Unmanned aerial vehicle carrying platform

Abstract

The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle carrying platform which comprises a center console and a bearing seat. The collaborative stabilizing and protecting unit is arranged between the center console and the bearing seat; the multi-locking unit is connected with the center console, and the multi-locking unit is connected with the collaborative stabilizing and protecting unit; the anti-seismic supporting unit is arranged on the outer side of the bottom end of the bearing seat and connected with the bearing seat; wherein the cooperative stabilizing and protecting unit comprises a multi-element cooperative assembly, a windproof shielding assembly and a clamping and fixing response assembly, by arranging the cooperative stabilizing and protecting unit, rapid disassembly and assembly between the equipment and the unmanned aerial vehicle can be achieved, in the material bearing process, all-directional shielding and protection can be conducted on borne materials, positioning and fixing of the materials can be achieved, and the equipment can be conveniently and rapidly disassembled and assembled. The stability of the materials during transportation is guaranteed, then the stability of the unmanned aerial vehicle during flight is guaranteed, the material putting efficiency can be improved, and the safety of the equipment during operation is greatly improved.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and particularly to an unmanned aerial vehicle carrying platform. Background Art

[0002] Today, with the rapid development of technology, unmanned aerial vehicle technology has penetrated into many fields and become an important force in promoting social development. Unmanned aerial vehicles can achieve diverse functions, such as aerial photography, environmental monitoring, cargo transportation, etc.

[0003] In recent years, the occasions of using unmanned aerial vehicles to deliver supplies to disaster areas, or to deliver rescue equipment to fire sites and drag cables have become more and more frequent. The use frequency of unmanned aerial vehicles is getting higher and higher. Therefore, there are many unmanned aerial vehicle delivery devices on the market at present, but most of these devices have many defects. Generally, the structure of the delivery device is relatively complex, and the hung supplies will be affected by air convection during flight, swaying left and right, which affects the flight stability of the unmanned aerial vehicle. Therefore, in view of the above situation, there is an urgent need to develop an unmanned aerial vehicle carrying platform to overcome the deficiencies in current practical applications. Summary of the Invention

[0004] The purpose of the present invention is to provide an unmanned aerial vehicle carrying platform to solve the problems raised in the above background art.

[0005] To achieve the above purpose, the present invention provides the following technical solutions: An unmanned aerial vehicle carrying platform, comprising: a central control console and a carrying seat, the carrying seat is arranged on the outer side of the bottom end of the central control console; a collaborative stabilization and protection unit, the collaborative stabilization and protection unit is arranged between the central control console and the carrying seat, and is used to cooperate with the central control console to realize the positioning of the carrying seat, and cooperate with the carrying seat to realize the all-round shielding protection and positioning stability of the hung supplies; a multi-lock unit, the multi-lock unit is connected to the central control console and is also connected to the collaborative stabilization and protection unit, and is used to cooperate with the collaborative stabilization and protection unit to realize the quick disassembly and assembly between the carrying platform and the unmanned aerial vehicle; an anti-seismic support unit, the anti-seismic support unit is arranged on the outer side of the bottom end of the carrying seat and is connected to the carrying seat, and is used to realize the support of the carrying platform and complete the shock absorption protection during takeoff and landing; wherein, the collaborative stabilization and protection unit includes: a multi-element collaborative component, a wind-proof shielding component and a clamping response component, the multi-element collaborative component is arranged inside the central control console, is connected to the multi-lock unit, and is also connected to the wind-proof shielding component arranged around the outer side of the top end of the carrying seat, and is used to cooperate with the central control console to realize the assembly of the carrying platform and the unmanned aerial vehicle, and synchronously complete the retraction and extension of the wind-proof shielding component to realize the wind shielding protection of the supplies located on the carrying seat. The wind-proof shielding component is also provided with a clamping response component, and the clamping response component is connected to the multi-element collaborative component through the wind-proof shielding component, and is used to cooperate with the multi-element collaborative component and the flipped wind-proof shielding component to realize the positioning stability of the supplies located on the carrying seat.

[0006] As a further solution of the present invention: The multi-element collaborative component includes: a central control motor, a central control rod, a collaborative disk, a power transmission guide plate, a positioning guide rail, a receiving box, a transfer cavity, a pressure input and output pipe, a self-service conduit, a retraction control gear, a force transmission slide rod, and a top push rod. The central control motor is fixedly connected to the inner top of the central control console. The output end of the central control motor is fixedly connected to the central control rod, and the other end of the central control rod is fixedly connected to the collaborative disk. A number of receiving boxes are arranged around the outside of the collaborative disk. The receiving boxes are fixedly connected to the central control console, and transfer cavities are symmetrically arranged inside. The transfer cavities are connected to the self-service conduits fixedly connected to the receiving boxes. The other ends of the self-service conduits are connected to the windproof shielding component. A power transmission guide plate connected to the multiple locking units is arranged between the receiving box and the collaborative disk. The bottom plate wall of the power transmission guide plate is slidably connected to the positioning guide rail fixedly connected to the inner side of the central control console. A force transmission slide rod is fixedly connected to the side plate wall of the power transmission guide plate close to the receiving box. A retraction control gear connected to the windproof shielding component is slidably connected to the outside of the force transmission slide rod. A spring is fixedly connected between the retraction control gear and the force transmission slide rod, which is used to cooperate with the movement of the power transmission guide plate to realize the retraction and extension of the windproof shielding component. A number of pressure input and output pipes connected to the transfer cavities are also arranged between the power transmission guide plate and the receiving box. The pressure input and output pipes are fixedly connected to the box wall of the receiving box. Pressure transmission members fixedly connected to the power transmission guide plate are oppositely arranged on the outside of the pressure input and output pipes. A top push rod is arranged between the power transmission guide plate and the collaborative disk. One end of the top push rod is rotatably connected to the collaborative disk, and the other end is rotatably connected to the power transmission guide plate, which is used to cooperate with the rotation of the collaborative disk to realize the lateral movement of the power transmission guide plate on the positioning guide rail.

[0007] As a further solution of the present invention: The windproof shielding component includes: a U-shaped frame, a power transmission rod, a steering gear, a communication pipe, a pressure guide seat, a support rotating rod, and a shielding baffle. The U-shaped frames are symmetrically arranged, one end is fixedly connected to the central control console, and the other end is fixedly connected to the bearing seat. A power transmission rod is rotatably connected between the two U-shaped frames. A steering gear meshed with the retraction control gear is fixedly connected to the power transmission rod. Pressure guide seats fixedly connected to the bearing seat are arranged on the outside of the two U-shaped frames. A support rotating rod is rotatably connected between the two pressure guide seats. A shielding baffle connected to the clamping response component is fixedly connected to the support rotating rod. The support rotating rod and the power transmission rod are connected by a synchronous energy transmission member, which is used to cooperate with the rotation of the power transmission rod to complete the retraction and extension of the shielding baffle. One end of the U-shaped frame connected to the central control console is also connected to the self-service conduit. The wall of the other end of the U-shaped frame is connected to the pressure guide seat through a communication pipe, which is used to cooperate with the multi-element collaborative component to realize the air diversion and complete the drive of the clamping response component.

[0008] As a further solution of the present invention: The clamping response component includes: a clamping plate, a directional sliding plate, an induction conduit, a square slider, a reaction plate, a driven plate, a pneumatic induction groove, and an induction piston. The clamping plate is arranged outside the shielding baffle, and a directional sliding plate that is slidably connected to the baffle wall of the shielding baffle is fixedly connected to the clamping plate. Square sliders are symmetrically arranged between the shielding baffle and the clamping plate. A pneumatic induction groove is arranged inside the square slider, and an induction conduit fixedly connected to the supporting rotating rod is arranged inside the pneumatic induction groove. One end of the induction conduit communicates with the pressure guiding seat, and an induction piston that is slidably connected to the pneumatic induction groove is fixedly connected to the outer side of the other end, which is used to cooperate with the air conveyed by the multi-component collaborative component to realize the lateral movement of the square slider. A reaction plate is rotatably connected to the square slider, and a driven plate is slidably connected to the inner side of the other end of the reaction plate. A spring is fixedly connected between the driven plate and the reaction plate, and the other end of the driven plate is rotatably connected to the clamping plate, which is used to cooperate with the movement of the square slider to realize the positioning and clamping of the materials on the bearing seat.

[0009] As a further solution of the present invention: The earthquake-resistant support unit includes: a grounding plate, a fixed column, a guiding and controlling column, an energy absorption groove, a damping disc, a shock-absorbing column, and a transmission and control rod. The grounding plates are symmetrically arranged outside the bottom end of the bearing seat. Shock-absorbing columns are symmetrically arranged between the grounding plates and the bearing seat. One end of the shock-absorbing column is fixedly connected to a damping disc that is slidably connected inside the energy absorption groove, and the other end is rotatably connected to the transmission and control rod. The energy absorption groove is arranged inside the shell wall of the bearing seat, and damping liquid is arranged inside the energy absorption groove. A buffer spring is fixedly connected between the damping disc and the bearing seat. The other end of the transmission and control rod is rotatably connected to the grounding plate. A fixed column is fixedly connected to the top end of the grounding plate, and a guiding and controlling column fixedly connected to the bearing seat is slidably connected inside the fixed column.

[0010] As a further solution of the present invention: The multiple locking unit includes: an L-shaped seat, a locking pressing plate, a telescopic device, a movable sliding frame, a positioning rod, and a connection and transmission control component. The L-shaped seats are symmetrically arranged outside the top end of the central control console. Locking pressing plates are arranged on the outer sides of the opposite ends of the two L-shaped seats. A telescopic device is fixedly connected between the locking pressing plate and the L-shaped seat on the same side, which is used to cooperate with the central control console to realize the longitudinal connection between the bearing platform and the drone. A movable sliding frame is fixedly connected to the outer side of the bottom end of the L-shaped seat. The movable sliding frame is slidably connected to a positioning rod fixedly connected to the top shell wall of the central control console. A spring is also fixedly connected between the movable sliding frame and the central control console. The movable sliding frame is also connected to the adjacent side energy transmission guide plate through the connection and transmission control component, which is used to cooperate with the movement of the energy transmission guide plate to realize the lateral connection between the bearing platform and the drone.

[0011] As a further solution of the present invention: The connection and transmission control assembly includes: a sensing and control board, a telescopic board, a steel wire rope, and a guide wheel. The sensing and control board is arranged on the outer side of the bottom end of the movable carriage and is rotatably connected to the adjacent energy transmission guide board. A telescopic board is slidably connected to the inner side of the other end of the sensing and control board. A spring is fixedly connected between the telescopic board and the sensing and control board. The other end of the telescopic board is fixedly connected to the steel wire rope. The other end of the steel wire rope passes through the guide wheel and is connected to the movable carriage. The guide wheel is fixedly connected to the console and is used to cooperate with the movement of the energy transmission guide board to realize the reverse movement of the movable carriage.

[0012] Compared with the prior art, the beneficial effects of the present invention are: During the operation of the device, the unmanned aerial vehicle (UAV) is placed on the outer side of the top end of the console, and the materials are placed on the bearing seat. The multi - element collaborative component drives the wind - proof and shielding component to retract. The wind - proof and shielding component surrounds and protects the materials on the bearing seat from the front, back, left, and right sides. The multi - element collaborative component can also synchronously drive multiple locking units, which are connected to the UAV, to achieve the rapid assembly between the carrying platform and the UAV. After the multi - element collaborative component completes the above operations, it continues to operate and drives the clamping response component on the wind - proof and shielding component. The clamping response component clamps and positions the materials on the bearing seat to prevent the materials from shaking during transportation. The UAV operates, drives the bearing seat to rise, and completes the transportation of the materials. When the UAV lands, the anti - seismic support unit contacts the ground, and the anti - seismic support unit can achieve shock absorption and protection, so that the equipment can maintain stability during take - off and landing. By setting the collaborative stabilization unit and cooperating with multiple locking units, this application can achieve the rapid disassembly and assembly between the equipment and the UAV, and can provide all - around shielding and protection for the carried materials during the process of carrying the materials, and realize the positioning and fixing of the materials, ensuring the stability of the materials during transportation, and further ensuring the stability of the UAV during flight. It can not only improve the material delivery efficiency, but also greatly improve the safety of the equipment during operation. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic structural diagram of the UAV carrying platform.

[0014] Figure 2 It is a cross - sectional view of the UAV carrying platform.

[0015] Figure 3 It is a schematic structural diagram of the multi - element collaborative component in the UAV carrying platform.

[0016] Figure 4 It is a cross - sectional view of the multi - element collaborative component in the UAV carrying platform.

[0017] Figure 5 It is a schematic structural diagram of the wind - proof and shielding component in the UAV carrying platform.

[0018] Figure 6 This is a schematic diagram of the structure of the clamped response component in the UAV carrying platform.

[0019] Figure 7 A cross-sectional view of the clamped response assembly in the UAV mounting platform.

[0020] Figure 8 for Figure 7 Schematic diagram of the enlarged structure at point A in the middle.

[0021] Figure 9 This is a schematic diagram of the structure of the seismic support unit in the UAV carrying platform.

[0022] Figure 10 This is a schematic diagram of the structure of multiple locking units in the UAV carrying platform.

[0023] In the figure: 1-UAV, 2-Center console, 3-Bearing seat, 4-Seismic support unit, 5-Multiple locking unit, 6-Cooperative stabilization unit, 7-Multiple cooperative components, 8-Wind shield component, 9-Clamping response component, 10-Center control motor, 11-Center control rod, 12-Cooperative disk, 13-Energy transmission guide plate, 14-Positioning guide rail, 15-Receiving box, 16-Transfer cavity, 17-Pressure delivery pipe, 18-Self-service catheter, 19-Pressure delivery part, 20-Retractable control gear, 21-Force guide slide rod, 22-Push rod, 23-U-shaped frame, 24-Energy transmission rod, 25-Steering gear, 26-Connecting pipe, 27- Pressure-guiding seat, 28-supporting rotating rod, 29-synchronous energy-guiding part, 30-shielding baffle, 31-clamp, 32-directional slide plate, 33-sensing duct, 34-square slider, 35-reaction plate, 36-driven plate, 37-air pressure sensing groove, 38-sensing piston, 39-grounding plate, 40-fixed column, 41-guide column, 42-energy absorption groove, 43-damping plate, 44-shock-absorbing column, 45-transmission rod, 46-L-type seat, 47-locking pressure plate, 48-retractor, 49-movable slide, 50-positioning rod, 51-sensing control plate, 52-retractable plate, 53-wire rope, 54-guide wheel, 55-blocking ring. DETAILED DESCRIPTION

[0024] The technical solution of the present application is further described in detail below in conjunction with specific implementation methods.

[0025] The embodiments of the present application are described in detail below, and examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present application, and cannot be understood as limiting the present application.

[0026] See also Figure 1 and Figure 2, in an embodiment of the present invention, a drone carrying platform includes: a central control console 2 and a bearing seat 3, the bearing seat 3 is arranged outside the bottom end of the central control console 2; a collaborative stabilizing and protecting unit 6, the collaborative stabilizing and protecting unit 6 is arranged between the central control console 2 and the bearing seat 3, and is used to cooperate with the central control console 2 to position the bearing seat 3, and cooperate with the bearing seat 3 to achieve all-round shielding protection and positioning stability of the hung materials; a multi-lock unit 5, the multi-lock unit 5 is connected to the central control console 2 and is also connected to the collaborative stabilizing and protecting unit 6, and is used to cooperate with the collaborative stabilizing and protecting unit 6 to achieve quick disassembly and assembly between the carrying platform and the drone 1; an anti-seismic support unit 4, the anti-seismic support unit 4 is arranged outside the bottom end of the bearing seat 3 and is connected to the bearing seat 3, and is used to support the carrying platform and complete shock absorption protection during takeoff and landing; wherein, the collaborative stabilizing and protecting unit 6 includes: a multi-element collaborative component 7, a wind-proof shielding component 8 and a clamping response component 9, the multi-element collaborative component 7 is arranged inside the central control console 2, is connected to the multi-lock unit 5, and is also connected to the wind-proof shielding component 8 arranged around the outside of the top end of the bearing seat 3, and is used to cooperate with the central control console 2 to assemble the carrying platform and the drone 1, and synchronously complete the retraction and extension of the wind-proof shielding component 8 to achieve wind shielding for the materials located on the bearing seat 3, and a clamping response component 9 is also arranged on the wind-proof shielding component 8, and the clamping response component 9 is connected to the multi-element collaborative component 7 through the wind-proof shielding component 8, and is used to cooperate with the multi-element collaborative component 7 and the flipped wind-proof shielding component 8 to achieve positioning stability of the materials located on the bearing seat 3.

[0027] In this embodiment, when the device is running, the drone 1 is placed outside the top end of the central control console 2, and the materials are placed on the bearing seat 3. The multi-element collaborative component 7 drives the wind-proof shielding component 8 to retract, and the wind-proof shielding component 8 completes the surrounding protection of the materials located on the bearing seat 3 from the front, back, left and right sides. The multi-element collaborative component 7 can also synchronously drive the multi-lock unit 5, and the multi-lock unit 5 is connected to the drone 1 to achieve quick assembly between the carrying platform and the drone 1. After the multi-element collaborative component 7 completes the above operations, it continues to run and drives the clamping response component 9 located on the wind-proof shielding component 8. The clamping response component 9 clamps and positions the materials located on the bearing seat 3 to prevent the materials from shaking during transportation. The drone 1 runs, drives the bearing seat 3 to rise, and completes the transportation of the materials. When the drone 1 lands, the anti-seismic support unit 4 contacts the ground, and the anti-seismic support unit 4 can achieve shock absorption protection, so that the equipment can maintain stability during takeoff and landing. Through the setting of the collaborative stabilizing and protecting unit 6 and the cooperation with the multi-lock unit 5, the present application can achieve quick disassembly and assembly between the equipment and the drone 1, and can perform all-round shielding protection on the carried materials during the process of carrying the materials, and achieve positioning and fixing of the materials, ensuring the stability of the materials during transportation, and further ensuring the stability of the drone 1 during flight. It can not only improve the material delivery efficiency, but also greatly improve the safety of the equipment during operation.

[0028] In one embodiment of the present invention, please refer to Figure 2 , Figure 3 and Figure 4 , the multi - collaborative component 7 includes: a central control motor 10, a central control rod 11, a collaborative disk 12, a power transmission guide plate 13, a positioning guide rail 14, a receiving box 15, a transfer cavity 16, a pressure input - output pipe 17, a self - help conduit 18, a retraction control gear 20, a force - guiding slide rod 21, and a top - pushing rod 22. The central control motor 10 is fixedly connected to the inner top of the central control console 2. The output end of the central control motor 10 is fixedly connected to the central control rod 11. The other end of the central control rod 11 is fixedly connected to the collaborative disk 12. A number of receiving boxes 15 are arranged around the outside of the collaborative disk 12. The receiving boxes 15 are fixedly connected to the central control console 2. Transfer cavities 16 are symmetrically arranged inside. The transfer cavities 16 are connected to the self - help conduits 18 fixedly arranged on the receiving boxes 15. The other ends of the self - help conduits 18 are connected to the wind - proof shielding component 8. A power transmission guide plate 13 connected to the multiple locking units 5 is arranged between the receiving boxes 15 and the collaborative disk 12. The bottom plate wall of the power transmission guide plate 13 is slidably connected to the positioning guide rail 14 fixedly arranged inside the central control console 2. A force - guiding slide rod 21 is fixedly connected to the side plate wall of the power transmission guide plate 13 close to the receiving box 15. A retraction control gear 20 connected to the wind - proof shielding component 8 is slidably connected to the outside of the force - guiding slide rod 21. A spring is fixedly connected between the retraction control gear 20 and the force - guiding slide rod 21, which is used to cooperate with the movement of the power transmission guide plate 13 to realize the retraction and extension of the wind - proof shielding component 8. A number of pressure input - output pipes 17 connected to the transfer cavities 16 are also arranged between the power transmission guide plate 13 and the receiving boxes 15. The pressure input - output pipes 17 are fixedly connected to the box wall of the receiving boxes 15. Pressure guiding members 19 fixedly connected to the power transmission guide plate 13 are arranged opposite to the outside of the pressure input - output pipes 17. A top - pushing rod 22 is arranged between the power transmission guide plate 13 and the collaborative disk 12. One end of the top - pushing rod 22 is rotatably connected to the collaborative disk 12, and the other end is rotatably connected to the power transmission guide plate 13, which is used to cooperate with the rotation of the collaborative disk 12 to realize the lateral movement of the power transmission guide plate 13 on the positioning guide rail 14.

[0029] In this embodiment, the pressure delivery member 19 includes a push rod fixedly connected to the energy transfer guide plate 13 and a piston fixedly connected to the push rod. The outer diameter of the piston is equal to the inner diameter of the pressure input / output pipe 17. Additionally, the receiving box 15 is arranged on the front, rear, left, and right sides of the cooperation disk 12 and is fixedly connected to the inner wall of the central control console 2. In the initial state, the pressure delivery member 19 is located outside the pressure input / output pipe 17. The central control motor 10 drives the cooperation disk 12 to rotate through the central control rod 11. The cooperation disk 12 cooperates with the top push rod 22 to drive the corresponding energy transfer guide plate 13 to move on the positioning guide rail 14. The energy transfer guide plate 13 drives the retraction / extension control gear 20 to move synchronously through the force guide slide rod 21 and the spring. During the movement of the retraction / extension control gear 20, the retraction / extension of the windproof shielding assembly 8 can be realized, covering the materials located on the bearing seat 3. During the movement of the energy transfer guide plate 13, the driving of the multiple locking units 5 can be synchronously completed to complete the connection with the unmanned aerial vehicle 1. Among them, a retaining ring 55 is also fixedly connected to the outside of the retraction / extension control gear 20. The retaining ring 55 is arranged inside the central control console 2. After the windproof shielding assembly 8 is flipped, the retaining ring 55 abuts against the inner wall of the central control console 2. As the energy transfer guide plate 13 continues to move, the retraction / extension control gear 20 no longer moves, and the spring between the force guide slide rod 21 and the retraction / extension control gear 20 is compressed, ensuring the stability of the windproof shielding assembly 8 after flipping. At the same time, the energy transfer guide plate 13 drives the piston to enter the inside of the pressure input / output pipe 17 through the push rod, driving the air inside the corresponding transfer cavity 16 to flow, and cooperating with the windproof shielding assembly 8 to complete the driving of the clamping response assembly 9. By setting the multi-cooperation assembly 7, the driving of the multiple locking units 5 and the windproof shielding assembly 8 can be completed simultaneously, and the driving of the clamping response assembly 9 can also be completed. This not only improves the convenience of the equipment during disassembly and assembly, but also can provide comprehensive shielding protection for the carried materials during the process of carrying the materials and realize the positioning and fixation of the materials, ensuring the stability of the materials during transportation.

[0030] In one embodiment of the present invention, please refer to Figure 1 and Figure 5, the windproof shielding component 8 includes: a U-shaped frame 23, a power transmission rod 24, a steering gear 25, a connecting pipe 26, a pressure guiding seat 27, a supporting rotating rod 28 and a shielding baffle 30. The U-shaped frames 23 are symmetrically arranged, one end is fixedly connected to the central control console 2, and the other end is fixedly connected to the bearing seat 3. A power transmission rod 24 is rotatably connected between the two U-shaped frames 23. A steering gear 25 meshed with the retracting and releasing control teeth 20 is fixedly connected to the power transmission rod 24. Pressure guiding seats 27 fixedly connected to the bearing seat 3 are arranged on the outer sides of the two U-shaped frames 23. A supporting rotating rod 28 is rotatably connected between the two pressure guiding seats 27. A shielding baffle 30 connected to the clamping response component 9 is fixedly connected to the supporting rotating rod 28. The supporting rotating rod 28 and the power transmission rod 24 are connected by a synchronous energy guiding member 29, which is used to complete the retracting and releasing of the shielding baffle 30 in cooperation with the rotation of the power transmission rod 24. One end of the U-shaped frame 23 connected to the central control console 2 is also connected to the self-service conduit 18. The wall of the other end of the U-shaped frame 23 is connected to the pressure guiding seat 27 through the connecting pipe 26, which is used to cooperate with the multi-element collaborative component 7 to realize the air diversion and complete the driving of the clamping response component 9.

[0031] In this embodiment, both of the two U-shaped frames 23 are of hollow structure. The two ends of the supporting rotating rod 28 respectively extend to the inner sides of the two pressure guiding seats 27. The synchronous energy guiding member 29 includes pulleys fixedly connected to the outer sides of the supporting rotating rod 28 and the power transmission rod 24, and the pulleys are connected by a belt. When the retracting and releasing control teeth 20 move, the retracting and releasing control teeth 20 cooperate with the steering gear 25 to drive the power transmission rod 24 to rotate. The power transmission rod 24 drives the supporting rotating rod 28 to rotate through the pulleys and the belt. The supporting rotating rod 28 drives the shielding baffle 30 to turn over. The top wall of the shielding baffle 30 abuts against the outer wall of the central control console 2 to realize the shielding protection. As the piston moves inside the pressure input and output pipe 17, the air inside the transfer cavity 16 enters the inside of the U-shaped frame 23 along the self-service conduit 18, enters the inside of the pressure guiding seat 27 along the U-shaped frame 23 and the connecting pipe 26, and enters the inside of the clamping response component 9 to complete the driving of the clamping response component 9. The clamping response component 9 cooperates with the turned-over shielding baffle 30 to position and clamp the materials on the bearing seat 3, thus ensuring the stability and safety of the materials during transportation. By setting the windproof shielding component 8, it can cooperate with the multi-element collaborative component 7 for automatic retracting and releasing, which is convenient for people to pick up and place the materials, and can provide all-round shielding protection for the carried materials during transportation, thereby avoiding damage to the materials and ensuring the smoothness of the material transportation.

[0032] In an embodiment of the present invention, please refer to Figure 5 , Figure 6 , Figure 7 and Figure 8, the clamping response assembly 9 includes: a clamping plate 31, a directional slide plate 32, an induction conduit 33, a square slider 34, a reaction plate 35, a driven plate 36, a pneumatic induction groove 37, and an induction piston 38. The clamping plate 31 is arranged outside the shielding baffle 30. A directional slide plate 32 slidably connected to the wall of the shielding baffle 30 is fixedly connected to the clamping plate 31. Square sliders 34 are symmetrically arranged between the shielding baffle 30 and the clamping plate 31. A pneumatic induction groove 37 is arranged inside the square slider 34. An induction conduit 33 fixedly connected to the supporting rotating rod 28 is arranged inside the pneumatic induction groove 37. One end of the induction conduit 33 communicates with the pressure guiding seat 27, and an induction piston 38 slidably connected to the pneumatic induction groove 37 is fixedly connected to the outside of the other end, which is used to cooperate with the air conveyed by the multi-element collaborative assembly 7 to realize the lateral movement of the square slider 34. A reaction plate 35 is rotatably connected to the square slider 34. The inside of the other end of the reaction plate 35 is slidably connected to a driven plate 36. A spring is fixedly connected between the driven plate 36 and the reaction plate 35. The other end of the driven plate 36 is rotatably connected to the clamping plate 31, which is used to cooperate with the movement of the square slider 34 to realize the positioning and clamping of the materials on the bearing seat 3.

[0033] In this embodiment, one end of the induction conduit 33 is fixedly connected to the supporting rotating rod 28, and the other end leads to the inside of the shielding baffle 30. The air entering the inside of the pressure guiding seat 27 enters the inside of the pneumatic induction groove 37 along the induction conduit 33. Cooperating with the induction piston 38, it drives the square slider 34 to perform lateral movement along the wall of the shielding baffle 30. The square slider 34 cooperates with the reaction plate 35 and the driven plate 36 to drive the clamping plate 31 to move. The clamping plate 31 moves towards the center of the bearing seat 3 under the restriction of the directional slide plate 32. The clamping plates 31 on the four sides complete the positioning and clamping of the materials on the bearing seat 3, thus ensuring the stability of the materials during transportation and effectively avoiding the overturning of the materials during transportation and delivery. By setting the clamping response assembly 9, it can cooperate with the multi-element collaborative assembly 7 and the windproof shielding assembly 8 to realize the positioning and clamping of the materials on the bearing seat 3, ensuring the stability of the materials during transportation, and further ensuring the stability of the unmanned aerial vehicle 1 during flight. It can not only improve the material delivery efficiency, but also greatly improve the safety of the equipment during operation.

[0034] In one embodiment of the present invention, please refer to Figure 1 and Figure 9, the seismic support unit 4 includes: a grounding plate 39, a fixed column 40, a guiding and controlling column 41, an energy absorption groove 42, a damping disc 43, a shock-absorbing column 44, and a transmission and control rod 45. The grounding plates 39 are symmetrically arranged on the outer sides of the bottom ends of the bearing seats 3. Shock-absorbing columns 44 are symmetrically arranged between the grounding plates 39 and the bearing seats 3. One end of each shock-absorbing column 44 is fixedly connected to a damping disc 43 that is slidably connected inside the energy absorption groove 42, and the other end is rotatably connected to a transmission and control rod 45. The energy absorption grooves 42 are arranged on the inner side of the shell wall of the bearing seats 3. Damping liquid is arranged inside the energy absorption grooves 42. A buffer spring is fixedly connected between the damping disc 43 and the bearing seats 3. The other end of the transmission and control rod 45 is rotatably connected to the grounding plate 39. A fixed column 40 is fixedly connected to the top end of the grounding plate 39. A guiding and controlling column 41 fixedly connected to the bearing seat 3 is slidably connected inside the fixed column 40.

[0035] In this embodiment, the fixed columns 40 are fixedly connected to the top ends of both ends of the grounding plate 39. A guiding and controlling column 41 is slidably connected inside the fixed column 40. The top end of the guiding and controlling column 41 is fixedly connected to the bearing seat 3. When the drone 1 lands, the grounding plate 39 contacts the ground. The guiding and controlling column 41 cooperates with the fixed column 40 for guiding. The grounding plate 39 drives the shock-absorbing column 44 to move through the transmission and control rod 45. The shock-absorbing column 44 drives the damping disc 43 to move inside the energy absorption groove 42. Cooperating with the damping liquid arranged inside the energy absorption groove 42 and the shock-absorbing spring arranged between the damping disc 43 and the bearing seat 3, the impact force received during the takeoff and landing process can be absorbed, ensuring the stability of the equipment during takeoff and landing. By setting the seismic support unit 4, the stability of the equipment during takeoff and landing can be improved, and the influence of vibration on the equipment during the placement process can be reduced, which is beneficial to improving the service life of the equipment.

[0036] In one embodiment of the present invention, please refer to Figure 1 and Figure 10 , the multiple locking unit 5 includes: an L-shaped seat 46, a locking pressing plate 47, a telescopic device 48, a movable sliding frame 49, a positioning rod 50, and a connection and transmission control component. The L-shaped seats 46 are symmetrically arranged on the outer sides of the top ends of the central control consoles 2. Locking pressing plates 47 are arranged on the outer sides of the opposite ends of the two L-shaped seats 46. A telescopic device 48 is fixedly connected between the locking pressing plate 47 and the L-shaped seat 46 on the same side for realizing the longitudinal connection between the bearing platform and the drone 1 in cooperation with the central control console 2. A movable sliding frame 49 is fixedly connected to the outer side of the bottom end of the L-shaped seat 46. The movable sliding frame 49 is slidably connected to a positioning rod 50 fixedly connected to the top shell wall of the central control console 2. A spring is also fixedly connected between the movable sliding frame 49 and the central control console 2. The movable sliding frame 49 is also connected to the adjacent energy transmission guide plate 13 through a connection and transmission control component for realizing the lateral connection between the bearing platform and the drone 1 in cooperation with the movement of the energy transmission guide plate 13.

[0037] In this embodiment, a locking pressing plate 47 is arranged between the L-shaped seat 46 and the center console 2. A telescopic device 48 is fixedly connected between the top end of the locking pressing plate 47 and the L-shaped seat 46. The telescopic device 48 is an electric telescopic rod. When the energy transmission guide plate 13 moves, it cooperates with the connection and control assembly to drive the movable carriage 49 to move along the positioning rod 50. The movable carriage 49 drives the L-shaped seat 46 to move synchronously. The L-shaped seats 46 on both sides clamp and fix the support legs of the drone 1 from both sides. The telescopic device 48 drives the locking pressing plate 47 to move downward, and the locking pressing plate 47 cooperates with the center console 2 to longitudinally clamp and fix the support legs of the drone 1. By setting the multiple locking units 5, it can cooperate with the multi-element collaborative assembly 7 to realize the quick disassembly and assembly between the drone 1 and the bearing platform, and can complete multiple fixations, improving the stability of the equipment during use and ensuring the stability and reliability of the equipment after installation.

[0038] In one embodiment of the present invention, please refer to Figure 10 , the connection and control assembly includes: a sensing plate 51, a telescopic plate 52, a steel wire rope 53 and a guide wheel 54. The sensing plate 51 is arranged on the outer side of the bottom end of the movable carriage 49 and is rotatably connected to the adjacent energy transmission guide plate 13. The inner side of the other end of the sensing plate 51 is slidably connected with a telescopic plate 52. A spring is fixedly connected between the telescopic plate 52 and the sensing plate 51. The other end of the telescopic plate 52 is fixedly connected with the steel wire rope 53. The other end of the steel wire rope 53 passes through the guide wheel 54 and is connected to the movable carriage 49. The guide wheel 54 is fixedly connected to the center console 2 and is used to realize the reverse movement of the movable carriage 49 in cooperation with the movement of the energy transmission guide plate 13.

[0039] In this embodiment, when the energy transmission guide plate 13 moves, it drives the steel wire rope 53 to move in cooperation with the sensing plate 51 and the telescopic plate 52. The steel wire rope 53 completes the pulling of the movable carriage 49. When the L-shaped seat 46 completes the lateral clamping, when the energy transmission guide plate 13 continues to move, the spring between the sensing plate 51 and the telescopic plate 52 is stretched, making the fixation of the L-shaped seat 46 on the drone 1 more stable.

[0040] The drone carrying platform can achieve rapid disassembly and assembly between the device and the drone 1 by setting up the collaborative stabilization and protection unit 6 and cooperating with the multiple locking units 5. During the process of carrying materials, it can provide all-round shielding and protection for the carried materials, and achieve positioning and fixation of the materials, ensuring the stability of the materials during transportation, and thus ensuring the stability of the drone 1 during flight. This not only improves the material delivery efficiency but also greatly enhances the safety of the device during operation. By setting up the multi-element collaborative component 7, it can simultaneously drive the multiple locking units 5 and the windproof shielding component 8, and also drive the clamping response component 9, which not only improves the convenience of the device during disassembly and assembly but also provides all-round shielding and protection for the carried materials during the process of carrying materials. By setting up the windproof shielding component 8, it can cooperate with the multi-element collaborative component 7 for automatic retraction and extension, facilitating people to pick up and place the materials, and providing all-round shielding and protection for the carried materials during transportation, thus avoiding damage to the materials and ensuring the smoothness of material transportation. By setting up the clamping response component 9, it can cooperate with the multi-element collaborative component 7 and the windproof shielding component 8 to achieve positioning and clamping of the materials on the bearing seat 3, ensuring the stability of the materials during transportation, and thus ensuring the stability of the drone 1 during flight. This not only improves the material delivery efficiency but also greatly enhances the safety of the device during operation. By setting up the seismic support unit 4, it can improve the stability of the device during takeoff and landing and reduce the impact of vibration during placement on the device, which is beneficial to improving the service life of the device. By setting up the multiple locking units 5, it can cooperate with the multi-element collaborative component 7 to achieve rapid disassembly and assembly between the drone 1 and the carrying platform, and complete multiple fixations, improving the stability of the device during use and ensuring the stability and reliability of the device after installation.

[0041] The above are only the preferred embodiments of the present invention. It should be noted that for those skilled in the art, without departing from the concept of the present invention, several modifications and improvements can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the implementation effect of the present invention and the practicality of the patent.

Claims

1. A drone carrying platform, characterized in that: include: A center console and a bearing seat, wherein the bearing seat is arranged outside the bottom end of the center console; A collaborative stabilization unit is provided between the center console and the bearing seat, and is used to cooperate with the center console to realize the positioning of the bearing seat, and cooperate with the bearing seat to realize all-round shielding and protection of the hanging materials and stable positioning; A multiple locking unit, the multiple locking unit is connected to the central console and the cooperative stabilization unit, and is used to cooperate with the cooperative stabilization unit to realize the rapid disassembly and assembly between the carrying platform and the UAV; An anti-seismic support unit, which is arranged on the outer side of the bottom end of the bearing seat and connected to the bearing seat, and is used to support the bearing platform and provide shock absorption protection during lifting and lowering; Among them, the collaborative stabilization unit includes: a multi-cooperative component, a windproof shield component and a clamping response component. The multi-cooperative component is arranged on the inner side of the center console, connected to the multiple locking units, and connected to the windproof shield component arranged around the outer side of the top of the supporting seat, and is used to cooperate with the center console to realize the assembly of the supporting platform and the drone, and simultaneously complete the retraction and release of the windproof shield component to realize wind shielding protection for materials on the supporting seat. A clamping response component is also arranged on the windproof shield component, and the clamping response component is connected to the multi-cooperative component through the windproof shield component, and is used to cooperate with the multi-cooperative component and the flipped windproof shield component to realize the positioning and stabilization of the materials on the supporting seat.

2. The UAV carrying platform according to claim 1, characterized in that: The multi-cooperative component includes: a central control motor, a central control rod, a cooperative disk, an energy transmission guide plate, a positioning guide rail, a receiving box, a transfer chamber, a pressure delivery tube, a self-service guide tube, a retractable control tooth, a force guide slide rod and a push rod. The central control motor is fixedly connected to the top of the inner side of the central control platform, the output end of the central control motor is fixedly connected to the central control rod, and the other end of the central control rod is fixedly connected to the cooperative disk. A plurality of receiving boxes are arranged around the outer side of the cooperative disk, the receiving box is fixedly connected to the central console, and a transfer chamber is symmetrically arranged on the inner side. The transfer chamber is connected to the self-service guide tube fixedly connected to the receiving box, and the other end of the self-service guide tube is connected to the windproof shielding component. An energy transmission guide plate connected to multiple locking units is arranged between the receiving box and the cooperative disk, and the bottom end plate wall of the energy transmission guide plate is fixedly connected to the positioning guide tube fixedly connected to the inner side of the central console. The cam is connected to the rail for sliding connection, and the energy transmission guide plate is fixedly connected with a force guiding slide bar on the plate wall on one side of the receiving box. The outer side of the force guiding slide bar is slidably connected with a retraction and extension control tooth connected to the windproof shield assembly. A spring is fixedly connected between the retraction and extension control tooth and the force guiding slide bar, and is used to cooperate with the movement of the energy transmission guide plate to realize the retraction and extension of the windproof shield assembly. A plurality of pressure delivery pipes connected to the transfer cavity are also provided between the energy transmission guide plate and the receiving box. The pressure delivery pipes are fixedly connected to the wall of the receiving box, and a pressure guide piece fixedly connected to the energy transmission guide plate is relatively provided on the outside of the pressure delivery pipe. A push rod is provided between the energy transmission guide plate and the cooperative disk, one end of the push rod is rotatably connected to the cooperative disk, and the other end is rotatably connected to the energy transmission guide plate, and is used to cooperate with the rotation of the cooperative disk to realize the lateral movement of the energy transmission guide plate on the positioning guide rail.

3. The UAV carrying platform according to claim 2, characterized in that: The U-shaped frame is symmetrically arranged, with one end fixedly connected to the center console and the other end fixedly connected to the bearing seat. An energy transmission rod is rotatably connected between the U-shaped frames on both sides, and a steering gear meshing with the retraction and release control tooth is fixedly connected to the energy transmission rod. Pressure-guiding seats fixedly connected to the bearing seat are arranged on the outer sides of the U-shaped frames on both sides. A supporting rotating rod is rotatably connected between the pressure-guiding seats on both sides, and a shielding baffle connected to the clamping response assembly is fixedly connected on the supporting rotating rod. The supporting rotating rod is connected to the energy transmission rod by a synchronous energy guiding part, which is used to cooperate with the rotation of the energy transmission rod to complete the retraction and release of the shielding baffle. The end of the U-shaped frame connected to the center console is also connected to the self-service duct, and the frame wall of the other end of the U-shaped frame is connected to the pressure guiding seat through a connecting pipe, which is used to cooperate with the multi-cooperative component to realize the diversion of air and complete the driving of the clamping response assembly.

4. The UAV carrying platform according to claim 3, characterized in that: The clamping response component includes: a clamping plate, a directional slide plate, a sensing tube, a square slider, a reaction plate, a driven plate, an air pressure sensing groove and a sensing piston, wherein the clamping plate is arranged on the outer side of the shielding baffle, and a directional slide plate which is slidably connected to the wall of the shielding baffle is fixedly connected to the clamping plate, a square slider is symmetrically arranged between the shielding baffle and the clamping plate, an air pressure sensing groove is arranged on the inner side of the square slider, a sensing tube which is fixedly connected to the supporting rotating rod is arranged on the inner side of the air pressure sensing groove, one end of the sensing tube is communicated with the pressure guiding seat, and a sensing piston which is slidably connected to the air pressure sensing groove is fixedly connected on the outer side of the other end, which is used to cooperate with the air transported by the multi-cooperative component to realize the lateral movement of the square slider, a reaction plate is rotatably connected to the square slider, a driven plate is slidably connected to the inner side of the other end of the reaction plate, a spring is fixedly connected between the driven plate and the reaction plate, and the other end of the driven plate is rotatably connected to the clamping plate, which is used to cooperate with the movement of the square slider to realize the positioning and clamping of materials on the bearing seat.

5. The UAV carrying platform according to claim 1, characterized in that: The anti-seismic support unit includes: a grounding plate, a fixed column, a guide column, an energy absorbing groove, a damping disk, a shock-absorbing column and a control rod. The grounding plate is symmetrically arranged on the outer side of the bottom end of the bearing seat, and the shock-absorbing columns are symmetrically arranged between the grounding plate and the bearing seat. One end of the shock-absorbing column is fixedly connected to the damping disk slidingly connected to the inner side of the energy absorbing groove, and the other end is rotatably connected to the control rod. The energy absorbing groove is arranged on the inner side of the shell wall of the bearing seat, and damping fluid is arranged inside the energy absorbing groove. A buffer spring is fixedly connected between the damping disk and the bearing seat, and the other end of the control rod is rotatably connected to the grounding plate, a fixed column is fixedly connected to the top end of the grounding plate, and a guide column fixedly connected to the bearing seat is slidably connected inside the fixed column.

6. The UAV carrying platform according to claim 2, characterized in that: The multiple locking unit includes: an L-shaped seat, a locking pressure plate, a telescope, a movable slide, a positioning rod and a connecting and controlling component. The L-shaped seat is symmetrically arranged on the outer side of the top end of the center console, and a locking pressure plate is arranged on the outer side of the opposite end of the L-shaped seats on both sides. A telescope is fixedly connected between the locking pressure plate and the L-shaped seat on the same side, which is used to cooperate with the center console to realize the longitudinal connection between the load-bearing platform and the UAV. A movable slide is fixedly connected to the outer side of the bottom end of the L-shaped seat, and the movable slide is slidably connected to the positioning rod fixedly connected to the shell wall of the top end of the center console. A spring is also fixedly connected between the movable slide and the center console. The movable slide is also connected to the adjacent side energy transmission guide plate through the connecting and controlling component, which is used to cooperate with the movement of the energy transmission guide plate to realize the lateral connection between the load-bearing platform and the UAV.

7. The UAV carrying platform according to claim 6, characterized in that: The connecting control assembly includes: a sensor control plate, a telescopic plate, a steel wire rope and a guide wheel. The sensor control plate is arranged on the outer side of the bottom end of the movable slide and is rotatably connected to the energy transmission guide plate on the adjacent side. The other end of the sensor control plate is slidably connected to the inner side with a telescopic plate. A spring is fixedly connected between the telescopic plate and the sensor control plate. The other end of the telescopic plate is fixedly connected to the steel wire rope. The other end of the steel wire rope passes through the guide wheel and is connected to the movable slide. The guide wheel is fixedly connected to the center console and is used to cooperate with the movement of the energy transmission guide plate to realize the reverse movement of the movable slide.

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