An aircraft delivery acceptance system

Abstract

The utility model provides a kind of aircraft delivery receiving system, including bottom plate, warehouse board, movable plate, receiving tray, slide rail component and closing device;Bottom plate connects warehouse board, and warehouse door is set on warehouse board and warehouse door, and warehouse door is connected with the mouth of warehouse by hinge rotation;The movable plate side is rotatably connected with bottom plate by pivot, and slide rail component is set on movable plate;Slide rail component includes track and driving part, and the receiving tray is fitted on track, and driving part is used to drive receiving tray reciprocating movement along track;The receiving tray includes receiving flat plate and baffle, and baffle is set around the outer edge of receiving flat plate;The utility model aims at presenting a kind of aircraft delivery receiving system, to be applicable to unmanned aerial vehicle delivery, in non-receiving goods state, receiving warehouse is closed to reduce occupied space, and compact structure, low manufacturing cost.In rainy and snowy weather, closed receiving warehouse can protect receiving equipment and prolong service life.

Description

Technical Field

[0001] This utility model belongs to the field of delivery receiving devices, and in particular relates to an aircraft delivery receiving system. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and their own program control devices. With the continuous development of UAV technology, they are widely used in various industries. UAVs used for cargo transportation are generally equipped with winches and mechanical grippers. The winch extends and retracts a rope, and the mechanical gripper connected to the rope grasps the cargo, enabling UAV cargo transportation. To facilitate UAV delivery, a cargo-retrieving device is required. Utility Model Content

[0003] In view of this, the present invention aims to propose an aircraft delivery receiving system suitable for drone delivery. When not receiving goods, the receiving compartment is closed to reduce space occupation, and the structure is compact and the manufacturing cost is low.

[0004] To achieve the above objectives, the technical solution of this utility model is implemented as follows:

[0005] An aircraft delivery and receiving system includes a base plate, a cargo hold plate, a movable plate, a receiving pallet, a slide rail assembly, and a closing device. The base plate is connected to the cargo hold plate, which has a cargo hold opening and a cargo hold door. The cargo hold door is rotatably connected to the cargo hold opening via a hinge. One side of the movable plate is rotatably connected to the base plate via a pivot, and a slide rail assembly is provided on the movable plate. The slide rail assembly includes a track and a drive component. The receiving pallet is mounted on the track, and the drive component drives the receiving pallet to reciprocate along the track. The receiving pallet includes a receiving plate and a baffle, with the baffle surrounding the outer edge of the receiving plate.

[0006] The closing device includes a rope, a threading ring, a top plate, a fixing ring, a spool, and a first motor. The spool is located between the bin plate and the movable plate, with both ends of the spool supported on the bottom plate via spool supports. The spool is connected to the first motor. The front ends of the movable plate are fixedly connected to the fixing rings on both sides. The upper end of the bin plate is connected to the top plate, which extends towards the movable plate. Threading rings are provided on both sides of the top plate. The rope includes two ropes, one end of which is wound around the spool, and the other end of which passes through the threading ring and is connected to the fixing ring.

[0007] Furthermore, the driving component includes a lead screw, a nut, a slider, and a second motor. The nut is mounted on the lead screw, the nut connects to the slider, the slider is mounted on the track, the receiving pallet is connected to the slider, and the second motor is connected to the lead screw.

[0008] Furthermore, the drive component includes a lead screw, a nut, a slider, and a handwheel. The nut is mounted on the lead screw, the nut connects to the slider, the slider is mounted on a track, the receiving pallet is connected to the slider, and the handwheel is connected to the lead screw.

[0009] Furthermore, the base plate, storage plate, movable plate, and receiving pallet are generally rectangular, and the interior of the base plate, storage plate, and receiving pallet constitutes a first accommodating space for storing goods.

[0010] Furthermore, the outer contour of the storage plate is larger than the outer contour of the movable plate, and the area of ​​the receiving plate is less than or equal to the area of ​​the movable plate.

[0011] Furthermore, the baffle is inclined outward and includes two side baffles and a front baffle. The two side baffles and the front baffle are respectively disposed on the two sides and the front of the receiving plate, and the end face of the baffle abuts against the bin plate.

[0012] Furthermore, the bottom plate, the storage plate, and the top plate constitute a second accommodating space, and the receiving pallet can be rotated around the pivot to be stored in the second accommodating space when it is moved into the movable plate.

[0013] Furthermore, it also includes a first motor driver and a second motor driver, which are electrically connected to the first motor and the second motor.

[0014] Compared with existing technologies, the aircraft delivery and receiving system of this utility model has the following advantages:

[0015] The aircraft delivery and receiving system described in this utility model unfolds the movable plate through a closing device when receiving goods, and pushes out the receiving pallet through a sliding rail component, so that the receiving compartment is in the unfolded state. The drone puts the goods into the receiving pallet, and then retracts the receiving pallet through the sliding rail component to bring the goods close to the compartment plate. The compartment door is then opened to retrieve the goods, which can be used in conjunction with drone delivery. In addition, when not receiving goods, the receiving compartment is closed, reducing the space occupied. Attached Figure Description

[0016] The accompanying drawings, which form part of this utility model, are used to provide a further understanding of the utility model. The illustrative embodiments of the utility model and their descriptions are used to explain the utility model and do not constitute an undue limitation of the utility model. In the drawings:

[0017] Figure 1 This is a schematic diagram of the overall structure of the aircraft delivery and receiving system according to an embodiment of the present utility model;

[0018] Figure 2 This is a schematic diagram of the deployed state of the aircraft delivery and receiving system according to an embodiment of the present invention;

[0019] Figure 3 This is a schematic diagram of the closed state of the aircraft delivery and receiving system according to an embodiment of the present invention;

[0020] Figure 4This is a schematic diagram of the cargo receiving status of the aircraft delivery receiving system according to an embodiment of the present invention;

[0021] Figure 5 This is a schematic diagram of the drive component structure according to Embodiment 1 of this utility model;

[0022] Figure 6 This is a schematic diagram of the drive component structure according to Embodiment 2 of this utility model.

[0023] Explanation of reference numerals in the attached figures:

[0024] 1-Base plate; 2-Spool support; 3-Hoard plate; 4-Spool; 5-Hoard opening; 6-Hoard door; 7-Top plate; 8-Threading ring; 10-Rope; 11-First motor; 12-Baffle; 13-Receiving plate; 14-Moving plate; 15-Fixing ring; 16-Railway; 17-Rotating shaft; 18-Rotating shaft support; 20-Receiving pallet; 21-Side baffle; 22-Front baffle; 24-Slider; 25-Nut; 26-Lead screw; 27-Second motor; 28-Handwheel; 29-Building; 30-Window; 100-UAV; 200-Windlass; 300-Robot arm; 400-Cargo. Detailed Implementation

[0025] It should be noted that, unless otherwise specified, the embodiments and features described in these embodiments can be combined with each other.

[0026] The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0027] like Figure 1 As shown, an aircraft delivery and receiving system includes a base plate 1, a cargo hold plate 3, a movable plate 14, a receiving pallet 20, a slide rail assembly, and a closing device. The base plate 1 is connected to the cargo hold plate 3, and the cargo hold plate 3 is provided with a cargo hold opening 5 and a cargo hold door 6. The cargo hold door 6 is rotatably connected to the cargo hold opening 5 via a hinge. One side of the movable plate 14 is rotatably connected to the base plate 1 via a pivot 17, and a slide rail assembly is provided on the movable plate 14. The slide rail assembly includes a track 16 and a drive component. The receiving pallet 20 is mounted on the track 16, and the drive component is used to drive the receiving pallet 20 to reciprocate along the track 16. The receiving pallet 20 includes a receiving plate 13 and a baffle 12, with the baffle 12 arranged around the outer edge of the receiving plate 13.

[0028] The closing device includes a rope 10, a threading ring 8, a top plate 7, a fixing ring 15, a spool 4, and a first motor 11. The spool 4 is located between the compartment plate 3 and the movable plate 14. Both ends of the spool 4 are mounted on the bottom plate 1 via spool supports 2, and the spool 4 is connected to the first motor 11. The front ends of the movable plate 14 are fixedly connected to the fixing rings 15. The top end of the compartment plate 3 is connected to the top plate 7, which extends towards the movable plate 14. Threading rings 8 are provided on both sides of the top plate 7. The rope 10 includes two ropes. One end of each rope 10 is wound around the spool 4, and the other end of each rope 10 is passed through the threading ring 8 and connected to the fixing ring 15.

[0029] The working principle of an aircraft delivery and receiving system is as follows: The receiving pallet is driven by a drive component to move forward or backward along a track; one end of the rope of the closing device is fixed to a fixed ring, the rope passes through a threaded loop, and the other end is fixed to a winding spool. A first motor rotates, driving the spool to rotate, tightening or loosening the rope, causing the entire movable plate to rotate around the axis; when the receiving compartment receives goods, the first motor first rotates, driving the spool to rotate, loosening the rope, and the rope causes the movable plate to rotate around the axis, such as... Figure 1 As shown, the movable plate unfolds; then the drive component moves the receiving pallet forward along the track, pushing out the receiving pallet, as shown. Figure 2 As shown, the receiving compartment is in the deployed state, and the drone places the goods onto the receiving pallet. After the receiving compartment receives the goods, the receiving pallet is driven by a drive unit to move backward along the track. The receiving pallet retracts into the movable plate, the goods on the receiving pallet approach the compartment plate, the compartment door opens, and the goods are removed.

[0030] In this preferred embodiment, when not receiving goods, the receiving pallet is driven by a drive component to move backward along the track. After the receiving pallet is retracted into the movable plate, the first motor drives the spool to rotate, tightening the rope. The rope then drives the movable plate to rotate around the pivot. Figure 3 As shown, the receiving compartment is closed. Closing the receiving compartment reduces space usage; additionally, in rainy or snowy weather, closing the receiving compartment protects it and extends its service life.

[0031] like Figure 5 As shown in the preferred embodiment of this utility model, the driving component includes a lead screw 26, a nut 25, a slider 24, and a second motor 27. The nut 25 is mounted on the lead screw 26 and connects to the slider 24. The slider 24 is mounted on the track 16, and the receiving pallet 20 is connected to the slider. The second motor 27 is connected to the lead screw 26. The second motor 27 drives the lead screw 26 to rotate, which in turn drives the slider 24 to move along the track 16 via the nut 25. The receiving pallet 20 is connected to the slider, thus enabling the receiving pallet to reciprocate along the track. Motor-driven operation saves time and effort.

[0032] like Figure 6As shown in the preferred embodiment of this utility model, the driving component includes a lead screw 26, a nut 25, a slider 24, and a handwheel 28. The nut 25 is mounted on the lead screw 26, and the nut 25 connects to the slider 24. The slider 24 is mounted on the track 16, and the receiving pallet 20 is connected to the slider. The handwheel 28 is connected to the lead screw 26. Manually turning the handwheel 28 drives the lead screw 26 to rotate, which in turn moves the slider 24 along the track 16 via the nut 25. The receiving pallet 20 is connected to the slider, thus enabling the receiving pallet to reciprocate along the track. Manual adjustment is supported.

[0033] like Figure 1 and Figure 3 As shown, the base plate 1, storage plate 3, movable plate 14, and receiving pallet 20 are generally rectangular, and the interior of the base plate 1, storage plate 3, and receiving pallet 20 constitutes a first accommodating space for storing goods. The structure is reasonable, and goods can be temporarily stored in the first accommodating space.

[0034] like Figure 4 As shown, the outer contour of the storage plate 3 is larger than the outer contour of the movable plate 14, and the area of ​​the receiving plate 13 is less than or equal to the area of ​​the movable plate 14. When the receiving pallet moves backward along the track driven by the driving component, the receiving pallet can be retracted into the movable plate.

[0035] like Figures 1 to 4 As shown, the baffle 12 is inclined outwards and includes two side baffles 21 and a front baffle 22. The two side baffles 21 and the front baffle 22 are respectively disposed on the two sides and the front side of the receiving plate 13, and the end face of the baffle 12 abuts against the storage plate 3. The baffle 12 can protect the goods.

[0036] like Figure 1 and Figure 3 As shown, the bottom plate 1, the storage plate 3, and the top plate 7 constitute a second accommodating space. When the receiving pallet 20 is moved into the movable plate 14, it can rotate around the pivot 17 and be stored in the second accommodating space. In the non-receiving state, when the receiving compartment is closed, the movable plate 14 and the receiving pallet 20 stored in the movable plate 14 can rotate around the pivot 17 and be smoothly stored in the second accommodating space, reducing the space occupied.

[0037] It also includes a first motor driver and a second motor driver, which are electrically connected to the first motor 11 and the second motor 27. The first motor driver and the second motor driver are used to control the motors.

[0038] The operating steps of an aircraft delivery and receiving system are as follows: When the drone 100 delivers the goods, the first motor is activated, rotating the spool to release the rope and unfold the movable plate. Then, the second motor 27 is activated, driving the lead screw 26 to rotate, which in turn drives the slider 24 to move along the track 16 via the nut 25, causing the receiving pallet 20 to move forward along the track and extend. The drone lowers the goods 400 via the winch 200, placing the goods on the receiving plate. The robotic arm 300 then opens and lowers the goods 400. After the drone flies away, the second motor 27 is activated to retract the receiving pallet 20, moving the goods outside the compartment door. The window is then opened to retrieve the goods. After the goods are retrieved, the first motor 11 is activated, and the receiving compartment closes.

[0039] like Figure 4 As shown, the aircraft delivery and receiving system of this utility model can be installed in the window 30 of building 29. The storage plate 3 is set on the window 30, and the base plate 1, storage plate 3, movable plate 14, receiving tray 20, sliding rail components and closing device are set outside the window. The drone 100 delivers the goods to the receiving tray 20, which can realize the recipient to pick up the goods at home, replacing the way of deliverymen climbing up the stairs to deliver goods or recipients going downstairs to pick up goods.

[0040] The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. An aircraft delivery and receiving system, characterized in that: The system includes a base plate (1), a storage plate (3), a movable plate (14), a receiving pallet (20), a slide rail component, and a closing device. The base plate (1) is connected to the storage plate (3), and the storage plate (3) is provided with a storage opening (5) and a storage door (6). The storage door (6) is rotatably connected to the storage opening (5) via a hinge. The movable plate (14) is rotatably connected to the base plate (1) via a pivot (17) on one side, and a slide rail component is provided on the movable plate (14). The slide rail component includes a track (16) and a drive component. The receiving pallet (20) is mounted on the track (16), and the drive component is used to drive the receiving pallet (20) to move back and forth along the track (16). The receiving pallet (20) includes a receiving plate (13) and a baffle (12). The baffle (12) is arranged around the outer edge of the receiving plate (13). The closing device includes a rope (10), a threading ring (8), a top plate (7), a fixing ring (15), a spool (4), and a first motor (11). The spool (4) is located between the bin plate (3) and the movable plate (14). Both ends of the spool (4) are mounted on the bottom plate (1) through spool supports (2). The spool (4) is connected to the first motor (11). The front ends of the movable plate (14) are fixedly connected to the fixing rings (15). The upper end of the bin plate (3) is connected to the top plate (7). The top plate (7) extends towards the movable plate (14). Threading rings (8) are provided on both sides of the top plate (7). The rope (10) includes two ropes. One end of each rope (10) is wound around the spool (4). The other end of each rope (10) is passed through the threading ring (8) and connected to the fixing ring (15).

2. The aircraft delivery and receiving system according to claim 1, characterized in that: The drive components include a lead screw (26), a nut (25), a slider (24), and a second motor (27). The nut (25) is mounted on the lead screw (26), the nut (25) is connected to the slider (24), the slider (24) is mounted on the track (16), the receiving pallet (20) is connected to the slider, and the second motor (27) is connected to the lead screw (26).

3. The aircraft delivery and receiving system according to claim 1, characterized in that: The drive components include a lead screw (26), a nut (25), a slider (24), and a handwheel (28). The nut (25) is mounted on the lead screw (26), the nut (25) is connected to the slider (24), the slider (24) is mounted on the track (16), the receiving pallet (20) is connected to the slider, and the handwheel (28) is connected to the lead screw (26).

4. The aircraft delivery and receiving system according to claim 1, characterized in that: The base plate (1), the storage plate (3), the movable plate (14) and the receiving pallet (20) are rectangular in shape, and the interior of the base plate (1), the storage plate (3) and the receiving pallet (20) constitutes a first accommodating space for storing goods.

5. The aircraft delivery and receiving system according to claim 4, characterized in that: The outer contour of the storage plate (3) is greater than the outer contour of the movable plate (14), and the area of ​​the receiving plate (13) is less than or equal to the area of ​​the movable plate (14).

6. The aircraft delivery and receiving system according to claim 5, characterized in that: The baffle (12) is inclined outward. The baffle (12) includes two side baffles (21) and a front baffle (22). The two side baffles (21) and the front baffle (22) are respectively arranged on the two sides and the front side of the receiving plate (13). The end face of the baffle (12) abuts against the bin plate (3).

7. The aircraft delivery and receiving system according to claim 1, characterized in that: The bottom plate (1), the storage plate (3) and the top plate (7) constitute the second accommodating space. When the receiving pallet (20) is moved into the movable plate (14), it can rotate around the pivot (17) and be stored in the second accommodating space.

8. The aircraft delivery and receiving system according to claim 2, characterized in that: It also includes a first motor driver and a second motor driver, which are electrically connected to the first motor (11) and the second motor (27).

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