A lightweight unmanned transportation platform

Through lightweight design and combination of chassis, protective covers, power devices and other components, the unmanned transportation platform is realized, land and air amphibious transportation is solved, adaptability problems in complex terrain environments, and the mobility and passability of the platform are improved.

CN116788550BActive Publication Date: 2025-07-25SOUTHWEST PETROLEUM UNIV
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Patent Information

Application Number
CN202310300660.0
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2023-03-24
Publication Date
2025-07-25
Estimated Expiration
2043-03-24

AI Technical Summary

Technical Problem

The existing unmanned transportation platforms are not adaptable enough in complex terrain environments, difficult to achieve high mobility and high passability, and lack the functions of amphibious transportation in land and air.

Method used

The lightweight platform design is adopted, combined with components such as chassis, protective cover, power unit, hydraulic cylinder and roller, to realize the amphibious transportation of the unmanned transportation platform, and the transportation of drones is realized through the opening and closing of the protective cover, and the combination of turbines and rollers is used to adapt to different terrain environments.

Benefits of technology

It realizes the rapid movement and stable transportation of the unmanned transportation platform in complex terrain, improves applicability, and can flexibly transport drones in an amphibious environment in land and air, enhancing the stability and adaptability of the platform.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application discloses a lightweight unmanned transportation platform, which includes: a platform, a chassis, a protective cover, a cylinder, a sealing strip, a solar panel, a camera, a power device, a fan blade, a first hydraulic cylinder, a sleeve, a spring, a support rod, a second hydraulic cylinder, a tooth groove, a mounting seat, a bottom plate, a first motor, a gear, a third hydraulic cylinder, a rotating rod, a roller, a second motor, a deflector, a turbine, an impeller, a floating block, a surrounding plate, a gasket, a base, an unmanned aerial vehicle, a storage battery, a positioning module and a control panel. The beneficial effects of the present application are that it uses a lightweight platform to achieve the unmanned transportation function, realizes the transfer function of the unmanned transportation platform through the platform, the chassis and the protective cover, can achieve the amphibious and aerial transportation function of the unmanned transportation platform, realizes the transportation of the unmanned aerial vehicle when the unmanned transportation platform is in use, and realizes the transportation function of the unmanned aerial vehicle, can achieve the amphibious and aerial transportation of the unmanned transportation platform, and can adjust the course to achieve rapid movement in complex terrains.
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Description

Technical Field

[0001] The present invention relates to a lightweight unmanned transportation platform, specifically to a lightweight unmanned transportation platform, belonging to the technical field of unmanned transportation platform applications. Background Art

[0002] Ground unmanned platforms integrate technologies such as vehicle walking, environmental perception, positioning and navigation, information fusion, planning and decision-making, control technology, and human-computer interaction. They embody the characteristics of multi-disciplinary cross-integration and are typical complexes of high-tech. Generally speaking, the progress of domestic research level has benefited to a certain extent from the improvement of hardware devices such as computers. The research and development of key technologies such as sensors, navigation and positioning, control, and body design of unmanned ground weapon mobile platforms still lag behind technologically advanced countries. Unmanned ground weapon mobile platforms are very different from manned vehicles in terms of mobility, cross-country ability, etc. From the current situation and development direction of ground unmanned combat platform military vehicles at home and abroad, it can be seen that there is still great potential for development of ground unmanned combat platforms, with a strong momentum of subverting traditional ground warfare tactics at one go. At the same time, attaching importance to and developing unmanned equipment and its technologies has become a significant feature of the development of high-tech weapons after the Cold War and has achieved initial results.

[0003] In the patent document "CN202121577080.9 A Plant Protection UAV Transportation Platform", it is convenient to improve the disassembly and assembly speed between the UAV (31) body and the transportation platform, effectively solving the problem that the installation steps are relatively cumbersome when the transmission transportation platform is installed with the UAV body, and greatly improving the transportation efficiency. However, currently, there are few light unmanned platforms with high mobility, high cross-country ability, and high reliability, and there is great room for development and potential. Since the combat tasks of unmanned platforms are developing from performing single tasks in a single terrain environment to performing multiple mainstream combat tasks in complex terrain environments and multi-domain terrain environments, the terrain environment, climate environment, battlefield situation, etc. faced by unmanned platforms are more complex and demanding, highlighting the characteristics of new configurations, high adaptability, and high cross-country ability. There is currently no lightweight unmanned transportation platform with a reasonable and reliable structure, high adaptability, and the ability to adapt to complex terrain environments. Summary of the Invention

[0004] In order to solve the deficiencies of the prior art, the present application uses a lightweight platform to achieve the unmanned transportation function. The transfer function of the unmanned transportation platform is realized by using a platform, a chassis, and a protective cover. At the same time, it can adapt to different terrain environments, can realize the amphibious transportation function of the unmanned transportation platform on land, water, and air, and improve the applicability of the unmanned transportation platform.

[0005] In order to solve the problems in the prior art: when the unmanned transport platform is in use, the transportation of the drone can be achieved by opening the protective cover, and the transportation function of the drone can be realized. The amphibious transportation of the unmanned transport platform can be realized by setting the flying chess, turbines and rollers.

[0006] In order to further solve the problems in the prior art: when the unmanned transport platform is in use, the rollers can be stored, and the turbine can be used to move stably when traveling on the waterway. At the same time, the heading can be adjusted to achieve stable movement of the unmanned transport platform. At the same time, support rods are provided to achieve stable taking off and landing of the unmanned transport platform to avoid damage to the unmanned transport platform, and the roller steering function can be realized to achieve rapid movement in complex terrain.

[0007] In order to solve the deficiencies in the prior art, the present application provides a lightweight unmanned transport platform, comprising: a platform, a chassis and a protective cover; wherein, a chassis is fixedly installed at the bottom of the platform, the platform and the chassis are both made of light materials, the top of the platform is rotatably connected to the protective cover, and the protective cover is connected to the platform through a cylinder, the platform and the chassis are both fixedly installed with a power device, a panel is fixedly installed on the top of the platform, the side wall of the panel is fixedly connected to a sealing gasket, and the sealing gasket is fitted with the protective cover, a base is fixedly installed on the surface of the platform, and a drone is clamped on the base; the platform is respectively fixedly connected to a first hydraulic cylinder and a second hydraulic cylinder, the telescopic end of the first hydraulic cylinder is fixedly connected to a sleeve, and the inside of the sleeve is connected to a support rod through a spring, the telescopic end of the second hydraulic cylinder is provided with a tooth groove, a mounting seat is fixedly connected to the inside of the chassis, a bottom plate is sealed and embedded in the mounting seat, and the bottom plate is rotatably connected to the telescopic end of the second hydraulic cylinder, the bottom of the bottom plate is connected to a rotating rod, and a roller is provided at the bottom of the rotating rod.

[0008] Furthermore, two symmetrically distributed protective covers are provided on the top of the platform, and sealing strips are fixedly connected to the edges of the two protective covers. The sealing strips are fitted and connected to each other, and solar panels are embedded and installed on the surface of the protective covers.

[0009] Furthermore, one side of the protective cover is fixedly connected to the camera and the radar sensor, and four evenly distributed power devices are respectively provided on both sides of the platform. Each of the power devices is rotatably connected to the fan blades, and the fan blades are fixedly connected to the drive shaft of the power device.

[0010] Further, the number of the first hydraulic cylinders is four, and each of the first hydraulic cylinders is located inside the chassis. The chassis is inserted through the sleeve in a penetrating manner, and the sleeve is slidably sealed inside the chassis. One end of a spring is fixedly connected to the inside of the sleeve, and the other end of the spring is fixedly connected to a support rod. The number of the support rods is two and they are symmetrically distributed on both sides of the chassis. Each of the support rods is in a U-shaped structure, and both ends of each support rod are slidably connected to the inside of the sleeve.

[0011] Further, the number of the second hydraulic cylinders is four, and the telescopic end of each of the second hydraulic cylinders is located inside the chassis. A toothed groove is formed on the surface of the telescopic end of the second hydraulic cylinder. The telescopic end of the second hydraulic cylinder is inserted through the top of the mounting seat in a penetrating manner, and the telescopic end of the second hydraulic cylinder is hermetically connected to the middle of the mounting seat. The toothed groove is located inside the mounting seat. The top of the bottom plate is fixedly connected to a first motor, and the output end of the first motor is fixedly connected to a gear, and the gear is meshed with the toothed groove.

[0012] Further, the number of the mounting seats is four, and the four mounting seats are evenly distributed around the chassis. Each of the mounting seats is in a circular structure, and the inside of each mounting seat is slidably connected to the bottom plate. The bottom of the bottom plate is respectively rotationally connected to a rotating rod and a third hydraulic cylinder, and the rotating rod and the third hydraulic cylinder are respectively located on both sides of the bottom plate.

[0013] Further, the third hydraulic cylinders are distributed in an inclined shape. The telescopic end of the third hydraulic cylinder is rotationally connected to the rotating rod. A motor for driving the roller to rotate is fixedly installed at the bottom of the rotating rod, and the output end of the motor is fixedly connected to the roller.

[0014] Further, a second motor is fixedly installed inside the chassis. The output end of the second motor is fixedly connected to a deflector, and the deflector is rotationally connected to the bottom of the chassis. A turbine is fixedly installed at the bottom of the chassis. An impeller is rotationally connected to the inside of the turbine. A driver is fixedly installed inside the turbine, and the output end of the driver is fixedly connected to the impeller. The turbine and the second motor are respectively located on both sides of the chassis. A floating block is fixedly connected to the bottom of the chassis, and the floating block is located between the turbine and the second motor.

[0015] Further, the enclosure is in a square hollow structure. The enclosure is located at the edge of the platform and inside the protective cover. The top of the enclosure is in an inclined structure, and a sealing gasket is provided on the inclined slope formed by the top of the enclosure, and the sealing gasket contacts the inner wall of the protective cover.

[0016] Further, a storage battery, a positioning module and a control panel are respectively fixedly installed on the surface of the platform. The control panel is electrically connected to the storage battery and the positioning module respectively. The storage battery is electrically connected to the solar panel through a converter.

[0017] The advantages of the present application are as follows: It provides a lightweight unmanned transportation platform with a reasonable and reliable structure, high adaptability, and the ability to adapt to complex terrain environments. It realizes the unmanned transportation function by using a lightweight platform, and realizes the transfer function of the unmanned transportation platform by adopting a platform, a chassis, and a protective cover. At the same time, it can adapt to different terrain environments and can achieve the three-way transportation function of water, land, and air for the unmanned transportation platform, improving the applicability of the unmanned transportation platform. When the unmanned transportation platform is in use, it can realize the transportation of the unmanned aerial vehicle by opening the protective cover and achieve the transportation function of the unmanned aerial vehicle. The three-way transportation of the unmanned transportation platform can be realized through the set flight chess, turbines, and rollers. When the unmanned transportation platform is in use, the rollers can be stored, and stable movement can be achieved through the turbines when traveling on water. At the same time, the course can be adjusted to realize the stable movement of the unmanned transportation platform. At the same time, support rods are provided to realize the stable takeoff and landing of the unmanned transportation platform, avoiding damage to the unmanned transportation platform, and the roller steering function can be realized to achieve rapid movement on complex terrains. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The drawings constituting a part of this application are used to provide a further understanding of this application, making other features, objectives, and advantages of this application more obvious. The schematic embodiments and descriptions of the drawings of this application are used to explain this application and do not constitute an improper limitation of this application. In the drawings:

[0019] Figure 1 is a schematic structural diagram of a lightweight unmanned transportation platform according to an embodiment of the present application;

[0020] Figure 2 is Figure 1 the first perspective structural diagram in the illustrated embodiment;

[0021] Figure 3 is Figure 2 the side view structural diagram in the illustrated embodiment;

[0022] Figure 4 is Figure 2 the bottom view structural diagram at the chassis in the illustrated embodiment;

[0023] Figure 5 is Figure 2 the top view structural diagram at the protective cover in the illustrated embodiment;

[0024] Figure 6 is Figure 2 the three-dimensional structural diagram at the enclosure panel in the illustrated embodiment;

[0025] Figure 7 is Figure 2 the three-dimensional structural diagram at the sleeve in the illustrated embodiment;

[0026] Figure 8 is Figure 2 Schematic diagram of the three-dimensional structure at the second hydraulic cylinder in the illustrated embodiment;

[0027] Figure 9 is Figure 2 Schematic diagram of the three-dimensional structure at the deflector in the illustrated embodiment;

[0028] Figure 10 is Figure 2 Top view structure diagram of the platform in the illustrated embodiment.

[0029] Meanings of the reference numerals in the figure:

[0030] 1. Platform, 2. Chassis, 3. Protective cover, 4. Cylinder, 5. Sealing strip, 6. Solar panel, 7. Camera, 8. Power device, 9. Fan blade, 10. First hydraulic cylinder, 11. Sleeve, 12. Spring, 13. Support rod, 14. Second hydraulic cylinder, 15. Tooth groove, 16. Mounting seat, 17. Base plate, 18. First motor, 19. Gear, 20. Third hydraulic cylinder, 21. Rotating rod, 22. Roller, 23. Second motor, 24. Deflector, 25. Turbine, 26. Impeller, 27. Floating block, 28. Enclosure, 29. Gasket, 30. Base, 31. Drone, 32. Battery, 33. Positioning module, 34. Control panel. Detailed implementation manners

[0031] In order to enable those skilled in the art of the present technology to better understand the solution of this application, the technical solutions in the embodiments of this application will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of this application. Obviously, the described embodiments are only a part of the embodiments of this application, rather than all the embodiments. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without making creative efforts shall fall within the protection scope of this application.

[0032] It should be noted that the terms "first", "second", etc. in the description and claims of this application and the above-mentioned drawings are used to distinguish similar objects, and do not necessarily need to describe a specific order or sequence. It should be understood that such used data can be interchanged under appropriate circumstances for the embodiments of this application described herein. In addition, the terms "including" and "having" and any variations thereof are intended to cover non-exclusive inclusion. For example, a process, method, system, product or device including a series of steps or units does not necessarily need to be limited to those clearly listed steps or units, but may include other steps or units not clearly listed or inherent to these processes, methods, products or devices.

[0033] In this application, the orientation or positional relationship indicated by terms such as "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", etc. is based on the orientation or positional relationship shown in the drawings. These terms are mainly used to better describe this application and its embodiments, and are not used to limit that the indicated device, element or component must have a specific orientation, or be constructed and operated in a specific orientation.

[0034] Moreover, in addition to being used to represent the orientation or positional relationship, some of the above terms may also be used to represent other meanings. For example, the term "upper" may also be used to represent a certain attachment relationship or connection relationship in some cases. For those of ordinary skill in the art, the specific meanings of these terms in this application can be understood according to the specific circumstances.

[0035] In addition, the terms "mount", "set", "provided with", "connected", "coupled", "socketed" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral structure; it can be a mechanical connection or an electrical connection; it can be directly connected, or indirectly connected through an intermediate medium, or there is internal communication between two devices, elements or components. For those of ordinary skill in the art, the specific meanings of the above terms in this application can be understood according to the specific circumstances.

[0036] It should be noted that, without conflict, the embodiments in this application and the features in the embodiments can be combined with each other. The following will detail this application with reference to the drawings and in combination with the embodiments.

[0037] Referring to Figures 1 to 10 , the lightweight unmanned transportation platform includes: a platform 1, a chassis 2, and a protective cover 3.

[0038] Referring to Figures 1 to 3 and Figures 5 to 6 , as a preferred solution, wherein, the chassis 2 is fixedly installed at the bottom of the platform 1, both the platform 1 and the chassis 2 are made of lightweight materials, the top of the platform 1 is rotatably connected to the protective cover 3, and the protective cover 3 is connected to the platform 1 through a cylinder 4. Power devices 8 are fixedly installed on both the platform 1 and the chassis 2. A guardrail 28 is fixedly installed on the top of the platform 1. The side wall of the guardrail 28 is fixedly connected to a gasket 29, and the gasket 29 is in fit connection with the protective cover 3. A base 30 is fixedly installed on the surface of the platform 1. A drone 31 is snap-fitted on the base 30. The protective cover 3 is used for protecting the top of the platform 1 and can be quickly opened when needed, facilitating the operation of the drone 31 on the base 30. When the protective cover 3 is closed, its fitting position is sealed by a sealing strip 5. At the same time, the bottom edge of the protective cover 3 contacts the gasket 29 on the guardrail 28 to achieve the contact seal of the protective cover 3.

[0039] Reference Figures 2 to 4 as well as Figure 7 As a specific solution, the platform 1 is fixedly connected to the first hydraulic cylinder 10 and the second hydraulic cylinder 14 respectively, the telescopic end of the first hydraulic cylinder 10 is fixedly connected to the sleeve 11, and the sleeve 11 is connected to the support rod 13 through the spring 12, and the telescopic end of the second hydraulic cylinder 14 is provided with a tooth groove 15, and the chassis 2 is fixedly connected with a mounting seat 16, and a bottom plate 17 is sealed and embedded in the mounting seat 16, and the bottom plate 17 is rotatably connected to the telescopic end of the second hydraulic cylinder 14, and the bottom of the bottom plate 17 is connected to the rotating rod 21, and the bottom of the rotating rod 21 is provided with a roller 22. The telescopic movement of the first hydraulic cylinder 10 can drive the sleeve 11 to move, so as to achieve the height adjustment of the support rod 13. When landing, the support rod 13 first contacts the ground, so that the spring 12 plays a buffering role in the compression process. When moving on the water surface, the first hydraulic cylinder 10 can shorten and drive the support rod 13 to move to the inside of the chassis 2, so as to play a storage role, so as to avoid the problem of grounding due to shallow river channels.

[0040] Reference Figures 1 to 3 as well as Figure 5 and Figure 10 As an expansion solution, two symmetrically distributed protective covers 3 are provided on the top of the platform 1. The edges of the two protective covers 3 are fixedly connected with sealing strips 5. The sealing strips 5 are fitted and connected to each other. Solar panels 6 are embedded and installed on the surface of the protective covers 3. The protective covers 3 are symmetrically distributed on both sides of the platform 1. The protective covers 3 are opened to both sides by the extension and contraction of the cylinder 4, thereby realizing the operation of the base 30 and the drone 31. During transportation, protection can be achieved by closing the protective covers 3, and at the same time, an effective sealing effect can be played.

[0041] Reference Figures 1 to 2 as well as Figure 5 , adopting such a scheme, one side of the protective cover 3 is fixedly connected to the camera 7 and the radar sensor, and four evenly distributed power devices 8 are respectively provided on both sides of the platform 1, each of the power devices 8 is rotatably connected to the fan blades 9, and the fan blades 9 are fixedly connected to the drive shaft of the driving machine of the power device 8. The camera 7 is used to shoot the picture in front of the unmanned transport platform 1, and sense the road conditions in front through the radar sensor, so as to facilitate timely change of direction to avoid obstacles. At the same time, power devices 8 are arranged around, and the driving machine installed on the power device 8 can drive the fan blades 9 to rotate inside it, thereby realizing the lifting function of the unmanned transport platform 1.

[0042] Reference Figures 2 to 4 as well as Figure 7, as an extended solution, the number of the first hydraulic cylinders 10 is four, and each of the first hydraulic cylinders 10 is located inside the chassis 2. The chassis 2 is inserted through the sleeve 11 in a penetrating manner. The sleeve 11 is slidably sealed inside the chassis 2. One end of a spring 12 is fixedly connected to the inside of the sleeve 11, and the other end of the spring 12 is fixedly connected to a support rod 13. The number of the support rods 13 is two and they are symmetrically distributed on both sides of the chassis 2. Each of the support rods 13 is of a U-shaped structure, and both ends of each of the support rods 13 are slidably connected to the inside of the sleeve 11. The first hydraulic cylinder 10 is used to drive the sleeve 11 to move, so as to realize the sealed sliding of the sleeve 11 at the bottom of the chassis 2, which is convenient for adjusting the height of the support rod 13 and the storage function. The buffer effect is realized by the movement of the support rod 13 inside the sleeve 11, which is convenient for the stable landing of the unmanned transportation platform 1.

[0043] Refer to Figure 2 , Figure 4 and Figure 8 , as a specific solution, the number of the second hydraulic cylinders 14 is four. The telescopic ends of each of the second hydraulic cylinders 14 are located inside the chassis 2, and tooth grooves 15 are formed on the surfaces of the telescopic ends of the second hydraulic cylinders 14. The telescopic ends of the second hydraulic cylinders 14 are inserted through the top of the mounting seat 16 in a penetrating manner. The telescopic ends of the second hydraulic cylinders 14 are hermetically connected to the middle of the mounting seat 16. The tooth grooves 15 are located inside the mounting seat 16. The top of the bottom plate 17 is fixedly connected to a first motor 18. The output end of the first motor 18 is fixedly connected to a gear 19, and the gear 19 is meshed with the tooth grooves 15. The second hydraulic cylinder 14 can drive the base 30 to move, which is convenient for adjusting the height between the roller 22 and the chassis 2. It can be used on terrains with complex road conditions. The position of the corresponding chassis 2 can be adjusted according to the height of the obstacle, improving the passing efficiency on complex terrains. When the first motor 18 drives the gear 19 to rotate and meshes with the tooth grooves 15, the first motor 18 drives the bottom plate 17 to rotate around the bottom of the telescopic end of the second hydraulic cylinder 14, thereby driving the bottom plate 17 to rotate inside the mounting seat 16 to adjust the direction of the roller 22.

[0044] Refer to Figures 2 to 4 , as an extended solution, the number of the mounting seats 16 is four. The four mounting seats 16 are evenly distributed around the chassis 2. Each of the mounting seats 16 is of a circular structure. The inside of each of the mounting seats 16 is slidably connected to the bottom plate 17. The bottom of the bottom plate 17 is respectively rotationally connected to a rotating rod 21 and a third hydraulic cylinder 20. The rotating rod 21 and the third hydraulic cylinder 20 are respectively located on both sides of the bottom plate 17. The mounting seat 16 is used for limiting the bottom plate 17, and at the same time, the bottom plate 17 can be rotated inside it, which is convenient for adjusting the horizontal angle of the bottom plate 17 to change the rotation direction of the roller 22. At the same time, the bottom plate 17 can be lifted inside the mounting seat 16, which is convenient for adjusting the height of the chassis 2.

[0045] Refer to Figures 2 to 4 , adopting such a solution, the third hydraulic cylinder 20 is distributed in an inclined shape. The telescopic end of the third hydraulic cylinder 20 is rotatably connected to the rotating rod 21. A motor for driving the roller 22 to rotate is fixedly installed at the bottom of the rotating rod 21, and the output end of the motor is fixedly connected to the roller 22. The third hydraulic cylinder 20 can drive the rotating rod 21 to rotate at the bottom of the bottom plate 17. During waterway and air transportation, the third hydraulic cylinder 20 can be shortened to drive the rotating rod 21 to be retracted.

[0046] Refer to Figures 2 to 4 and Figure 9 , as an extended solution, a second motor 23 is fixedly installed inside the chassis 2. The output end of the second motor 23 is fixedly connected to the guide vane 24. The guide vane 24 is rotatably connected to the bottom of the chassis 2. A turbine 25 is fixedly installed at the bottom of the chassis 2. An impeller 26 is rotatably connected inside the turbine 25. A driver is fixedly installed inside the turbine 25, and the output end of the driver is fixedly connected to the impeller 26. The turbine 25 and the second motor 23 are respectively located on both sides of the chassis 2. A floating block 27 is fixedly connected to the bottom of the chassis 2. The floating block 27 is located between the turbine 25 and the second motor 23. By arranging the turbine 25 at the bottom of the chassis 2, the impeller 26 can be driven by the driver to rotate inside it to achieve water surface transportation. At the same time, the guide vane 24 is driven by the second motor 23 to rotate for flow disturbance to change the moving direction. The buoyancy of the lightweight unmanned transportation platform can be increased through the floating block 27 to achieve the stable transportation of the unmanned transportation platform 1.

[0047] Refer to Figures 2 to 3 and Figure 6 , adopting such a solution, the enclosure panel 28 is of a square hollow structure. The enclosure panel 28 is located at the edge of the platform 1. The enclosure panel 28 is located inside the protective cover 3. The top of the enclosure panel 28 is of an inclined structure. A sealing gasket 29 is provided on the inclined slope formed at the top of the enclosure panel 28. The sealing gasket 29 contacts the inner wall of the protective cover 3. When the protective cover 3 is closed, its bottom contacts the sealing gasket 29 at the top of the enclosure panel 28. By setting the top of the enclosure panel 28 as an inclined structure, it is convenient for the sealing gasket 29 to be closely attached to the protective cover 3.

[0048] Refer to Figure 10 , as an extended solution, a storage battery 32, a positioning module 33 and a control panel 34 are respectively fixedly installed on the surface of the platform 1. The control panel 34 is electrically connected to the storage battery 32 and the positioning module 33 respectively. The storage battery 32 is electrically connected to the solar panel 6 through a converter. Photoelectric conversion can be carried out through the solar panel 6 on the top of the protective cover 3, and the electric energy can be stored in the storage battery 32 through the converter to play the role of supplying power to the unmanned transportation platform 1 and improving the endurance of the unmanned transportation platform 1.

[0049] In the technical solution of this application, the entire lightweight unmanned transportation platform uses the lightweight platform 1 to achieve the unmanned transportation function. When the unmanned transportation platform 1 is in air transportation, the lifting and lowering of the platform 1 and the chassis 2 are realized through the operation of the power device 8. At this time, the third hydraulic cylinder 20 shortens and drives the rotating rod 21 to rotate, which drives the rollers 22 to be retracted, so that the rollers 22 move above the support rod 13. When landing, the support rod 13 touches the ground first. At this time, the support rod 13 moves inside the sleeve 11, and the elastic spring 12 plays a buffering role, which can effectively protect the transportation platform 1 from damage; during water transportation, the first hydraulic cylinder 10 shortens to drive the sleeve 11 to move inside the chassis 2. At this time, both the support rod 13 and the rollers 22 are retracted. The floating block 27 plays a floating role, and the rotation of the impeller 26 in the turbine 25 provides the moving power. When moving, when the second motor 23 drives the deflector 24 to rotate, the moving direction is controlled by the deflector 24;

[0050] During land transportation, the third hydraulic cylinder 20 extends to push the support rod 13 to rotate to a vertical position, so that the rollers 22 touch the ground to provide support. The rotation of the rollers 22 drives the platform 1 and the chassis 2 to move. When moving, when the first motor 18 drives the gear 19 to rotate, the gear 19 meshes with the tooth groove 15 at the telescopic end of the second hydraulic cylinder 14, thereby driving the chassis 2 to rotate inside the mounting seat 16. When the bottom plate 17 rotates at the bottom of the telescopic end of the second hydraulic cylinder 14, it drives the support rod 13 and the rollers 22 to turn, thereby realizing the control of the direction. At the same time, the second hydraulic cylinder 14 extends to drive the bottom plate 17 to move inside the mounting seat 16, so that the bottom plate 17 moves inside the mounting seat 16 at the bottom, thereby adjusting the height of the chassis 2 to be suitable for the height of the ground. The road surface conditions are monitored by the camera 7, and the height of each roller 22 is adjusted to adapt to the movement on different uneven road surfaces. At the same time, after the chassis 2 is raised, it has an effective obstacle avoidance function, which improves the practicability of the unmanned transportation platform 1; when in use, the cylinder 4 extends to drive the protective cover 3 to rotate around the platform 1, realizing the opening of the protective cover 3, realizing the transportation of the drone 31 on the base 30, and information collection is realized through the drone 31. When moving, the cylinder 4 shortens to drive the two protective covers 3 to close. At this time, the sealing strips 5 are driven to fit together to achieve sealing. At the same time, the inner wall of the bottom of the protective cover 3 contacts the sealing gasket 29 on the surrounding plate 28, realizing the effective sealing of the bottom of the protective cover 3, avoiding rainwater from entering the inside of the protective cover 3, and improving the practicability of the unmanned transportation platform 1.

[0051] The above are only specific embodiments of this application and are not used to limit this application. For those skilled in the art, various changes and modifications can be made to this application. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of this application shall be included within the protection scope of this application.

Claims

1. A lightweight unmanned transportation platform, characterized in that: The lightweight unmanned transportation platform includes: a platform (1), a chassis (2), and a protective cover (3); Among them, the chassis (2) is fixedly installed at the bottom of the platform (1). Both the platform (1) and the chassis (2) are made of lightweight materials. The top of the platform (1) is rotatably connected to the protective cover (3), and the protective cover (3) is connected to the platform (1) through a cylinder (4). Power devices (8) are fixedly installed on both the platform (1) and the chassis (2). A guardrail (28) is fixedly installed on the top of the platform (1). The side wall of the guardrail (28) is fixedly connected to a sealing gasket (29), and the sealing gasket (29) is in fit connection with the protective cover (3). A base (30) is fixedly installed on the surface of the platform (1), and a drone (31) is snap-fitted on the base (30); The platform (1) is fixedly connected to a first hydraulic cylinder (10) and a second hydraulic cylinder (14) respectively. The telescopic end of the first hydraulic cylinder (10) is fixedly connected to a sleeve (11), and a support rod (13) is connected to the inside of the sleeve (11) through a spring (12). A tooth groove (15) is provided at the telescopic end of the second hydraulic cylinder (14). An installation seat (16) is fixedly connected to the inside of the chassis (2). A bottom plate (17) is hermetically fitted inside the installation seat (16), and the bottom plate (17) is rotatably connected to the telescopic end of the second hydraulic cylinder (14). The bottom of the bottom plate (17) is connected to a rotating rod (21), and a roller (22) is provided at the bottom of the rotating rod (21); On the top of the platform (1), there are two symmetrically distributed protective covers (3). At the edges of the two protective covers (3), there are sealing strips (5) fixedly connected. The sealing strips (5) are connected in a mutually fitting manner. On the surface of the protective cover (3), a solar panel (6) is embedded and installed. One side of the protective cover (3) is fixedly connected to a camera (7) and a radar sensor. On both sides of the platform (1), there are four uniformly distributed power devices (8) respectively. Inside each power device (8), a fan blade (9) is rotationally connected, and the fan blade (9) is fixedly connected to the drive shaft of the drive motor of the power device (8). The number of the first hydraulic cylinders (10) is four. Each first hydraulic cylinder (10) is located inside the chassis (2). The chassis (2) is inserted through the sleeve (11). The sleeve (11) is hermetically slidable inside the chassis (2). One end of a spring (12) is fixedly connected inside the sleeve (11), and the other end of the spring (12) is fixedly connected to a support rod (13). The number of the support rods (13) is two and they are symmetrically distributed on both sides of the chassis (2). Each support rod (13) is of a U-shaped structure, and both ends of each support rod (13) are slidably connected inside the sleeve (11). The number of the second hydraulic cylinders (14) is four. The telescopic ends of each second hydraulic cylinder (14) are located inside the chassis (2), and on the surface of the telescopic end of the second hydraulic cylinder (14), there is a tooth groove (15). The telescopic end of the second hydraulic cylinder (14) is inserted through the top of the mounting seat (16). The telescopic end of the second hydraulic cylinder (14) is hermetically connected to the middle of the mounting seat (16). The tooth groove (15) is located inside the mounting seat (16). On the top of the bottom plate (17), a first motor (18) is fixedly connected. The output end of the first motor (18) is fixedly connected to a gear (19), and the gear (19) is meshed with the tooth groove (15). The number of the mounting seats (16) is four. The four mounting seats (16) are uniformly distributed around the chassis (2). Each mounting seat (16) is of a circular structure. Inside each mounting seat (16), it is slidably connected to the bottom plate (17). The bottom of the bottom plate (17) is rotationally connected to a rotating rod (21) and a third hydraulic cylinder (20) respectively. The rotating rod (21) and the third hydraulic cylinder (20) are located on both sides of the bottom plate (17).

2. The lightweight unmanned transportation platform according to claim 1, wherein: The third hydraulic cylinder (20) is distributed in an inclined shape. The telescopic end of the third hydraulic cylinder (20) is rotationally connected to the rotating rod (21). At the bottom of the rotating rod (21), a motor for driving the roller (22) to rotate is fixedly installed, and the output end of the motor is fixedly connected to the roller (22).

3. A lightweight unmanned transportation platform according to claim 1, characterized in that: A second motor (23) is fixedly installed inside the chassis (2). The output end of the second motor (23) is fixedly connected to a deflector (24). The deflector (24) is rotatably connected to the bottom of the chassis (2). And a turbine (25) is fixedly installed at the bottom of the chassis (2). An impeller (26) is rotatably connected inside the turbine (25). A driver is fixedly installed inside the turbine (25), and the output end of the driver is fixedly connected to the impeller (26). The turbine (25) and the second motor (23) are respectively located on both sides of the chassis (2). A floating block (27) is fixedly connected to the bottom of the chassis (2), and the floating block (27) is located between the turbine (25) and the second motor (23).

4. A lightweight unmanned transportation platform according to claim 1, characterized in that: The enclosure (28) is of a square hollow structure. The enclosure (28) is located at the edge of the platform (1). The enclosure (28) is located inside the protective cover (3). The top of the enclosure (28) is of an inclined structure. A sealing gasket (29) is provided on the inclined slope formed at the top of the enclosure (28), and the sealing gasket (29) contacts the inner wall of the protective cover (3).

5. A lightweight unmanned transportation platform according to claim 1, characterized in that: A storage battery (32), a positioning module (33) and a control panel (34) are respectively fixedly installed on the surface of the platform (1). The control panel (34) is electrically connected to the storage battery (32) and the positioning module (33) respectively. The storage battery (32) is electrically connected to the solar panel (6) through a converter.

Citation Information

Patent Citations

  • Plant protection unmanned aerial vehicle transportation platform

    CN214876736U

  • Unmanned transportation platform

    CN220054191U