Modular, quickly assembled high-rise landing platform

Abstract

The application discloses a modular and quickly-assembled high-rise building landing platform, and belongs to the technical field of high-rise building landing equipment, which comprises multiple sets of counterweight bases, bearing main beams, spliced landing panels, conical surface guiding self-locking plug-in buckle assemblies, segmented wind-resistant fences and corner warning and protection assemblies. The components are connected through uniform plug-in interfaces, and the platform can be quickly assembled and disassembled by one person without any assembling tools such as wrenches and bolts. The modular and quickly-assembled high-rise building landing platform can realize the technical targets of zero damage to roof surfaces, extremely fast assembly, adaptation to complex wind fields on roofs, modular and free splicing, and quick disassembly, transportation and reuse.

Description

Technical Field

[0001] This invention relates to the field of high-rise building lifting and lowering equipment technology, and in particular to a modular, rapidly assembled high-rise building lifting and lowering platform. Background Technology

[0002] With the continuous improvement of urban low-altitude economy and high-rise building fire emergency rescue systems, rooftop drones and small manned vertical take-off and landing (VTOL) aircraft are increasingly being used in high-rise fire rescue, high-altitude personnel search and rescue, material resupply, and routine building inspections. Dedicated rooftop take-off and landing platforms are core infrastructure equipment for ensuring the safe take-off and landing of these aircraft. Currently, existing rooftop take-off and landing platforms are mainly divided into three categories, all of which have significant technical shortcomings and cannot meet the actual needs of rapid emergency deployment, non-destructive rooftop installation, and convenient disassembly and reuse. The first type is the integral welded fixed rooftop lifting platform. This type of platform is formed by welding the entire steel structure as a single piece, resulting in high structural strength but also extremely heavy weight, making rooftop hoisting and transportation difficult. The installation process requires on-site hot work welding, which poses a significant fire hazard on the roof and damages the original waterproof membrane due to the high temperature. Furthermore, the platform cannot be disassembled, and the installation cycle takes 1-2 days, making it unsuitable for emergency scenarios such as sudden fires or other emergencies requiring rapid setup of lifting and lowering points. When not in use, the platform permanently occupies rooftop space and cannot be moved or reused.

[0003] The second type is the bolt-assembled modular lifting platform. This type of platform breaks down the overall structure into small modules, but the modules are fixed together by a large number of high-strength bolts and pins. The assembly process requires professional tools such as wrenches and screwdrivers, making module alignment difficult and the assembly process cumbersome. The complete assembly time still exceeds 1 hour, resulting in a slow emergency response speed. At the same time, the bolts are prone to corrosion after long-term exposure to wind and sun, making disassembly extremely difficult and preventing rapid disassembly and turnover.

[0004] The third type is the simple flat landing pad. This type of product is just a whole piece of anti-slip steel plate laid flat on the roof. There is no overall rigid frame or wind-resistant protection structure. The roof has complex wind fields such as building flow around, lateral turbulence, and eddies. During the take-off and landing process, the aircraft is very susceptible to deviation and rollover accidents due to crosswinds, resulting in extremely poor take-off and landing safety. At the same time, the pad has no cushioning structure. The impact of the aircraft landing can easily cause the surface of the pad to deform, resulting in a short service life.

[0005] In addition, most existing take-off and landing platforms require drilling and anchoring into the roof, penetrating the roof's waterproof and insulation layers, which can easily lead to roof leaks later on. This makes property management approval extremely difficult and cannot meet the needs of retrofitting existing high-rise buildings.

[0006] In summary, existing rooftop lifting platforms generally suffer from industry pain points such as slow assembly speed, the need for specialized tools, damage to rooftops, inability to adapt to rooftop turbulence, and poor reusability. There is a lack of modular lifting platforms on the market that do not require drilling or welding and are specifically adapted to complex rooftop wind fields. Based on the above-mentioned shortcomings of existing technologies, this invention proposes a new type of modular rapid assembly high-rise lifting platform. Summary of the Invention

[0007] The purpose of this invention is to provide a modular, rapidly assembled high-rise building lifting platform, which solves the technical problems of existing rooftop lifting platforms, such as long assembly cycles, reliance on tools, damage to rooftop waterproofing, weak resistance to rooftop turbulence, and inability to be quickly disassembled and reused. The invention aims to achieve the technical goals of zero damage to the rooftop, extremely rapid assembly, adaptation to complex rooftop wind fields, modular free splicing, and rapid disassembly, transportation, and reuse.

[0008] To achieve the above objectives, the present invention provides a modular, rapid-assembly high-rise building lifting and lowering platform, including multiple sets of counterweight bases, load-bearing main beams, spliced ​​lifting and lowering panels, conical guide self-locking buckle components, segmented wind-resistant barriers, and corner warning and protection components. The counterweight base array is laid flat on the roof of the building. The base has a hollow counterweight cavity inside, which is filled with counterweight blocks to achieve pure gravity fixation. The bottom surface of the counterweight base is fully covered with anti-slip buffer rubber pads. The load-bearing main beam is a lightweight beam with a uniform module. The two ends of the main beam are integrally connected to a tapered guide self-locking buckle assembly. Multiple load-bearing main beams are blindly inserted and automatically locked to the counterweight base through the tapered guide self-locking buckle assembly, splicing together to form a complete rectangular rigid load-bearing frame. The bottom of the spliced ​​take-off and landing panel is integrally formed with elastic buckles, which can be detachably snapped and fixed above the load-bearing main beam. The spliced ​​take-off and landing panels are seamlessly spliced ​​together to form a complete aircraft take-off and landing plane. The conical guide self-locking buckle assembly includes a conical plug female seat and a conical plug male seat. The conical plug female seat is located on the surface of the counterweight base, and the conical plug male seat is located at the bottom of the load-bearing main beam. All the above components use a unified plug-in interface, and no assembly tools such as wrenches and bolts are required during the entire assembly and disassembly process. A single person can independently complete the rapid assembly and disassembly of the platform.

[0009] Preferably, the conical plug-in sub-base includes a conical guide head, a compression spring, and locking tongues on both sides of the compression spring, and also includes a hidden unlocking block connected to the compression spring; the conical plug-in female base matches the conical plug-in sub-base, and a limiting hole is provided on the conical plug-in female base at a position corresponding to the side locking tongue; The tapered guide head enables blind insertion assembly without precise alignment. During the pressing down of the load-bearing main beam, the locking tongue automatically retracts. After assembly, the locking tongue automatically pops out and locks into the limiting hole to complete self-locking. The locking tongue can be retracted by moving the unlocking block, enabling rapid separation of the module.

[0010] Preferably, the counterweight base is provided with a horizontal splicing slot on the side, and adjacent bases are pre-positioned through the slot. The length and width of the platform can be freely expanded according to the size of the rooftop site to adapt to different take-off and landing size requirements from 2m×2m to 5m×5m.

[0011] Preferably, the load-bearing main beam adopts a hollow I-beam structure, with the self-weight of a single main beam not exceeding 18kg, achieving lightweight while maintaining the overall structural load-bearing strength, and meeting the requirements for single-person manual handling and assembly.

[0012] Preferably, the spliced ​​take-off and landing panel has an integrated honeycomb buffer layer inside, and the surface of the spliced ​​take-off and landing panel is printed with aircraft take-off and landing positioning marks and rotor airflow guide grooves. Sealing strips are provided at the splicing gaps of the panel.

[0013] Preferably, the segmented wind-resistant enclosure is plugged into the four perimeter of the rigid load-bearing frame, the wind-resistant enclosure is equipped with vertical guide louvers, and the height of the wind-resistant enclosure on the windward side is greater than the height of the wind-resistant enclosure on the leeward side.

[0014] Preferably, the corner warning and protection components are plugged into and fixed at the four corners of the supporting frame, integrating anti-collision corner guards and audible and visual warning lights. The warning lights can be automatically turned on and off according to the ambient light, adapting to rooftop nighttime and foggy conditions with poor visibility.

[0015] Preferably, the installation method of the high-rise building lifting platform includes the following steps: S1. Roof pretreatment: Clean up debris and protruding components in the pre-designed installation area on the roof to ensure that the installation base is flat and clean; S2. Base installation and fixing: Place multiple sets of gravity counterweight base modules according to the preset platform size, complete the pre-assembly of the base through the side slots, fill the counterweight block into the hollow counterweight cavity of the base, and rely on gravity to complete the anchorless anti-slip fixing. S3. Assembly of the load-bearing frame: Align the tapered plug-in sub-seat at the bottom of the load-bearing main beam with the tapered plug-in female seat inserted into the counterweight base, and automatically align it by relying on the tapered surface guide. The plug-in assembly automatically locks itself, and the whole rigid load-bearing frame is quickly assembled. S4. Installation of lifting panels: The spliced ​​lifting panels are snapped together and fixed above the load-bearing main beam from top to bottom, aligning the panel gaps to form a complete and flat lifting working surface. S5. Assembly of protective components: Insert segmented wind-resistant enclosure modules into the four sides of the load-bearing frame, and insert corner warning and protection modules into the four corners. Once assembled, it can be put into use.

[0016] Furthermore, during disassembly, the enclosure and warning module are removed in sequence, the main beam frame is disassembled by moving the unlocking lever, and finally the base and counterweight are moved to complete the disassembly and storage.

[0017] Therefore, the present invention employs the above-mentioned modular, rapid-assembly high-rise building lifting platform, and the technical effects are as follows: 1. Significantly improved assembly efficiency, suitable for emergency rescue scenarios: This invention requires no welding, bolts, or any assembly tools. It can be operated independently by a single person. The entire machine takes only 10 minutes to assemble and only 8 minutes to disassemble. It can quickly set up emergency take-off and landing points on rooftops in case of emergencies such as fires, and its emergency response capability is far superior to traditional platforms.

[0018] 2. Zero damage to the roof, suitable for existing high-rise buildings: The gravity counterweight fixing method does not damage the roof waterproofing layer or insulation layer, requires no modification to the building structure, and is easy to approve by the property management. It can be directly used on the roof of all existing high-rise and super high-rise buildings.

[0019] 3. Specifically adapted to complex wind fields on rooftops: Unlike ordinary flat-ground take-off and landing platforms, it adopts asymmetrical segmented airflow deflectors to specifically solve the problems of rooftop building eddies and crosswind interference, greatly improving the safety of aircraft take-off and landing in windy weather.

[0020] 4. High modularity and versatility, with freely adjustable size: All components have a unified plug-in module, which can be freely spliced ​​to fit the size of the rooftop space, adapting to different working conditions such as narrow rooftops and open rooftops; the modules have a high degree of standardization, and damaged modules can be replaced individually for later maintenance without disassembling the entire platform.

[0021] 5. Lightweight and easy to transport, with good reusability and economy: The lightweight design allows for manual handling by a single person, and the modules can be stacked and stored after disassembly, taking up very little space; the modules are corrosion-resistant and have high structural strength, and can be repeatedly disassembled and reused more than 30 times, significantly reducing the overall operating cost of the low-altitude rescue platform.

[0022] The technical solution of the present invention will be further described in detail below with reference to the accompanying drawings and embodiments. Attached Figure Description

[0023] Figure 1 This is a partial structural schematic diagram of an embodiment of a modular, rapidly assembled high-rise building lifting platform according to the present invention; Figure 2 This is an exploded structural diagram of the conical guide self-locking buckle assembly of an embodiment of a modular, rapid-assembly high-rise building lifting platform of the present invention.

[0024] Figure Labels 1. Counterweight base; 2. Load-bearing main beam; 3. Wind-resistant enclosure; 4. Conical plug-in female seat; 5. Conical plug-in female seat; 6. Compression spring; 7. Locking tongue; 8. Limiting hole; 9. Audible and visual warning light. Detailed Implementation

[0025] The technical solution of the present invention will be further described below with reference to the accompanying drawings and embodiments.

[0026] Unless otherwise defined, the technical or scientific terms used in this invention shall have the ordinary meaning understood by one of ordinary skill in the art to which this invention pertains. The terms "first," "second," and similar terms used in this invention do not indicate any order, quantity, or importance, but are merely used to distinguish different components. Terms such as "comprising" or "including" mean that the element or object preceding the word encompasses the elements or objects listed following the word and their equivalents, without excluding other elements or objects. Terms such as "connected" or "linked" are not limited to physical or mechanical connections, but can include electrical connections, whether direct or indirect. Terms such as "upper," "lower," "left," and "right" are used only to indicate relative positional relationships; when the absolute position of the described object changes, the relative positional relationship may also change accordingly.

[0027] Example 1: Standard 3m×3m modular lifting platform for high-rise building rooftops (mainstream application example) This embodiment is a standard specification platform adapted to the rooftops of ordinary high-rise residential and commercial buildings in cities. It is the core and most commonly used implementation method of this invention. The overall size is 3m×3m, which can be adapted to most rooftop open spaces and meet the routine take-off and landing operation needs of small and medium-sized fire-fighting drones and inspection drones.

[0028] like Figure 1 The diagram shows the structure of the take-off and landing platform. In this embodiment, nine sets of counterweight bases 1 are arranged in an array. Adjacent counterweight bases 1 are precisely engaged and pre-positioned through side horizontal splicing slots to ensure that the bases are arranged neatly without deviation. The hollow counterweight cavity inside each set of counterweight bases 1 is filled with a 25kg standard concrete counterweight block. The bottom surface of the base is fully covered with anti-slip buffer rubber pads, which are tightly attached to the roof. The anti-slip fixation without drilling or anchoring is achieved by pure gravity, which completely protects the roof's waterproof and thermal insulation structure.

[0029] The counterweight base 1 has a pre-installed integrated tapered plug-in female seat 4 on its top surface, corresponding to 12 hollowed-out I-beam load-bearing main beams 2 with a uniform 1m module. The self-weight of a single main beam is controlled at 15kg, meeting the requirements for single-person manual handling and alignment assembly; the bottom of the main beam has an integrated tapered plug-in female seat 5, such as... Figure 2 As shown, it includes a tapered guide head, double-sided compression springs 6, locking tongues 7, and a side-concealed unlocking block. During assembly, precise manual alignment is not required; the tapered guide head automatically corrects deviation. After the main beam is pressed vertically downwards, the locking tongues 7 are compressed and retract, automatically popping out to engage with the limiting holes 8 of the tapered plug-in female seat 4, completing the mechanical self-locking. No wrenches, bolts, or other assembly tools are needed throughout the process. The locking time for a single plug-in connection does not exceed 8 seconds. It can be quickly assembled into a 3m×3m integral rectangular rigid load-bearing frame with an overall flatness error ≤2mm, no assembly gaps, and strong structural stability.

[0030] Nine modular, interlocking takeoff and landing panels are snapped onto the top of the load-bearing frame. The bottom of each panel has an integrally formed elastic buckle that directly engages and fixes to the pre-set snap-fit ​​points on the main load-bearing beam 2, ensuring seamless splicing between the panels. The panels are internally integrated with a high-density honeycomb buffer layer, which can effectively absorb the impact load of the aircraft landing. The surface of the panels is printed with standard aircraft takeoff and landing positioning lines and rotor airflow guide channels, which can orderly guide the downwash airflow of the aircraft rotor and prevent airflow backflow from interfering with the takeoff and landing attitude. Sealing strips are installed at the panel splicing gaps to prevent rainwater and dust from entering the frame and causing structural corrosion.

[0031] The supporting frame is surrounded by segmented wind-resistant barriers 3, which adopt the asymmetrical height design of this invention. The barrier height on the windward side is 1.2m and the barrier height on the leeward side is 0.6m. Vertical guide louvers are evenly distributed on the barrier body, which can effectively guide the flow around the roof building, lateral turbulence and eddies, and realize the stable take-off and landing of aircraft under strong wind conditions. Corner warning and protection components are inserted at the four corners of the frame, integrating flexible anti-collision corner guards and photosensitive automatic start-stop sound and light warning lights 9. They provide anti-collision protection during the day and automatically activate the warning lights at night and in low visibility environments such as heavy fog, to ensure the safety of rooftop operations and aircraft take-off and landing.

[0032] This embodiment can be operated by a single person throughout the entire process. The complete assembly takes 9-10 minutes. When disassembling, simply move the hidden unlocking lever on the side to separate the enclosure, panel, main beam frame and base module in sequence. The disassembled modules can be stacked and stored, and can be repeatedly reused. It is fully adapted to the routine drone inspection and emergency fire rescue take-off and landing scenarios of high-rise buildings.

[0033] Example 2: 2m×2m Mini Emergency Take-Off and Landing Platform on a Narrow Rooftop (Example of a Limited Site) This embodiment is designed for the scenario of super high-rise building rooftops with dense equipment and limited open space. The overall size is 2m×2m. It is designed for rapid deployment of small emergency rescue drones and micro inspection aircraft, and is suitable for restricted working conditions such as old high-rise buildings, dense rooftop machine rooms, and numerous pipelines.

[0034] This embodiment uses a rectangular array of 4 sets of counterweight bases. The bases are quickly pre-positioned by side splicing slots. Each counterweight cavity is filled with a 20kg counterweight block. The lightweight counterweight layout is suitable for the load-bearing conditions of a small roof. The anti-slip rubber pads on the bottom of the base fully cover and adhere to the roof, preventing platform slippage and displacement.

[0035] It is equipped with 8 lightweight hollow I-beam load-bearing main beams 2, each weighing 14kg, which can be easily transported and assembled by a single person; the tapered guide self-locking buckle components at both ends of the main beams blindly plug into the tapered plug-in female seat 4 of the base and automatically lock, quickly build a small rigid load-bearing frame, and the assembly is without deviation or loosening.

[0036] The top of the frame is fitted with four small, interlocking take-off and landing panels. The panel structure is the same as in Example 1, integrating a honeycomb buffer layer, airflow guide channels, and positioning markings to meet the requirements of precise take-off and landing, as well as cushioning and shock absorption for small aircraft. Lightweight segmented wind-resistant barriers 3 are installed on the four sides of the frame, retaining the vertical airflow guide louver structure to adapt to local turbulence conditions on rooftops. Small corner warning and protection components are installed at the four corners to meet the needs of collision prevention and warning in confined spaces.

[0037] This embodiment features a compact structure and faster assembly and disassembly. A single person can complete assembly in 8 minutes and disassembly in 7 minutes. It occupies minimal rooftop space and enables rapid emergency deployment in the event of a sudden emergency. It solves the industry problem of not being able to deploy a landing platform on a small rooftop and lacking landing points for emergency rescue.

[0038] Example 3: 5m×5m large-scale rescue take-off and landing platform on an open rooftop (heavy-load extended example) This embodiment is designed for the rooftop of super high-rise public buildings with open, unobstructed spaces and ample room. The overall design is expanded into a large 5m×5m platform, which is suitable for heavy-load take-off and landing operations of large fire rescue drones and small manned vertical take-off and landing aircraft, meeting the needs of emergency rescue for major high-rise emergencies and large-volume material transfer.

[0039] This embodiment uses 25 sets of counterweight bases arranged in an array. Multiple sets of bases are pre-positioned as a whole through side splicing slots. Each counterweight cavity is filled with a 30kg weighted counterweight block to improve the overall anti-overturning and anti-slip performance of the platform, making it suitable for heavy loads and complex working conditions with strong winds. The entire roof requires no drilling or structural modification.

[0040] Multiple sets of uniform modular load-bearing main beams 2 are added as supporting components. All main beams, bases and panel interfaces are completely universal. They are connected and locked one by one by the conical guide self-locking buckle components. The expanded load-bearing frame has uniform overall rigidity and no local stress concentration problem. It can bear the maximum 500kg take-off and landing load of aircraft, which fully meets the operation requirements of large rescue equipment.

[0041] The large-size take-off and landing panel is fully covered and seamless, with the buffer pad, airflow guiding structure and sealing structure intact. The wind-resistant enclosure adopts an asymmetrical layout with varying heights throughout, and the windward side is heightened to enhance wind resistance. Vertical louvers throughout the enclosure guide large-scale turbulence on the roof, significantly improving the take-off and landing stability of heavy-load aircraft. The four corner warning and protection components are working properly and are suitable for nighttime and inclement weather operation scenarios for large equipment.

[0042] This embodiment is based on a unified modular interface for free expansion. It does not require new molds or structural modifications. Size expansion can be achieved simply by adding or removing standard modules. It has strong versatility and expandability and is suitable for large-scale low-altitude emergency rescue operation scenarios.

[0043] Example 4: Adaptation Example for High and Low Temperatures, Rain and Snow, and Harsh Environments (Durability Condition Example) This embodiment is based on the standard platform structure of Embodiment 1 and is adapted and verified for harsh outdoor rooftop conditions such as high and low temperatures, rain, snow, and sun exposure. All module steel structure surfaces are treated with hot-dip galvanizing for corrosion protection. The counterweight base 1 rubber pad is made of weather-resistant modified rubber material, which can withstand extreme temperature environments of -30℃ to 70℃. The panel sealing strip is made of aging-resistant silicone material, which can resist rain and snow erosion for a long time.

[0044] The locking tongue 7 of the cone-shaped self-locking latch assembly is made of stainless steel with rust resistance. It will not rust or jam after long-term outdoor use and will still maintain the functions of quick plugging and one-button unlocking. The windproof enclosure 3 has a louvered structure that can quickly drain rain, snow and dust, and prevent debris from accumulating and affecting the use of the platform. It can be used outdoors all year round in all weather conditions. It has excellent durability and meets the needs of long-term normalized deployment.

[0045] Assembly generality description of the embodiments: All the above embodiments strictly follow the core structure of this invention, which features a unified plug-in interface, tool-free quick assembly, and gravity-based non-destructive fixing. The assembly process is completely consistent, and size, load, and scenario adaptation are achieved only by adding or removing standard modular units. There is no need to change the core structure and working principle, which fully demonstrates the universality, flexibility, and mass production capability of the modular design of this invention.

[0046] Therefore, the present invention adopts the above-mentioned modular rapid assembly high-rise building lifting platform, which has a simple structure and solves the technical problems of existing roof lifting platforms such as long assembly cycle, tool dependence, damage to roof waterproofing, weak resistance to roof turbulence, and inability to be quickly disassembled and reused. It achieves the technical goals of zero damage to the roof, extremely rapid assembly, adaptation to complex roof wind fields, modular free splicing, and rapid disassembly, transportation and reuse.

[0047] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and not to limit them. Although the present invention has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can still be made to the technical solutions of the present invention, and these modifications or equivalent substitutions cannot cause the modified technical solutions to deviate from the spirit and scope of the technical solutions of the present invention.

Claims

1. A modular, rapidly assembled high-rise building lifting platform, characterized in that: Includes multiple sets of counterweight bases, load-bearing main beams, spliced ​​lifting and lowering panels, conical guide self-locking buckle components, segmented wind-resistant barriers, and corner warning and protection components; The counterweight base array is laid flat on the rooftop. The counterweight base has a hollow counterweight cavity inside, which is filled with counterweight blocks to achieve pure gravity fixation. The bottom surface of the counterweight base is fully covered with anti-slip buffer rubber pads. The load-bearing main beam is a lightweight beam with a uniform module. The two ends of the main beam are integrally connected to a tapered guide self-locking buckle assembly. Multiple load-bearing main beams are blindly inserted and automatically locked to the counterweight base through the tapered guide self-locking buckle assembly, splicing together to form a complete rectangular rigid load-bearing frame. The bottom of the spliced ​​take-off and landing panel is integrally formed with elastic buckles, which can be detachably snapped and fixed above the load-bearing main beam. The spliced ​​take-off and landing panels are seamlessly spliced ​​together to form a complete aircraft take-off and landing plane. The conical guide self-locking buckle assembly includes a conical plug female seat and a conical plug male seat. The conical plug female seat is located on the surface of the counterweight base, and the conical plug male seat is located at the bottom of the load-bearing main beam.

2. The modular, rapid-assembly high-rise building lifting platform according to claim 1, characterized in that: The conical plug-in sub-base includes a conical guide head, a compression spring, and locking tongues on both sides of the compression spring. It also includes a hidden unlocking block connected to the compression spring. The conical plug-in female base matches the conical plug-in sub-base, and a limiting hole is provided on the conical plug-in female base at the position corresponding to the side locking tongue.

3. The modular, rapid-assembly high-rise building lifting platform according to claim 1, characterized in that: The counterweight base is provided with a horizontal splicing slot on the side. Adjacent bases are pre-positioned through the slot, and the length and width of the platform can be freely expanded according to the size of the rooftop site to accommodate different take-off and landing size requirements from 2m×2m to 5m×5m.

4. The modular, rapid-assembly high-rise building lifting platform according to claim 1, characterized in that: The load-bearing main beam adopts a hollow I-beam structure, and the self-weight of a single main beam is no more than 18kg.

5. The modular, rapid-assembly high-rise building lifting platform according to claim 1, characterized in that: The spliced ​​take-off and landing panel integrates a honeycomb buffer layer inside, and the surface of the spliced ​​take-off and landing panel is printed with aircraft take-off and landing positioning marks and rotor airflow guide grooves. Sealing strips are set at the splicing gaps of the panel.

6. The modular, rapid-assembly high-rise building lifting platform according to claim 1, characterized in that: The segmented wind-resistant enclosure is plugged into the four perimeter of the rigid load-bearing frame, and the wind-resistant enclosure is equipped with vertical guide louvers.

7. The modular, rapid-assembly high-rise building lifting platform according to claim 1, characterized in that: The corner warning and protection components are plugged into and fixed at the four corners of the supporting frame, integrating anti-collision corner guards and audible and visual warning lights.

8. The modular, rapid-assembly high-rise building lifting platform according to claim 1, characterized in that: The installation method for this high-rise building lifting platform includes the following steps: S1. Roof pretreatment: Clean up debris and protruding components in the pre-designed installation area on the roof to ensure that the installation base is flat and clean; S2. Base installation and fixing: Place multiple sets of counterweight base modules according to the preset platform size, complete the pre-assembly of the base through the side slots, fill the counterweight blocks into the hollow counterweight cavity of the counterweight base, and rely on gravity to complete the anchorless anti-slip fixing. S3. Assembly of the load-bearing frame: Align the tapered plug-in sub-seat at the bottom of the load-bearing main beam with the tapered plug-in female seat inserted into the counterweight base, and automatically align it by relying on the tapered surface guide. The plug-in assembly automatically locks itself, and the whole rigid load-bearing frame is quickly assembled. S4. Installation of lifting panels: The spliced ​​lifting panels are snapped together and fixed above the load-bearing main beam from top to bottom, aligning the panel gaps to form a complete and flat lifting working surface. S5. Assembly of protective components: Insert segmented wind-resistant barriers into the four sides of the load-bearing frame, and insert corner warning and protective components into the four corners. Once assembled, it can be put into use.

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