Modularized intelligent low-altitude aircraft take-off and landing platform facing complex scene

Abstract

The invention provides a modularized intelligent low-altitude aircraft take-off and landing platform for complex scenes, and relates to the field of aerospace equipment and constructional engineering. The modularized intelligent low-altitude aircraft take-off and landing platform for the complex scene comprises a plurality of supporting parts and a plurality of panel parts, and the multiple supporting parts are spliced to form a supporting unit; the multiple panel components are arranged on the upper portion of the supporting unit, the multiple panel components are spliced to form a take-off and landing panel, and the take-off and landing panel is used for bearing an aircraft. According to the modularized lifting platform provided by the invention, the supporting units are formed by splicing the supporting components, the lifting panels are formed by splicing the panel components, and then the modularized lifting platform is formed, so that the modularized lifting platform can be quickly constructed and disassembled in different use scenes, and the requirements of diversified use scenes are met; the advantages of quick assembly, high stability, high adaptability and the like are realized; as the platform area and the functional modules can be expanded according to requirements, the use requirements of various types of low-altitude aircrafts can be met.

Description

[0001] This application claims the right of priority to the application document with the title "A Modular Takeoff and Landing Platform" and application number 2025104521970, which was filed on April 10, 2024. The entire content of this application is included in the above-mentioned application document and does not exceed the scope of the above-mentioned application document. Technical Field

[0002] The present invention relates to the fields of aerospace equipment and construction engineering, and particularly to a modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios. Background Art

[0003] With the continuous expansion of the application scenarios of unmanned aerial vehicles, electric vertical takeoff and landing aircraft, etc. in the fields of logistics transportation, emergency rescue, aerial inspection, and urban commuting, the demand for safe and efficient low-altitude takeoff and landing infrastructure is increasing day by day. The existing takeoff and landing platforms generally include the following categories: 1. Simple fixed platforms: Flat areas are built on the tops of buildings or on the ground, which are difficult to disassemble, install, and move, and have high requirements for the use site; 2. Movable takeoff and landing vehicles: Modified using trucks or other vehicles, the platform area is limited, and there are limitations in application in complex terrains or extreme environments; 3. Inflatable or foldable platforms: They are convenient to deploy and have good portability, but it is difficult to balance high load-bearing capacity or weather resistance.

[0004] The above solutions still have deficiencies in terms of flexibility, modularity, stability, and scalability, and it is difficult to meet the high-efficiency deployment and safe takeoff and landing requirements of diverse use scenarios (such as rooftops, ship decks, rugged terrains, etc.). Summary of the Invention

[0005] The present invention provides a modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios to solve the problems that the existing technology still has deficiencies in terms of flexibility, modularity, stability, and scalability.

[0006] The present invention provides a modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios, including: A plurality of support components, and the plurality of support components are spliced to form a support unit; A plurality of panel components, the plurality of panel components are arranged on the upper part of the support unit, and the plurality of panel components are spliced to form a takeoff and landing panel, and the takeoff and landing panel is used for carrying the aircraft.

[0007] According to the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, adjacent two of the panel components are connected by a locking component.

[0008] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, the panel component includes: A bracket assembly, the bracket assembly is arranged on the upper part of the support unit; A lower panel, the lower panel is arranged on the upper part of the bracket assembly; An upper panel, the upper panel is arranged on the upper part of the lower panel, and an anti-slip coating is arranged on the upper surface of the upper panel.

[0009] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, the panel component further includes: An upper support plate, arranged between the lower panel and the upper panel, the upper support plate is provided with a plurality of hollow parts, and the plurality of hollow parts are arranged in an array.

[0010] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, the bracket assembly includes: A bottom bracket, the bottom bracket is arranged on the upper part of the support unit; An upper bracket, the upper bracket is arranged on the upper part of the bottom bracket, the lower panel is arranged on the upper part of the upper bracket, and both the upper bracket and the bottom bracket are of a hollow structure.

[0011] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, the support component includes: Support rods, the support rods are arranged vertically, and adjacent two support rods are arranged at intervals, and the upper ends of adjacent two support rods are connected by a connecting frame; A transverse connecting piece, the first end of the transverse connecting piece is connected with the support rods in the same group through a pipe clamp connecting piece, and the second end of the transverse connecting piece is connected with the support rods in the adjacent group through a pipe clamp connecting piece; A base assembly, the base assembly is arranged at the lower end of the support rod.

[0012] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, the middle parts of adjacent two support rods are connected by a reinforcing pipe, and both ends of the reinforcing pipe are connected with adjacent two support rods through a pipe sleeve connecting piece.

[0013] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, a lifting regulator is arranged between the base assembly and the lower end of the support rod, and the lifting regulator is used to adjust the height of the support rod.

[0014] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, wherein the support rod is provided with an attitude sensor for detecting the state of the support rod.

[0015] A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, wherein the base assembly is a magnetic adsorption assembly or a vacuum adsorption assembly.

[0016] The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention is composed of multiple support components spliced to form a support unit, and multiple panel components spliced to form a takeoff and landing panel, thereby forming a modular takeoff and landing platform. It can be quickly assembled and disassembled in different usage scenarios to meet the needs of diverse usage scenarios, and has the advantages of fast assembly, high stability, and strong adaptability. Since the platform area and functional modules can be expanded as needed, the usage requirements of various types of low-altitude aircraft can be met. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the technical solutions in the present invention or the prior art, the following will briefly introduce the drawings required for the description of the embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative efforts.

[0018] Figure 1 is one of the three-dimensional structure schematic diagrams of the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention.

[0019] Figure 2 is Figure 1 the partial enlarged structure schematic diagram at A in

[0020] Figure 3 is the exploded structure schematic diagram of the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention.

[0021] Figure 4 is the second three-dimensional structure schematic diagram of the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention.

[0022] Reference Signs: 100, Support member; 110, Locking component; 120, Support rod; 130, Connecting frame; 140, Lateral connecting member; 150, Base assembly; 151, Upper base; 152, Lower base; 153, Spring; 160, Reinforcing tube; 170, Pipe clamp connecting member; 180, Power interface or data interface; 190, Central support rod; 191, Connecting rod; 200, Panel member; 210, Lower panel; 220, Upper panel; 230, Upper support plate; 240, Bottom bracket; 250, Upper bracket. Detailed implementation

[0023] To make the objectives, technical solutions, and advantages of the present invention clearer, the technical solutions in the present invention will be clearly and completely described below in conjunction with the accompanying drawings of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, rather than all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without making creative efforts fall within the scope of protection of the present invention.

[0024] In the description of the embodiments of the present invention, it should be noted that the orientation or positional relationships indicated by the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. are based on the orientation or positional relationships shown in the accompanying drawings. These are only for the convenience of describing the embodiments of the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as a limitation on the embodiments of the present invention. In addition, the terms "first", "second", and "third" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance.

[0025] In the description of the embodiments of the present invention, it should be noted that unless otherwise clearly specified and limited, the terms "connected" and "connected" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the embodiments of the present invention can be understood according to specific circumstances.

[0026] In an embodiment of the present invention, unless otherwise clearly defined and limited, the first feature being "on" or "under" the second feature may mean that the first and second features are in direct contact, or the first and second features are indirectly in contact through an intermediate medium. Moreover, the first feature being "above", "over" and "on top of" the second feature may mean that the first feature is directly above or obliquely above the second feature, or merely indicates that the horizontal height of the first feature is higher than that of the second feature. The first feature being "under", "beneath" and "underneath" the second feature may mean that the first feature is directly below or obliquely below the second feature, or merely indicates that the horizontal height of the first feature is lower than that of the second feature.

[0027] In the description of this specification, the description referring to terms such as "an embodiment", "some embodiments", "an example", "a specific example", or "some examples", etc. means that the specific features, structures, materials, or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the embodiments of the present invention. In this specification, the schematic representations of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described may be combined in a suitable manner in any one or more embodiments or examples. In addition, without contradiction, those skilled in the art can combine and combine the different embodiments or examples described in this specification and the features of different embodiments or examples.

[0028] The following combines Figures 1 - 4 to describe the specific structure and working principle of the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios of the present invention.

[0029] Figure 1 Fig. 1 schematically shows one of the three-dimensional structures of the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention. As Figure 1 shown, the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios includes a plurality of support components 100 and a plurality of panel components 200. The support components 100 are used to support the panel components 200, and the plurality of support components 100 are spliced to form a support unit. The panel components 200 form a takeoff and landing interface in direct contact with the aircraft. The plurality of panel components 200 are arranged on the upper part of the support unit, and the plurality of panel components 200 are spliced to form a takeoff and landing panel. The takeoff and landing panel can carry the aircraft, and a plane is formed on the upper part of the takeoff and landing panel to provide sufficient takeoff and landing space for the aircraft.

[0030] The modular intelligent low-altitude aircraft takeoff and landing platform provided by the present invention forms a support unit by splicing multiple support components 100, and forms a takeoff and landing panel by splicing multiple panel components 200, thereby forming a modular takeoff and landing platform, which can be quickly assembled and disassembled in different usage scenarios to meet the needs of diverse usage scenarios. For example, in the urban emergency rescue scenario, the platform area can be expanded by increasing the number of support units to meet the simultaneous takeoff and landing of multiple drones; in the shipboard application scenario, some panel components 200 can be quickly disassembled for maintenance without the need for overall replacement. The coordinated operation of the attitude sensor and the lifting regulator enables the platform to adapt to the undulation of the sea or ground settlement in real time, maintain dynamic balance, and has the advantages of rapid assembly, high stability, and strong adaptability; since the platform area and functional modules can be expanded according to requirements, the usage needs of various types of low-altitude aircraft can be met.

[0031] In an embodiment of the present invention, Figure 2 is Figure 1 a partial enlarged structural schematic diagram of point A in Figure 2 As shown, the size and shape of each panel component 200 are the same, which is convenient for the interchange and unified assembly of the panel components 200, effectively reducing the assembly requirements and improving the assembly efficiency. Adjacent two panel components 200 are connected by a buckle assembly 110. Specifically, the panel component 200 is rectangular, but its shape is not limited thereto, and it can also be a regular polygon (such as a hexagon, a square, etc.) or other regular shapes to adapt to different usage scenarios and installation requirements. For example, in the urban emergency rescue scenario, the rectangular panel components 200 can be quickly spliced into a regular rectangular platform; while on the ship's deck, the regular polygon panel components 200 can more flexibly adapt to the irregular deck layout.

[0032] One of the adjacent two panel components 200 is provided with a buckle, and the other of the adjacent two panel components 200 is provided with a locking ring, and the buckle is snap-connected with the locking ring, thereby firmly splicing the adjacent panel components 200 together to form an integral takeoff and landing panel. This connection method not only simplifies the installation process but also significantly improves the assembly efficiency of the takeoff and landing panel, enabling the modular takeoff and landing platform to be quickly assembled and disassembled in different usage scenarios. For example, in an emergency rescue mission, the operator can complete the assembly of the platform within a few minutes, and after the mission is completed, the modular takeoff and landing platform can be quickly disassembled and stored, which is convenient for transportation and storage.

[0033] In addition, using a buckle and a lock ring for connection also has a certain degree of flexibility, and the connection strength and stability can be adjusted according to actual needs. For example, in an environment with strong winds or complex terrain, the firmness of the connection can be improved by increasing the number of buckles or optimizing the structure of the buckles. At the same time, the snap connection method of the buckle and the lock ring facilitates modular expansion, and the area and shape of the platform can be flexibly adjusted according to the takeoff and landing requirements of the aircraft. Of course, the connection method between the two panel components 200 is not limited to this, and bolt connection or other connection methods can also be used.

[0034] It should be noted here that the dimensions of the panel component 200 include but are not limited to the length, width, and thickness of the panel component 200. The dimensions of the panel component 200 (including length, width, and thickness) can be customized according to the actual application scenario.

[0035] In an embodiment of the present invention, Figure 3 An exploded structural schematic diagram of the modular intelligent low-altitude aircraft takeoff and landing platform provided by the present invention is illustrated, as Figure 3 shown, the panel component 200 includes a bracket assembly, a lower panel 210, and an upper panel 220. The bracket assembly is disposed on the upper part of the support unit. The bracket assembly is used to provide support for the lower panel 210 and the upper panel 220. Setting the bracket assembly not only enhances the structural strength of the panel component 200, but also increases the contact area between the support component 100 and the lower panel 210, effectively dispersing the pressure generated during the takeoff and landing of the aircraft, thereby improving the load-bearing capacity and anti-deformation ability of the platform.

[0036] The lower panel 210 is disposed on the upper part of the bracket assembly. Both the lower panel 210 and the upper panel 220 are rectangular plate bodies, and a layered design is adopted to enhance the structural strength and functionality. The lower panel 210 is connected to the bracket assembly. The main function of the lower panel 210 is to bear the impact force during the takeoff and landing of the aircraft and evenly transfer the force to the bracket assembly and the support unit. The material of the lower panel 210 is high-strength aluminum alloy or composite material to ensure its stability under high-load conditions.

[0037] The upper panel 220 is disposed on the upper part of the lower panel 210. An anti-slip coating is provided on the upper surface of the upper panel 220 for providing the friction force during the takeoff and landing of the aircraft to prevent the aircraft from slipping. The anti-slip coating can adopt a material with a high friction coefficient, such as a rubber-based coating or a polymer composite material, to meet the usage requirements under different weather conditions. In addition, the material of the upper panel 220 is preferably carbon fiber. This material has the characteristics of light weight, high strength, and corrosion resistance, and can significantly improve the load-bearing capacity and anti-fatigue performance of the platform without increasing the weight.

[0038] In a preferred embodiment of the present invention, a landing aid mark is provided on the upper surface of the upper panel 220. The aircraft can take off and land according to the landing aid mark, improving the take-off and landing safety of the aircraft in various environments. The landing aid mark not only provides intuitive visual guidance for the aircraft, but also optimizes the safety and efficiency during take-off and landing through a variety of technological innovations.

[0039] In an embodiment of the present invention, the panel component 200 further includes an upper support plate 230. The upper support plate 230 is disposed between the lower panel 210 and the upper panel 220. The upper support plate 230 is provided with a plurality of hollow portions, and the plurality of hollow portions are arranged in an array. The hollow portions are regular hexagons, making the upper support plate 230 a honeycomb structure. The honeycomb structure not only significantly reduces the weight of the upper support plate 230, but also significantly improves its compressive and bending resistance capabilities. In addition, the honeycomb structure can effectively disperse the impact force generated during the take-off and landing of the aircraft without increasing the weight, thereby protecting the lower panel 210 and the support unit from excessive stress. This design is particularly suitable for scenarios that require high load-bearing capacity and lightweight structures, such as the take-off and landing of large unmanned aerial vehicles or electric vertical take-off and landing aircraft (eVTOL). In addition, the array arrangement of the honeycomb structure enables the upper support plate 230 to evenly disperse the vertical and horizontal stresses generated during the take-off and landing of the aircraft, effectively absorbing and dispersing the impact force, and preventing structural deformation or damage caused by local stress concentration. Preferably, the material of the upper support plate 230 is metal or aramid. Of course, the material of the upper support plate 230 is not limited thereto, and other materials can also be used.

[0040] In an embodiment of the present invention, the bracket assembly includes a bottom bracket 240 and an upper bracket 250. The bottom bracket 240 is a rectangular frame body, and the size of the bottom bracket 240 is adapted to the size of the upper panel 220. The bottom bracket 240 is disposed on the upper part of the support unit, and the bottom bracket 240 and the upper part of the support unit can be connected by bolts or a locking component. The upper bracket 250 is a circular frame body. Of course, the shape of the upper bracket 250 is not limited thereto, and it can also be rectangular or other shapes. The upper bracket 250 is disposed on the upper part of the bottom bracket 240, and the lower panel 210 is disposed on the upper part of the upper bracket 250. Both the upper bracket 250 and the bottom bracket 240 are hollow structures. The hollow structure design of the upper bracket 250 and the bottom bracket 240 significantly reduces the weight of the bracket assembly while ensuring the strength of the bracket assembly, making the entire platform lighter and more convenient for transportation and installation. In addition, the hollow design of the bracket assembly also allows for quick adjustment of the height and angle of the platform in complex terrains or extreme environments to adapt to different usage scenarios.

[0041] In an embodiment of the present invention, Figure 4Schematically shows the second three-dimensional structure diagram of the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention, as Figure 1 and Figure 4 shown, the support member 100 includes a support rod 120, a transverse connecting member 140, and a base assembly 150. The support rod 120 is a hollow round tube, and the stress is evenly distributed on the cross-section of the hollow round tube, which can effectively resist external impacts and loads. Of course, the specific type of the support rod 120 is not limited to this, and other shaped profiles such as square tubes or angle irons can also be used, and the specific selection depends on the requirements of the actual application scenario. The length and outer diameter of each support rod 120 are equal, and the modular splicing and expansion are facilitated by adopting a standardized design.

[0042] The support rods 120 are vertically arranged, and adjacent support rods 120 are arranged at intervals. Multiple support rods 120 enclose a rectangular frame, and the distance between adjacent support rods 120 is equal. The distance between adjacent support rods 120 can be adjusted according to actual needs to adapt to different terrains and usage scenarios. The upper ends of adjacent support rods 120 are connected by a connecting frame 130. Preferably, pipe clamp connectors 170 are provided at the upper ends of adjacent support rods 120, and the two ends of the connecting frame 130 are connected to the two pipe clamp connectors 170 in a one-to-one correspondence by bolts. This connection method not only improves the firmness of the connection between adjacent support rods 120, but also enables quick disassembly and quick assembly. The bottom bracket 240 abuts against the connecting frame 130 to provide support for the bottom bracket 240.

[0043] The function of the transverse connecting member 140 is to connect the support rods 120 of the same group with the support rods 120 of the adjacent group to form an integral support unit. The transverse connecting member 140 is in the shape of an X-shaped frame, and this design can evenly disperse stress and improve the overall stability of the support unit. Of course, the shape of the transverse connecting member 140 is not limited to this, and other shapes (such as cross-shaped, triangular, etc.) can also be adopted according to actual needs. The first end of the transverse connecting member 140 is connected to the support rods 120 of the same group by two pipe clamp connectors 170, and the second end of the transverse connecting member 140 is connected to the support rods 120 of the adjacent group by two pipe clamp connectors 170. The two pipe clamp connectors 170 on the same support rod 120 are arranged at intervals in the vertical direction. Using the pipe clamp connectors 170 to connect the support rods 120 and the transverse connecting member 140 allows the support unit to be flexibly adjusted in different scenarios. In this embodiment, two transverse connecting members 140 are provided between adjacent support rods 120. Of course, the number of the transverse connecting members 140 is not limited to this, and three, four or more numbers can also be provided.

[0044] The base assembly 150 is provided at the lower end of the support rod 120. The function of the base assembly 150 is to increase the contact area with the foundation, thereby improving the stability of the support unit. The design of the base assembly 150 can select different structural forms according to the actual scenario.

[0045] In an embodiment of the present invention, the middle parts of two adjacent support rods 120 are connected by a reinforcing pipe 160. The reinforcing pipe 160 is horizontally arranged. The two ends of the reinforcing pipe 160 are connected to two adjacent support rods 120 through sleeve connectors. The sleeve connector is a detachable connection device. Using this connection method is not only firm and reliable, but also convenient for quick disassembly and reassembly. The reinforcing pipe 160 can not only enhance the connection between adjacent support rods 120, but also evenly disperse the stress when the aircraft takes off and lands or the platform is subjected to external force impact, preventing structural deformation or damage caused by excessive local stress. For example, in the case of strong wind or the impact during aircraft takeoff and landing, the reinforcing pipe 160 can effectively absorb and disperse the impact force, protecting the stability of the support rod 120 and the entire support unit. In addition, through the connection of the reinforcing pipe 160, two adjacent support rods 120 form an integral frame structure, significantly enhancing the bending and torsional stiffness of the support unit. This design is particularly suitable for scenarios that require high stability and high load-bearing capacity, such as the takeoff and landing of large unmanned aircraft or electric vertical takeoff and landing aircraft.

[0046] In an embodiment of the present invention, a lifting regulator (not shown) is provided between the base assembly 150 and the lower end of the support rod 120. The lifting regulator is used to adjust the height of the support rod 120. Preferably, the lifting regulator is an electric push rod or a hydraulic push rod. By setting the lifting regulator, the height of each support rod 120 can be precisely adjusted so that the upper end surfaces of the support rods 120 are in the same plane, thereby providing a stable takeoff and landing platform for the aircraft.

[0047] The design of the lifting regulator enables the modular takeoff and landing platform to adapt to various complex terrains and usage scenarios: In rough or uneven terrains, the lifting regulator can precisely adjust the height of each support rod 120 to ensure that the platform remains level. For example, in mountainous areas or construction sites, the platform height can be quickly adjusted through the lifting regulator to adapt to different ground conditions. On the ship deck, the lifting regulator can work in coordination with the base assembly 150 to adjust the platform height in real time to adapt to the dynamic changes of the waves. For example, in the case of wave fluctuations, the lifting regulator can automatically adjust the height of the support rod 120 to ensure that the platform always remains level, providing a stable takeoff and landing environment for the aircraft. In urban emergency rescue scenarios, the lifting regulator can quickly adjust the platform height to adapt to different rescue needs. For example, on the top of a high-rise building or in a narrow street, the platform height can be flexibly adjusted through the lifting regulator to ensure the safe takeoff and landing of the aircraft.

[0048] In an embodiment of the present invention, the support rod 120 is provided with an attitude sensor for detecting the state of the support rod 120. The attitude sensor is an inclination sensor or a gyroscope. Both the attitude sensor and the lifting regulator are electrically connected to the control system. The attitude sensor continuously detects the state of the support rod 120 and sends the attitude information of the support rod 120 to the control system. The control system receives the attitude information sent by the attitude sensor and analyzes it through a built-in algorithm to ensure the accuracy and reliability of the data. According to the analysis result, the control system generates a corresponding control signal for adjusting the height of the lifting regulator. After receiving the control signal, the lifting regulator immediately adjusts the height of the support rod 120. This rapid response ensures that the platform can maintain a horizontal state in real time in a dynamic environment.

[0049] In a preferred embodiment of the present invention, a wind speed sensor is provided on the take-off and landing platform. The wind speed sensor is used to continuously monitor the wind speed and direction in the environment, providing key environmental information for the take-off and landing of the aircraft. By accurately detecting the wind speed, it can ensure that the aircraft takes off and lands under safe environmental conditions, thereby improving the safety and reliability of the aircraft.

[0050] In an embodiment of the present invention, the base assembly 150 includes an upper base 151 and a lower base 152. The upper base 151 is detachably connected to the lower end of the support rod 120. The detachable connection method is adopted between the upper base 151 and the lower end of the support rod 120, which is convenient for quick installation and disassembly and improves the deployment efficiency of the platform. The detachable connection can adopt various methods, such as bolt connection, snap connection, etc. The upper base 151 and the lower base 152 are hinged by a pin shaft. This connection method allows relative rotation between the upper base 151 and the lower base 152 within a certain range, which is especially suitable for uneven terrain or dynamic environments and can effectively adapt to the undulation and changes of the ground. At least two springs 153 are arranged between the upper base 151 and the lower base 152. The springs 153 are distributed on both sides of the pin shaft, and the springs 153 are used for shock absorption. When the base assembly 150 is subjected to external impact or vibration, the springs 153 absorb the impact energy through their own elastic deformation, thereby reducing the vibration transmitted to the support rod 120 and the entire platform.

[0051] In a preferred embodiment of the present invention, the base assembly 150 is a magnetic adsorption assembly or a vacuum adsorption assembly. The design of the base assembly 150 using a magnetic adsorption assembly or a vacuum adsorption assembly significantly enhances the stability of the modular takeoff and landing platform in a shaky environment. Specifically, on the ship deck, the magnetic adsorption assembly can firmly adsorb on the metal surface, resisting the influence brought by the waves and the ship's shaking. The high-strength adsorption force of the magnetic chuck ensures that the platform remains stable in a dynamic environment, providing a safe takeoff and landing environment for the aircraft. On a smooth surface such as the top of a high-rise building, the vacuum adsorption assembly can firmly adsorb, resisting the influence brought by the wind force and the building's shaking, providing a safe takeoff and landing environment for the aircraft.

[0052] In a preferred embodiment of the present invention, a power interface or a data interface 180 is provided on the modular intelligent low-altitude aircraft takeoff and landing platform facing complex scenarios. The main function of the power interface is to provide charging support for the aircraft. By connecting with the battery system of the aircraft, the power interface can quickly and safely charge the aircraft to ensure that it has sufficient power before performing tasks. The main function of the data interface is to provide communication support for the aircraft. By connecting with the control system of the aircraft, the data interface can achieve two-way data transmission. Specifically, the power interface and / or the data interface are provided on the connecting frame 130. Of course, the installation position of the power interface and / or the data interface is not limited thereto, and it can also be provided on the panel component 200 or other positions.

[0053] In a preferred embodiment of the present invention, the modular intelligent low-altitude aircraft takeoff and landing platform facing complex scenarios further includes a plurality of central support mechanisms. The plurality of central support mechanisms are arranged on the rectangular frame and are located below the panel component 200. The main function of the central support mechanism is to support the central area of the takeoff and landing panel to ensure the stability and anti-deformation ability of the takeoff and landing panel when bearing the pressure of the aircraft. Since the central area of the takeoff and landing panel is usually the part with the greatest pressure during the takeoff and landing of the aircraft, the design of the central support mechanism can effectively disperse the pressure and improve the overall load-bearing capacity of the platform. The central support mechanism includes central support rods 190. The central support rods 190 are vertically arranged, and a plurality of central support rods 190 are arranged in an array. Adjacent two central support rods 190 are arranged at intervals. A plug hole is provided at the center of the lower base 152. The upper ends of the central support rods 190 are inserted and connected with the corresponding plug holes one by one. The plug-in connection method not only facilitates installation but also ensures a firm connection between the central support rods 190 and the base. A connecting rod 191 is arranged between adjacent two central support rods 190. The connecting rod 191 is horizontally arranged, and both ends of the connecting rod 191 are detachably connected with adjacent two central support rods 190. Preferably, both ends of the connecting rod 191 are connected with adjacent two central support rods 190 through pipe clamp connectors 170.

[0054] The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios provided by the present invention forms a support unit by splicing a plurality of support components 100, and forms a takeoff and landing panel by splicing a plurality of panel components 200, thereby forming a modular takeoff and landing platform. It can be quickly assembled and disassembled in different usage scenarios to meet the needs of diverse usage scenarios. For example, in the urban emergency rescue scenario, the platform area can be expanded by increasing the number of support units to meet the simultaneous takeoff and landing of multiple drones; in the shipboard application scenario, some panel components 200 can be quickly disassembled for maintenance without overall replacement. The coordinated work of the attitude sensor and the lifting regulator enables the platform to adapt to the undulation of the sea waves or the ground settlement in real time and maintain dynamic balance, with the advantages of rapid assembly, high stability and strong adaptability; since the platform area and functional modules can be expanded according to requirements, the usage needs of various types of low-altitude aircraft can be met.

[0055] Construction method of the modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios: Prepare the support component 100, and set a lifting regulator between the base assembly 150 and the lower end of the support rod 120; Prepare the panel component 200, and set a landing aid mark on the upper surface of the upper panel 220; According to the on-site terrain and usage requirements, select the corresponding number of support components 100 and panel components 200, splice a plurality of support components 100 to form a support unit, arrange a plurality of panel components 200 on the upper part of the support unit, and splice a plurality of panel components 200 to form a takeoff and landing panel; Control the lifting regulator through the control system to automatically level the modular takeoff and landing platform; After the modular takeoff and landing platform is leveled, the takeoff and landing state can be monitored and auxiliary functions can be provided for the aircraft; After use, the modular takeoff and landing platform can be quickly disassembled and recycled.

[0056] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios, characterized in that Including: A plurality of support members (100), and the plurality of support members (100) are spliced to form a support unit; A plurality of panel members (200), the plurality of panel members (200) are arranged on the upper part of the support unit, and the plurality of panel members (200) are spliced to form a takeoff and landing panel for carrying an aircraft.

2. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 1, wherein Adjacent two of the panel members (200) are connected by a locking component (110).

3. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 1, characterized in that, The panel member (200) includes: A bracket assembly arranged on the upper part of the support unit; A lower panel (210) arranged on the upper part of the bracket assembly; An upper panel (220) arranged on the upper part of the lower panel (210), and an anti-slip coating is provided on the upper surface of the upper panel (220).

4. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 3, characterized in that The panel member (200) further includes: An upper support plate (230) arranged between the lower panel (210) and the upper panel (220), and a plurality of hollow parts are provided on the upper support plate (230), and the plurality of hollow parts are arranged in an array.

5. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 3, characterized in that, The bracket assembly includes: A bottom bracket (240) arranged on the upper part of the support unit; An upper bracket (250) arranged on the upper part of the bottom bracket (240), the lower panel (210) is arranged on the upper part of the upper bracket (250), and both the upper bracket (250) and the bottom bracket (240) are hollow structures.

6. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to any one of claims 1 to 5, characterized in that, The support member (100) includes: A support rod (120) vertically arranged, adjacent two support rods (120) are arranged at intervals, and the upper ends of adjacent two support rods (120) are connected by a connecting frame (130); A transverse connecting member (140), the first end of the transverse connecting member (140) is connected to the support rods (120) of the same group by a pipe clamp connecting member (170), and the second end of the transverse connecting member (140) is connected to the support rods (120) of the adjacent group by a pipe clamp connecting member (170); A base assembly (and the base assembly (150) is arranged at the lower end of the support rod (120).

7. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 6, characterized in that, The middle parts of adjacent two support rods (120) are connected by a reinforcing pipe (160), and both ends of the reinforcing pipe (160) are connected to adjacent two support rods (120) by pipe sleeve connecting members.

8. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 6, characterized in that A lifting regulator is arranged between the base assembly (150) and the lower end of the support rod (120), and the lifting regulator is used to adjust the height of the support rod (120).

9. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 6, wherein The support rod (120) is provided with an attitude sensor for detecting the state of the support rod (120).

10. The modular intelligent low-altitude aircraft takeoff and landing platform for complex scenarios according to claim 6, characterized in that The base assembly (150) is a magnetic adsorption assembly or a vacuum adsorption assembly.

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