WO2019042245A1 - 无人机用货物收发系统及货物的收取和寄送方法 - Google Patents

无人机用货物收发系统及货物的收取和寄送方法 Download PDF

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Publication number
WO2019042245A1
WO2019042245A1 PCT/CN2018/102484 CN2018102484W WO2019042245A1 WO 2019042245 A1 WO2019042245 A1 WO 2019042245A1 CN 2018102484 W CN2018102484 W CN 2018102484W WO 2019042245 A1 WO2019042245 A1 WO 2019042245A1
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WO
WIPO (PCT)
Prior art keywords
cargo
drone
work area
baffle plate
lifting mechanism
Prior art date
Application number
PCT/CN2018/102484
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 WO2019042245A1 publication Critical patent/WO2019042245A1/zh
Priority to US16/803,693 priority Critical patent/US11964778B2/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/30—Launching, take-off or landing arrangements for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
    • 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
    • B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
    • 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
    • B64F1/18—Visual or acoustic landing aids
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/90—Launching from or landing on platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
    • B66F7/06—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported by levers for vertical movement
    • B66F7/065—Scissor linkages, i.e. X-configuration
    • E—FIXED CONSTRUCTIONS
    • E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
    • E01F3/00—Landing stages for helicopters, e.g. located above buildings
    • 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
    • B64F1/32—Ground or aircraft-carrier-deck installations for handling freight
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
    • B64U2101/64—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for parcel delivery or retrieval

Definitions

  • the invention relates to a cargo receiving and dispatching system for a drone and a method for collecting and sending goods.
  • a cargo transmission and reception system for a drone comprising:
  • a support assembly comprising a landing platform mountable on a building, the landing platform having a work surface provided with a work area for landing of the drone and placement of the supply;
  • a barrier assembly disposed adjacent an edge of the work surface and at least partially above a plane of the work surface such that the barrier assembly separates the work area from a side of the barrier assembly away from the work area open.
  • a method for collecting goods includes the following steps:
  • the drone is landed on the work area of the above-mentioned cargo transmission and reception system for a drone;
  • the drone places the cargo on the work area
  • the drone flies away from the work area
  • the cargo is removed from the side of the isolation assembly remote from the work area.
  • a method for delivering goods comprising the following steps:
  • the drone is landed on the work area
  • the drone collects the cargo and carries the cargo away from the work area. .
  • FIG. 1 is a structural view showing a fully deployed state in which a cargo transmission and reception system for a drone according to an embodiment is mounted on a building;
  • FIG. 2 is a structural view showing a standby state in which a cargo transmission and reception system for a drone shown in FIG. 1 is installed on a building;
  • FIG. 3 is an electrical connection diagram of the cargo transmission and reception system for the unmanned aerial vehicle shown in FIG. 1;
  • FIG. 4 is a schematic structural view of another angle of the barrier assembly of the cargo transceiving system for the unmanned aerial vehicle shown in FIG. 1;
  • Figure 5 is an enlarged view of a portion I of the barrier assembly shown in Figure 4.
  • FIG. 6 is a schematic structural view showing a semi-expanded state of the cargo transmission and reception system for the unmanned aerial vehicle shown in FIG. 1;
  • Figure 7 is an enlarged view of a portion II of the cargo transmission and reception system for the unmanned aerial vehicle shown in Figure 6;
  • Figure 8 is an enlarged view of a portion III of the cargo transmission and reception system for the unmanned aerial vehicle shown in Figure 6;
  • FIG. 9 is a schematic structural view of a lifting mechanism of the cargo transmission and reception system for a drone shown in FIG. 1;
  • FIG. 10 is a schematic structural view showing a fully deployed state of a cargo transmitting and receiving system for a drone according to another embodiment
  • Figure 11 is a schematic view showing the structure of the semi-expanded state of the cargo transmission and reception system for the unmanned aerial vehicle shown in Figure 10;
  • FIG. 12 is a schematic structural view showing an unfolded state of a cargo transmission and reception system for a drone according to another embodiment
  • Figure 13 is a schematic view showing the structure of the pickup state of the cargo transmission and reception system for the unmanned aerial vehicle shown in Figure 12;
  • Fig. 14 is a view showing the configuration of the folded state of the cargo transmitting and receiving system for the unmanned aerial vehicle shown in Fig. 12.
  • an unmanned aerial cargo receiving and dispatching system 10 of an embodiment is used for temporary storage of express delivery, so that the drone can unload the goods on the unmanned cargo receiving and dispatching system 10, and the user collects; or The user places the goods on the unmanned cargo receiving and dispatching system 10, and the drone picks up the pieces.
  • the UAV cargo transceiving system 10 can be installed outside the building 20, and the building 20 is a balcony or a window.
  • the UAV cargo transceiving system 10 can be installed on the outside of the user's balcony fence and below the window sill. and many more.
  • the cargo handling system 10 for the drone includes a support assembly 100, an electronic control assembly 200, a barrier assembly 300, and a lifting mechanism 400.
  • the support assembly 100 can be secured to the building 20.
  • the support assembly 100 is a support structure for the entire unmanned cargo handling system 10 that is capable of landing for drones and storage of cargo.
  • the support assembly 100 includes a fixing base 110 and a landing platform 120.
  • the mount 110 can be fixed to the building 20.
  • the mount 110 is a support and fixed component of the entire unmanned cargo handling system 10.
  • the mount 110 includes two spaced and parallelly disposed mounting posts 112 that are each mountable to the building 20.
  • the landing platform 120 is mounted on the mount 110.
  • the landing platform 120 has a work surface 122 on which a work area (not labeled) for drone landing and cargo placement is provided.
  • the landing platform 120 is generally in the shape of a square plate, and the work area is located in the middle of the work surface 122.
  • the landing platform 120 is rotatably coupled to the fixed base 110 to enable the working surface 122 to be horizontal, so that the working area can be placed and the drone is lowered, and the working surface 122 can be vertical. Tilting in a straight or relatively vertical direction to enable the landing platform 120 to be in close proximity to the building 20 such that the landing gear 120 can be in close proximity to the building 20 when the drone cargo handling system 10 is in a standby state.
  • the landing platform 120 is provided with a holding portion (not shown), and the fixing base 110 is provided with the holding portion.
  • the mating device (not shown) is engaged with the mating phase by the retaining portion to fix the landing platform 120 to the building 20.
  • the mating device can be an electronic lock that can be unlocked according to a control signal from a drone or a user's client.
  • the supporting assembly 100 further includes a driving member 130.
  • the driving member 130 is a telescopic rod.
  • the two ends of the driving member 130 are respectively opposite to the fixing base 110 and the middle of the landing platform 120.
  • the driving member 130 can be telescoped to drive the landing platform 120 to rotate.
  • one end of the landing platform 120 is rotatably coupled to the two fixing posts 112.
  • the driving member 130 is a telescopic hydraulic cylinder or an electric strut.
  • the driving members 130 are two, and one ends of the two driving members 130 are respectively rotatably connected to the two fixing posts 112, and the other ends are rotatably connected to the central portions of opposite sides of the landing platform 120.
  • the number of the driving members 130 is not limited to two, and may be one or more than three.
  • the driving member 130 is not mounted on the fixing base 110, and the two ends of the driving member 130 are respectively The middle portion of the building 20 and the baffle plate are rotatably connected; when the number of the driving members 130 is greater than three, the partial driving member 130 can be rotatably connected to the fixing base 110 and the lifting platform 120, and the other portion of the driving member 130 is rotatably connected to the landing platform 120. And building 20.
  • the driving member 130 is not limited to being configured as a telescopic rod.
  • the driving member 130 may also be a stepping motor.
  • the driving member 130 is connected to the rotating shaft connecting the fixing base 110 and the landing platform 120 to realize the take-off and landing.
  • the landing platform 120 when the surface 122 is horizontally disposed; or the end of the support rod away from the landing platform 120 may also be directly rotatably connected to the building 20.
  • the number of support bars can be set as needed.
  • the support rod is a telescopic rod.
  • the fixing base 110 is not limited to the structure of the above-mentioned fixing post 112.
  • the fixing base 110 may also be a plate-like structure, a regular or irregular block structure or the like.
  • the electronic control unit 200 is used to control the operation of the cargo transmission and reception system 10 for the drone.
  • the electronic control component 200 is capable of receiving a control signal.
  • the control signal is a control signal sent by the drone, or the control signal may also be a control signal sent by the user through the client, wherein the client may be an electronic device, such as a mobile phone or a computer.
  • the electronic control assembly 200 can also send a feedback signal to the drone or user's client to enable the drone to land, unload or pick up based on the feedback signal, or to enable the user to place the item based on the feedback signal.
  • the electronic control assembly 200 is mounted on a fixed post 112 of the mount 110.
  • the electronic control unit 200 is electrically connected to the mating device disposed on the fixed base 110, and sends a control signal to the electronic control unit 200 through the drone or the user's client.
  • the electronic control unit 200 controls the engaging device to unlock according to the control signal.
  • the electronic control assembly 200 is not limited to being mounted on the fixed base 110.
  • the electronic control assembly 200 can also be mounted on the building 20, the landing platform 120, and the like.
  • the electronic control assembly 200 is electrically connected to the driving member 130, and the electronic control assembly 200 can control the operation of the driving member 130. Specifically, the electronic control assembly 200 is capable of controlling the operation of the drive member 130 in accordance with the control signal.
  • the barrier assembly 300 is disposed adjacent the edge of the work surface 122 when horizontal and at least partially above the plane of the work surface 122 when horizontal, to enable the barrier assembly 300 to separate the work area from the side of the barrier assembly 300 remote from the work area. .
  • the height of the portion above the plane of the working surface 122 when the blocking assembly 300 is horizontal is greater than or equal to the distance from the rotor of the drone to the working surface 122.
  • the barrier assembly 300 includes a baffle 310 and a movable door 320.
  • the baffle 310 can be located at an edge of the work surface 122 near horizontal and can be positioned at least partially above the plane of the work surface 122 when horizontal. That is, the work area is located on one side of the baffle 310, and the baffle plate 310 is located between the building 20 and the work area. And the height of the portion above the plane of the working surface 122 when the baffle plate 310 is horizontal is greater than or equal to the distance from the rotor of the drone to the working surface 122.
  • the blocking plate 310 is provided with a pick-and-place port 312 for picking up and dropping the goods, and the pick-and-place port 312 is for the user to pick up and release the goods from the side of the baffle plate 310 away from the working area.
  • the baffle plate 310 is substantially in the shape of a square plate.
  • the baffle plate 310 has two opposite surfaces, one of which is a blocking surface 314, and the blocking surface 314 is disposed adjacent to the working area, and the pick-and-place port 312 penetrates the two surfaces.
  • the movable door 320 is movably mounted on the baffle plate 310, and the movable door 320 can cover the pick-and-place port 312.
  • the movable door 320 and the baffle plate 310 can collectively separate the working area from the side of the baffle plate 310 away from the working area, the user
  • the side away from the work area picks up the goods through the pick-and-place port 312, which can isolate the user and the drone.
  • the movable door 320 is mounted on the surface of the baffle plate 310 away from the blocking surface 314.
  • the movable door 320 and the baffle plate 310 are both transparent members, such as glass, acrylic, etc., thereby reducing the obstruction of the baffle 310 and the movable door 320 to the user's field of view.
  • the illustrated embodiment there are two movable doors 320, and two movable doors 320 are movably mounted on the baffle plate 310, and the two movable doors 320 cooperate to shield the pick-and-place port 312.
  • the two movable doors 320 are respectively provided with a locking hole 322.
  • the blocking plate 310 is mounted with an electronic lock 330.
  • the electronic lock 330 can be inserted into the locking holes 322 of the two movable doors 320.
  • the electronic lock 330 is electrically connected to the electronic control component 200, and the electronic control component 200 can control the unlocking of the electronic lock 330.
  • the electronic control component 200 can control the electronic lock 330 to be unlocked according to a control signal sent by the user to enable the user to push the movable door 320 open. That is, without receiving the control signal, the electronic lock 330 remains locked so that the movable door 320 cannot be opened.
  • the barrier assembly 300 further includes a slide rail 340 fixed on the baffle plate 310.
  • the movable door 320 is mounted on the slide rail 340 and slidable along the slide rail 340, and the movable door is realized by sliding the movable door 320. 320 is turned on and off.
  • two slide rails 340 are disposed on the surface of the baffle plate 310 away from the blocking surface 314 and are spaced apart in parallel.
  • the pick-and-place port 312 is located between the two slide rails 340.
  • the opposite sides of each movable door 320 are slidable along the two slide rails 340, respectively.
  • the opening and closing of the movable door 320 is not limited to the sliding manner.
  • the movable door 320 can also be rotatably connected with the blocking plate 310.
  • the sliding rail 340 can be omitted and rotated by the opposite blocking plate 310.
  • the door 320 is used to open and close the movable door 320; the movable door 320 is not limited to two.
  • the movable door 320 may also be one, and one of the movable door 320 and the baffle plate 310 has a locking hole 322, and the other is installed.
  • Electronic lock 330 is not limited to the sliding manner.
  • the movable door 320 can also be rotatably connected with the blocking plate 310.
  • the sliding rail 340 can be omitted and rotated by the opposite blocking plate 310.
  • the door 320 is used to open and close the movable door 320; the movable door 320 is not limited to two.
  • the movable door 320 may also be one, and one
  • the movable door 320 may also adopt an automatic induction opening function, that is, a motion driver and a human body sensing device of the movable door 320.
  • the human body sensing device may be an infrared sensor or an ultrasonic sensor.
  • the baffle plate 310 can be moved to enable the baffle plate 310 to be located at the edge of the work surface 122 near the horizontal and can be at least partially above the plane of the work surface 122 when horizontal.
  • the drone can be lowered to the working area when the working surface 122 is horizontal, and the baffle 310 can also be located above the working area when the working surface 122 is horizontal and spaced and opposed to the working surface 122 when horizontal, so that the baffle 310 can Cooperating with the movable door 320 to block the work area to prevent the goods in the work area from being wet by the rain and to prevent the drone from falling to the work area.
  • the baffle plate 310 when the baffle plate 310 is parallel or inclined with respect to the vertical direction, the baffle plate 310 is located between the building 20 and the work area, the work area is exposed, and the drone can be lowered to the work area; the baffle plate 310 is located above the work area.
  • the position of the pick-and-place port 312 corresponds to the position of the work area. Specifically, when the working surface 122 is horizontally above the working area and spaced apart from the horizontal working surface 122, the blocking surface 314 is parallel to the working surface 122; and the position of the pick-and-place 312 is opposite to the working area. correspond.
  • the baffle 310 can be rotated to enable the baffle 310 to be located adjacent the edge of the work surface 122 and can be positioned above the work area.
  • One end of the baffle plate 310 is rotatably connected to the fixing base 110, and the other end is a free end.
  • the free end of the baffle plate 310 can be higher than the end of the baffle plate near the fixed seat 110 so that the movable door 320 and the baffle plate 310 together can block the working area.
  • the plates 310 are spaced apart from one side of the work area.
  • the end of the baffle plate 310 away from the fixing base 110 is provided with a buckle 315 .
  • the fixing base 110 is provided with an engaging portion 114 that can be engaged with the buckle 315 . It is also rotatable to an end closer to the fixing base 110 than the free end of the blocking plate 310, so that the engaging portion 114 can be engaged with the buckle 315 to prevent the blocking when the engaging portion 114 is engaged with the buckle 315.
  • the plate 310 is rotated to limit the baffle plate 310.
  • baffle plate 310 is rotated to be closer to the free end of the baffle plate 310 than the end of the baffle plate 310 so that the baffle plate 310 in the standby state is close to the building 20 to reduce the height of the baffle plate 310 protruding from the building 20.
  • the engaging portion 114 is a card slot that is opened in the fixing base 110 , and the buckle 315 can be received in the engaging portion 114 and engaged with the engaging portion 114 .
  • the engaging portion 114 may also be a hook provided on the fixing base 110.
  • the card slots 114 are two, and the two card slots 114 are respectively located on the two fixing posts 112, and the buckles 315 correspond to two. It should be noted that the number of the card slot 114 and the buckle 315 is not limited to two, and may be one or more than two. The number of the card slot 114 and the buckle 315 may be set as needed.
  • the baffle plate 310 can be brought close to the landing platform 120, so that when the engaging portion 114 is engaged with the buckle 315, the baffle plate 310 can also prevent the landing platform 120 from rotating, that is, the landing platform 120 is close to the building 20 At this time, the baffle plate 310 can also be brought close to the landing platform 120.
  • the baffle plate 310 prevents the landing platform 120 from rotating in a direction away from the building 20.
  • the air cargo transceiver system 10 further includes a telescopic member 500.
  • One end of the telescopic member 500 is rotatably connected to the middle portion of the baffle plate 310, and the other end is rotatably connected to the fixing base 110.
  • the telescopic member 500 can be telescoped to drive the baffle plate 310 to rotate. The above activities of the baffle plate 310 are achieved.
  • the telescopic member 500 is a telescopic hydraulic cylinder or an electric strut.
  • the telescopic members 500 are two, and one end of each of the two telescopic members 500 is rotatably connected to the two fixing posts 112, and the other end is rotatably connected to the central portions of the opposite sides of the baffle plate 310.
  • the end of the telescopic member 500 away from the baffle plate 310 is not limited to being rotatably connected to the fixing base 110.
  • one end of the telescopic member 500 away from the baffle plate 310 may also be rotatably connected to the landing platform 120 or the building 20.
  • the number of the telescopic members 500 is not limited to two, and may be one or more than three.
  • the telescopic member 500 When the telescopic member 500 is one, at this time, the telescopic member 500 is not connected to the fixing base 110, and the two ends of the telescopic member 500 are respectively The middle portion of the baffle plate 310 is rotatably connected to the building 20, or the end of the telescopic member 500 away from the baffle plate 310 may also be rotatably coupled to the landing platform 120.
  • the number of the telescopic members 500 is more than three, the partial telescopic members 500 may be rotatably connected to the fixing base 110 and the baffle plate 310, and the other portion of the telescopic members 500 may be rotatably connected to the baffle plate 310 and the building 20; or, all the telescopic members 500 may be rotatably connected.
  • the landing platform 120 and the baffle plate 310 When the telescopic member 500 is one, at this time, the telescopic member 500 is not connected to the fixing base 110, and the two ends of the telescopic member
  • the rotation of the baffle plate 310 is not limited to the manner of the telescopic member 500.
  • the baffle plate 310 and the fixing base 110 are rotatably connected through a rotating shaft, and a stepping motor is mounted on the fixing base 110, and the stepping motor is used.
  • the rotary shaft drive connection that is, the stepping motor drives the rotating shaft to rotate, so as to realize the rotation of the baffle plate 310; or, the baffle plate 310 can be directly connected to the fixed seat 110, the working platform or the building 20 by using a rotating mechanism connection.
  • the rotating mechanism includes a connecting rod, a first rotating shaft, a second rotating shaft, a first motor and a second motor, and one end of the connecting rod is rotatably connected to the fixed seat 110, the work platform or the building 20 through the first rotating shaft, and the other end is passed through the second
  • the rotating shaft is rotatably connected with the baffle 310; the first motor is mounted on the fixed seat 110, the landing platform 120 or the building 20, the first motor is connected to the first rotating shaft, the second motor is mounted on the blocking plate 310, and the second motor is
  • the second rotating shaft is drivingly connected to enable the first motor and the second motor to respectively drive the first rotating shaft and the second rotating shaft to rotate, and at least one of the driving link and the blocking plate 310 rotates In order to drive the baffle plate 310 to rotate; at this time, the first motor and the second motor are both stepping motors.
  • the barrier plate 310 can be moved, and is not limited to being rotated.
  • a slide rail 340 can be provided, the barrier plate 310 can be disposed to be slidable in a vertical direction, and the slide rail 340 can be disposed on the building 20
  • the upper or the fixed seat 110, or a bracket may be disposed, and the sliding rail 340 is disposed on the bracket.
  • the blocking plate 310 slides onto the working surface 122 of the landing platform 120 to Isolate users and drones.
  • the baffle plate 310 is movable, and the landing platform 120 cannot be rotated. At this time, the landing platform 120 is in a horizontal state of the working surface 122; or, the baffle plate 310 is inactive, and the landing platform 120 can Rotating, at this time, the baffle plate 310 is in a state of being parallel to the vertical direction or inclined with respect to the vertical direction, and the baffle plate 310 is disposed near the edge of the work surface 122 when horizontally and at least partially above the plane of the work surface 122 when horizontal And in the vertical direction, one end of the baffle plate 310 near the fixing base 110 is lower than the free end of the baffle plate 310; or, the baffle plate 310 and the landing platform 120 cannot rotate, then the landing platform 120 is always at the working surface.
  • the baffle plate 310 is in a horizontal state, and the baffle plate 310 is always in a state of being parallel to the vertical direction or inclined with respect to the vertical direction. At this time, the baffle plate 310 is disposed near the edge of the work surface 122 and at least partially located above the plane of the work surface 122. And in the vertical direction, one end of the baffle plate 310 near the fixing base 110 is lower than the free end of the baffle plate 310.
  • the rotation of the landing platform 120 and the baffle plate 310 can be linked to the opening or closing of the window or the glass curtain wall.
  • the baffle plate 310 can be used as a window door or an exterior façade wall of the building 20, that is, the baffle plate 310 can be manually or electrically opened or closed by the user when the cargo is not required to be used for receiving and dispatching the cargo.
  • Door 320 can be omitted.
  • the lifting mechanism 400 is expandable and contractible, the lifting mechanism 400 is mounted on the landing platform 120, and is located in the working area.
  • the lifting mechanism 400 can be elongated toward the pick-and-place port 312.
  • the lifting mechanism 400 can carry goods and can drive the goods to be lifted and lowered. .
  • the blocking surface 314 and the working surface 122 are parallel, the position of the lifting mechanism 400 corresponds to the position of the pick-and-place port 312.
  • the lifting mechanism 400 is electrically connected to the electronic control unit 200, and the electronic control unit 200 can control the expansion and contraction mechanism 400 to expand and contract according to the control signal, thereby realizing the automatic lifting and lowering of the lifting mechanism 400.
  • the landing platform 120 is provided with a receiving groove 124.
  • the receiving groove 124 is located in the working area, the lifting mechanism 400 is installed in the receiving groove 124, and the lifting mechanism 400 can extend out of the receiving groove 124.
  • the lifting mechanism 400 is disposed in the housing groove 124, which not only facilitates the attachment of the lifting mechanism 400, but also protects the lifting mechanism 400, and can also reduce standby time.
  • the thickness of the unmanned cargo handling system 10 is such as to reduce the height of the building 20 of the drone cargo receiving and dispatching system during standby.
  • the bottom of the receiving groove 124 is a hollow structure to facilitate the discharge of water entering the receiving groove 124, and can also reduce the weight of the landing platform 120.
  • the lifting mechanism 400 includes a support frame 410 and a push rod motor 420.
  • the support frame 410 can be telescoped, and the support frame 410 is mounted on the landing platform 120 and located in the work area.
  • the support frame 410 can carry goods and drive the goods to be lifted and lowered.
  • the support frame 410 includes a support plate 412, a strip-shaped first support member 414, a hinge seat 415, a strip-shaped second support member 416, and a slide seat 417.
  • the support plate 412 is capable of carrying cargo and is capable of moving the cargo up and down.
  • the support plate 412 is a flat plate structure, and the support plate 412 is disposed in parallel with the working surface 122.
  • the support plate 412 can extend out of the receiving groove 124.
  • One end of the first support member 414 is rotatably coupled to the landing platform 120.
  • the hinge seat 415 is hinged from the end of the first support member 414 away from the landing platform 120, and the interface seat 415 abuts against the support plate 412 and is slidable on the landing platform 120.
  • the middle portion of the second support member 416 is hinged to the middle portion of the first support member 414, and one end of the second support member 416 is rotatably coupled to the support plate 412.
  • the sliding seat 417 is hinged to the end of the second supporting member 416 away from the supporting plate 412.
  • the sliding seat 417 abuts the landing platform 120 and is slidable on the landing platform 120 to drive the supporting plate 412 to move up and down.
  • the lifting mechanism 400 further includes a guiding rail 430.
  • the guiding rail 430 is fixed on the landing platform 120.
  • One end of the first supporting member 414 away from the hinge seat 415 is rotatably connected with the guiding rail 430, and the sliding seat 417 is slidable along the guiding rail 430.
  • the guide rail 430 is disposed on the bottom of the receiving groove 124.
  • the pusher motor 420 is capable of driving the support frame 410 to expand and contract.
  • the push rod motor 420 is electrically coupled to the electronic control assembly 200 to enable the electronic control assembly 200 to control the operation of the push rod motor 420.
  • the electronic control unit 200 can control the operation of the push rod motor 420 according to the control signal.
  • the push rod motor 420 is housed in the receiving groove 124.
  • the push rod motor 420 is rotatably connected to one end of the first support member 414 away from the support plate 412 and one end of the second support member 416 away from the support plate 412.
  • the push rod motor 420 can drive the second support member 416 to slide away from the end of the support plate 412. .
  • the lifting mechanism 400 further includes a first connecting shaft 440 and a second connecting shaft 450.
  • the first connecting shaft 440 rotatably connects one end of the first supporting member 414 away from the supporting plate 412 and the guiding rail 430, and the second connecting shaft 450 and
  • the second support member 416 is rotatably connected to one end of the support plate 412.
  • the push rod motor 420 is rotatably connected to the first connecting shaft 440 and the second connecting shaft 450, so as to push the second connecting shaft 450 to move by the expansion and contraction of the push rod motor 420.
  • the second support member 416 is driven to slide away from the end of the support plate 412.
  • the first support member 414 and the second support member 416 are both two, the two first support members 414 are opposite and parallel, and the two second support members 416 are opposite and parallel, one
  • the first support member 414 corresponds to a second support member 416.
  • the guide rails 430 correspond to two, the two guide rails 430 are parallel and spaced apart, and one second support member 416 corresponds to one guide rail 430;
  • the first connecting shaft 440 moves the two first support members 414 away from the support plate 412.
  • One end is rotatably connected to the two guiding rails 430
  • the second connecting shaft 450 is rotatably connected to one end of the two second supporting members 416 away from the supporting plate 412.
  • the number of the first support member 414 and the second support member 416 is not limited to two, and the first support member 414 and the second support member 416 may also be one.
  • the guide rail 430 corresponds to one; or There may be three or more support members 414 and second support members 416.
  • the number of guide rails 430 is equal to the number of second support members 416, and the first connecting shaft 440 moves the plurality of first support members 414 away from the support.
  • One end of the plate 412 is rotatably connected to the plurality of guide rails 430, and the second connecting shaft 450 is rotatably connected to one end of the plurality of second supporting members 416 away from the supporting plate 412.
  • the number of the guide rails 430 and the support frame 410 can be set as needed.
  • the lifting mechanism 400 is not limited to adopting the above structure.
  • the structure of the lifting mechanism 400 may further include only the supporting plate 412 and the push rod motor 420.
  • the push rod motor 420 is fixed at the bottom of the receiving groove 124, and the push rod motor 420 is The push rod is fixedly connected to the support plate 412, and the support plate 412 is directly driven to move up and down by the expansion and contraction of the push rod motor 420.
  • the UAV cargo transceiver system 10 further includes a pressure sensor 600 electrically connected to the electronic control unit 200.
  • the pressure sensor 600 is mounted on the lifting mechanism 400, and the pressure sensor 600 is capable of detecting the lifting mechanism 400.
  • the weight of the load, the electronic control assembly 200 can also control the expansion and contraction mechanism 400 to expand and contract according to the weight carried on the lifting mechanism 400.
  • the pressure sensor 600 may be installed at the bottom of the support plate 412 or may be mounted on the guide rail 430 and located between the guide rail 430 and the bottom of the receiving groove 124; wherein the pressure sensor 600 can detect the support of the support frame 410
  • the weight carried on the plate 412, the electronic control assembly 200 is also capable of controlling the operation of the pusher motor 420 based on the weight carried on the support frame 410.
  • the barrier assembly 300 further includes an inductor 700 electrically coupled to the electronic control assembly 200, the sensor 700 being capable of sensing the state of the movable door 320. That is, the sensor 700 can sense whether the movable door 320 is in the closed state or in the open state. The sensor 700 can feed back the state of the movable door 320 to the electronic control unit 200.
  • the electronic control unit 200 can also control the expansion and contraction mechanism 400 to expand and contract according to the state of the movable door 320.
  • the inductor 700 is a contact micro switch or a proximity switch.
  • the electronic control assembly 200 is also capable of controlling the operation of the drive member 130 based on the weight carried on the lift mechanism 400 and the state of the movable door 320. For example, when the cargo is taken away, the weight carried on the lifting mechanism 400 is zero. If the state of the movable door 320 is open, the electronic control unit 200 controls the driving member 130 to not rotate the landing platform 120; if the cargo is taken away Thereafter, the weight carried on the lifting mechanism 400 is zero, and the state of the movable door 320 is closed. The electronic control unit 200 controls the driving member 130 to drive the lifting and lowering platform 120 to rotate, so that the landing platform 120 is close to the building 20.
  • the barrier assembly 300 further includes an alarm 800 that is capable of issuing an alarm based on the status of the active door 320 to alert the user to close the movable door 320.
  • the alarm 800 can be a buzzer, a vibrator or a flashing light.
  • the alarm 800 is electrically connected to the electronic control assembly 200, and the electronic control assembly 200 controls the alarm 800 to operate according to the state of the movable door 320 fed back by the sensor 700 and the timing.
  • the alarm 800 may be mounted on the baffle plate 310 or may be built into the electronic lock 330. It should be noted that the alarm device 800 may be omitted. In this case, the unmanned vehicle cargo transmission/reception system 10 does not have a function of issuing an alarm.
  • the blocking surface 314 is provided with a positioning beacon 316 for the drone to land, so that the drone can accurately land on the working area of the landing platform 120.
  • the positioning beacons 316 are two, and two positioning beacons 316 are located on the blocking surface 314 .
  • the two positioning beacons 316 are disposed on the diagonal of the blocking surface 314 and are respectively adjacent to each other.
  • the two opposite corners of the baffle 310 are disposed. That is, when the plane in which the blocking surface 314 is located can intersect the plane in which the working surface 122 is horizontally disposed, the positioning beacon 316 is visible to the drone, if the blocking plate 310 is located above the working area, and is active When the door 320 collectively shields the work area, the location beacon 316 is not visible to the drone.
  • the number of positioning beacons 316 is not limited to two, and the positioning beacons 316 may be one or more than two, and the number of positioning beacons 316 may be set as needed.
  • the positioning beacon 316 is a static pattern, and the blocking plate 310 is further provided with a receiving groove 318.
  • the side wall of the receiving groove 318 is mounted with a light source (not shown), and the positioning beacon 316 is disposed in the receiving groove 318.
  • the accommodating groove 318 is located on the baffle plate 310, and the number of the accommodating grooves 318 corresponds to the number of the positioning beacons 316.
  • the positioning beacon 316 is not limited to being disposed on the baffle plate 310, and may be disposed, for example, on the working surface 122 of the landing platform 120 as long as the drone is visible during the landing.
  • the above-described unmanned cargo cargo receiving and receiving system 10 has at least the following advantages:
  • the barrier assembly 300 of the above-described drone cargo transceiver system 10 is disposed near the edge of the work surface 122 and at least partially above the plane of the work surface 122, the barrier assembly 300 moves the work area away from the barrier assembly 300. One side of the area is separated. Then, when the above-mentioned unmanned cargo transceiver system 10 is installed, the user and the drone can be blocked by simply moving the side of the barrier assembly 300 away from the work area toward the user, thereby reducing the user's The possibility of drone contact is more secure.
  • the movable door 320 is movably mounted on the baffle plate 310 by opening the access port 312 for the user to pick up and place the cargo on the baffle plate 310, and the movable door 320 can cover the pick-and-place port 312, and the landing platform
  • the working area for the drone landing and cargo placement of 120 is located on the other side of the baffle 310.
  • the baffle 310 is placed between the building 20 and the work area.
  • the baffle plate 310 and the movable door 320 can be used to isolate the user and the drone, and can facilitate the pick-and-place of the goods.
  • the baffle plate 310 of the above-described unmanned cargo cargo transmission and reception system 10 can be positioned above the work area, so that the baffle plate 310 can block the work area together with the movable door 320, thereby being able to block the cargo on the work area. To reduce the possibility of cargo being wet by rain.
  • the working surface 122 can also be tilted vertically or in a vertical direction so that the landing platform 120 can be close to the building 20, take off and land.
  • the baffle 310 can also be moved to be close to the landing platform 120, so that the above-mentioned unmanned cargo transceiving system 10 can stand by, the baffle 310 and the landing platform 120 can be connected to the building.
  • the object 20 is close to realize the folding of the above-mentioned unmanned cargo transceiving system 10 to reduce the degree of protrusion of the unmanned cargo transceiving system 10 relative to the building 20, and to reduce wind, especially in coastal areas. Damage to the cargo handling system 10 for drones.
  • the elevating mechanism 400 can elongate to catch the cargo without avoiding the height difference.
  • the goods are caused to fall directly on the platform; at the same time, when the drone is to load the goods, the lifting mechanism 400 can be extended to facilitate the loading of the goods by the drone.
  • the lifting mechanism 400 can be extended to facilitate the user to collect the goods.
  • the pressure sensor 600 and the sensor 700 assist the electronic control unit 200 to control the movement of the baffle platen 310, the landing platform 120 and the lifting mechanism 400, thereby facilitating automatic control of the unmanned cargo cargo receiving and receiving system 10, and controlling more aspects. .
  • the positioning beacon 316 can assist the drone to position during the take-off and landing process, so that the drone can accurately land on the landing platform 120.
  • the baffle plate 310 is located between the drone and the user, and can also block the working noise of a part of the drone from being transmitted to the user.
  • the fixing base 110 can also be omitted.
  • the driving member 130 is directly mounted on the building 20, that is, the driving member 130 is rotatably connected to the building 20 at one end away from the landing platform 120.
  • the driving member 130 can also be omitted.
  • the landing platform 120 may not have a rotating function; or, the blocking plate 310 may not be movable.
  • the telescopic member 500 may also be omitted; or the lifting mechanism 400 may be omitted.
  • the cargo transceiving system 10 does not have the function of driving the cargo to elevate or lower; or the positioning beacon 316 can be omitted as long as the drone can be accurately landed.
  • the method for collecting goods is a method for collecting goods based on the above-described cargo receiving and dispatching system 10 for a drone, and the method for collecting the goods can be used for the delivery of the drone, and the user picks up the pieces.
  • the method of collecting the goods includes the following steps:
  • Step S31 Rotating the landing platform 120 to level the working surface 122 of the landing platform 120, and moving the baffle 310 to an edge near the working surface 122 and parallel or inclined with respect to the vertical direction.
  • FIG. 2 is an initial state of the cargo transmitting and receiving system 10 for a drone, that is, the standby state is that both the landing platform 120 and the blocking plate 310 are close to the building 20, and the landing platform 120 and the blocking plate 310 are The side away from the fixed seat 110 is facing downward, at this time, the blocking surface 314 faces the building 20, and the movable door 320 and the electronic lock 330 are both closed.
  • the drone when the drone needs to land, the drone sends a control signal A1, and the electronic control unit 200 controls the driving member 130 to drive the take-off and landing platform 120 to rotate according to the control signal A1 until the working surface 122 of the landing platform 120 At the same time, the electronic control unit 200 controls the extension of the extension member 500 according to the control signal A1 to rotate the barrier plate 310, and rotates the barrier plate 310 until the end of the barrier plate 310 away from the fixed seat 110 faces upward. At this time, the unmanned vehicle cargo receiving and receiving system 10 is in a fully deployed state.
  • the free end of the baffle plate 310 is higher than the end of the baffle plate 310 near the fixed seat 110, and the movable door 320 and the baffle plate 310 together separate the working area from the side of the baffle plate 310 away from the working area.
  • the baffle plate 310 is located between the building 20 and the work area, and the work area is exposed to facilitate the drone landing.
  • step S31 is not limited to the above manner.
  • the initial state of the baffle plate 310 is close to the building 20, and the blocking surface 314 faces the building 20,
  • the free end of the baffle plate 310 is higher than the end of the baffle plate 310 near the fixed seat 110.
  • the movable door 320 and the baffle plate 310 together separate the working area from the side of the baffle plate 310 away from the working area, and the landing platform 120 rises.
  • the starting state is the working surface 122 level.
  • step S31 is: moving the baffle plate 310 until the baffle plate 310 moves to the edge near the working surface 122 and is parallel or inclined with respect to the vertical direction, and the free end of the baffle plate 310 An end of the baffle plate 310 is adjacent to the fixed seat 110 to expose the work area.
  • the step S31 is: rotating the landing platform 120 to level the working surface 122 of the landing platform 120.
  • the landing platform 120 and the baffle plate 310 are both inactive, or the starting position of the landing platform 120 and the baffle plate 310 is: the working surface 122 of the landing platform 120 is horizontal, and the baffle plate 310 is close to the working surface 122.
  • the edge is parallel or inclined with respect to the vertical direction, the free end of the baffle plate 310 is higher than the end of the baffle plate 310 near the fixed seat 110, and the working area is exposed, and the movable door 320 and the baffle plate 310 together keep the working area away from the baffle plate 310
  • the one side of the work area is separated, and step S31 can also be omitted.
  • the movement of the take-off and landing platform 120 and the baffle plate 310 is controlled by the electronic control unit 200 according to a control signal from the drone.
  • Step S32 The drone is landed on the work area of the unmanned cargo cargo receiving and receiving system 10.
  • the movable door 320 shields the pick-and-place port 312, and the movable door 320 and the baffle plate 310 together move the working area and the baffle plate 310 away from the working area.
  • One side is separated.
  • the drone performs a fall based on a feedback signal from the electronic control unit 200. That is, when the above-described unmanned vehicle cargo transmitting and receiving system 10 completes step S31, the electronic control unit 200 sends a feedback signal B1 to the drone, and the drone receives the feedback signal B1 and then drops to the work area.
  • the drone is dropped according to the positioning beacon 316 on the blocking surface 314 of the baffle 310.
  • the cargo carried on the drone is located above the lift mechanism 400.
  • Step S33 The drone places the goods on the work area.
  • the step of placing the cargo on the work area by the drone is that the drone places the cargo on the lift mechanism 400 at the work area. More specifically, the step of placing the cargo on the work area by the drone includes: the lift mechanism 400 is extended until the lift mechanism 400 abuts the cargo on the drone; the drone unloads the cargo; the cargo is unloaded at the lift mechanism 400 After the upper portion, the lifting mechanism 400 is shortened, and the cargo moves with the lifting mechanism 400.
  • the electronic control unit 200 controls the elevating mechanism 400 to elongate according to the control signal.
  • the weight of the lifting mechanism 400 detected by the pressure sensor 600 changes, and the electronic control unit 200 controls the push rod motor 420 to stop driving the support frame 410 to elongate.
  • the electronic control unit 200 sends a feedback signal, and the drone unloads the cargo onto the lifting mechanism 400 according to the feedback signal. After the cargo is unloaded on the lifting mechanism 400, the drone sends a control signal, and the electronic control unit 200 controls the lifting mechanism 400 to shorten according to the control signal, and the cargo moves with the lifting mechanism 400.
  • the drone when the drone falls to the work area, the drone sends a control signal A2, and the electronic control unit 200 controls the push rod motor 420 to drive the support frame 410 to extend according to the control signal A2, and extends the support plate 412 out of the receiving slot 124.
  • the electronic control unit 200 controls the push rod motor 420 to drive the support frame 410 to extend according to the control signal A2, and extends the support plate 412 out of the receiving slot 124.
  • the weight carried by the pressure sensor 600 detected on the lifting mechanism 400 changes, and the electronic control assembly 200 is pushed according to the control.
  • the rod motor 420 stops driving the support frame 410 to elongate.
  • the electronic control unit 200 sends a feedback signal B2 to the drone, and the drone unloads the cargo onto the support plate 412 according to the feedback signal B2; the cargo is unloaded in the lifting mechanism 400.
  • the drone sends a control signal A3, and the electronic control unit 200 controls the lifting mechanism 400 to shorten according to the control signal A3, and the cargo moves with the lifting mechanism 400 until the supporting plate 412 is flush with the working surface 122.
  • the drone can directly unload the cargo on the work area.
  • Step S34 The drone flies away from the work area.
  • the drone after the drone sends out the control signal A3, the drone stays away from the work area for a period of time to provide the lifting mechanism 400 with a shortened time.
  • Step S35 The baffle plate 310 is moved to the upper side of the work area and spaced and opposed to the work surface 122 when horizontal, so that the baffle plate 310 and the movable door 320 together shield the goods at the work area.
  • the electronic control unit 200 controls the telescopic member 500 to shorten, and drives the baffle plate 310 to rotate toward the working area until the baffle plate 310 is located above the working area.
  • the baffle plate 310 and the movable door 320 together block the cargo on the work area, that is, the semi-expanded state of the unmanned cargo cargo receiving and receiving system 10, as shown in FIG.
  • a control signal A4 is issued, and the electronic control unit 200 controls the expansion of the telescopic member 500 according to the control signal A4.
  • the blocking surface 314 is parallel to the work surface 122.
  • step S35 may be omitted.
  • Step S36 The movable door 320 is opened to expose the pick-and-place port 312.
  • the user when the user needs to take the pickup, the user sends a control signal C to the electronic control component 200.
  • the electronic control component 200 controls the electronic lock 330 to unlock according to the control signal C, and the user opens the movable door 320 to enable The pick-and-place port 312 is exposed.
  • the movable door is not limited to be opened in the above manner to expose the pick-and-place port 312.
  • the electronic lock 330 may not be used. In this case, the user directly opens the movable door 320.
  • Step S37 The goods are taken out from the side of the isolation assembly 300 away from the work area.
  • the step of removing the cargo from the side of the isolation assembly 300 away from the work area includes: opening the movable door 320 mounted on the baffle plate 310 near the edge of the work surface 122 to expose the pick-and-place port 312; The side of the board 310 away from the work area is taken from the pick-and-place port 312.
  • the step of removing the cargo from the pick-and-place port 312 on the side of the baffle plate 310 away from the work area includes: elevating the elevating mechanism 400 toward the pick-and-place port 312 to drive the goods on the elevating mechanism 400 toward The pick-and-place port 312 moves to take out the cargo from the pick-and-place port 312 on the side of the baffle plate 310 away from the work area; then close the movable door 320 and shorten the lift mechanism 400.
  • the pressure sensor 600 detects that the weight carried on the support plate 412 is zero, and the electronic control unit 200 confirms that the goods have been taken away, and the electric
  • the control unit 200 controls the push rod motor 420 to drive the support frame 410 to be shortened so that the support plate 412 is received in the receiving groove 124.
  • the sensor 700 confirms that the movable door 320 is in the closed state, and the electronic lock 330 is locked.
  • the sensor 700 detects that the movable door 320 is in an open state and feeds back to the electronic control assembly 200, and the electronic control assembly 200 controls the elevating mechanism 400 to elongate according to the feedback.
  • the electronic control assembly 200 controls the push rod motor 420 to drive the support frame 410 to elongate.
  • Step S38 Rotating the landing platform 120 such that the working surface 122 of the landing platform 120 is vertical or inclined with respect to the vertical direction, and the blocking plate 310 is rotated.
  • the end of the blocking plate 310 near the fixing base 110 is higher than the free end of the blocking plate 310. .
  • the landing platform 120 is close to the building 20, and the baffle plate 310 is adjacent to the landing platform 120.
  • the landing platform 120 is located between the building 20 and the baffle plate 310, and the working surface 122 of the landing platform 120 and the baffle plate 310 are The blocking faces 314 are opposite.
  • step S38 includes: after the sensor 700 confirms that the movable door 320 is in the closed state, the electronic control component 200 controls the driving component 130 to drive the landing platform 120 to rotate, so that the working surface 122 of the landing platform 120 is vertical or relatively vertical.
  • the direction is inclined, and the control expansion member 500 is shortened, and the baffle plate 310 is rotated such that one end of the baffle plate 310 adjacent to the fixing base 110 is higher than the free end of the baffle plate 310.
  • both the take-off and landing platform 120 and the baffle plate 310 are unable to rotate, then it is not necessary to rotate the take-off and landing platform 120 and the rotating baffle plate 310, and only the movable door 320 is closed to allow the movable door 320 to cover the pick-and-place port 312. If the landing platform 120 cannot rotate, the baffle 310 can be rotated, and only the movable door 320 is closed to shield the movable door 320 from the pick-and-place port 312, and the baffle plate 310 is rotated, so that the end of the baffle plate 310 near the fixed seat 110 is higher than the blocking block.
  • the free end of the plate 310 is sufficient; if the blocking plate 310 is unable to rotate, the landing platform 120 can be rotated. At this time, the movable door 320 is closed to shield the movable door 320 from the pick-and-place port 312, and the landing platform 120 is rotated to make the landing platform 120.
  • the working surface 122 of the 120 is vertically or inclined with respect to the vertical direction, and the landing platform 120 is adjacent to the building 20.
  • the method for collecting the above-mentioned goods can be conveniently collected by using the above-mentioned cargo receiving and dispatching system for the drone, realizing the delivery of the drone, picking up the user, and reducing the possibility of the user contacting the drone, and being more secure.
  • a method for mailing a cargo is a method for mailing a cargo based on the above-described cargo receiving and dispatching system 10 for a drone, and the method for sending the cargo can be used for a mailing of a user and a pickup of the drone.
  • the method of sending the goods includes the following steps:
  • Step S41 Rotating the landing platform 120 to level the working surface 122 of the landing platform 120, and moving the baffle 310 above the working area and spaced and opposite the working surface 122 when horizontal, so that the baffle 310 and the activity Doors 320 collectively shield the cargo at the work area.
  • FIG. 2 is an initial state of the cargo transmitting and receiving system 10 for a drone, that is, the standby state is that both the landing platform 120 and the blocking plate 310 are close to the building 20, and the landing platform 120 and the blocking plate 310 are The side away from the fixed seat 110 is facing downward, at this time, the blocking surface 314 faces the building 20, and the movable door 320 and the electronic lock 330 are both closed.
  • rotating the take-off and landing platform 120 and moving the baffle plate 310 relative to the landing platform 120 is controlled by the electronic control component 200 according to a control signal sent by the user.
  • the electronic control unit 200 controls the driving member 130 to drive the take-off and landing platform 120 to rotate according to the control signal D1 until the working surface 122 of the landing platform 120 and the horizontal direction Parallel; at the same time, the electronic control unit 200 controls the extension of the extension member 500 according to the control signal D1 to rotate the barrier plate 310 until the baffle plate 310 is positioned above the work area, and the baffle plate 310 and the movable door 320 together shield the work area.
  • the unmanned cargo cargo receiving and receiving system 10 is in a semi-expanded state, as shown in FIG.
  • the blocking surface 314 is parallel to the work surface 122.
  • step S41 is not limited to the above manner.
  • the initial state of the baffle plate 310 is close to the building 20, and the blocking surface 314 faces the building 20.
  • the free end of the baffle plate 310 is higher than the end of the baffle plate 310 near the fixed seat 110.
  • the movable door 320 and the baffle plate 310 together separate the working area from the side of the baffle plate 310 away from the working area, and the landing platform 120 rises.
  • the starting state is the working surface 122 level.
  • step S41 is: moving the baffle plate 310 until the baffle plate 310 moves to the edge near the working surface 122 and is parallel or inclined with respect to the vertical direction, and the free end of the baffle plate 310 An end of the baffle plate 310 is adjacent to the fixed seat 110 to expose the work area.
  • the starting state of the blocking plate 310 is close to the edge of the working surface 122 and Parallel or inclined with respect to the vertical direction, the free end of the baffle plate 310 is higher than the end of the baffle plate 310 adjacent to the fixed seat 110, and the movable door 320 and the baffle plate 310 together separate the working area from the side of the baffle plate 310 away from the working area.
  • the blocking surface 314 is away from the building 20.
  • the step S41 is: rotating the landing platform 120 to level the working surface 122 of the landing platform 120.
  • the landing platform 120 and the baffle plate 310 are both inactive, or the starting position of the landing platform 120 and the baffle plate 310 is: the working surface 122 of the landing platform 120 is horizontal, and the baffle plate 310 is close to the working surface 122.
  • the edge is parallel or inclined with respect to the vertical direction, the free end of the baffle plate 310 is higher than the end of the baffle plate 310 near the fixed seat 110, and the working area is exposed, and the movable door 320 and the baffle plate 310 together keep the working area away from the baffle plate 310
  • the one side of the work area is separated, and step S41 can also be omitted.
  • Step S42 The movable door 320 is opened to expose the pick-and-place port 312.
  • the electronic control unit 200 feeds back a signal E1 to the user to prompt the user to place the goods; the user issues a control signal D2, and the electronic control unit 200 controls the electronic
  • the lock 330 is unlocked, and the user opens the movable door 320 to expose the pick-and-place port 312.
  • step S42 is not limited to the above manner, and the electronic control unit 200 may control the electronic lock 330 to be unlocked when the baffle plate 310 is located above the work area.
  • Step S43 The goods are placed on the work area.
  • the electronic control unit 200 controls the lifting mechanism 400 to extend toward the pick-and-place port 312; the user places the goods on the lifting mechanism 400; the lifting mechanism 400 is shortened, and the goods are moved with the lifting mechanism. 400 sports.
  • the electronic control unit 200 controls the push rod motor 420 to drive the support frame 410 to elongate, and causes the support plate 412 to extend out of the work area 112.
  • the electronic control unit 200 controls the elevating mechanism 400 to extend toward the pick-and-place port 312 in a step of: after the user opens the movable door 320, the sensor 700 detects the movable door.
  • the 320 is in an open state and is fed back to the electronic control assembly 200.
  • the electronic control assembly 200 controls the push rod motor 420 to drive the support frame 410 to elongate and extend the support plate 412 out of the work area 112.
  • the lifting mechanism 400 is shortened, and the step of moving the cargo along with the lifting mechanism 400 is: after the user places the cargo on the lifting mechanism 400, the weight of the lifting mechanism 400 detected by the pressure sensor 600 changes, and the electronic control component 200 is loaded.
  • the lifting mechanism 400 has been placed.
  • the electronic control unit 200 controls the lifting mechanism 400 to be shortened. More specifically, the electronic control unit 200 controls the push rod motor 420 to drive the support frame 410 to be shortened until the support plate 412 is flush with the working surface 122.
  • the state of the unmanned cargo cargo receiving and receiving system 10 is still in the state shown in FIG. .
  • Step S44 The movable door 320 is closed to cause the movable door 320 to cover the pick-and-place port 312.
  • the user closes the movable door 320 so that the movable door 320 shields the pick-and-place port 312, and the electronic lock 330 is locked.
  • Step S45 The baffle plate 310 is moved relative to the landing platform 120 until the baffle plate 310 moves to an edge near the working surface 122 and is parallel or inclined with respect to the vertical direction to expose the work area.
  • the drone when the drone needs to take the pickup, the drone sends a control signal F1 to the electronic control unit 200, and the electronic control unit 200 controls the extension of the extension member 500 according to the control signal F1 to rotate the blocking plate 310.
  • the unmanned vehicle cargo receiving and receiving system 10 is in a fully deployed state. That is, after the step S45, the free end of the baffle plate 310 is higher than the end of the baffle plate 310 near the fixed seat 110, and the movable door 320 and the baffle plate 310 together separate the working area from the side of the baffle plate 310 away from the working area.
  • the baffle plate 310 is located between the building 20 and the work area, and the work area is exposed to facilitate the drone landing.
  • step S45 may be omitted.
  • Step S46 The drone is landed on the work area.
  • the electronic control unit 200 sends a feedback signal E2 to the drone, and the drone confirms that it can fall behind and then descends to the working area.
  • the electronic control unit 200 does not need to send a feedback signal E2 to the drone, and the drone directly falls onto the work area.
  • Step S47 The drone collects the goods and carries the goods away from the work area.
  • the drone after the drone is dropped to the work area, the drone sends a control signal F2, and the electronic control unit 200 controls the elevating mechanism 400 to extend according to the control signal F2.
  • the state is as shown in FIG.
  • the cargo on the 400 abuts the bottom of the drone; the drone fixes the cargo; the lifting mechanism 400 is shortened; the drone carries the cargo away from the work area.
  • the pressure sensor 600 detects a change in the weight of the load on the lifting mechanism 400, confirming that the cargo has been lifted by the lifting mechanism 400 and the bottom of the drone fuselage
  • the electronic control unit 200 controls the lifting mechanism 400 to stop elongating.
  • the step of collecting the cargo by the drone is: when the lifting mechanism 400 abuts the cargo fixing device at the bottom of the UAV fuselage, the electronic control component 200 sends a feedback signal E3 to the drone, and the feedback cargo has been unmanned.
  • the cargo securing device at the bottom of the fuselage is abutted, at which point the drone fixes the cargo.
  • the lifting mechanism 400 is shortened, and the step of the drone flying away from the working area is: after the drone fixes the cargo, the drone sends a control signal F3 to the electronic control component 200, The electronic control unit 200 controls the lifting assembly 400 to be shortened according to the control signal F3, and the drone flies away from the working area. More specifically, the electronic control unit 200 controls the push rod motor 420 to drive the support frame 410 to be shortened according to the control signal F3 until the support plate 412 is received in the receiving slot 124, and the drone carries the cargo away from the work area.
  • the manner in which the drone collects the cargo is not limited to the above manner, and the drone can bring the telescopic fixing device to directly raise and fix the cargo. At this time, the lifting mechanism 400 is not required to drive the cargo to rise and fix.
  • Step S48 Rotating the landing platform 120 to move the landing platform 120 such that the working surface 122 is vertical or inclined relative to the vertical direction, and rotating the baffle plate 310 such that one end of the baffle plate 310 adjacent to the fixing base 110 is higher than the baffle plate 310. Free end.
  • step S48 when the drone flies away from the work area, the control signal F4 is issued, and the electronic control unit 200 controls the driving member 130 to drive the take-off and landing platform 120 to rotate according to the control signal F4, and controls the expansion and contraction member 500 to shorten to block the baffle plate.
  • the 310 rotates and returns to the standby state, so that the drone cargo conveying system 10 is brought close to the building 20 and returns to the standby state, that is, the state shown in FIG.
  • both the take-off and landing platform 120 and the baffle plate 310 are unable to rotate, then it is not necessary to rotate the take-off and landing platform 120 and the rotating baffle plate 310, and only the movable door 320 is closed to allow the movable door 320 to cover the pick-and-place port 312. If the landing platform 120 cannot rotate, the baffle 310 can be rotated, and only the movable door 320 is closed to shield the movable door 320 from the pick-and-place port 312, and the baffle plate 310 is rotated, so that the end of the baffle plate 310 near the fixed seat 110 is higher than the blocking block.
  • the free end of the plate 310 is sufficient; if the blocking plate 310 is unable to rotate, the landing platform 120 can be rotated. At this time, the movable door 320 is closed to shield the movable door 320 from the pick-and-place port 312, and the landing platform 120 is rotated to make the landing platform 120.
  • the working surface 122 of the 120 is vertically or inclined with respect to the vertical direction, and the landing platform 120 is adjacent to the building 20.
  • the mailing method of the above-mentioned goods can be conveniently collected by using the above-mentioned cargo receiving and dispatching system for the drone, realizing the mailing of the user, the pickup of the drone, and reducing the possibility of the user contacting the drone, and being more secure. .
  • the cargo transmitting and receiving system 40 for a drone has substantially the same structure as the cargo transmitting and receiving system 10 for a drone, except that the end of the telescopic member 41 away from the baffle 42 is The takeoff and landing platform 43 is rotatably connected.
  • the utility model also has the effect of the unmanned cargo transmission/reception system 10.
  • the cargo transmitting and receiving system for a drone has substantially the same structure as the cargo transmitting and receiving system 10 for a drone, and the difference is that the structure and the movable mode of the blocking component (not shown) are different.
  • the barrier assembly includes a baffle plate 51 that is slidable in a vertical direction, and the baffle plate 51 is disposed near the edge of the working surface 52a of the landing platform 52 when the blocker 51 is horizontal, and the baffle plate 51 can be at least partially horizontal.
  • the work surface 52a is positioned above the plane, and the work area is separated from the side of the baffle 51 away from the work area. That is, there is no need to provide a pick-and-place port on the baffle plate 51, and no movable door is required.
  • the baffle plate 51 is slidably mounted on the mount 53.
  • the baffle 51 separates the working area from the side of the blocking 512 away from the working area, and at this time.
  • the maximum height of the portion of the baffle 51 above the plane where the working surface 52a is located to the plane of the working surface 52a is greater than the height of the rotor of the drone to the plane of the working surface 52a to isolate the user and the drone. That is, the expanded state of FIG.
  • the step of removing the cargo from the side of the isolating assembly 51 away from the working area includes: the baffle plate 51 sliding in a vertically downward direction; the cargo is removed from the side of the baffle plate 51 away from the working area, and the state of the object is as shown in the figure. 13 is shown.
  • the function of the lifting mechanism 54 is different from that of the lifting mechanism 400.
  • the landing platform 52 does not have the receiving groove 124 of the landing platform 120.
  • the landing platform 52 is provided with a sliding slot 52b extending from the working area toward the baffle 51.
  • the lifting mechanism 54 is mounted in the sliding slot 52b and can extend along the sliding slot 52b. The direction is slid so that the lifting mechanism 54 can drive the cargo to lift and lower and can drive the cargo to slide.
  • the elevating mechanism 54 of the present embodiment not only has a lifting function of the elevating mechanism 400, but also has a function of being slidable in the chute 52b.
  • the guide rail 430 is slidably coupled to the side wall of the chute 52b.
  • the chute 52b may penetrate the surface of the working surface 52a of the landing platform 52 and the working surface 52a, or may have a structure similar to the receiving groove 124.
  • the drone places the goods on the work area in such a manner that the drone places the goods on the lifting mechanism 54 at the work area.
  • the step of removing the cargo from the side of the isolating assembly 51 away from the working area includes: the lifting mechanism 54 drives the cargo to slide along the chute 52b toward the baffle 51, and the baffle 51 slides in a vertically downward direction. 51 Take the goods away from the side of the work area.
  • the take-off and landing platform 52 is rotated to make the working surface 52a of the landing platform 52 vertical or inclined with respect to the vertical direction, that is, the landing platform 52 is close to
  • the baffle plate 51 one side of the working surface 52a away from the landing platform 52 is opposite to the blocking surface 314 of the baffle plate 310, and the baffle plate 51 is located between the landing platform 52 and the building 60, and is folded, that is, as shown in FIG. Shown.
  • the blocker 51 is further slid in a direction of a vertical upward direction so that the baffle plate 51 moves the working area and the baffle plate 51 away from the working area. The step of separating one side.
  • the utility model also has the effect of the unmanned cargo transmission/reception system 10.

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Abstract

一种无人机用货物收发系统(10)，包括支承组件(100)和阻隔组件(300)。支承组件(100)包括能够安装在建筑物(20)上的起降平台(120)，起降平台(120)具有作业面(122)，作业面(122)上设有供无人机降落和货物放置的作业区域；阻隔组件(300)靠近作业面(122)的边缘设置并且至少部分位于作业面(122)所在平面的上方，以使阻隔组件(300)将作业区域与阻隔组件(300)远离作业区域的一侧分隔开。

Description

无人机用货物收发系统及货物的收取和寄送方法 技术领域
本发明涉及一种无人机用货物收发系统及货物的收取和寄送方法。
背景技术
随着无人机技术的快速发展，无人机已经应用到快递行业进行货物的配送，然而，目前的城市高层建筑家庭用户配套的无人机起降设施一般是在用户阳台的外侧、窗台的下方等安装供无人机起降的固定式平台，无人机在起降过程中存在着用户与无人机接触的可能性，具有安全隐患。
发明内容
基于此，有必要提供一种较为安全的无人机用货物收发系统。
此外，还提供一种货物的收取方法和一种货物的寄送方法。
一种无人机用货物收发系统，包括：
支承组件，包括能够安装在建筑物上的起降平台，所述起降平台具有作业面，所述作业面上设有供无人机降落和供货物放置的作业区域；及
阻隔组件，靠近所述作业面的边缘设置并且至少部分位于所述作业面所在平面的上方，以使所述阻隔组件将所述作业区域与所述阻隔组件远离所述作业区域的一侧分隔开。
一种货物的收取方法，包括如下步骤：
所述无人机降落至上述无人机用货物收发系统的所述作业区域上；
所述无人机将所述货物放置在所述作业区域上；
所述无人机飞离所述作业区域；及
从所述隔离组件远离所述作业区域的一侧取走所述货物。
一种货物的寄送方法，包括如下步骤：
将货物放置在上述无人机用货物收发系统的所述作业区域处；
所述无人机降落至所述作业区域上；及
所述无人机收取所述货物，并携带所述货物飞离所述作业区域。。
本发明的一个或多个实施例的细节在下面的附图和描述中提出。本发明的其它特征、目的和优点将从说明书、附图以及权利要求书变得明显。
附图说明
为了更清楚地说明本发明实施例或现有技术中的技术方案，下面将对实施例或现有技术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的前提下，还可以根据这些附图获得其他实施例的附图。
图1为一实施方式的无人机用货物收发系统安装在建筑物上的全展开状态的结构图；
图2为图1所示的无人机用货物收发系统安装在建筑物上的待机状态的结构图；
图3为图1所示的无人机用货物收发系统的电连接图；
图4为图1所示的无人机用货物收发系统的阻隔组件的另一角度的结构示意图；
图5为图4所示的阻隔组件的I部的放大图；
图6为图1所示的无人机用货物收发系统的半展开状态的结构示意图；
图7为图6所示的无人机用货物收发系统的Ⅱ部的放大图；
图8为图6所示的无人机用货物收发系统的Ⅲ部的放大图；
图9为图1所示的无人机用货物收发系统的升降机构的结构示意图；
图10为另一实施方式的无人机用货物收发系统的全展开状态的结构示意图；
图11为图10所示的无人机用货物收发系统的半展开状态的结构示意图；
图12为另一实施方式的无人机用货物收发系统的展开状态的结构示意图；
图13为图12所示的无人机用货物收发系统的取物状态的结构示意图；
图14为图12所示的无人机用货物收发系统的折叠状态的结构示意图。
具体实施方式
为了便于理解本发明，下面将参照相关附图对本发明进行更全面的描述。
如图1所示，一实施方式的无人机用货物收发系统10，用于快递的临时存储，以供无人机将货物卸载在该无人机用货物收发系统10上，用户收取；或者，用户将货物放置在该无人机用货物收发系统10上，无人机取件。该无人机用货物收发系统10能够安装在建筑物20的外部，建筑物20为阳台或窗户，例如，该无人机用货物收发系统10可以安装在用户的阳台围栏的外侧、窗台的下方等等。其中，该无人机用货物收发系统10包括支承组件100、电控组件200、阻隔组件300和升降机构400。
支承组件100能够固定在建筑物20上。支承组件100为整个无人机用货物收发系统10的支撑结构，该支承组件100能够供无人机降落和货物的存放。其中，支承组件100包括固定座110和起降平台120。
固定座110能够固定在建筑物20上。固定座110为整个无人机用货物收发系统10的支撑和固定部件。具体在图示的实施例中，固定座110包括两个间隔且平行设置的固定柱112，两个固定柱112均能够固定在建筑物20上。
起降平台120安装在固定座110上。起降平台120具有作业面122，作业面122上设有供无人机降落和货物放置的作业区域(未标示)。具体在图示的实施例中，起降平台120大致为方形板状，作业区域位于作业面122的中部。
请一并参阅图2，具体地，起降平台120与固定座110转动连接，以使作业面122能够水平，而使作业区域能够供货物放置和无人机降落，作业面122还能够竖直或者相对竖直方向倾斜，以使起降平台120能够贴近建筑物20，从而使无人机用货物收发系统10在待机状态时，起降平台120能够贴近建筑物20。
进一步地，为了起降平台120能够更加稳固地贴近建筑物20而不被风力吹动，在起降平台120上设置有卡持部(图未标)，固定座110上设置与卡持部配合的配合装置(图未标)，通过卡持部与配合配相卡合以将起降平台120 固定在建筑物20上。例如，配合装置可以为电子锁，可根据无人机或用户的客户端发出的控制信号控制解锁。
具体地，起降平台120的一端与固定座110转动连接，支承组件100还包括驱动件130，驱动件130为伸缩杆，驱动件130的两端分别与固定座110和起降平台120的中部转动连接，驱动件130能够伸缩而驱动起降平台120转动。具体在图示的实施例中，起降平台120的一端与两个固定柱112均转动连接。
具体地，驱动件130为伸缩式液压缸或电动撑杆。
进一步地，驱动件130为两个，两个驱动件130的一端分别与两个固定柱112转动连接，另一端均与起降平台120的相对的两侧的中部转动连接。
可以理解，驱动件130的数量不限于为两个，也可以为一个或者大于三个，当驱动件130为一个时，驱动件130不安装在固定座110上，驱动件130的两端分别与建筑物20和阻隔板的中部转动连接；当驱动件130的数量大于三个时，可以使部分驱动件130转动连接固定座110和起降平台120，另一部分驱动件130转动连接起降平台120和建筑物20。
或者，驱动件130也不限于设置为伸缩杆，例如，驱动件130还可以为步进电机，此时，驱动件130与连接固定座110和起降平台120的转轴传动连接，以实现起降平台120的转动；此时，为了起降平台120具有足够的支撑力，支承组件100还包括支撑杆，支撑杆的两端分别与固定座110和起降平台120转动连接，支撑杆能够支撑作业面122水平设置时的起降平台120；或者，支撑杆远离起降平台120的一端也可以直接与建筑物20转动连接。支撑杆数量可以根据需要进行设定。其中，支撑杆为伸缩杆。
或者，固定座110也不限于为上述固定柱112的结构，例如固定座110还可以为板状结构、规则或不规则的块状结构等。
电控组件200用于控制无人机用货物收发系统10的工作。其中，电控组件200能够接收控制信号。其中，控制信号为无人机发出的控制信号，或者，控制信号也可以是用户通过客户端发出的控制信号，其中，客户端可以为电子设备，例如手机、电脑等。电控组件200还能够向无人机或用户的客户端发出反馈信号，以使无人机能够根据反馈信号降落，卸货或取货，或使用户 能够根据反馈信号放置货物。具体在图示的实施例中，电控组件200安装在固定座110的一个固定柱112上。电控组件200和固定座110上设置的配合装置电连接，通过无人机或用户的客户端向电控组件200发出控制信号，电控组件200根据控制信号控制配合装置解锁。
可以理解，电控组件200不限于安装在固定座110上，例如，电控组件200还可以安装在建筑物20、起降平台120上等。
请一并参阅图3，电控组件200与驱动件130电连接，电控组件200能够控制驱动件130的工作。具体地，电控组件200能够根据控制信号控制驱动件130的工作。
阻隔组件300靠近水平时的作业面122的边缘设置并且至少部分位于水平时的作业面122所在平面的上方，以使阻隔组件300能够将作业区域与阻隔组件300远离作业区域的一侧分隔开。其中，阻隔组件300位于水平时的作业面122所在平面的上方的部分的高度大于或等于无人机的旋翼到作业面122的距离。
请一并参阅图4，在图示的实施例中，阻隔组件300包括阻隔板310和活动门320。
阻隔板310能够位于靠近水平时的作业面122的边缘处并且能够至少部分位于水平时的作业面122所在平面的上方。即作业区域位于阻隔板310的一侧，而使阻隔板310位于建筑物20和作业区域之间。且阻隔板310位于水平时的作业面122所在平面的上方的部分的高度大于或等于无人机的旋翼到作业面122的距离。
阻隔板310上开设有用于取放货物的取放口312，取放口312供用户从阻隔板310远离作业区域的一侧取放货物。具体地，阻隔板310大致为方形板状。阻隔板310具有两个相对的表面，其中一个表面为阻隔面314，阻隔面314靠近作业区域设置，取放口312贯通该两个表面。
活动门320能够活动地安装在阻隔板310上，活动门320能够遮蔽取放口312，活动门320和阻隔板310能够共同将作业区域与阻隔板310远离作业区域的一侧分隔开，用户远离作业区域的一侧通过取放口312取货物，就 能够起到隔离用户和无人机的作用。具体地，活动门320安装在阻隔板310远离阻隔面314的表面上。
其中，活动门320和阻隔板310均为透明件，例如，玻璃、亚克力等，从而降低阻隔板310和活动门320对用户视野的遮挡。
具体在图示的实施例中，活动门320为两个，两个活动门320均活动地安装在阻隔板310上，且两个活动门320共同配合能够遮蔽取放口312。
请一并参阅图5，进一步地，两个活动门320上均开设有锁孔322，阻隔板310上安装有电子锁330，电子锁330能够插入到两个活动门320的锁孔322中，以实现两个活动门320的锁止。其中，电子锁330与电控组件200电连接，电控组件200能够控制电子锁330的解锁。具体地，电控组件200能够根据用户发出的控制信号控制电子锁330解锁，以使用户能够推开活动门320。即在没有接收到控制信号的情况下，电子锁330保持锁止，以使活动门320不能被打开。
进一步地，阻隔组件300还包括滑轨340，滑轨340固定在阻隔板310上，活动门320安装在滑轨340上，并沿滑轨340能够滑动，通过滑动活动门320，而实现活动门320的打开和关闭。
具体在图示的实施例中，滑轨340两个，两个滑轨340均设置在阻隔板310远离阻隔面314的表面上，且平行间隔，取放口312位于两个滑轨340之间，每个活动门320的相对的两侧分别沿两个滑轨340能够滑动。
可以理解，实现活动门320的打开和关闭也不限于采用滑动的方式，例如，还可以将活动门320与阻隔板310转动连接，此时，滑轨340可以省略，通过相对阻隔板310转动活动门320，以实现活动门320的打开和关闭；活动门320不限于为两个，例如，活动门320还可以为一个，活动门320和阻隔板310中的一个开设锁孔322，另一个安装电子锁330。或者，活动门320也可以采用自动感应开启功能，即设置活动门320的运动驱动器和人体感应装置，人体感应装置可以为红外传感器或超声波传感器，当人手在阻隔板310的上方时，活动门320自动打开，打开后人体感应装置检测不到人手一定时间后自动关闭活动门320。
请一并参阅图6，进一步地，阻隔板310能够活动，以使阻隔板310能 够位于靠近水平时的作业面122的边缘处并且能够至少部分位于水平时的作业面122所在平面的上方，而使无人机能够在作业面122水平时降落至作业区域，阻隔板310还能够在作业面122水平时位于作业区域的上方并与水平时的作业面122间隔且相对，以使阻隔板310能够与活动门320共同遮挡作业区域，以防止作业区域内的货物被雨淋湿，并阻止无人机降落至作业区域。即当阻隔板310相对竖直方向平行或倾斜时，阻隔板310位于建筑物20和作业区域之间，作业区域露出，而使无人机能够降落至作业区域；阻隔板310位于作业区域的上方时，取放口312的位置与作业区域的位置相对应。具体地，阻隔板310在作业面122水平时位于作业区域的上方并与水平时的作业面122间隔且相对时，阻隔面314与作业面122平行；且取放口312的位置与作业区域相对应。
具体在图示的实施例中，阻隔板310能够转动而使阻隔板310能够位于靠近作业面122的边缘处和能够位于作业区域的上方。阻隔板310的一端与固定座110转动连接，另一端为自由端，阻隔板310的自由端能够高于阻隔板靠近固定座110的一端以使活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开。
请一并参阅图7和图8，进一步地，阻隔板310远离固定座110的一端设有卡扣315，固定座110上设有与卡扣315能够卡合的卡合部114，阻隔板310还能够转动至靠近固定座110的一端高于阻隔板310的自由端，以使卡合部114能够与卡扣315相卡合，当卡合部114与卡扣315相卡合时以阻止阻隔板310发生转动，以对阻隔板310进行限位。且阻隔板310转动至靠近固定座110的一端高于阻隔板310的自由端，以使在待机状态时的阻隔板310贴近建筑物20，以减少阻隔板310相对建筑物20突出的高度。
具体地，卡合部114为开设于固定座110上的卡槽，卡扣315能够收容于卡合部114内而与卡合部114相卡合。或者，卡合部114还可以为设置在固定座110上的卡勾。
具体在图示的实施例中，卡槽114为两个，两个卡槽114分别位于开设于两个固定柱112上，卡扣315对应为两个。需要说明的是，卡槽114和卡扣315的数量不限于为两个，也可以为一个或者大于两个，卡槽114和卡扣 315的数量可根据需要进行设置。
更进一步地，在作业面122竖直或者相对竖直方向倾斜、且阻隔板310靠近固定座1110的一端高于阻隔板310的自由端时，起降平台120能够位于阻隔板310和建筑物之间，而使阻隔板310能够贴近起降平台120，而使当卡合部114与卡扣315相卡合时阻隔板310还能够阻止起降平台120转动，即起降平台120贴近建筑物20时，阻隔板310也能够贴近起降平台120，上述无人机用货物收发系统10待机时，阻隔板310阻止起降平台120朝远离建筑物20的方向转动。
无人机用货物收发系统10还包括伸缩件500，伸缩件500的一端与阻隔板310的中部转动连接，另一端与固定座110转动连接，伸缩件500能够伸缩以驱动阻隔板310转动，以实现阻隔板310的上述活动。具体地，伸缩件500为伸缩式液压缸或电动撑杆。
具体在图示的实施例中，伸缩件500为两个，两个伸缩件500的一端分别与两个固定柱112转动连接，另一端均与阻隔板310的相对的两侧的中部转动连接。
可以理解，伸缩件500远离阻隔板310的一端不限于与固定座110转动连接，例如，伸缩件500远离阻隔板310的一端也可以与起降平台120或建筑物20转动连接。伸缩件500的数量也不限于为两个，也可以为一个或者大于三个，当伸缩件500为一个时，此时，伸缩件500不与固定座110连接，伸缩件500的两端分别与阻隔板310的中部和建筑物20转动连接，或者，伸缩件500远离阻隔板310的一端也可以与起降平台120转动连接。当伸缩件500的数量大于三个时，可以使部分伸缩件500转动连接固定座110和阻隔板310，另一部分伸缩件500转动连接阻隔板310和建筑物20；或者，所有伸缩件500转动连接起降平台120和阻隔板310。
或者，实现阻隔板310的转动也不限于为上述伸缩件500的方式，例如，将阻隔板310与固定座110通过转轴转动连接，在固定座110上安装步进电机，通过步进电机与该转轴传动连接，即步进电机驱动转轴转动，以实现阻隔板310地转动；或者，还可以直接采用转动机构连接将阻隔板310连接至固定座110、作业平台或建筑物20上，此时，该转动机构包括连杆、第一转 轴、第二转轴、第一电机和第二电机，连杆的一端通过第一转轴与固定座110、作业平台或建筑物20转动连接，另一端通过第二转轴与阻隔板310转动连接；第一电机安装在固定座110、起降平台120或建筑物20上，第一电机与第一转轴传动连接，第二电机安装阻隔板310上，第二电机与第二转轴传动连接，以使第一电机和第二电机能够分别驱动第一转轴和第二转轴转动，而带动连杆和阻隔板310中的至少一个转动，以带动阻隔板310转动；此时，第一电机和第二电机均为步进电机。
或者，实现阻隔板310能够活动，也不限于采用转动的方式，例如，还可以设置滑轨340，将阻隔板310设置为在竖直方向上能够滑动地，滑轨340可以设置在建筑物20上或固定座110上，或者还可以设置一个支架，将滑轨340设置在支架上，当无人机需要降落至作业区域时，阻隔板310滑动至起降平台120的作业面122上，以隔离用户和无人机。
可以理解，在其他实施例中，阻隔板310活动，起降平台120不能转动，此时，起降平台120处于作业面122呈水平的状态；或者，阻隔板310不能活动，起降平台120能够转动，此时，阻隔板310处于相对竖直方向平行或相对竖直方向倾斜的状态，阻隔板310靠近水平时的作业面122的边缘设置并且至少部分位于水平时的作业面122所在平面的上方，且在竖直方向上，阻隔板310靠近固定座110的一端低于阻隔板310的自由端；或者，阻隔板310和起降平台120都不能转动，那么，起降平台120一直处于作业面122呈水平的状态，阻隔板310一直处于相对竖直方向平行或相对竖直方向倾斜的状态，此时，阻隔板310靠近作业面122的边缘设置并且至少部分位于作业面122所在平面的上方，且在竖直方向上，阻隔板310靠近固定座110的一端低于阻隔板310的自由端。
其中，起降平台120和阻隔板310的转动可与窗户或玻璃幕墙开启和关闭进行联动。或者，阻隔板310可作为建筑物20的窗门或外立面幕墙，即平时在不需要配合无人机进行货物收发情况下，阻隔板310可由用户手动或电动开启或关闭，此时，活动门320可以省略。
升降机构400能够伸缩，升降机构400安装在起降平台120上，并位于作业区域内，升降机构400能够朝靠近取放口312的方向伸长，升降机构400 能够承载货物，并且能够带动货物升降。其中，阻隔面314和作业面122平行时，升降机构400的位置与取放口312的位置相对应。
具体地，升降机构400与电控组件200电连接，电控组件200能够根据控制信号控制控制升降机构400伸缩，从而实现升降机构400的自动升降。
具体地，起降平台120上开设有收容槽124，收容槽124位于作业区域内，升降机构400安装在收容槽124内，且升降机构400能够伸出收容槽124。通过在起降平台120上设置收容槽124，将升降机构400设置在收容槽124内，不仅能够方便升降机构400的安装，也能够对升降机构400起到保护作用，而且还能够减小待机时的无人机用货物收发系统10的厚度，以达到减小待机时的无人机货物收发系统突出建筑物20的高度。
进一步地，收容槽124的底部为镂空结构，以便于进入收容槽124中的水的排出，而且还能够降低起降平台120重量的作用。
请一并参阅图9，具体在图示实施例中，升降机构400包括支撑架410和推杆电机420。
支撑架410能够伸缩，支撑架410安装在起降平台120上，并位于作业区域内，支撑架410能够承载货物，并且带动货物升降。具体地，支撑架410包括支撑板412、条形的第一支撑件414、铰接座415、条形的第二支撑件416和滑动座417。
支撑板412能够承载货物，并且能够带动货物升降。其中，支撑板412为平板结构，支撑板412与作业面122平行设置；支撑板412能够伸出收容槽124。
第一支撑件414的一端与起降平台120转动连接。
铰接座415与第一支撑件414远离起降平台120的一端铰接，交接座415与支撑板412相抵接，并在起降平台120上能够滑动。
第二支撑件416的中部与第一支撑件414的中部铰接，第二支撑件416的一端与支撑板412转动连接。
滑动座417与第二支撑件416远离支撑板412的一端铰接，滑动座417与起降平台120相抵接，并在起降平台120上能够滑动而带动支撑板412升降。
具体地，升降机构400还包括导向轨430，导向轨430固定在起降平台120上，第一支撑件414远离铰接座415的一端与导向轨430转动连接，滑动座417沿导向轨430能够滑动。更具体地，导向轨430设置在收容槽124的底部上。
推杆电机420能够驱动支撑架410伸缩。推杆电机420与电控组件200电连接，以使电控组件200能够控制推杆电机420的工作。具体地，电控组件200能够根据控制信号控制推杆电机420工作。
具体地，推杆电机420收容于收容槽124内。推杆电机420与第一支撑件414远离支撑板412的一端、第二支撑件416远离支撑板412的一端均转动连接，推杆电机420能够驱动第二支撑件416远离支撑板412的一端滑动。
进一步地，升降机构400还包括第一连接轴440和第二连接轴450，第一连接轴440将第一支撑件414远离支撑板412的一端和导向轨430转动连接，第二连接轴450与第二支撑件416远离支撑板412的一端转动连接，推杆电机420与第一连接轴440、第二连接轴450均转动连接，从而通过推杆电机420的伸缩以推动第二连接轴450运动而带动第二支撑件416远离支撑板412的一端滑动。
具体在图示的实施例中，第一支撑件414和第二支撑件416均为两个，两个第一支撑件414相对且平行设置，两个第二支撑件416相对且平行设置，一个第一支撑件414对应一个第二支撑件416。此时，导向轨430对应为两个，两个导向轨430平行且间隔设置，一个第二支撑件416对应一个导向轨430；第一连接轴440将两个第一支撑件414远离支撑板412的一端分别和两个导向轨430转动连接，第二连接轴450与两个第二支撑件416远离支撑板412的一端均转动连接。
可以理解，第一支撑件414和第二支撑件416的数量不限于为两个，第一支撑件414和第二支撑件416也可以为一个，此时，导向轨430对应为一个；或者第一支撑件414和第二支撑件416也可以为三个以上，此时，导向轨430的数量与第二支撑件416的数量相等，第一连接轴440将多个第一支撑件414远离支撑板412的一端分别与多个导向轨430转动连接，第二连接轴450与多个第二支撑件416远离支撑板412的一端均转动连接。其中，导 向轨430和支撑架410的数量可以根据需要进行设置。
或者，升降机构400也不限于采用上述结构，例如，升降机构400的结构还可以为仅包括支撑板412和推杆电机420，推杆电机420固定在收容槽124的底部，推杆电机420的推杆与支撑板412固定连接，通过推杆电机420的伸缩直接带动支撑板412升降。
请再次参阅图3，进一步地，无人机用货物收发系统10还包括与电控组件200电连接的压力传感器600，压力传感器600安装在升降机构400上，压力传感器600能够检测升降机构400上承载的重量，电控组件200还能够根据升降机构400上承载的重量控制升降机构400伸缩。具体地，压力传感器600可以安装在支撑板412的底部，也可以安装在导向轨430上，并位于导向轨430和收容槽124的底部之间；其中，压力传感器600能够检测支撑架410的支撑板412上承载的重量，电控组件200还能够根据支撑架410上承载的重量控制推杆电机420的工作。
进一步地，阻隔组件300还包括与电控组件200电连接的感应器700，感应器700能够感应活动门320的状态。即感应器700能够感应活动门320是处于关闭状态，还是处于打开状态。其中，感应器700能够将活动门320的状态反馈给电控组件200，电控组件200还能够根据活动门320的状态控制升降机构400伸缩。具体地，感应器700为接触微动开关或接近开关。
进一步地，电控组件200还能够根据升降机构400上承载的重量和活动门320的状态控制驱动件130的工作。例如，当货物被取走后，升降机构400上承载的重量为零，若活动门320的状态为打开，电控组件200控制驱动件130不带动起降平台120转动；若当货物被取走后，升降机构400上承载的重量为零，且活动门320的状态为关闭，电控组件200控制驱动件130带动起降平台120转动，而使起降平台120贴近建筑物20。
进一步地，阻隔组件300还包括警报器800，警报器800能够根据活动门320的状态发出警报，以提醒用户关闭活动门320。警报器800可以为蜂鸣器、震动器或闪烁灯。具体地，警报器800与电控组件200电连接，电控组件200根据感应器700反馈的活动门320的状态以及计时时间控制警报器800工作。其中，警报器800可以安装在阻隔板310上，也可以内置于电子 锁330内。需要说明的是，警报器800也可以省略，此时，无人机用货物收发系统10不具有发出警报的功能。
进一步地，阻隔面314上设有供无人机降落的定位信标316，以便于无人机准确地降落至起降平台120的作业区域上。
请再次参阅图1，具体地，定位信标316为两个，两个定位信标316均位于阻隔面314上，两个定位信标316设置在阻隔面314的对角线上，并分别靠近阻隔板310的两个对角设置。即当阻隔面314所在的平面能够与水平设置时的作业面122所在的平面相交时，定位信标316对于无人机而言是可见的，若阻隔板310位于作业区域的上方，并与活动门320共同遮蔽作业区域时，定位信标316相对无人机不可见。
可以理解，定位信标316的数量也不限于为两个，定位信标316也可以为一个或大于两个，定位信标316的数量可以根据需要进行设置。
具体地，定位信标316为静态图案，阻隔板310上还开设有容置槽318，容置槽318的侧壁上安装有光源(图未示)，定位信标316设置在容置槽318的底部上，以便于无人机在夜晚也能够准确地降落。更具体地，容置槽318位于阻隔板310上，且容置槽318的数量与定位信标316的数量相对应。
可以理解，定位信标316也不限于设置在阻隔板310上，例如还可以设置在起降平台120的作业面122上，只要无人机在降落过程中对其可见即可。
上述无人机用货物收发系统10至少有以下优点：
(1)由于上述无人机用货物收发系统10的阻隔组件300靠近作业面122的边缘设置并且至少部分位于作业面122所在平面的上方，以使阻隔组件300将作业区域与阻隔组件300远离作业区域的一侧分隔开，那么，在安装上述无人机用货物收发系统10，只需将阻隔组件300远离作业区域的一侧朝向用户，就能够阻隔用户和无人机从而降低了用户与无人机接触的可能性，更加的安全。
(2)通过在阻隔板310上开设有供用户取放货物的取放口312，将活动门320活动地安装在阻隔板310上，并且活动门320能够遮蔽取放口312，而起降平台120的供无人机降落和货物放置的作业区域位于阻隔板310的另一侧，在安装无人机用货物收发系统10时，使阻隔板310位于建筑物20和 作业区域之间，就能够使阻隔板310和活动门320能够共同隔离用户和无人机，且能够方便货物的取放。
(3)上述无人机用货物收发系统10的阻隔板310能够位于作业区域的上方，而使阻隔板310能够与活动门320共同遮挡作业区域，从而能够对作业区域上的货物起到遮挡作用，以减少货物被雨水淋湿的可能性。
(4)由于上述无人机用货物收发系统10的起降平台120能够转动，以作业面122还能够竖直或者相对竖直方向倾斜，以使起降平台120能够贴近建筑物20，起降平台120贴近建筑物20时，阻隔板310还能够活动至贴近起降平台120，从而使上述无人机用货物收发系统10能够在待机的时候，阻隔板310和起降平台120均能够与建筑物20贴近，从而实现上述无人机用货物收发系统10的可折叠，以减少无人机用货物收发系统10相对建筑物20的凸出程度，而降低风，特别是在沿海地区的台风，对无人机用货物收发系统10的损害。
(5)由于上述无人机用货物收发系统10具有能够伸缩的升降机构400，使得当无人机要卸载货物时，升降机构400能够将伸长以接住货物，而避免因为存在高度差而造成货物直接掉落在平台上；同时，当无人机要装载货物时，升降机构400能够将伸长以方便无人机装载货物。另外当用户需要取货时，升降机构400能够将伸长以方便用户收取货物。
(6)通过压力传感器600、感应器700辅助电控组件200控制阻隔板310、起降平台120和升降机构400的运动，有利于实现无人机用货物收发系统10的自动化控制，控制更加方面。
(7)定位信标316可以辅助无人机在起降过程中定位，以便于无人机准确地降落至起降平台120上。
(8)阻隔板310位于无人机和用户之间，也可以阻隔一部分无人机的工作噪声传导至用户。
可以理解，固定座110也可以省略，此时，驱动件130直接安装在建筑物20上，即驱动件130远离起降平台120的一端与建筑物20转动连接；或者，驱动件130也可以省略，此时，起降平台120可以不具有转动功能；或者，阻隔板310也可以为不能活动，此时，伸缩件500也可以省略；或者， 升降机构400也可以省略，此时，无人机用货物收发系统10不具有带动货物升降的功能；或者，定位信标316也可以省略，只要能够能够使无人机准确降落即可。
一实施方式的货物的收取方法，为基于上述无人机用货物收发系统10的一种货物的收取方法，该货物的收取方法可用于无人机送件，用户取件。该货物的收取方法包括以下步骤：
步骤S31：转动起降平台120以使起降平台120的作业面122水平，和将阻隔板310活动至靠近作业面122的边缘处并相对竖直方向平行或倾斜。
如图2所示，图2为无人机用货物收发系统10的起始状态，即待机状态为：起降平台120和阻隔板310均贴近建筑物20，且起降平台120和阻隔板310远离固定座110的一侧均朝下，此时，阻隔面314朝向建筑物20，活动门320和电子锁330都处于关闭状态。
在本实施方式中，当无人机需要降落时，无人机发出控制信号A1，电控组件200根据控制信号A1控制驱动件130带动起降平台120转动，直至起降平台120的作业面122与水平方向平行；同时，电控组件200根据控制信号A1控制伸缩件500伸长，以使阻隔板310转动，而使阻隔板310转动，直至阻隔板310远离固定座110的一端朝上设置。此时，无人机用货物收发系统10为全展开状态。即经过步骤S31之后，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开。此时，阻隔板310位于建筑物20和作业区域之间，作业区域露出，以便于无人机降落。
需要说明的是，步骤S31也不限于为上述方式，在其它实施例中，若只有阻隔板310能够活动，阻隔板310的起始状态为贴近建筑物20，且阻隔面314朝向建筑物20，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开，而起降平台120的起始状态即为作业面122水平，此时，步骤S31为：使阻隔板310活动，直至阻隔板310活动至靠近作业面122的边缘处并相对竖直方向平行或倾斜，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，以使作业区域露出。若只有起降平台120为能够转动的， 且起降平台120的起始状态为贴近建筑物20设置，而阻隔板310不能活动，阻隔板310的起始状态为靠近作业面122的边缘处并相对竖直方向平行或倾斜，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开，阻隔面314远离建筑物20，此时，步骤S31为：转动起降平台120以使起降平台120的作业面122水平。若起降平台120和阻隔板310均是不能活动的，或者说起降平台120和阻隔板310的起始状态即为：起降平台120的作业面122水平，阻隔板310靠近作业面122的边缘处并相对竖直方向平行或倾斜，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，且作业区域露出，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开，那么，步骤S31也可以省略。
进一步地，转动起降平台120和阻隔板310的活动是电控组件200根据无人机发出的控制信号进行控制的。
步骤S32：无人机降落至无人机用货物收发系统10的作业区域上。
具体地，无人机降落至无人机用货物收发系统10的作业区域上时，活动门320遮蔽取放口312，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开。
在本实施方式中，无人机根据电控组件200发出的反馈信号进行降落。即当上述无人机用货物收发系统10完成步骤S31时，电控组件200向无人机发出反馈信号B1，无人机接收到反馈信号B1后降落至作业区域。
进一步地，无人机根据阻隔板310的阻隔面314上的定位信标316进行降落。
进一步地，无人机降落至作业区域时，无人机上携带的货物位于升降机构400的上方。
步骤S33：无人机将货物放置在作业区域上。
具体地，无人机将货物放置在作业区域上的步骤为：无人机将货物放置在作业区域处的升降机构400上。更具体地，无人机将货物放置在作业区域上的步骤包括：升降机构400伸长，直至升降机构400与无人机上的货物相抵接；无人机卸载货物；待货物卸载在升降机构400上后，升降机构400缩 短，货物随升降机构400运动。
在本实施方式中，当无人机降落至作业区域时，无人机发出的控制信号，电控组件200根据控制信号控制升降机构400伸长。当升降机构400伸长到与无人机上的货物相抵接时，压力传感器600检测到的升降机构400上承载的重量发生变化，电控组件200控制推杆电机420停止驱动支撑架410伸长，电控组件200发出反馈信号，无人机根据反馈信号将货物卸载至升降机构400上。待货物卸载在升降机构400上后，无人机发出控制信号，电控组件200根据控制信号控制升降机构400缩短，货物随升降机构400运动。
即：当无人机降落至作业区域时，无人机发出控制信号A2，电控组件200根据控制信号A2控制推杆电机420驱动支撑架410伸长，并使支撑板412伸出收容槽124，如图1所示；当支撑架410伸长到支撑板412与无人机上的货物相抵接时，压力传感器600检测到的升降机构400上承载的重量发生变化，电控组件200根据控制推杆电机420停止驱动支撑架410伸长，此时，电控组件200向无人机发出反馈信号B2，无人机根据反馈信号B2将货物卸载至支撑板412上；待货物卸载在升降机构400上后，无人机发出控制信号A3，电控组件200根据控制信号A3控制升降机构400缩短，货物随升降机构400运动，直至支撑板412与作业面122平齐。
需要说明的是，若没有升降机构400，无人机可以直接将货物卸载在作业区域上。
步骤S34：无人机飞离作业区域。
在本实施方式中，在无人机发出控制信号A3后，无人机停留一端时间后再飞离作业区域，以给升降机构400提供缩短的时间。
步骤S35：将阻隔板310活动至作业区域的上方并与水平时的作业面122间隔且相对，以使阻隔板310与活动门320共同遮蔽作业区域处的货物。
在本实施方式中，无人机飞离起降平台120后，电控组件200控制伸缩件500缩短，而带动阻隔板310朝靠近作业区域的方向转动，直至阻隔板310位于作业区域的上方，阻隔板310与活动门320共同遮挡作业区域上的货物，即为无人机用货物收发系统10的半展开状态，如图6所示。
具体地，无人机飞离起降平台120时发出控制信号A4，电控组件200根 据控制信号A4控制伸缩件500缩短。
进一步地，当阻隔板310位于作业区域的上方，阻隔板310与活动门320共同遮挡作业区域上的货物时，阻隔面314与作业面122平行。
需要说明的是，若阻隔板310是不能活动的，步骤S35可以省略。
步骤S36：打开活动门320，以使取放口312露出。
在本实施方式中，当用户需要取件时，用户向电控组件200发出控制信号C，此时，电控组件200根据控制信号C控制电子锁330解锁，用户将活动门320打开，以使取放口312露出。
需要说明的是，不限于采用上述方式打开活动门以使取放口312露出，例如，可以不用电子锁330，此时，用户直接将活动门320打开即可。
步骤S37：从隔离组件300远离作业区域的一侧取走货物。
具体地，从隔离组件300远离作业区域的一侧取走货物的步骤包括：打开安装在靠近作业面122的边缘处的阻隔板310上的活动门320，以使取放口312露出；在阻隔板310远离作业区域的一侧从取放口312取走货物。
具体地，在阻隔板310远离作业区域的一侧从取放口312取走货物的步骤包括：将升降机构400朝靠近取放口312的方向伸长，以带动升降机构400上的货物朝靠近取放口312运动，在阻隔板310远离作业区域的一侧从取放口312取出货物；然后关闭活动门320和将升降机构400缩短。
具体地，在货物取出后，用户将活动门320关闭，以使电子锁330锁止，压力传感器600检测到支撑板412上承载的重量为零，电控组件200确认货物已被取走，电控组件200控制推杆电机420驱动支撑架410缩短，以使支撑板412收容于收容槽124中，同时，感应器700确认活动门320处于关闭状态，使电子锁330锁止。
进一步地，感应器700检测到活动门320为打开状态，并将反馈至电控组件200，电控组件200根据该反馈控制升降机构400伸长。
进一步地，电控组件200控制推杆电机420驱动支撑架410伸长。
需要说明的是，若没有升降机构400，用户直接从取放口312取出货物即可。
步骤S38：转动起降平台120以使起降平台120的作业面122竖直或者 相对竖直方向倾斜，转动阻隔板310，在阻隔板310靠近固定座110的一端高于阻隔板310的自由端。
即此时，起降平台120贴近建筑物20，阻隔板310贴近起降平台120，起降平台120位于建筑物20和阻隔板310之间，起降平台120的作业面122与阻隔板310的阻隔面314相对。
具体地，步骤S38包括：感应器700确认活动门320处于关闭状态后，电控组件200控制驱动件130带动起降平台120转动，以使起降平台120的作业面122竖直或者相对竖直方向倾斜，和控制伸缩件500缩短，阻隔板310转动，以使阻隔板310靠近固定座110的一端高于阻隔板310的自由端。
需要说明的是，若起降平台120和阻隔板310均不能转动，那么，无需转动起降平台120和转动阻隔板310，只需关闭活动门320以使活动门320遮蔽取放口312即可；若起降平台120不能转动，阻隔板310能够转动，只需关闭活动门320以使活动门320遮蔽取放口312，转动阻隔板310，使阻隔板310靠近固定座110的一端高于阻隔板310的自由端即可；若阻隔板310不能转动，起降平台120能转动，此时，关闭活动门320以使活动门320遮蔽取放口312，转动起降平台120以使起降平台120的作业面122竖直或者相对竖直方向倾斜，起降平台120贴近建筑物20即可。
上述货物的收取方法通过使用上述无人机用货物收发系统能够方便快递的收取，实现无人机送件，用户取件，且能够降低了用户与无人机接触的可能性，更加的安全。
一实施方式的货物的寄送方法，为基于上述无人机用货物收发系统10的一种货物的寄送方法，该货物的寄送方法可用于用户寄件，无人机取件。该货物的寄送方法包括以下步骤：
步骤S41：转动起降平台120以使起降平台120的作业面122水平，和将阻隔板310活动至作业区域的上方并与水平时的作业面122间隔且相对，以使阻隔板310与活动门320共同遮蔽作业区域处的货物。
如图2所示，图2为无人机用货物收发系统10的起始状态，即待机状态为：起降平台120和阻隔板310均贴近建筑物20，且起降平台120和阻隔板310远离固定座110的一侧均朝下，此时，阻隔面314朝向建筑物20，活动 门320和电子锁330都处于关闭状态。
其中，转动起降平台120和使阻隔板310相对起降平台120活动是电控组件200根据用户发出的控制信号进行控制的。
在本实施方式中，当用户需要寄件时，用户发出控制信号D1，电控组件200根据控制信号D1控制驱动件130带动起降平台120转动，直至起降平台120的作业面122与水平方向平行；同时，电控组件200根据控制信号D1控制伸缩件500伸长，而使阻隔板310转动，直至阻隔板310位于作业区域的上方，阻隔板310与活动门320共同遮蔽作业区域。此时，无人机用货物收发系统10为半展开状态，如图6所示。
进一步地，当阻隔板310位于作业区域的上方，阻隔板310与活动门320共同遮挡作业区域时，阻隔面314与作业面122平行。
需要说明的是，步骤S41也不限于为上述方式，在其它实施例中，若只有阻隔板310能够活动，阻隔板310的起始状态为贴近建筑物20，且阻隔面314朝向建筑物20，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开，而起降平台120的起始状态即为作业面122水平，此时，步骤S41为：使阻隔板310活动，直至阻隔板310活动至靠近作业面122的边缘处并相对竖直方向平行或倾斜，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，以使作业区域露出。若只有起降平台120为能够转动的，且起降平台120的起始状态为贴近建筑物20设置，而阻隔板310不能活动，阻隔板310的起始状态为靠近作业面122的边缘处并相对竖直方向平行或倾斜，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开，阻隔面314远离建筑物20，此时，步骤S41为：转动起降平台120以使起降平台120的作业面122水平。若起降平台120和阻隔板310均是不能活动的，或者说起降平台120和阻隔板310的起始状态即为：起降平台120的作业面122水平，阻隔板310靠近作业面122的边缘处并相对竖直方向平行或倾斜，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，且作业区域露出，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的 一侧分隔开，那么，步骤S41也可以省略。
步骤S42：打开活动门320，以使取放口312露出。
在本实施方式中，当无人机用货物收发系统10为半展开状态时，电控组件200向用户反馈信号E1，以提示用户可以放置货物；用户发出控制信号D2，电控组件200控制电子锁330解锁，用户将活动门320打开，以使取放口312露出。
需要说明的是，步骤S42不限于上述方式，也可以在阻隔板310位于作业区域的上方时，电控组件200控制电子锁330解锁。
步骤S43：将货物放置在作业区域上。
具体地，在用户将活动门320打开之后，电控组件200控制升降机构400朝靠近取放口312的方向伸长；用户将货物放置在升降机构400上；升降机构400缩短，货物随升降机构400运动。
在本实施方式中，在用户将活动门320打开之后，电控组件200控制推杆电机420驱动支撑架410伸长，并使支撑板412伸出作业区域112。
进一步地，在用户将活动门320打开之后，电控组件200控制升降机构400朝靠近取放口312的方向伸长的步骤为：在用户将活动门320打开之后，感应器700检测到活动门320处于打开状态，并将该打开状态反馈给电控组件200，电控组件200控制推杆电机420驱动支撑架410伸长，并使支撑板412伸出作业区域112。
具体地，升降机构400缩短，货物随升降机构400运动的步骤为：用户将货物放置在升降机构400上后，压力传感器600检测到的升降机构400上承载的重量发生变化，电控组件200货物已放置在升降机构400上，此时，电控组件200控制升降机构400缩短。更具体地，电控组件200控制推杆电机420驱动支撑架410缩短，直至支撑板412与作业面122平齐，此时，无人机用货物收发系统10的状态仍然为图6所示状态。
需要说明的是，若没有升降机构400，用户打开活动门320之后可以直接将货物放置在作业区域上。
步骤S44：关闭活动门320，以使活动门320遮蔽取放口312。
在本实施方式中，用户放置货物后，用户关闭活动门320，以使活动门 320遮蔽取放口312，电子锁330锁止。
步骤S45：使阻隔板310相对起降平台120活动，直至阻隔板310活动至靠近作业面122的边缘处并相对竖直方向平行或倾斜，以使作业区域露出。
在本实施方式中，当无人机需要取件时，无人机向电控组件200发出控制信号F1，电控组件200根据控制信号F1控制伸缩件500伸长，以使阻隔板310转动，直至阻隔板310远离固定座110的一端高于靠近固定座110的一端。此时，无人机用货物收发系统10为全展开状态。即经过步骤S45之后，阻隔板310的自由端高于阻隔板310靠近固定座110的一端，活动门320和阻隔板310共同将作业区域与阻隔板310远离作业区域的一侧分隔开。此时，阻隔板310位于建筑物20和作业区域之间，作业区域露出，以便于无人机降落。
需要说明的是，若阻隔板不能活动，步骤S45可以省略。
步骤S46：无人机降落至作业区域上。
在本实施例中，待无人机用货物收发系统10为全展开状态时，电控组件200向无人机发出反馈信号E2，无人机确认可以降落后，再降落至作业区域。
需要说明的是，若阻隔板不能活动，电控组件200无需向无人机发出反馈信号E2，无人机直接降落至作业区域上即可。
步骤S47：无人机收取货物，并携带货物飞离作业区域。
在本实施方式中，无人机降落至作业区域后，无人机发出控制信号F2，电控组件200根据控制信号F2控制升降机构400伸长，此时状态如图1所示，直至升降机构400上的货物与无人机底部相抵接；无人机固定货物；升降机构400缩短；无人机携带货物飞离作业区域。
具体地，当升降机构400上的货物与无人机底部相抵接时，压力传感器600检测到升降机构400上的承载的重量发生变化，确认货物已经升降机构400与无人机机身底部的货物固定装置相抵接，电控组件200控制升降机构400停止伸长。
具体地，无人机收取货物的步骤为：在升降机构400与无人机机身底部的货物固定装置相抵接时，电控组件200向无人机发出反馈信号E3，反馈货物已经与无人机机身底部的货物固定装置相抵接，此时，无人机将货物固定。
具体地，无人机固定货物的步骤之后，升降机构400缩短，无人机飞离作业区域的步骤为：待无人机固定好货物后，无人机向电控组件200发出控制信号F3，电控组件200根据控制信号F3控制升降组件400缩短，无人机飞离作业区域。更具体地，电控组件200根据控制信号F3控制推杆电机420驱动支撑架410缩短，直至支撑板412收容于收容槽124中，无人机携带货物飞离作业区域。
需要说明的是，无人机收取货物的方式不限于上述方式，无人机可以自带伸缩固定装置，直接将货物升起和固定，此时，无需升降机构400带动货物上升固定。
步骤S48：转动起降平台120以使起降平台120，以使作业面122竖直或者相对竖直方向倾斜，转动阻隔板310，以使阻隔板310靠近固定座110的一端高于阻隔板310的自由端。
具体地，步骤S48为：无人机飞离作业区域时，发出控制信号F4，电控组件200根据控制信号F4控制驱动件130带动起降平台120转动，和控制伸缩件500缩短以使阻隔板310转动，回到待机状态，以使无人机用货物收发系统10贴近建筑物20，回到待机状态，即图2所示的状态。
需要说明的是，若起降平台120和阻隔板310均不能转动，那么，无需转动起降平台120和转动阻隔板310，只需关闭活动门320以使活动门320遮蔽取放口312即可；若起降平台120不能转动，阻隔板310能够转动，只需关闭活动门320以使活动门320遮蔽取放口312，转动阻隔板310，使阻隔板310靠近固定座110的一端高于阻隔板310的自由端即可；若阻隔板310不能转动，起降平台120能转动，此时，关闭活动门320以使活动门320遮蔽取放口312，转动起降平台120以使起降平台120的作业面122竖直或者相对竖直方向倾斜，起降平台120贴近建筑物20即可。
上述货物的寄件方法通过使用上述无人机用货物收发系统能够方便快递的收取，实现用户寄件，无人机取件，且能够降低了用户与无人机接触的可能性，更加的安全。
请一并参阅图10和图11，另一实施方式的无人机用货物收发系统40与 无人机用货物收发系统10的结构大致相同，区别在于，伸缩件41远离阻隔板42的一端与起降平台43转动连接。
由于无人机用货物收发系统40与无人机用货物收发系统10的结构大致相同，因此，也具有无人机用货物收发系统10的效果。
请一并参阅图12，又一实施方式的无人机用货物收发系统，与无人机用货物收发系统10的结构大致相同，区别在于，阻隔组件(图未标)的结构和活动方式不同。在本实施例中，阻隔组件包括能够在竖直方向上滑动的阻隔板51，阻隔板51靠近水平时的起降平台52的作业面52a的边缘设置，阻隔板51能够至少部分位于水平时的作业面52a所在平面的上方，而将作业区域与阻隔板51远离作业区域的一侧分隔开。即阻隔板51上无需设置取放口，也无需活动门。
具体地，阻隔板51能够滑动地安装在固定座53上。
此时，在货物收取时，在无人机降落至无人机用货物收发系统50的作业区域上时，阻隔板51将作业区域与阻隔512远离作业区域的一侧分隔开，且此时，阻隔板51位于水平时的作业面52a所在的平面的上方的部分到作业面52a所在平面的最大高度大于无人机的旋翼到作业面52a所在平面的高度，以隔离用户和无人机，即为图12的展开状态。从隔离组件51远离作业区域的一侧取走货物的步骤包括：阻隔板51朝竖直向下的方向滑动；在阻隔板51远离作业区域的一侧取走货物，此时取物状态如图13所示。
进一步地，在本实施方式中，升降机构54的功能与升降机构400也有所不同，起降平台52不具有起降平台120的收容槽124。在本实施例中，起降平台52上开设有滑槽52b，滑槽52b从作业区域向靠近阻隔板51的方向延伸，升降机构54安装在滑槽52b内，并且能够沿滑槽52b的延伸方向滑动，以使升降机构54能够带动货物升降和能够带动货物滑动。本实施方式的升降机构54不仅具有升降机构400的升降功能，还具有能够在滑槽52b中滑动的功能。此时，具体地，导向轨430与滑槽52b的侧壁滑动连接。滑槽52b可以贯通起降平台52的作业面52a与作业面52a相对的面，也可以为具有类似 于收容槽124的结构。
此时，在货物收取时，无人机将货物放置在作业区域上的步骤为：无人机将货物放置在作业区域处的升降机构54上。从隔离组件51远离作业区域的一侧取走货物的步骤包括：升降机构54带动货物沿滑槽52b朝靠近阻隔板51的方向滑动，阻隔板51朝竖直向下的方向滑动，在阻隔板51远离作业区域的一侧取走货物。
那么，在阻隔板51远离作业区域的一侧取走货物之后，转动起降平台52以使起降平台52的作业面52a竖直或者相对竖直方向倾斜，即此时，起降平台52贴近阻隔板51，起降平台52远离的作业面52a的一面与阻隔板310的阻隔面314相对，阻隔板51位于起降平台52和建筑物60之间，此时为折叠状态，即如图14所示。无人机降落至无人机用货物收发系50的作业区域上的步骤之前，还包括阻隔板51朝竖直向上的方向滑动，以使阻隔板51将作业区域与阻隔板51远离作业区域的一侧分隔开的步骤。
由于无人机用货物收发系统50与无人机用货物收发系统10的结构大致相同，因此，也具有无人机用货物收发系统10的效果。
以上所述实施例的各技术特征可以进行任意的组合，为使描述简洁，未对上述实施例中的各个技术特征所有可能的组合都进行描述，然而，只要这些技术特征的组合不存在矛盾，都应当认为是本说明书记载的范围。
以上所述实施例仅表达了本发明的几种实施方式，其描述较为具体和详细，但并不能因此而理解为对发明专利范围的限制。应当指出的是，对于本领域的普通技术人员来说，在不脱离本发明构思的前提下，还可以做出若干变形和改进，这些都属于本发明的保护范围。因此，本发明专利的保护范围应以所附权利要求为准。

Claims (28)

  1. 一种无人机用货物收发系统，包括：
    支承组件，包括能够安装在建筑物上的起降平台，所述起降平台具有作业面，所述作业面上设有供无人机降落和供货物放置的作业区域；及
    阻隔组件，靠近所述作业面的边缘设置并且至少部分位于所述作业面所在平面的上方，以使所述阻隔组件将所述作业区域与所述阻隔组件远离所述作业区域的一侧分隔开。
  2. 根据权利要求1所述的无人机用货物收发系统，其特征在于，所述阻隔组件包括阻隔板和活动门，所述阻隔板靠近所述作业面的边缘设置并且至少部分位于所述作业面所在平面的上方，所述阻隔板上开设有用于取放所述货物的取放口，所述活动门能够活动地安装在所述阻隔板上，所述活动门能够遮蔽所述取放口，所述活动门和所述阻隔板能够共同将所述作业区域与所述阻隔板远离所述作业区域的一侧分隔开。
  3. 根据权利要求2所述的无人机用货物收发系统，其特征在于，所述阻隔板能够活动，以使所述阻隔板能够位于靠近所述作业面的边缘处并且能够至少部分位于所述作业面所在平面的上方，而使所述无人机能够降落至所述作业区域，所述阻隔板还能够位于所述作业区域的上方并与所述作业面间隔且相对，以使所述阻隔板能够与所述活动门共同遮挡所述作业区域，并阻止所述无人机降落至所述作业区域。
  4. 根据权利要求3所述的无人机用货物收发系统，其特征在于，所述阻隔板能够转动而使所述阻隔板能够位于靠近所述作业面的边缘处和能够位于所述作业区域的上方，所述支承组件还包括能够固定在所述建筑物上的固定座，所述起降平台安装在所述固定座上，所述阻隔板的一端与所述固定座转动连接，另一端为自由端，所述阻隔板的所述自由端能够高于所述阻隔板靠近所述固定座的一端以使所述活动门和所述阻隔板能够共同将所述作业区域与所述阻隔板远离所述作业区域的一侧分隔开。
  5. 根据权利要求4所述的无人机用货物收发系统，其特征在于，所述无 人机用货物收发系统还包括伸缩件，所述伸缩件的一端与所述阻隔板的中部转动连接，另一端与所述固定座和所述起降平台中的一个转动连接，所述伸缩件能够伸缩以驱动所述阻隔板转动。
  6. 根据权利要求4所述的无人机用货物收发系统，其特征在于，所述阻隔板远离所述固定座的一端设有卡扣，所述固定座上设有与所述卡扣能够卡合的卡合部，所述阻隔板还能够转动至靠近所述固定座的一端高于所述阻隔板的所述自由端，以使所述卡合部能够与所述卡扣相卡合。
  7. 根据权利要求6所述的无人机用货物收发系统，其特征在于，所述起降平台与所述固定座转动连接，以使所述作业面能够水平而使所述作业区域能够供所述货物放置和所述无人机降落，和使所述作业面还能够竖直或者相对竖直方向倾斜，以使在所述阻隔板靠近所述固定座的一端高于所述阻隔板的所述自由端时，所述起降平台能够位于所述阻隔板和所述建筑物之间，并使所述阻隔板能够贴近所述起降平台，其中，所述阻隔板能够位于靠近水平时的所述作业面的边缘处并且能够至少部分位于水平时的所述作业面所在平面的上方，所述阻隔板能够在所述作业面水平时位于所述作业区域的上方并与水平时的所述作业面间隔且相对。
  8. 根据权利要求2～7任一项所述的无人机用货物收发系统，其特征在于，还包括能够伸缩的升降机构，所述升降机构安装在所述起降平台上，并位于所述作业区域，所述升降机构能够朝靠近所述取放口的方向伸长，所述升降机构能够承载所述货物，并且能够带动所述货物升降。
  9. 根据权利要求8所述的无人机用货物收发系统，其特征在于，所述升降机构包括：
    能够伸缩的支撑架，安装在所述起降平台上，并位于所述作业区域内，所述支撑架能够承载所述货物，并且能够带动所述货物升降；
    推杆电机，能够驱动所述支撑架伸缩。
  10. 根据权利要求9所述的无人机用货物收发系统，其特征在于，所述起降平台上开设有收容槽，所述收容槽位于所述作业区域内，所述升降机构 安装在所述收容槽内，且所述升降机构能够伸出收容槽。
  11. 根据权利要求10所述的无人机用货物收发系统，其特征在于，所述收容槽的底部为镂空结构。
  12. 根据权利要求8所述的无人机用货物收发系统，其特征在于，还包括电控组件及与所述电控组件电连接的压力传感器，所述电控组件能够接收控制信号，并且能够向所述无人机发送反馈信号，所述电控组件与所述升降机构均电连接，所述电控组件能够根据控制信号控制所述升降机构伸缩，所述压力传感器安装在所述升降机构上，所述压力传感器能够检测所述升降机构上承载的重量，所述电控组件还能够根据所述重量控制所述升降机构伸缩。
  13. 根据权利要求12所述的无人机用货物收发系统，其特征在于，所述阻隔组件还包括与所述电控组件电连接的感应器，所述感应器能够感应所述活动门的状态，并且能够将所述活动门的状态反馈给所述电控组件，所述电控组件还能够根据所述活动门的状态控制所述升降机构伸缩。
  14. 根据权利要求1所述的无人机用货物收发系统，其特征在于，所述起降平台能够转动，以使所述作业面能够水平而使所述作业区域能够供所述货物放置和所述无人机降落，所述作业面还能够竖直或者相对竖直方向倾斜，所述阻隔组件靠近水平时的所述作业面的边缘设置，所述阻隔组件能够至少部分位于水平时的所述作业面所在的平面的上方而将所述作业区域与所述阻隔组件远离所述作业区域的一侧分隔开。
  15. 根据权利要求14所述的无人机用货物收发系统，其特征在于，所述阻隔组件包括能够在竖直方向上滑动的阻隔板，所述阻隔板靠近水平时的所述作业面的边缘设置，所述阻隔板能够至少部分位于水平时的所述作业面所在平面的上方，而将所述作业区域与所述阻隔板远离所述作业区域的一侧分隔开。
  16. 根据权利要求15所述的无人机用货物收发系统，其特征在于，所述起降平台上开设有滑槽，所述滑槽从所述作业区域向靠近所述阻隔板的方向延伸，所述无人机用货物收发系统还包括用于放置所述货物且能够伸缩的升 降机构，所述升降机构安装在所述滑槽内，并且能够沿所述滑槽的延伸方向滑动，以使所述升降机构能够带动所述货物升降和能够带动所述货物滑动。
  17. 根据权利要求14所述的无人机用货物收发系统，其特征在于，所述起降平台为方形板状，所述支承组件还包括固定座和驱动件，所述固定座能够固定在所述建筑物上，所述固定座与所述起降平台的一侧转动连接，所述驱动件为伸缩杆，所述驱动件的两端分别与所述固定座和所述起降平台的中部转动连接，所述驱动件能够伸缩而驱动所述起降平台转动。
  18. 根据权利要求1所述的无人机用货物收发系统，其特征在于，所述阻隔组件具有阻隔面，所述阻隔面靠近所述作业区域设置，所述阻隔面上设有供所述无人机降落的定位信标。
  19. 一种货物的收取方法，包括如下步骤：
    所述无人机降落至权利要求1所述的无人机用货物收发系统的所述作业区域上；
    所述无人机将所述货物放置在所述作业区域上；
    所述无人机飞离所述作业区域；及
    从所述隔离组件远离所述作业区域的一侧取走所述货物。
  20. 根据权利要求19所述的货物的收取方法，其特征在于，所述从所述隔离组件远离所述作业区域的一侧取走所述货物的步骤包括：打开安装在靠近所述作业面的边缘处的阻隔板上的活动门，以使所述取放口露出；在所述阻隔板远离所述作业区域的一侧从所述取放口取走所述货物；
    所述无人机降落至所述无人机用货物收发系统的作业区域上时，所述活动门遮蔽所述取放口，所述活动门和所述阻隔板共同将所述作业区域与所述阻隔板远离所述作业区域的一侧分隔开。
  21. 根据权利要求20所述的货物的收取方法，其特征在于，在所述无人机飞离所述作业区域的步骤之后，在所述打开安装在阻隔板上的活动门的步骤之前，还包括将所述阻隔板活动至所述作业区域的上方并与水平时的所述作业面间隔且相对，以使所述阻隔板与所述活动门共同遮挡所述作业区域处 的所述货物的步骤；
    所述无人机降落至所述无人机用货物收发系统的作业区域上的步骤之前，还包括将所述阻隔板活动至靠近所述作业面的边缘处并相对竖直方向平行或倾斜。
  22. 根据权利要求20所述的货物的收取方法，其特征在于，所述无人机将所述货物放置在所述作业区域上的步骤包括：将安装在所述作业区域处的升降机构伸长，直至所述升降机构与所述无人机上的所述货物相抵接；所述无人机卸载所述货物；待所述货物卸载在所述升降机构上后，所述升降机构缩短，所述货物随所述升降机构运动。
  23. 根据权利要20所述的货物的收取方法，其特征在于，所述无人机将所述货物放置在所述作业区域上的步骤为：所述无人机将所述货物放置在所述作业区域处的升降机构上；
    所述在所述阻隔板远离所述作业区域的一侧从所述取放口取走所述货物的步骤包括：将所述升降机构朝靠近所述取放口的方向伸长，以带动所述升降机构上的所述货物朝靠近所述取放口运动，在所述阻隔板远离所述作业区域的一侧从所述取放口取出所述货物；然后关闭所述活动门和将所述升降机构缩短。
  24. 根据权利要求19所述的货物的收取方法，其特征在于，所述从所述隔离组件远离所述作业区域的一侧取走所述货物的步骤包括：将靠近所述作业面的边缘处的所述阻隔板朝竖直向下的方向滑动；在所述阻隔板远离所述作业区域的一侧取走所述货物；
    所述无人机降落至所述无人机用货物收发系统的作业区域上时，所述阻隔板将所述作业区域与所述阻隔板远离所述作业区域的一侧分隔开。
  25. 根据权利要求19～24任一项所述的货物的收取方法，其特征在于，在所述无人机降落至所述的无人机用货物收发系统的作业区域上的步骤之前，还包括转动所述起降平台，以使所述起降平台的作业面水平的步骤；
    所述从所述隔离组件远离所述作业区域的一侧取走所述货物的步骤之 后，还包括转动所述起降平台，以使所述作业面竖直或者相对竖直方向倾斜的步骤。
  26. 一种货物的寄送方法，包括如下步骤：
    将货物放置在权利要求1所述的无人机用货物收发系统的所述作业区域处；
    所述无人机降落至所述作业区域上；及
    所述无人机收取所述货物，并携带所述货物飞离所述作业区域。
  27. 根据权利要求26所述的货物的寄送方法，其特征在于，所述将货物放置在所述无人机用货物收发系统的所述作业区域处的步骤包括：打开位于所述作业区域的上方并与水平时的所述作业面间隔且相对的阻隔板上的活动门，以使所述取放口露出；将所述货物从所述取放口放至所述作业区域处；然后关闭所述活动门，以遮蔽所述取放口，以使所述阻隔板与所述活动门共同遮挡所述作业区域处的所述货物；
    所述将货物放置在所述无人机用货物收发系统的所述作业区域处的步骤之后，所述无人机降落至所述作业区域上的步骤之前，还包括将所述阻隔板活动至靠近所述作业面的边缘处并且相对竖直方向平行或倾斜，以使所述活动门和所述阻隔板共同将所述作业区域与所述阻隔板远离所述作业区域的一侧分隔开的步骤。
  28. 根据权利要求27所述的货物的寄送方法，其特征在于，所述将所述货物从所述取放口放至所述作业区域处的步骤为：将所述货物从所述取放口放至所述作业区域内的升降机构上；
    所述无人机收取所述货物，并携带所述货物飞离所述作业区域的步骤包括：将所述升降机构伸长，直至所述升降机构上的所述货物与所述无人机底部相抵接；所述无人机固定所述货物；所述升降机构缩短；所述无人机携带所述货物飞离所述作业区域。
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CN105825652A (zh) * 2016-04-18 2016-08-03 汪禹 一种用于无人机传递物件的收发装置
CN205675246U (zh) * 2016-06-22 2016-11-09 衢州市依科达节能技术有限公司 一种无人机货物输送装置
CN205971863U (zh) * 2016-08-02 2017-02-22 浙江水利水电学院 一种无人机阳台快递接收装置
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US11964778B2 (en) 2017-08-31 2024-04-23 Pengyue ZHOU Apparatus for receiving and sending parcel by drone

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