522在轨道上移动的移动吊架驱动件。其中，轨道521安装在室内并距离地面有一定高度，多个移动吊架522竖直向下延伸，该移动吊架522用于从货物过渡装置52接收无人机3卸载的包裹2和电池1，拆分包裹2和电池1并分别转移至收取包裹分拣系统和电池充电系统（具体为电池充电柜54）；该移动吊架522同时用于从电池充电系统和配送包裹分拣系统分别接收待无人机3装载的电池1和包裹2，组合电池1和包裹2并转移至货物过渡装置53。
优选的，对于上述电池及包裹转移装置52的结构，在本发明的某些实施例中，也可利用其它机构进行代替，此处不作唯一限定，例如设置一竖直转轴，在转轴的顶部设置至少一横杆，转轴转动时带动横杆以该转轴为轴心转动，将移动吊架522连于横杆远离转轴的一端的端部，横杆以该转轴为轴心转动能够带动移动吊架522到达各工作位。
进一步地，在本发明的一个实施例中，如图13，移动吊架522包括滑块5221、伸缩单元5222和夹取件5223。其中，滑块5221与轨道521连接且可在轨道521上滑动，伸缩单元5222与滑块5221固定连接且竖直向下延伸，该伸缩单元5222可通过伸缩改变长度，以调节夹取件5223相对于地面的高度，夹取件5223固定连接在伸缩单元5222远离滑块5221的一端，该夹取件5223用于夹取和释放电池1。具体地，该夹取件5223具有向下的第二开口，在电池1的外壳11的两相对侧面上设置有卡槽113，在第二开口的内壁上设有与卡槽配合的第三卡扣5224。另外，在夹取件5223内或电池及包裹转移装置52的其它部分设置有与电池1内的通信单元相配合的通信单元，电池1内的通信单元接收到夹取件5223或电池及包裹转移装置52的其它部分的通信单元发送的控制信号后控制驱动组件13驱动夹持组件14夹取和释放包裹2。
进一步地，货物过渡装置53可采用如上述自动终端所述的货物升降台42（为了结构的简化，货物升降台42中的第二移位滚轮422可不设置），以及水平滑轨531，货物升降台42可在水平滑轨531上滑动。该水平滑轨531的一端延伸至无人机起降平台51区域以使货物升降台42能在无人机3停留时运动至无人机3的下方，另一端延伸至轨道521的下方。该货物过渡装置53用于接收无人机3卸载下来的电池1及包裹2并转移至轨道521的下方，以便于移动吊架522夹取电池1和包裹2，或者从移动吊架522接收无人机3待装载的电池1和包裹2，并将电池1和包裹2转移至起降平台51区域并装载至无人机3。
进一步地，在本发明的一个实施例中，上述转运中心还包括只用于转运包裹2的第一传送装置55和第二传送装置56。其中，第一传送装置55和第二传送装置56的一端设置在轨道521的下方。第一传送装置56从移动吊架522接收无人机3卸载的包裹2，即当其中一移动吊架522夹持电池1和包裹2并移动至第一传送装置55靠近522一端的上方时，移动吊架522的伸缩单元5222向下伸长以使包裹2靠近第一传送装置55，然后控制电池1的夹持组件14释放包裹2，第一传送装置55接收包裹2后将包裹2传送至收取货物分拣系统或其它物流配送环节。第二传送装置56将待无人机3装载的包裹2从配送包裹分拣系统或其它物流配送环节传送至轨道521的下方，当移动吊架522夹持待无人机3装载的电池1并移动至第二传送装置56靠近522一端的上方时，移动吊架522的伸缩单元5222向下伸长并控制电池1的夹持组件14夹取包裹2。优选的，第一传送装置55和第二传送装置56均为皮带传动或滚轮传动。具体地，上述收取包裹分拣系统用于对收取的包裹2根据配送信息进行分类，放置于不同的区域或者转移至不同的区域；上述配送包裹分拣系统根据配送信息将包裹2分配给不同的无人机3。可以理解的是，也可以不设置收取包裹分拣系统，直接将无人机3卸载的包裹由第一传送装置55传送至其它物流配送环节，例如陆路运输环节。或者，也可以不设置配送包裹分拣系统，由其它物流配送环节，例如陆路运输环节，直接转移至第二传送装置。
进一步地，在本发明的一个实施例中，电池充电系统包括电池充电柜54和电池取放机构542，电池充电柜54分隔成多个呈阵列排布的充电格541，该充电格541用于为电池1充电。具体地，在充电格541的内壁上设置有与电池1的电源接口114匹配的第二接口，同时设置有用于固定电池1的卡扣。电池取放机构542设置在充电格541具有开口的一侧，用于接收移动吊架522上的电池1并放入充电格541内，充电格541将电池1固定并为电池1充电；电池取放机构542还可用于将充电格541内的电池1取出，并由移动吊架522接收并固定。同一电池充电柜54可以设置有多个电池取放机构542。
进一步地，电池取放机构542包括设置在电池充电柜54一侧的第二水平导轨5421、滑动连接在第二水平导轨5421上的第二竖直导轨5422、滑动连接在第二竖直导轨5422上的第三水平导轨5423、滑动连接在第三水平导轨5423上的电池承托架5424，以及用于驱动第二竖直导轨5422在第二水平导轨5421上滑动的第五驱动件、用于驱动第三水平导轨5423在第二竖直导轨5422上滑动的第六驱动件和用于驱动电池承托架5424在第三水平导轨5423上滑动的第七驱动件，以使电池承托架5424能够进行三自由度运动（上述电池取放机构542也可利用能够实现三自由度运动的工业机器人替代）。电池承托架5424的顶部开设有电池固定接口5425，其结构与上述包裹2上的第一凹槽211和第二凹槽212的结构相同。在本发明的一个具体实施例中，第二水平导轨5421包括平行设置在电池充电柜54顶部和底部且水平设置的两条轨道，第二竖直导轨5422包括竖直设置在第二水平导轨5421之间且相互平行的两条轨道，第三水平导轨5423包括水平设置在第二竖直导轨5422之间且相互平行的两条轨道，第三水平导轨5423与第二水平导轨5422垂直，以实现电池承托架5424能伸入或伸出充电格541。电池取放机构542接收移动吊架522上的电池1并放入充电格541内，充电格541对电池1固定并充电的过程为：当其中一移动吊架522夹持无人机3卸载的电池1并移动至靠近电池充电柜54一侧的区域时，电池承托架5424移动直至电池承托架5424上的电池固定接口5425位于电池1的夹持组件14的正下方，此时电池承托架5424向上移动或移动吊架522向下伸长直至电池1的夹持组件14能够固定住电池承托架5424的电池固定接口5425。待电池与电池承托架5424对接后，移动吊架522释放电池1，电池承托架5424向下移动以带动电池1与移动吊架522分离，然后电池承托架5424移动并将电池放入电池充电柜54空置的一充电格541内直至该充电格541固定住电池1并开始充电，在充电格541固定电池1之后电池1释放电池固定接口5425，电池承托架5424与电池1脱离并转移出该充电格。电池取放机构542将充电格541内的电池1取出，并由移动吊架522接收并固定的过程为：通过电池承托架5424的移动将充好电的电池1从充电格541取出并转移到移动吊架522上的夹取件5223的正下方，电池承托架5424向上移动以使电池1推入夹取件5223内，使得电池1的卡槽113与夹取件5223的卡扣配合并使夹取件5233夹持住电池1，然后电池1的驱动组件13驱动夹持组件14放开电池承托架5424，然后电池承托架5424移动以脱离电池1。
进一步地，在本发明的一个具体实施例中，如图12，轨道521为环形导轨，多个无人机起降平台51设置在环形导轨的一侧且并排设置，货物过渡装置53设置在无人机起降平台51与环形导轨之间，电池充电柜54设置在环形导轨的另一侧，货物过渡装置53、第一传送装置55、电池取放机构542及第二传送装置56围绕设置在环形导轨的周围，并按移动吊架522沿轨道521移动的方向设置货物过渡装置53、第一传送装置55、电池取放机构542及第二传送装置56的位置顺序。优选的，上述轨道521也可为直线导轨，无人机起降平台51分别设于轨道521的两端，无人机3分别在轨道521的两端进行卸载和装载电池1和包裹2，当然也可由其他结构替代，此处不作唯一限定。
在本实施例中，转运中心的工作原理如下：无人机3降落在无人机起降平台51上，货物过渡装置53接收无人机3卸载的电池1和包裹2并将电池1和包裹2转移至轨道521的下方，移动吊架525降低夹取件5223的高度夹取电池1和包裹2，然后移动吊架525提升夹取件5223的高度并转移至第一传送装置55靠近移动吊架522一端的上方，移动吊架522降低夹取件5223高度，电池1的夹持组件14释放包裹2，第一传送装置55接收包裹2并传送至收取包裹分拣系统，移动吊架522继续移动至靠近电池充电柜54一侧的区域，通过电池取放机构542将移动吊架522上的电池1转移到充电格541内进行充电，电池取放机构542将待无人机3装载的电池1转移到移动吊架522上，移动吊架522继续移动并转移至第二传送装置56靠近移动吊架522一端的上方，移动吊架522降低5223的高度并且电池1的夹持组件14夹取待无人机3装载的包裹2，移动吊架522继续移动并转移至货物过渡装置53的上方，货物过渡装置53接收移动吊架522上的电池1和包裹2并转移到空载的无人机3上，无人机3起飞运送包裹2。
需要说明的是，转运中心设置有多个移动吊架522，电池1与包裹2的拆分与组合同步进行，货物过渡装置53将无人机3卸载的电池1和包裹2转移至移动吊架522后随即可从另一移动吊架522接收待无人机3装载的电池1和包裹2。
以上所述仅为本发明的较佳实施例而已，并不用以限制本发明，凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等，均应包含在本发明的保护范围之内。

Claims (16)

  1. 一种电池，其特征在于，包括电池本体、与所述电池本体相连且用于夹取和释放包裹的夹持机构。
  2. 如权利要求1所述的电池，其特征在于，所述电池本体包括外壳以及设置在所述外壳内的电池组；所述夹持机构包括设置在所述外壳内的驱动组件，以及与所述驱动组件驱动连接且用于在所述驱动组件的驱动下进行开合运动以夹取或释放包裹的夹持组件。
  3. 如权利要求2所述的电池，其特征在于，所述夹持组件包括第一夹持板和第二夹持板，所述驱动组件包括第一驱动器、与所述第一驱动器的输出轴相连且用于驱动所述第一夹持板和所述第二夹持板转动的齿轮组；
    和/或，所述包裹的包装箱体的上端面设有与所述第一夹持板匹配的第一凹槽，以及与所述第二夹持板匹配的第二凹槽。
  4. 如权利要求2或3所述的电池，其特征在于，所述外壳的两相对侧面上设有用于与外部设备相连的卡槽；
    和/或，所述外壳的一侧面上裸露有电源接口。
  5. 如权利要求1至3任一项所述的电池，其特征在于，还包括通信单元，所述通信单元用于和外部设备通信，以实现外部设备控制夹持机构夹取和释放包裹。
  6. 一种无人机，其特征在于，包括如权利要求1至5任一项所述的电池，所述无人机的底部具有用于容纳所述电池且开口向下的电池仓。
  7. 一种自动终端，其特征在于，包括具有储物柜的储物台，所述储物柜内设有用于更换如权利要求1至5任一项所述的电池并为所述电池充电的电池更换机构。
  8. 如权利要求7所述的自动终端，其特征在于，所述电池更换机构包括第一竖直导轨、滑动连接在所述第一竖直导轨上的第一水平导轨、设置在所述第一水平导轨下方且用于夹持所述电池的至少一个电池夹持件，以及用于驱动所述第一水平导轨在所述第一竖直导轨上滑动的竖直驱动件和用于驱动所述电池夹持件在所述第一水平导轨上滑动的水平驱动件，所述电池上设有电源接口，所述电池夹持件内设置有与所述电源接口匹配的第一接口。
  9. 一种转运中心，其特征在于，用于配合无人机快递实现包裹中转，所述转运中心包括用于为如权利要求1至5任一项所述的电池进行充电的电池充电柜、用于转移所述电池和所述包裹的电池及包裹转移装置，所述电池的夹持机构用于夹取和释放所述包裹。
  10. 如权利要求9所述的转运中心，其特征在于，所述电池及包裹转移装置包括轨道、活动连接在所述轨道上的多个移动吊架、以及用于驱动所述移动吊架在所述轨道上移动的移动吊架驱动件。
  11. 如权利要求9所述的转运中心，其特征在于，所述电池充电柜包括用于为所述电池充电的多个充电格、用于将所述电池及包裹转移装置上的所述电池转移至所述充电格内且用于将所述充电格内的所述电池转移至所述电池及包裹转移装置的电池取放机构，所述电池取放机构位于所述充电格具有开口的一侧。
  12. 如权利要求9所述的转运中心，其特征在于，还包括用于将所述电池和所述包裹从无人机转移至所述电池及包裹转移装置的货物过渡装置。
  13. 如权利要求12所述的货物过渡装置，还包括水平滑轨、与所述水平滑轨滑动连接的货物升降台。
  14. 如权利要求12所述的转运中心，其特征在于，还包括用于将所述包裹传送至物流配送环节的第一传送装置、以及用于从物流配送环节运送待装载的所述包裹的第二传送装置，所述货物过渡装置、所述第一传送装置、所述电池充电柜及所述第二传送装置依次设置于所述电池及包裹转移装置的外围。
  15. 货物的拆装方法，利用如权利要求7或8所述的自动终端对货物进行拆装，所述货物包括如权利要求1至5任一项所述的电池和包裹，其特征在于，包括以下步骤：
    将所述货物从外部设备卸下；
    所述电池更换机构将所述货物中的所述电池和所述包裹拆分，并对所述电池的电池本体充电；
    将所述包裹置于存储位暂存；
    将充电完成的所述电池与存储位上的待配送的所述包裹组合形成所述货物；
    将所述货物装载于所述外部设备。
  16. 货物的拆装方法，利用权力要求9至14任一项所述的转运中心对货物进行拆装，所述货物包括如权利要求1至5任一项所述的电池和包裹，其特征在于，包括以下步骤：
    将所述货物从外部设备卸下；
    所述电池及包裹转移装置将所述货物具有的所述电池和所述包裹拆分，并将所述电池转移至所述电池充电柜；
    将所述包裹转移至物流配送环节；
    所述电池充电柜对拆分后的所述电池充电；
    将所述电池充电柜内充电完成的所述电池与物流配送环节接收的待配送的所述包裹组合形成所述货物；
    将所述货物装载于所述外部设备。
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