Communication single-pipe tower

Abstract

The utility model provides a communication single-pipe tower which comprises a tower body and an unmanned aerial vehicle airport arranged on the tower body. The unmanned aerial vehicle airport comprises a take-off and landing platform arranged on one side of a tower body and a supporting assembly arranged between the take-off and landing platform and the tower body, and the supporting assembly is located below the take-off and landing platform and comprises a first supporting beam, a second supporting beam and a plurality of first reinforcing beams connected between the first supporting beam and the second supporting beam, a first included angle formed between the first supporting beam and the tower body is larger than a second included angle formed between the second supporting beam and the tower body. According to the communication single-pipe tower, under the condition that the bearing capacity of a communication antenna is not affected, the problems of tower installation and structural stability of an unmanned aerial vehicle airport are solved, the utilization rate of the communication tower is increased, the construction cost of the unmanned aerial vehicle airport can be reduced, and development of low-altitude economy is obviously promoted.

Description

Technical Field

[0001] This utility model relates to the field of communication tower construction technology, and in particular to a single-tube communication tower. Background Technology

[0002] A communication tower is a type of iron tower used for wireless network signal transmission. Its primary function is to support signal transmission, providing support for signal transmitting antennas and ensuring the normal operation of wireless communication systems. These towers are typically built on the ground, rooftops, or mountaintops, using angle steel supplemented with steel plates, or entirely constructed of steel pipes. While numerous and widely distributed, and with reliable power supplies, existing communication towers were initially designed only to support base station antennas and other communication equipment. They lack the installation space and load-bearing capacity required for drone airports, failing to meet drone parking needs. This hinders the improvement of communication tower utilization, the development of the low-altitude economy, and the reduction of drone airport construction costs. Utility Model Content

[0003] In view of this, the present invention aims to propose a single-tube communication tower to improve the utilization rate of communication towers.

[0004] To achieve the above objectives, the technical solution of this utility model is implemented as follows:

[0005] A single-tube communication tower includes a tower body and an unmanned aerial vehicle (UAV) airport installed on the tower body;

[0006] The drone airport includes a take-off and landing platform located on one side of the tower, and a support assembly located between the take-off and landing platform and the tower. The support assembly is located below the take-off and landing platform and includes a first support beam and a second support beam arranged at intervals, and multiple first reinforcing beams connecting the first support beam and the second support beam. The first angle formed between the first support beam and the tower is greater than the second angle formed between the second support beam and the tower.

[0007] Furthermore, multiple triangular structures are formed between the first reinforcing beam, the first supporting beam, and the second supporting beam.

[0008] Furthermore, the take-off and landing platform includes longitudinal beams arranged radially on both sides of the tower body, and multiple transverse beams arranged between the two longitudinal beams. Each longitudinal beam extends horizontally, and a support net is provided on the frame formed by the longitudinal beams and the transverse beams. The unmanned aerial vehicle (UAV) cabin is provided on the support net. The support components are two sets corresponding to each longitudinal beam, and the first support beam and the second support beam in each set of support components are connected to the corresponding longitudinal beam.

[0009] Furthermore, a tie beam is provided between the tower body and each of the longitudinal beams, and each tie beam corresponds to each of the support components and is located above the lifting platform. The third angle formed by each tie beam and the tower support is smaller than the second angle.

[0010] Furthermore, multiple second reinforcing beams are provided between each of the cable-stayed beams and the lifting platform, and each of the second reinforcing beams is arranged sequentially at intervals along the extension direction of the lifting platform.

[0011] Furthermore, each of the cable-stayed beams and the corresponding longitudinal beams and multiple second reinforcing beams form multiple triangular structures; and / or, each of the longitudinal beams and the tower body, each of the first supporting beams and the tower body, each of the second supporting beams and the tower body, each of the first reinforcing beams and the corresponding first and second supporting beams, each of the cable-stayed beams and the tower body, and each of the second reinforcing beams and the corresponding cable-stayed beams and longitudinal beams can be detachably connected.

[0012] Furthermore, the tower body is provided with a ladder, and the support network is provided with an opening located near the tower body, and the opening is provided corresponding to the ladder; and / or, the multiple crossbeams include a first crossbeam located between the connection points of the two first support beams and the longitudinal beam, and a second crossbeam located between the connection points of the two second support beams and the longitudinal beam, and the drone cabin is located between the first crossbeam and the second crossbeam.

[0013] Furthermore, the cross-section of the tower body is hexagonal; and / or, the cross-sectional area of ​​the tower body gradually decreases from bottom to top.

[0014] Furthermore, the tower body comprises multiple tower segments, which are connected from bottom to top.

[0015] Furthermore, the height h of the lifting platform on the tower body is between 5 and 7 meters.

[0016] Compared with the prior art, this utility model has the following advantages:

[0017] This utility model of a single-tube communication tower, through a drone airport mainly composed of a take-off and landing platform and supporting components, can solve the problems of drone airport installation on the tower and the structural stability of the drone airport without reducing the communication tower's ability to support communication antennas. It improves the utilization rate of the communication tower and reduces the construction cost of the drone airport, which has a significant impact on the development of the low-altitude economy.

[0018] Furthermore, the first reinforcing beam, the first support beam, and the second support beam form a triangular structure, which leverages the high strength of the triangle to enhance structural strength. Longitudinal beams are radially distributed on both sides of the tower, and multiple horizontal beams extend horizontally between the longitudinal beams. A support net for UAV takeoff and landing is installed on the frame formed by the longitudinal and horizontal beams. The entire frame structure is simple, easy to assemble, and helps reduce overall cost. The support net also reduces weight while ensuring support. Diagonal tie beams are installed between the tower and each longitudinal beam, with each tie beam corresponding to a support component. This allows the connection points between the tie beams and the takeoff and landing platform, the first support beam and the takeoff and landing platform, and the second support beam and the takeoff and landing platform to be staggered. Compared to having all connection points in the same location, this facilitates the transfer and distribution of the load on the takeoff and landing platform, improving the structural stability of the platform.

[0019] In addition, multiple second reinforcing beams are installed and arranged at intervals along the direction of the landing platform. This arrangement enhances the tensile strength of the cable-stayed beams, ensuring better structural stability of the landing platform. The cable-stayed beams, their corresponding longitudinal beams, and the multiple second reinforcing beams form several triangular structures, leveraging the stability characteristics of triangles to improve platform stability. Furthermore, the use of detachable connections facilitates disassembly, assembly, maintenance, and replacement. Ladders and access openings facilitate maintenance of the communication tower and drone airfield, improving the convenience of equipment upkeep. The drone bay is positioned between the first and second crossbeams, providing reliable support and connection points for the drone bay, ensuring a reliable connection between the drone bay and the landing platform.

[0020] Furthermore, by gradually decreasing the cross-sectional area of ​​the communication tower from bottom to top, the cross-sectional area at the top can be reduced, decreasing wind resistance, enhancing overall rigidity, improving the tower's wind resistance and stability, and also saving materials and reducing costs. By dividing the tower into multiple sub-segments and connecting them from bottom to top, the construction process can be simplified, construction difficulty reduced, construction speed increased, and manufacturing costs lowered. Setting the take-off and landing platform between 5-7 meters avoids the disadvantages of excessively high-altitude winds affecting drone landing stability, interference between drone rotors and antennas during take-off and landing, and instability caused by a shift in the tower's center of gravity due to an excessively high platform installation height. Attached Figure Description

[0021] The accompanying drawings, which form part of this utility model, are used to provide a further understanding of the utility model. The illustrative embodiments of the utility model and their descriptions are used to explain the utility model and do not constitute an undue limitation of the utility model. In the drawings:

[0022] Figure 1 This is a schematic diagram of the overall structure of the communication single-tube tower described in this embodiment of the utility model;

[0023] Figure 2 This is a schematic diagram of the structure of the unmanned aerial vehicle airport described in an embodiment of the present invention;

[0024] Figure 3 This is a schematic diagram of the structure of the support component described in an embodiment of the present utility model;

[0025] Figure 4 This is a top view of the take-off and landing platform described in this embodiment of the utility model;

[0026] Figure 5 This is a schematic diagram of the installation steel pipe structure described in an embodiment of the present utility model;

[0027] Figure 6 This is a schematic diagram of the U-shaped clip structure described in an embodiment of the present utility model;

[0028] Figure 7 This is a schematic diagram of the ladder installation structure according to an embodiment of the present utility model;

[0029] Explanation of reference numerals in the attached figures:

[0030] 1. Tower body; 11. First tower section; 12. Second tower section; 13. Third tower section; 14. Fourth tower section; 141. Installation steel pipe; 1411. Reinforcing plate; 15. Ladder; 16. Clamp; 17. Antenna mast; 171. First antenna mast; 172. Second antenna mast;

[0031] 2. Unmanned Aerial Vehicle (UAV) Airport; 21. Take-off and Landing Platform; 211. Longitudinal Beam; 212. Crossbeam; 2121. First Crossbeam; 2122. Second Crossbeam; 2123. Third Crossbeam; 2124. Fourth Crossbeam; 2125. Fifth Crossbeam; 213. Support Net; 214. Opening; 2141. Opening Longitudinal Beam; 22. Support Component; 221. First Support Beam; 2211. First Angle; 222. Second Support Beam; 2221. Second Angle; 223. First Reinforcing Beam; 23. Diagonal Tie Beam; 231. Third Angle; 233. Second Reinforcing Beam;

[0032] 3. U-shaped clips; 4. Unmanned aerial vehicle (UAV) compartment. Detailed Implementation

[0033] It should be noted that, unless otherwise specified, the embodiments and features described in these embodiments of the present invention can be combined with each other.

[0034] In the following description, specific details such as particular system architectures and techniques are set forth for illustrative purposes and not for limitation, in order to provide a thorough understanding of the embodiments of this application. However, those skilled in the art will understand that this application may also be implemented in other embodiments without these specific details. In other instances, detailed descriptions of well-known systems, apparatuses, circuits, and methods have been omitted so as not to obscure the description of this application with unnecessary detail.

[0035] In the description of this utility model, it should be noted that if terms such as "upper," "lower," "inner," or "outer" appear, indicating orientation or positional relationship, they are based on the orientation or positional relationship shown in the accompanying drawings and are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. Furthermore, if terms such as "first" or "second" appear, they are also used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0036] Furthermore, in the description of this utility model, unless otherwise explicitly defined, the terms "installation," "connection," "joining," and "connector" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model in light of the specific circumstances.

[0037] The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0038] This embodiment relates to a single-tube communication tower, which can solve the problems of tower installation and structural stability of UAV airport 2 without affecting the load-bearing capacity of the communication antenna, improve the utilization rate of the communication tower, reduce the construction cost of UAV airport 2, and strongly promote the development of low-altitude economy.

[0039] In terms of overall structure, such as Figures 1 to 2 As shown, the communication single-tube tower of this embodiment includes a tower body 1 and a drone airport 2 installed on the tower body 1.

[0040] Furthermore, the drone airport 2 includes a take-off and landing platform 21 located on one side of the tower 1, and a support assembly 22 located between the take-off and landing platform 21 and the tower 1. The support assembly 22 is located below the take-off and landing platform 21 and includes a first support beam 221 and a second support beam 222 arranged at intervals between the upper and lower parts, and multiple first reinforcing beams 223 connecting the first support beam 221 and the second support beam 222. The first included angle 2211 formed between the first support beam 221 and the tower 1 is greater than the second included angle 2221 formed between the second support beam 222 and the tower 1.

[0041] At this point, with the above configuration, the UAV airport 2, consisting of a take-off and landing platform 21 and supporting components, can solve the problems of tower installation and structural stability of the UAV airport 2 without reducing the communication tower's ability to support the communication antenna. This improves the utilization rate of the communication tower and reduces the construction cost of the UAV airport 2, which can contribute to the development of the low-altitude economy.

[0042] Meanwhile, by setting up support components 22 and arranging the first support beam 221 and the second support beam 222 at vertical intervals, and with the first included angle 2211 formed between the first support beam 221 and the tower body 1 being greater than the second included angle 2221 formed between the second support beam 222 and the tower body 1, the first support beam 221 and the second support beam 222 can form multiple triangular structures between the lifting platform 21 and the tower body 1, and the stability characteristics of the triangular structure can be used to improve the structural strength.

[0043] Based on the above overview, in detail, in this embodiment, the communication monotube tower also has an antenna mast 17 at the top, consisting of a first antenna mast 171 and a second antenna mast 172 from top to bottom, used to install communication antennas and realize the communication function of the communication monotube tower. Furthermore, in this embodiment, the antenna installed on the antenna mast 172 can adopt various structures of antenna equipment well known to those skilled in the art, which will not be elaborated further.

[0044] In this embodiment, as a preferred implementation, such as Figure 2 and Figure 3 As shown, multiple first reinforcing beams 223, first supporting beams 221, and second supporting beams 222 form multiple triangular structures. The advantage of this arrangement is that the triangular structure formed by the first reinforcing beams 223, first supporting beams 221, and second supporting beams 222 can be utilized to enhance the structural strength by leveraging the stability inherent in triangular structures.

[0045] In this embodiment, as a preferred implementation, such as Figure 4As shown, the take-off and landing platform 21 includes longitudinal beams 211 arranged radially on both sides of the tower body 1, and multiple transverse beams 212 arranged between the two longitudinal beams 211. Each longitudinal beam 211 extends horizontally, and a support net 213 is provided on the frame formed by each longitudinal beam 211 and each transverse beam 212. The unmanned aerial vehicle (UAV) cabin 4 is provided on the support net 213. The support components 22 are two sets corresponding to each longitudinal beam 211, and the first support beam 221 and the second support beam 222 in each set of support components 22 are connected to the corresponding longitudinal beam 211.

[0046] It is understandable that the longitudinal beams 211 arranged radially on both sides of the tower body 1, and the multiple transverse beams 212 extending horizontally between the two longitudinal beams 211, with a support net 213 on the frame formed by the longitudinal beams 211 and the transverse beams 212, result in a simple frame structure that is easy to assemble and helps reduce overall costs. The support net 213 also ensures support while reducing weight. In specific implementation, the take-off and landing platform 21 should be between 3.4m and 3.7m long and between 1.1m and 1.3m wide to ensure sufficient installation space for the drone cabin 4. Furthermore, the drone cabin 4 can adopt structures such as cabins or warehouses for parking drones that are well known to those skilled in the art, and will not be described in detail here.

[0047] In this embodiment, as a preferred implementation, such as Figure 2 As shown, a tie beam 23 is provided between the tower body 1 and each longitudinal beam 211. Each tie beam 23 corresponds to each support component 22 and is located above the lifting platform 21. The third angle 231 formed by each tie beam 23 and the support of the tower body 1 is smaller than the second angle 2221.

[0048] The advantage of this arrangement is that diagonal bracing beams 23 are provided between the tower body 1 and each longitudinal beam 211, and the diagonal bracing beams 23 correspond one-to-one with each support component 22. This allows the connection points between the diagonal bracing beams 23 and the lifting platform 21, the connection points between the first support beam 221 and the lifting platform 21, and the connection points between the second support beam 222 and the lifting platform 21 to be staggered. Compared to having all connection points in the same position, this arrangement is more conducive to the transmission and distribution of the load-bearing force of the lifting platform 21, thereby improving the structural stability of the lifting platform 21.

[0049] In practice, the cable-stayed beam 23 and the lifting platform 21 can also form a triangular structure. The stability of the triangular structure can be used to improve the pulling effect and ensure that the lifting platform 21 has better structural stability.

[0050] In this embodiment, as a preferred implementation, such as Figure 2As shown, multiple second reinforcing beams 233 are provided between each cable-stayed beam 23 and the lifting platform 21, and each second reinforcing beam 233 is arranged sequentially at intervals along the extension direction of the lifting platform 21.

[0051] The installation of multiple second reinforcing beams 233, arranged sequentially and at intervals along the direction of the lifting platform 21, facilitates the transmission and distribution of the load-bearing force of the lifting platform 21, enhances the pulling effect of the cable-stayed beams 23, and ensures that the lifting platform 21 has good structural stability.

[0052] In this embodiment, as a preferred implementation, such as Figure 2 As shown, each cable-stayed beam 23, its corresponding longitudinal beam 211, and multiple second reinforcing beams 233 form several triangular structures. Specifically, each cable-stayed beam 23, its corresponding longitudinal beam 211, and the tower body 1 form a triangular structure, as do the second reinforcing beams 233, the cable-stayed beams 23, and the corresponding longitudinal beams 211. By utilizing the stability characteristics of triangular structures, the stability of the platform can be improved through these multiple triangular structures formed by the cable-stayed beams 23, their corresponding longitudinal beams 211, and the second reinforcing beams 233.

[0053] Furthermore, each longitudinal beam 211 and tower body 1, each first support beam 221 and tower body 1, each second support beam 222 and tower body 1, each first reinforcing beam 223 and its corresponding first support beam 221 and second support beam 222, each diagonal tie beam 23 and tower body 1, and each second reinforcing beam 233 and its corresponding diagonal tie beam 23 and longitudinal beam 211 can be detachably connected. By using a detachable connection method, disassembly, assembly, maintenance and replacement can be facilitated, reducing the difficulty of installation and maintenance and helping to reduce costs.

[0054] In this specific implementation, each diagonal tie beam 23 is connected to the corresponding longitudinal beam 211 and multiple second reinforcing beams 233 by bolting. The bolting can effectively ensure the structural strength and also enable convenient assembly and disassembly.

[0055] In this embodiment, as a preferred implementation, such as Figure 4 and Figure 7 As shown, a ladder 15 is provided on the tower body 1, and an opening 214 is provided on the support net 213 near the tower body 1, with the opening 214 corresponding to the ladder 15. Here, by correspondingly setting the ladder 15 and the maintenance opening 214, it is convenient for staff to maintain the communication tower and the UAV airport 2, thus improving the convenience of equipment maintenance.

[0056] Furthermore, in this embodiment, the multiple crossbeams include a first crossbeam 2121 located between the connection points of the two first support beams 221 and the longitudinal beam 211, and a second crossbeam 2122 located between the connection points of the two second support beams 222 and the longitudinal beam 211, with the drone cabin 4 situated between the first crossbeam 2121 and the second crossbeam 2122. Moreover, placing the drone cabin 4 between the first crossbeam 2121 and the second crossbeam 2122 provides reliable support and connection points for the drone cabin 4, facilitating its reliable arrangement.

[0057] In practical implementation, the multiple crossbeams 212 include a first crossbeam 2121, a second crossbeam 2122, several third crossbeams 2123 and a fourth crossbeam 2124, and a fifth crossbeam 2125. An open longitudinal beam 2141 is positioned between the fourth crossbeam 2124 and the fifth crossbeam 2125, forming an opening 214 with the fourth and fifth crossbeams 2125. This ensures the relative position of the opening 214 and the ladder 15, reducing the operational risks for maintenance personnel.

[0058] Secondly, in this embodiment, the ladder 15 can be installed on the tower body 1 by means of a clamp 16 known to those skilled in the art, and an array is arranged from bottom to top on the tower body 1 to facilitate climbing by installation and maintenance personnel.

[0059] In this embodiment, as a preferred implementation, the cross-section of the tower body 1 is hexagonal. By optimizing the shape of the tower body 1, the stability of the tower body 1 can be improved. At the same time, by setting the cross-sectional area of ​​the communication tower body 1 to gradually decrease from bottom to top, the cross-sectional area at the top can be reduced, the wind resistance at the top can be reduced, the overall rigidity can be enhanced, the wind resistance of the communication tower body 1 can be improved, the stability of the communication tower can be improved, and materials can also be saved, which helps to reduce costs and weight.

[0060] In addition, in specific implementation, the tower body 1 in this embodiment can be set as a regular hexagon. Besides being set as a hexagon, the cross-section can also be set as a regular dodecagon, regular octagon or circle, etc., according to the requirements of the stability of the tower structure.

[0061] In this embodiment, as a preferred implementation, such as Figure 1 As shown, tower body 1 comprises multiple tower segments, which are connected from bottom to top. By dividing tower body 1 into multiple tower segments and connecting them from bottom to top, the construction process of communication towers can be simplified, the construction difficulty reduced, the construction speed increased, and manufacturing costs also reduced.

[0062] In a specific implementation, the multiple tower segments in this embodiment include four tower segments 1, which are, from top to bottom, the first tower segment 11, the second tower segment 12, the third tower segment 13 and the fourth tower segment 14.

[0063] In addition, it should be noted that the design of the tower body and the division of tower sections of the communication tower should comply with national or industry standards such as the Unified Standard for Reliability Design of Building Structures GB 50068-2018, the Code for Design of Building Structures GB 50009-2012, the Standard for Design of Steel Structures GB50017-2017, the Standard for Design of Tall Structures GB 50135-2019, the Code for Design of Steel Tower and Mast Structures for Mobile Communication Engineering YD / T 5131-2019, and the Code for Seismic Design of Structures GB 50191-2012, to ensure that the design of the communication tower body complies with the specifications.

[0064] In this embodiment, as a preferred implementation, the height h of the take-off and landing platform 21 on the tower 1 is between 5 and 7 meters. Setting the take-off and landing platform 21 between 5 and 7 meters can avoid the disadvantages of the drone's inconvenience during take-off and landing caused by excessively high-altitude winds affecting the stability of the drone during landing, and interference between the drone's rotor and antenna during take-off and landing. At the same time, it can also avoid the problem of communication tower instability caused by the change of the center of gravity of the communication tower due to the excessive installation height of the take-off and landing platform 21.

[0065] In addition, it is worth mentioning that if the height of the take-off and landing platform 21 is set too low, it may interfere with ground objects. The drone may collide with pedestrians or trees on the ground during take-off and landing, causing danger. Therefore, the height of the take-off and landing platform 21 should not be set too low. In specific implementation, the drone cabin 4 should be at least 2m away from the tower 1 during installation to avoid the airflow generated by the drone during take-off and landing interfering with the tower 1 and affecting flight safety.

[0066] In detail, in this embodiment, the tower body 1 has a total height of 40m and consists of a first tower section 11, a second tower section 12, a third tower section 13, and a fourth tower section 14 from top to bottom. The total weight of the tower is 8.98 tons. The lifting platform 21 is located 6m above the ground, and installation steel pipes 141 are welded to the tower body 1 at 4m, 5m, 6m, and 7.5m. The installation steel pipes 141 are reinforced by circumferentially welded reinforcing plates 1411. The installation steel pipes 141 at 4m and 5m are installed with support components 22 made of angle steel by U-shaped clamps 3. The support components 22 are reinforced by four first reinforcing beams 223 made of angle steel.

[0067] Furthermore, the lifting platform 21 is installed on the installation steel pipe 141 at 6m using U-shaped clamps 3. At 7.5m, the installation steel pipe 141 is installed on the inclined tie beam 23 made of angle steel using U-shaped clamps 3. The inclined tie beam 23 is reinforced to the longitudinal beam 211 by two second reinforcing beams 233 made of angle steel. All longitudinal beams 211 and transverse beams 212 constituting the lifting platform 21 are made of angle steel. The lifting platform 21 is approximately 3.65m long and 1.2m wide.

[0068] In this embodiment, during the installation of the UAV airport 2, the fourth tower section 14 is first fixed to the ground. Then, the fourth tower section 14 to the first tower section 11 are sequentially inserted from bottom to top to form the communication single-tube tower body 1. Next, the UAV airport 2 installation steel pipe 141 is welded onto the tower body 1 of the communication single-tube tower, and a reinforcing plate 1411 is welded around the installation steel pipe 141 to reinforce the installation steel pipe 141.

[0069] Furthermore, the installation steel pipe 141 for installing the first support beam 221 is connected to the first support beam 221 via U-shaped clamps 3, and the installation steel pipe 141 for installing the second support beam 222 is connected to the second support beam 222 via U-shaped clamps 3. The first support beam 221 and the second support beam 222 are reinforced by multiple first reinforcing beams 223, and the support assembly 22 is connected to the lifting platform 21 to support the lifting platform 21.

[0070] Then, the mounting steel pipe 141 for installing the lifting platform 21 is connected to the longitudinal beam 211 of the lifting platform 21 via U-shaped clamps 3 to fix the lifting platform 21. Finally, the mounting steel pipe 141 for installing the diagonal tie beam 23 is connected to the diagonal tie beam 23 via U-shaped clamps 3, connecting the diagonal tie beam 23 to the lifting platform 21 to provide a pulling effect and ensure the stability of the lifting platform 21.

[0071] Furthermore, the cable-stayed beams 23 are connected to the landing platform 21 via multiple second reinforcing beams 233, which can transfer and distribute the load-bearing force of the landing platform 21, thereby further enhancing the pulling effect of the cable-stayed beams 23 on the landing platform 21 and improving the structural stability of the landing platform 21. Finally, the drone cabin 4 is placed on the landing platform 21 and fixed between the first crossbeam 2121 and the second crossbeam 2122, ensuring that the distance between the drone cabin 4 and the tower body 1 is not less than 2m.

[0072] The single-tube communication tower described in this utility model solves the problems of tower installation and structural stability of UAV airport 2 without affecting the load-bearing capacity of the communication antenna, improves the utilization rate of the communication tower, reduces the construction cost of UAV airport 2, and strongly promotes the development of low-altitude economy.

[0073] The above are merely preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A single-tube communication tower, characterized in that: Includes a tower body (1) and a drone airport (2) located on the tower body; The unmanned aerial vehicle airport (2) includes a take-off and landing platform (21) located on one side of the tower (1) and a support assembly (22) located between the take-off and landing platform (21) and the tower (1). The support assembly (22) is located below the take-off and landing platform (21) and includes a first support beam (221) and a second support beam (222) arranged at intervals between the upper and lower parts, and multiple first reinforcing beams (223) connecting the first support beam (221) and the second support beam (222). The first angle (2211) formed between the first support beam (221) and the tower (1) is greater than the second angle (2221) formed between the second support beam (222) and the tower.

2. The communication single-tube tower according to claim 1, characterized in that: Multiple triangular structures are formed between the first reinforcing beam (223), the first supporting beam (221), and the second supporting beam (222).

3. The communication single-tube tower according to claim 1, characterized in that: The take-off and landing platform (21) includes longitudinal beams (211) arranged on both sides of the tower body (1) along the radial direction of the tower body (1), and multiple cross beams (212) arranged between the two longitudinal beams (211). Each of the longitudinal beams (211) extends horizontally, and a support net (213) is provided on the frame formed by each of the longitudinal beams (211) and each of the cross beams (212). The unmanned aerial vehicle (UAV) cabin (4) is provided on the support net (213). The support components (22) are two sets that correspond one-to-one with each of the longitudinal beams (211), and the first support beam (221) and the second support beam (222) in each set of support components (22) are connected to the corresponding longitudinal beam (211).

4. The communication single-tube tower according to claim 3, characterized in that: An inclined tie beam (23) is provided between the tower body (1) and each of the longitudinal beams (211). Each of the inclined tie beams (23) corresponds to each of the support components (22) and is located above the lifting platform (21). The third angle (231) formed by each of the inclined tie beams (23) and the support of the tower body (1) is smaller than the second angle (2221).

5. The communication single-tube tower according to claim 4, characterized in that: Multiple second reinforcing beams (233) are provided between each of the cable-stayed beams (23) and the lifting platform (21), and each of the second reinforcing beams (233) is arranged sequentially at intervals along the extension direction of the lifting platform (21).

6. The communication single-tube tower according to claim 5, characterized in that: Each of the aforementioned cable-stayed beams (23) forms multiple triangular structures with the corresponding longitudinal beams (211) and the multiple second reinforcing beams (233); and / or, Each of the longitudinal beams (211) and the tower body (1), each of the first support beams (221) and the tower body (1), each of the second support beams (222) and the tower body (1), each of the first reinforcing beams (223) and the corresponding first support beams (221) and second support beams (222), each of the diagonal bracing beams (23) and the tower body (1), and each of the second reinforcing beams (233) and the corresponding diagonal bracing beams (23) and longitudinal beams (211) can be detachably connected.

7. The communication single-tube tower according to claim 3, characterized in that: The tower body (1) is provided with a ladder (15), and the support net (213) is provided with an opening (214) arranged near the tower body (1), and the opening (214) is provided corresponding to the ladder (15); and / or, The multiple crossbeams (212) include a first crossbeam (2121) located between the connection points of the two first support beams (221) and the longitudinal beam (211), and a second crossbeam (2122) located between the connection points of the two second support beams (222) and the longitudinal beam (211), and the unmanned aerial vehicle (UAV) cabin (4) is located between the first crossbeam (2121) and the second crossbeam (2122).

8. The communication single-tube tower according to claim 1, characterized in that: The cross-section of the tower body (1) is hexagonal; and / or the cross-sectional area of ​​the tower body (1) is gradually reduced from bottom to top.

9. The communication single-tube tower according to any one of claims 1 to 8, characterized in that: The tower body (1) includes multiple tower sections, which are connected from bottom to top.

10. The communication single-tube tower according to claim 9, characterized in that: The height h of the lifting platform (21) on the tower body (1) is between 5 and 7 m.

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