A drone carrying platform

Abstract

The present invention relates to the field of drone technology, and specifically to a drone carrying platform, comprising: a center console and a bearing seat; a collaborative stabilization unit, wherein the collaborative stabilization unit is arranged between the center console and the bearing seat; a multiple locking unit, wherein the multiple locking unit is connected to the center console and to the collaborative stabilization unit; and an anti-seismic support unit, wherein the anti-seismic support unit is arranged on the outer side of the bottom end of the bearing seat and is connected to the bearing seat; wherein the collaborative stabilization unit comprises: a multi-component collaborative component, a windproof shielding component and a clamping response component. By providing the collaborative stabilization unit, rapid disassembly and assembly between the equipment and the drone can be achieved, and in the process of carrying materials, the carried materials can be fully shielded and protected, and the positioning and fixation of the materials can be achieved, thereby ensuring the stability of the materials during transportation, and further ensuring the stability of the drone during flight, which not only improves the efficiency of material delivery, but also greatly improves the safety of the equipment during operation.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles (UAVs), in particular to a UAV carrying platform. Background Art

[0002] With the rapid development of science and technology, drone technology has penetrated into many fields and become an important force in promoting social development. Drones can realize diverse functions such as aerial photography, environmental monitoring, cargo transportation, etc.

[0003] In recent years, drones have become increasingly used to deliver supplies to disaster areas, deploy rescue equipment, and drag cables to fire scenes. With the increasing frequency of drone use, numerous drone delivery systems are now available on the market. However, these systems often have numerous drawbacks. Furthermore, the materials being delivered are subject to air convection during flight, causing them to sway sideways and affect the stability of the drone. Therefore, there is an urgent need to develop a drone-mounted platform to overcome these shortcomings in current practical applications. Summary of the Invention

[0004] The purpose of the present invention is to provide a UAV carrying platform to solve the problems raised in the above background technology.

[0005] To achieve the above object, the present invention provides the following technical solutions:

[0006] A UAV carrying platform comprises: a center console and a bearing seat, wherein the bearing seat is arranged on the outer side of the bottom end of the center console; a collaborative stabilization unit, wherein the collaborative stabilization unit is arranged 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 hanging materials and stable positioning; a multiple locking unit, wherein the multiple locking unit is connected to the center console and to the collaborative stabilization unit, and is used to cooperate with the collaborative stabilization unit to realize rapid disassembly and assembly between the carrying platform and the UAV; an anti-seismic support unit, wherein the anti-seismic support unit is arranged on the outer side of the bottom end of the bearing seat, and is connected to the bearing seat, and is used to realize support of the carrying platform and complete reduction during takeoff and landing. Earthquake protection; wherein, 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, which is used to cooperate with the center console to realize the assembly of the supporting platform and the UAV, and simultaneously complete the retraction and extension of the windproof shield component to realize windproof protection of materials on the supporting seat. A clamping response component is also provided on the windproof shield component, which is connected to the multi-cooperative component through the windproof shield component, which is used to cooperate with the multi-cooperative component and the flipped windproof shield component to realize the stable positioning of materials on the supporting seat.

[0007] 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, an energy transmission guide plate, a positioning guide rail, a receiving box, a transfer chamber, a pressure delivery pipe, a self-service conduit, a retraction and extension control tooth, a force guide slide and a push rod. The central control motor is fixedly connected to the top inner side of the central 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 box is fixedly connected to the central console, and a transfer chamber is symmetrically arranged on the inside. The transfer chamber is connected to the self-service conduit fixedly connected to the receiving box, and the other end of the self-service conduit 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 collaborative disk, and the bottom end plate wall of the energy transmission guide plate is fixedly connected to the central console. The cam is fixedly connected to the gear train of the driving mechanism, and the cam is fixedly connected to the gear train of the driving mechanism, and the cam is fixedly connected to the gear train of the driving mechanism, and the cam is fixedly connected to the gear train of the driving mechanism, and the cam is fixedly connected to the gear train of the driving mechanism.

[0008] The cam is connected to the control stand at one end and the support frame at the other end is connected to the control stand at the other end.

[0009] As a further solution of the present invention: the clamping response component includes: a splint, a directional slide, a sensing tube, a square slider, a reaction plate, a driven plate, an air pressure sensing groove and a sensing piston. The splint is arranged on the outside of the shielding baffle, and a directional slide that is slidably connected to the shielding baffle wall is fixedly connected to the splint. A square slider is symmetrically arranged between the shielding baffle and the splint, an air pressure sensing groove is arranged on the inside of the square slider, and a sensing tube fixedly connected to the supporting rotating rod is arranged on the inside of the air pressure sensing groove. One end of the sensing tube is communicated with the pressure guide seat, and the other end is fixedly connected to the outside of the sensing piston that is slidably connected to the air pressure sensing groove, which is used to cooperate with the air delivered by the multi-cooperative 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 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 splint, which is used to cooperate with the movement of the square slider to realize the positioning and clamping of materials on the supporting seat.

[0010] As a further solution of the present invention: the seismic support unit includes: a grounding plate, a fixed column, a guide column, an energy absorption groove, a damping disk, a shock-absorbing column and a control rod. The grounding plate is symmetrically arranged on the outside of the bottom end of the bearing seat, and 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 inside the energy absorption groove in a sliding connection, and the other end is rotatably connected to the control rod. The energy absorption groove is arranged on the inner side of the bearing seat shell wall, and damping fluid is arranged inside the energy absorption 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 of the grounding plate, and a guide column fixedly connected to the bearing seat is slidably connected inside the fixed column.

[0011] As a further solution of the present invention: 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 of the center console, and a locking pressure plate is provided 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 carrying 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 top shell wall 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 carrying platform and the UAV.

[0012] As a further solution of the present invention: the connection and 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 outside 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 slidingly 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.

[0013] Compared with the prior art, the present invention has the following beneficial effects:

[0014] When the device is running, the drone is placed on the outside of the top of the center console, and the materials are placed on the carrier. The multi-cooperative component drives the windproof shield component to fold up, and the windproof shield component completes the surrounding protection of the materials on the carrier from the front, back, left and right sides. The multi-cooperative component can also synchronously complete the driving of the multiple locking units, and the multiple locking units are connected to the drone to achieve rapid assembly between the carrying platform and the drone. After the multi-cooperative component completes the above operations, it continues to run and drives the clamping response component on the windproof shield component. The clamping response component clamps and positions the materials on the carrier to prevent the materials from shaking during transportation. The machine runs, driving the carrier to rise and complete the transportation of materials. When the UAV lands, the anti-seismic support unit contacts the ground. The anti-seismic support unit can achieve shock absorption protection, so that the equipment can remain stable during take-off and landing. This application sets a collaborative stabilization unit and cooperates with multiple locking units to achieve rapid disassembly and assembly between the equipment and the UAV, and can provide all-round shielding and protection for the carried materials in the process of carrying materials, and realize the positioning and fixation of materials, ensuring the stability of materials during transportation, and then ensuring the stability of the UAV during flight, which not only improves the efficiency of material delivery, but also greatly improves the safety of the equipment during operation. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 This is a structural diagram of the UAV carrying platform.

[0016] Figure 2 This is a cross-sectional view of the UAV carrying platform.

[0017] Figure 3 Schematic diagram of the structure of multiple collaborative components in the UAV carrying platform.

[0018] Figure 4 A cross-sectional view of the multiple collaborative components in the drone-mounted platform.

[0019] Figure 5 This is a schematic diagram of the structure of the windproof shield component in the UAV carrying platform.

[0020] Figure 6 This is a schematic diagram of the structure of the clamping response component in the UAV carrying platform.

[0021] Figure 7 A cross-sectional view of the clamped response component in the UAV carrier platform.

[0022] Figure 8 for Figure 7 Schematic diagram of the enlarged structure at point A in the middle.

[0023] Figure 9 This is a schematic diagram of the structure of the seismic support unit in the UAV carrying platform.

[0024] Figure 10 This is a schematic diagram of the structure of the multiple locking units in the UAV carrying platform.

[0025] In the figure: 1-UAV, 2-Center console, 3-Bearing seat, 4-Seismic support unit, 5-Multi-locking unit, 6-Cooperative stabilization unit, 7-Multi-cooperative component, 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-Receiver box, 16-Adapter cavity, 17-Pressure delivery pipe, 18-Self-service guide pipe, 19-Pressure guide, 20-Retraction and extension control gear, 21-Force guide slide, 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-clamping plate, 32-directional slide plate, 33-sensing tube, 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-shaped seat, 47-locking pressure plate, 48-telescopic device, 49-movable slide, 50-positioning rod, 51-sensing control plate, 52-telescopic plate, 53-wire rope, 54-guide wheel, 55-retaining ring. DETAILED DESCRIPTION

[0026] The technical solution of this application is further described in detail below in conjunction with specific implementation methods.

[0027] The following describes in detail embodiments of the present application. 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 are not to be construed as limiting the present application.

[0028] See also Figure 1 and Figure 2In one embodiment of the present invention, a UAV carrying platform includes: a center console 2 and a supporting seat 3, wherein the supporting seat 3 is arranged on the outer side of the bottom end of the center console 2; a collaborative stabilization unit 6, wherein the collaborative stabilization unit 6 is arranged between the center console 2 and the supporting seat 3, and is used to cooperate with the center console 2 to realize the positioning of the supporting seat 3, and cooperate with the supporting seat 3 to realize all-round shielding and protection of hanging materials and stable positioning; a multiple locking unit 5, wherein the multiple locking unit 5 is connected to the center console 2 and to the collaborative stabilization unit 6, and is used to cooperate with the collaborative stabilization unit 6 to realize rapid disassembly and assembly between the carrying platform and the UAV 1; an anti-seismic support unit 4, wherein the anti-seismic support unit 4 is arranged on the outer side of the bottom end of the supporting seat 3 and is connected to the supporting seat 3, and is used to realize support for the carrying platform and to realize full coverage of the protection and stable positioning of the hanging materials. Shock absorption protection is completed during take-off and landing; wherein, the collaborative stabilization unit 6 includes: a multi-cooperative component 7, a windproof shield component 8 and a clamping response component 9, the multi-cooperative component 7 is arranged on the inner side of the center console 2, connected to the multiple locking units 5, and connected to the windproof shield component 8 arranged around the outside of the top of the supporting seat 3, for cooperating with the center console 2 to realize the assembly of the supporting platform and the UAV 1, and synchronously complete the retraction and extension of the windproof shield component 8 to realize windproof protection of the materials on the supporting seat 3, and a clamping response component 9 is also provided on the windproof shield component 8, and the clamping response component 9 is connected to the multi-cooperative component 7 through the windproof shield component 8, for cooperating with the multi-cooperative component 7 and the flipped windproof shield component 8 to realize the stable positioning of the materials on the supporting seat 3.

[0029] In this embodiment, when the device is running, the drone 1 is placed on the outside of the top of the center console 2, and the materials are placed on the supporting seat 3. The multi-cooperative component 7 drives the windproof shield component 8 to be folded, and the windproof shield component 8 completes the surrounding protection of the materials on the supporting seat 3 from the front, back, left and right sides. The multi-cooperative component 7 can also synchronously complete the driving of the multiple locking units 5, and the multiple locking units 5 are connected to the drone 1 to realize the rapid assembly between the carrying platform and the drone 1. After completing the above operations, the multi-cooperative component 7 continues to operate and drives the clamping response component 9 on the windproof shield component 8. The clamping response component 9 clamps and positions the materials on the supporting seat 3 to prevent the materials from being lost during transportation. When shaking occurs, the drone 1 runs, driving the supporting base 3 to rise and complete the transportation of materials. When the drone 1 lands, the anti-seismic support unit 4 contacts the ground. The anti-seismic support unit 4 can achieve shock absorption protection, so that the equipment can remain stable during take-off and landing. The present application sets a collaborative stabilization unit 6 and cooperates with the multiple locking units 5 to achieve rapid disassembly and assembly between the equipment and the drone 1. In the process of carrying materials, the carried materials can be fully shielded and protected, and the positioning and fixation of the materials can be achieved, thereby ensuring the stability of the materials during transportation, and then ensuring the stability of the drone 1 during flight, which not only improves the efficiency of material delivery, but also greatly improves the safety of the equipment during operation.

[0030] In one embodiment of the present invention, please refer to Figure 2 、 Figure 3 and Figure 4 The multi-functional collaborative component 7 includes: a central control motor 10, a central control rod 11, a collaborative disk 12, an energy transmission guide plate 13, a positioning guide rail 14, a receiving box 15, a transfer cavity 16, a pressure delivery pipe 17, a self-service conduit 18, a retractable control tooth 20, a guide slide 21 and a push rod 22. The central control motor 10 is fixedly connected to the top of the inner side of the central console 2, the output end of the central control motor 10 is fixedly connected to the central control rod 11, and the other end of the central control rod 11 is fixedly connected to the collaborative disk 12. , a plurality of receiving boxes 15 are arranged around the outside of the cooperative plate 12, the receiving box 15 is fixedly connected to the center console 2, and a transfer cavity 16 is symmetrically arranged on the inside. The transfer cavity 16 is connected to the self-service conduit 18 fixedly connected to the receiving box 15, and the other end of the self-service conduit 18 is connected to the windproof shield component 8. An energy transfer guide plate 13 connected to the multiple locking unit 5 is arranged between the receiving box 15 and the cooperative plate 12. The bottom end wall of the energy transfer guide plate 13 is fixedly connected to the inner side of the center console 2 The positioning guide rail 14 is slidably connected, and the energy transmission guide plate 13 is fixedly connected to the wall of the receiving box 15 on one side with a guide slide bar 21. The outer side of the guide slide bar 21 is slidably connected to a retractable control tooth 20 connected to the windproof shield component 8. A spring is fixedly connected between the retractable control tooth 20 and the guide slide bar 21 to cooperate with the movement of the energy transmission guide plate 13 to realize the retraction and extension of the windproof shield component 8. There are also several connecting rods with the transfer cavity 11 between the energy transmission guide plate 13 and the receiving box 15. 6 is connected to the pressure delivery pipe 17, the pressure delivery pipe 17 is fixedly connected to the box wall of the receiving box 15, and a pressure guide 19 fixedly connected to the energy transfer guide plate 13 is arranged on the outer side of the pressure delivery pipe 17. A push rod 22 is provided between the energy transfer guide plate 13 and the cooperative disk 12, and one end of the push rod 22 is rotatably connected to the cooperative disk 12, and the other end is rotatably connected to the energy transfer guide plate 13, for cooperating with the rotation of the cooperative disk 12 to realize the lateral movement of the energy transfer guide plate 13 on the positioning guide rail 14.

[0031] In this embodiment, the pressure guide member 19 includes a push rod fixedly connected to the energy transmission 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 delivery pipe 17, and the receiving box 15 is arranged on the front, back, left and right sides of the cooperative disk 12, and is fixedly connected to the inner wall of the center console 2. In the initial state, the pressure guide member 19 is located on the outside of the pressure delivery pipe 17, and the central control motor 10 drives the cooperative disk 12 to rotate through the central control rod 11, and the cooperative disk 12 cooperates with the push rod 22 to drive the corresponding energy transmission guide plate 13 to move on the positioning guide rail 14, and the energy transmission guide plate 13 drives the retraction and extension control gear 20 to move synchronously through the guide slide rod 21 and the spring. During the movement of the retraction and extension control gear 20, the windproof shield component 8 can be retracted and extended to cover the materials on the bearing seat 3. During the movement, the energy transmission guide plate 13 can synchronously complete the driving of the multiple locking unit 5 and complete the connection with the drone 1, wherein the outer side of the retraction and extension control gear 20 is also fixedly connected and set The spring between the force guide rod 21 and the retraction control tooth 20 is compressed, ensuring the stability of the wind shield assembly 8 after the flip. At the same time, the energy transmission guide plate 13 drives the piston into the inner side of the pressure delivery pipe 17 through the push rod, driving the air inside the corresponding adapter chamber 16 to flow, and cooperating with the wind shield assembly 8 to complete the driving of the clamping response assembly 9. By setting up the multi-functional collaborative assembly 7, the driving of the multiple locking units 5 and the wind shield assembly 8 can be completed at the same time, and the driving of the clamping response assembly 9 can also be completed. It not only improves the convenience of the equipment during disassembly and assembly, but also can provide all-round shielding and protection for the carried materials in the process of carrying materials, and realizes the positioning and fixation of materials, thereby ensuring the stability of materials during transportation.

[0032] In one embodiment of the present invention, please refer to Figure 1 and Figure 5, the windproof shield assembly 8 includes: a U-shaped frame 23, an energy transmission rod 24, a steering gear 25, a connecting pipe 26, a pressure guide seat 27, a supporting rotating rod 28 and a shielding baffle 30. The U-shaped frame 23 is symmetrically arranged, one end is fixedly connected to the center console 2, and the other end is fixedly connected to the bearing seat 3. The U-shaped frames 23 on both sides are rotatably connected with the energy transmission rod 24, and the energy transmission rod 24 is fixedly connected with the steering gear 25 engaged with the retractable control gear 20. The outer sides of the U-shaped frames 23 on both sides are provided with a pressure guide seat 27 fixedly connected to the bearing seat 3, and the pressure guide seats 2 on both sides are fixedly connected to the bearing seat 3. 7 is rotatably connected with a supporting rotating rod 28, and 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 is connected to the energy transmission rod 24 through a synchronous energy guide 29, which is used to cooperate with the rotation of the energy transmission rod 24 to complete the retraction and extension of the shielding baffle 30. One end of the U-shaped frame 23 is connected to the center console 2 and is also connected to the self-service duct 18. The frame wall of the other end of the U-shaped frame 23 is connected to the pressure guide seat 27 through a connecting pipe 26, which is used to cooperate with the multi-functional collaborative component 7 to realize the diversion of air and complete the driving of the clamping response component 9.

[0033] In this embodiment, the U-shaped frames 23 on both sides are hollow structures, and the two ends of the supporting rotating rod 28 are respectively connected to the inner sides of the pressure-guiding seats 27 on both sides. The synchronous energy guide member 29 includes a pulley fixedly connected to the supporting rotating rod 28 and the outer side of the energy transmission rod 24, and the pulleys are connected by a belt. When the retractable control gear 20 moves, the retractable control gear 20 cooperates with the steering gear 25 to drive the energy transmission rod 24 to rotate, and the energy transmission rod 24 drives the supporting rotating rod 28 to rotate through the pulley and the belt, and the supporting rotating rod 28 drives the shielding baffle 30 to flip over. The top plate wall of the shielding baffle 30 abuts against the outer wall of the center console 2 to achieve shielding protection. As the piston moves inside the pressure delivery pipe 17, the rotating The air inside the receiving chamber 16 enters the inside of the U-shaped frame 23 along the self-service duct 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, completing the driving of the clamping response component 9. The clamping response component 9 cooperates with the flipped shielding baffle 30 to position and clamp the materials on the supporting seat 3, thereby ensuring the stability and safety of the materials during transportation. By setting up the windproof shielding component 8, it can cooperate with the multi-functional collaborative component 7 to automatically retract and release, making it convenient for people to take and put away materials, and can provide all-round shielding and protection for the carried materials during transportation, thereby avoiding damage to the materials and ensuring the smooth transportation of materials.

[0034] In one embodiment of the present invention, please refer to Figure 5 、 Figure 6 、 Figure 7 and Figure 8The clamping response component 9 includes: a clamping plate 31, a directional slide 32, a sensing tube 33, a square slider 34, a reaction plate 35, a driven plate 36, an air pressure sensing groove 37 and an induction piston 38. The clamping plate 31 is arranged on the outside of the shielding baffle 30. The clamping plate 31 is also fixedly connected to the directional slide 32 that is slidably connected to the wall of the shielding baffle 30. A square slider 34 is symmetrically arranged between the shielding baffle 30 and the clamping plate 31. An air pressure sensing groove 37 is arranged inside the square slider 34. A sensing tube 33 fixedly connected to the supporting rotating rod 28 is arranged inside the air pressure sensing groove 37. One end of the sensing tube 33 is communicated with the pressure-guiding seat 27, and the other end is fixedly connected to the outside of a sensing piston 38 that is slidably connected to the air pressure sensing groove 37, which is used to cooperate with the air delivered by the multi-cooperative component 7 to realize the lateral movement of the square slider 34, and a reaction plate 35 is rotatably connected to the square slider 34, and a driven plate 36 is slidably connected to the other end of the reaction plate 35. A spring is fixedly connected between the driven plate 36 and the reaction plate 35, and 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 supporting seat 3.

[0035] The air in the pressure guide seat 27 is fed into the air pressure sensing groove 37 along the sensing pipe 33, and the sensing piston 38 is used to drive the square slider 34 to move horizontally 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 toward the center of the supporting 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 supporting seat 3, thereby ensuring the stability of the materials during transportation and effectively preventing the materials from overturning during transportation and delivery. By setting the clamping response component 9, it can cooperate with the multi-functional collaborative component 7 and the windproof shielding component 8 to achieve the positioning and clamping of the materials on the supporting seat 3, ensuring the stability of the materials during transportation, and then ensuring the stability of the drone 1 during flight, which not only improves the efficiency of material delivery, but also greatly improves the safety of the equipment during operation.

[0036] In one embodiment of the present invention, please refer to Figure 1 and Figure 9The anti-seismic support unit 4 includes: a grounding plate 39, a fixed column 40, a guide column 41, an energy absorbing groove 42, a damping disc 43, a shock-absorbing column 44 and a control rod 45. The grounding plate 39 is symmetrically arranged on the outside of the bottom end of the bearing seat 3, and a shock-absorbing column 44 is symmetrically arranged between the grounding plate 39 and the bearing seat 3. One end of the shock-absorbing column 44 is fixedly connected to the damping disc 43 inside the energy absorbing groove 42 in a sliding connection, and the other end is rotatably connected to the control rod 45. The energy absorbing groove 42 is arranged on the inner side of the shell wall of the bearing seat 3, and a damping fluid is arranged inside the energy absorbing groove 42. A buffer spring is fixedly connected between the damping disc 43 and the bearing seat 3, and the other end of the control rod 45 is rotatably connected to the grounding plate 39. A fixed column 40 is fixedly connected to the top of the grounding plate 39, and a guide column 41 fixedly connected to the bearing seat 3 is slidably connected inside the fixed column 40.

[0037] In this embodiment, the fixed column 40 is fixedly connected and arranged at the top of both ends of the grounding plate 39, and a guide column 41 is slidingly connected on the inner side of the fixed column 40. The top of the guide column 41 is fixedly connected to the supporting seat 3. When the UAV 1 lands, the grounding plate 39 contacts the ground, and the guide column 41 cooperates with the fixed column 40 for guidance. The grounding plate 39 drives the shock-absorbing column 44 to move through the transmission rod 45, and the shock-absorbing column 44 drives the damping disc 43 to move inside the energy absorption groove 42. Cooperating with the damping fluid arranged inside the energy absorption groove 42 and the shock-absorbing spring arranged between the damping disc 43 and the supporting seat 3, it can absorb the impact received during the take-off and landing process, thereby ensuring the stability of the equipment during take-off and landing. By setting the anti-seismic support unit 4, the stability of the equipment during take-off and landing can be improved, and the impact of vibration on the equipment during placement can be reduced, which is conducive to improving the service life of the equipment.

[0038] 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 pressure plate 47, a retractor 48, a movable slide 49, a positioning rod 50 and a connecting and controlling assembly. The L-shaped seat 46 is symmetrically arranged on the outer side of the top of the center console 2. A locking pressure plate 47 is provided on the outer side of the opposite end of the L-shaped seat 46 on both sides. A retractor 48 is fixedly connected between the locking pressure plate 47 and the L-shaped seat 46 on the same side, which is used to cooperate with the center console 2 to realize the longitudinal connection between the carrying platform and the drone 1. A movable slide 49 is fixedly connected to the outer side of the bottom end of the L-shaped seat 46. The movable slide 49 is slidably connected to the positioning rod 50 fixedly connected to the top shell wall of the center console 2. A spring is also fixedly connected between the movable slide 49 and the center console 2. The movable slide 49 is also connected to the adjacent side energy transmission guide plate 13 through the connecting and controlling assembly, which is used to cooperate with the movement of the energy transmission guide plate 13 to realize the lateral connection between the carrying platform and the drone 1.

[0039] In this embodiment, a locking pressure plate 47 is provided between the L-shaped seat 46 and the center console 2, and a telescopic device 48 is fixedly connected between the top of the locking pressure 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 transmission control component to drive the movable slide 49 to move along the positioning rod 50, and the movable slide 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, and the telescopic device 48 drives the locking pressure plate 47 to move downward. The locking pressure plate 47 cooperates with the center console 2 to clamp and fix the support legs of the drone 1 longitudinally. By setting up multiple locking units 5, it can cooperate with the multi-functional collaborative component 7 to realize rapid disassembly and assembly between the drone 1 and the carrying platform, and can complete multiple fixations, thereby improving the stability of the equipment during use and ensuring the stability and reliability of the equipment after installation.

[0040] In one embodiment of the present invention, please refer to Figure 10 The connection and control assembly includes: a sensor control plate 51, a telescopic plate 52, a wire rope 53 and a guide wheel 54. The sensor control plate 51 is arranged on the outside of the bottom end of the movable slide 49 and is rotatably connected to the energy transmission guide plate 13 on the adjacent side. The other end of the sensor control plate 51 is slidably connected to the inner side with a telescopic plate 52. A spring is fixedly connected between the telescopic plate 52 and the sensor control plate 51. The other end of the telescopic plate 52 is fixedly connected to the wire rope 53. The other end of the wire rope 53 passes through the guide wheel 54 and is connected to the movable slide 49. The guide wheel 54 is fixedly connected to the center console 2, and is used to cooperate with the movement of the energy transmission guide plate 13 to realize the reverse movement of the movable slide 49.

[0041] In this embodiment, when the energy transmission guide plate 13 moves, it cooperates with the sensor control plate 51 and the telescopic plate 52 to drive the wire rope 53 to move, and the wire rope 53 completes the pulling of the movable slide 49. When the L-shaped seat 46 completes the horizontal clamping, the energy transmission guide plate 13 continues to move, and the spring located between the sensor control plate 51 and the telescopic plate 52 is stretched, so that the L-shaped seat 46 fixes the drone 1 more stably.

[0042] The UAV carrying platform, by setting a collaborative stabilization unit 6 and cooperating with the multiple locking units 5, can realize rapid disassembly and assembly between the equipment and the UAV 1, and can provide all-round shielding and protection for the carried materials in the process of carrying materials, and realize the positioning and fixation of materials, thereby ensuring the stability of materials during transportation, and thus ensuring the stability of the UAV 1 during flight, which not only improves the efficiency of material delivery, but also greatly improves the safety of the equipment during operation. By setting up multiple collaborative components 7, it can simultaneously complete the driving of the multiple locking units 5 and the windproof shielding components 8, and can also complete the driving of the clamping response components 9, which not only improves the convenience of the equipment during disassembly and assembly, but also can provide all-round shielding and protection for the carried materials in the process of carrying materials. By setting up the windproof shielding component 8, it can cooperate with the multiple collaborative components 7 to automatically retract and release, making it convenient for people to take and put materials, and can During the transportation process, the carried materials are shielded and protected in all directions to avoid damage to the materials and ensure the smoothness of material transportation. By setting up the clamping response component 9, it can cooperate with the multi-functional collaborative component 7 and the windproof shielding component 8 to realize the positioning and clamping of the materials on the carrying seat 3, ensuring the stability of the materials during transportation, and then ensuring the stability of the drone 1 during flight, which not only improves the efficiency of material delivery, but also greatly improves the safety of the equipment during operation. By setting up the anti-seismic support unit 4, the stability of the equipment during take-off and landing can be improved, and the impact of vibration on the equipment during placement can be reduced, which is beneficial to improving the service life of the equipment. By setting up multiple locking units 5, it can cooperate with the multi-functional collaborative component 7 to realize rapid disassembly and assembly between the drone 1 and the carrying platform, and can complete multiple fixations, thereby improving the stability of the equipment during use and ensuring the stability and reliability of the equipment after installation.

[0043] The above are only preferred embodiments of the present invention. It should be pointed out that for those skilled in the art, several modifications and improvements can be made without departing from the concept of the present invention. These should also be regarded as the scope of protection of the present invention. These will not affect the effect of the implementation of the present invention and the practicality of the patent.

Claims

1. A UAV carrying platform, characterized in that: include: A center console and a supporting seat, wherein the supporting seat is arranged on the outer side of the bottom end of the center console; A collaborative stabilization unit is provided between the center console and the support base, and is used to cooperate with the center console to realize the positioning of the support base, and cooperate with the support base to realize all-round shielding and protection of the hanging materials and stable positioning; A multiple locking unit connected to the center console and to the collaborative stabilization unit, for cooperating with the collaborative stabilization unit to achieve rapid assembly and disassembly between the carrying platform and the UAV; The anti-seismic support unit is arranged on the outside of the bottom end of the bearing seat and is connected to the bearing seat to support the bearing platform and provide shock absorption protection during lifting and lowering; 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 end of the load-bearing seat, and is used to cooperate with the center console to realize the assembly of the load-bearing platform and the drone, and simultaneously complete the retraction and deployment of the windproof shield component to realize wind shielding protection for materials on the load-bearing seat. The windproof shield component is also provided with a clamping response component, which 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 stable positioning of materials on the load-bearing seat; The multi-functional collaborative component includes: a central control motor, a central control rod, a collaborative disk, an energy transmission guide plate, a positioning guide rail, a receiving box, a transfer chamber, a pressure delivery pipe, a self-service guide tube, a retraction and extension control tooth, a force guide slide rod and a push rod. The central control motor is fixedly connected to the top inner side of the central 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 box is fixedly connected to the central console, and a transfer chamber is symmetrically arranged on the inside. 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 collaborative 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 fixedly connected to the gear train of the driving mechanism, and the cam is fixedly connected to the gear train of the driving mechanism, and the cam is fixedly connected to the gear train of the driving mechanism, and the cam is fixedly connected to the gear train of the driving mechanism.

2. The UAV carrying platform according to claim 1, characterized in that: The U-shaped frame is connected to the center console at one end and 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-functional collaborative component to realize air diversion and complete the driving of the clamping response component.

3. The UAV carrying platform according to claim 2, characterized in that: The clamping response component includes: a splint, a directional slide, a sensing tube, a square slider, a reaction plate, a driven plate, an air pressure sensing groove and a sensing piston. The splint is arranged on the outside of the shielding baffle, and a directional slide that is slidably connected to the shielding baffle wall is fixedly connected to the splint. A square slider is symmetrically arranged between the shielding baffle and the splint, an air pressure sensing groove is arranged on the inside of the square slider, and a sensing tube fixedly connected to the supporting rotating rod is arranged on the inside of the air pressure sensing groove. One end of the sensing tube is communicated with the pressure guide seat, and the other end is fixedly connected to the outside of the sensing piston that is slidably connected to the air pressure sensing groove, which is used to cooperate with the air delivered by the multi-functional 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 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 splint, which is used to cooperate with the movement of the square slider to realize the positioning and clamping of materials on the supporting seat.

4. 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 absorption groove, a damping disk, a shock-absorbing column and a control rod. The grounding plate is symmetrically arranged on the outside of the bottom end of the bearing seat, and 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 inside the energy absorption groove and is slidingly connected, and the other end is rotatably connected to the control rod. The energy absorption groove is arranged on the inner side of the bearing seat shell wall, and damping fluid is arranged inside the energy absorption 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 of the grounding plate, and a guide column fixedly connected to the bearing seat is slidably connected inside the fixed column.

5. 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 assembly. 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 provided 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 carrying platform and the drone. 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 assembly, which is used to cooperate with the movement of the energy transmission guide plate to realize the lateral connection between the carrying platform and the drone.

6. The UAV carrying platform according to claim 5, characterized in that: The connecting transmission control component 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 slidingly connected to the inner side of the other end of the sensor control 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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