Communication three-pipe tower

Abstract

The utility model provides a communication three-pipe tower which comprises a tower body with three tower columns, a transverse beam assembly arranged on the tower body and an unmanned aerial vehicle airport arranged on one side of the tower body. Each transverse beam assembly comprises a transverse reinforcing beam arranged between every two adjacent tower columns. The unmanned aerial vehicle airport comprises a take-off and landing platform arranged on one transverse reinforcing beam and a supporting beam assembly and / or a cable-stayed beam assembly arranged between the take-off and landing platform and the tower body, the take-off and landing platform is located on one side of the tower body, the supporting beam assembly is located below the take-off and landing platform, and the cable-stayed beam assembly is located above the take-off and landing platform. According to the communication three-pipe tower, an existing communication three-pipe tower can be energized under the condition that the bearing capacity of a communication antenna is not affected, the communication three-pipe tower can have the function of an unmanned aerial vehicle airport, and the structure of the unmanned aerial vehicle airport has high stability.

Description

Technical Field

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

[0002] A communication tower is a type of iron tower used for wireless network signal transmission. Its main purpose is to support signal transmission, provide support for signal transmitting antennas, and ensure the normal operation of wireless communication systems. These towers are typically built on the ground, rooftops, or mountaintops, and are constructed using angle steel supplemented with steel plates or entirely 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 unmanned aerial vehicle (UAV) airports, failing to meet the parking needs of UAVs. This hinders the improvement of communication tower utilization and the reduction of UAV airport construction costs. Utility Model Content

[0003] In view of this, the present invention aims to propose a communication triple-tube tower that, without affecting the load-bearing capacity of the communication antenna, empowers the existing communication triple-tube tower to have the function of an unmanned aerial vehicle (UAV) airport, and the UAV airport structure has high stability.

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

[0005] A three-tube communication tower includes a tower body with three tower columns, a transverse beam assembly on the tower body, and a drone airport located on one side of the tower body.

[0006] The transverse beam assembly includes a transverse reinforcing beam disposed between two adjacent tower columns. The UAV airport includes a take-off and landing platform disposed on one of the transverse reinforcing beams, and a support beam assembly and / or a cable tie beam assembly disposed between the take-off and landing platform and the main tower body. The take-off and landing platform is located on one side of the main tower body, the support beam assembly is located below the take-off and landing platform, and the cable tie beam assembly is located above the take-off and landing platform.

[0007] Furthermore, the multiple tower columns include a first tower column, a second tower column, and a third tower column. The multiple transverse reinforcing beams are located in the same horizontal plane and include a first transverse reinforcing beam disposed between the first tower column and the second tower column, a second transverse reinforcing beam disposed between the first tower column and the third tower column, and a third transverse reinforcing beam disposed between the second tower column and the third tower column. The lifting platform is disposed on the third transverse reinforcing beam.

[0008] Furthermore, the take-off and landing platform includes a first platform longitudinal beam and a second platform longitudinal beam spaced apart on the third transverse reinforcing beam, and multiple platform crossbeams disposed between the first platform longitudinal beam and the second platform longitudinal beam. The first platform longitudinal beam and the second platform longitudinal beam extend horizontally away from the first tower column, and a support net is provided on the frame formed by the first platform longitudinal beam, the second platform longitudinal beam and each of the platform crossbeams. The unmanned aerial vehicle (UAV) cabin is provided on the support net.

[0009] Furthermore, the support beam assembly includes a first support unit disposed between the second tower column and the first platform longitudinal beam, and a second support unit disposed between the third tower column and the second platform longitudinal beam.

[0010] Furthermore, the first support unit includes a first support beam and a second support beam disposed between the second tower column and the first platform longitudinal beam, and multiple first reinforcing beams disposed between the first support beam and the second support beam, the second support beam being located below the first support beam, and / or, the second support unit includes a third support beam and a fourth support beam disposed between the third tower column and the second platform longitudinal beam, and multiple second reinforcing beams disposed between the third support beam and the fourth support beam, the fourth support beam being located below the third support beam.

[0011] Furthermore, the first support beam, the second support beam, and the multiple first reinforcing beams form multiple triangular structures, and the third support beam, the fourth support beam, and the multiple second reinforcing beams also form multiple triangular structures. Alternatively, the end of the second support beam furthest from the second tower column is connected to the connection point between the first support beam and the second tower column, and the end of the fourth support beam furthest from the third tower column is connected to the connection point between the third support beam and the third tower column.

[0012] Furthermore, the cable-stayed beam assembly includes a first cable-stayed beam disposed between the second tower column and the first platform longitudinal beam, and a second cable-stayed beam disposed between the third tower column and the second platform longitudinal beam.

[0013] Furthermore, the connection point between the first cable-stayed beam and the first platform longitudinal beam is located between the connection point between the second tower column and the first support unit and the first platform longitudinal beam, and the connection point between the second cable-stayed beam and the second platform longitudinal beam is located between the connection point between the third tower column and the second support unit and the second platform longitudinal beam.

[0014] Furthermore, the main body of the tower includes a third diagonal brace disposed between the first tower column and the third transverse reinforcing beam, the third diagonal brace being located above the transverse beam assembly, and / or, the main body of the tower is provided with a ladder, the support network is provided with an opening arranged near the third transverse reinforcing beam, and the opening is provided corresponding to the ladder.

[0015] Furthermore, the height h of the lifting platform on the main body of the tower is between 4 and 6 meters.

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

[0017] This utility model of a three-tube communication tower can solve the problem of installing UAV airports on towers without affecting the load-bearing capacity of the communication antenna, enabling the three-tube communication tower to function as a UAV airport, improving the utilization rate of the communication tower. Furthermore, the transverse beam assembly can strengthen the structural strength of the tower body, and the support beam assembly or diagonal tie beam assembly between the main body of the tower body and the take-off and landing platform of the UAV airport can strengthen the structural strength of the take-off and landing platform, giving the UAV airport structure high stability.

[0018] Furthermore, by setting up multiple tower columns and arranging multiple transverse reinforcing beams on the same horizontal plane, the number of reinforcing beams can be reduced while ensuring structural reliability, thus reducing production costs. The first and second platform longitudinal beams are spaced apart on the third transverse reinforcing beam, and multiple platform transverse beams are located between them. Both the first and second platform longitudinal beams extend horizontally away from the first tower column, and a support net is provided on the frame formed by the longitudinal and transverse beams. This simplifies the overall frame structure, facilitates assembly, and reduces overall costs. The support net also reduces weight while maintaining structural integrity.

[0019] Secondly, the first support unit located between the second tower column and the first platform longitudinal beam, and the second support unit located between the third tower column and the second platform longitudinal beam, create a reliable force transmission path between the support unit and the tower column and platform longitudinal beam, providing reliable support for the platform and improving the stability of the take-off and landing platform. Setting multiple support beams within a support unit and adding multiple reinforcing beams between multiple support beams effectively increases the structural strength of the support unit and enhances its support effect. By arranging multiple support units, the overall stability of the UAV airport structure can be enhanced. Similarly, the formation of multiple triangular structures between the first support beam, the second support beam, and multiple first reinforcing beams, as well as between the third support beam, the fourth support beam, and multiple second reinforcing beams, utilizes the high strength of triangular structures to improve the structural strength of the support unit.

[0020] Furthermore, by setting up a first and a second inclined tie beam, with the first inclined tie beam positioned between the second tower column and the first platform longitudinal beam, and the second inclined tie beam positioned between the third tower column and the second platform longitudinal beam, the first and second inclined tie beams, in conjunction with the first and second support units, can effectively transfer and distribute the weight of the landing platform. This enhances the pulling effect of the inclined tie beams and improves the structural stability of the landing platform. By placing the connection point between the first inclined tie beam and the first platform longitudinal beam between the second tower column and the first support unit and the first platform longitudinal beam, and by placing the connection point between the second inclined tie beam and the second platform longitudinal beam between the third tower column and the second support unit and the second platform longitudinal beam, multiple force transmission channels can be established through staggered connection points. This further facilitates the transfer and distribution of the load-bearing capacity of the landing platform, improving its structural stability.

[0021] Furthermore, the installation of a third diagonal brace connected to the first tower column and the third crossbeam, in conjunction with the first and second diagonal braces, further enhances the tensile strength of the diagonal brace by distributing the weight of the landing platform to the first tower column, thereby improving the structural stability of the landing platform. Simultaneously, the inclusion of ladders and maintenance openings facilitates maintenance of the communication tower and drone airport, improving the convenience of equipment maintenance, reducing maintenance risks, and enhancing maintenance safety. Positioning the landing platform between 4-6 meters avoids the drawbacks of excessively high-altitude winds affecting drone landing stability and interference between drone rotors and antennas during takeoff and landing. It also prevents instability in the communication tower caused by a shift in the tower's center of gravity due to an excessively high landing platform installation height. Attached Figure Description

[0022] 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:

[0023] Figure 1 This is a schematic diagram of the overall structure of the communication three-tube tower according to an embodiment of the present utility model;

[0024] Figure 2 This is a schematic diagram of the left side structure of the unmanned aerial vehicle airport described in an embodiment of this utility model;

[0025] Figure 3 This is a schematic diagram of the right side structure of the unmanned aerial vehicle airport described in an embodiment of the present invention;

[0026] Figure 4 for Figure 2 A schematic diagram of the connection structure at point AA;

[0027] Figure 5 for Figure 2 A schematic diagram of the connection structure at BB;

[0028] Figure 6 This is a schematic diagram of the structure of the support component described in an embodiment of the present utility model;

[0029] Figure 7 This is a top view of the take-off and landing platform described in this embodiment of the utility model;

[0030] Explanation of reference numerals in the attached figures:

[0031] 1. The tower body;

[0032] 11. Tower Column; 111. First Tower Column; 112. Second Tower Column; 113. Third Tower Column;

[0033] 12. Transverse beam assembly; 121. Transverse reinforcing beam; 1211. First transverse reinforcing beam; 1212. Second transverse reinforcing beam; 1213. Third transverse reinforcing beam;

[0034] 13. Reinforced inclined beam; 14. Ladder; 15. Antenna frame;

[0035] 2. Unmanned aerial vehicle (UAV) airport;

[0036] 21. Lifting and lowering platform; 211. First platform longitudinal beam; 212. Second platform longitudinal beam; 213. Platform crossbeam; 214. Support net; 215. Opening;

[0037] 22. Support beam assembly; 221. First support unit; 2211. First support beam; 2212. Second support beam; 2213. First reinforcing beam; 222. Second support unit; 2221. Third support beam; 2222. Fourth support beam; 2223. Second reinforcing beam;

[0038] 23. Cable-stayed beam assembly; 231. First cable-stayed beam; 232. Second cable-stayed beam; 233. Third cable-stayed beam;

[0039] 4. Unmanned aerial vehicle (UAV) warehouse. Detailed Implementation

[0040] It should be noted that, unless otherwise specified, the embodiments and features described in these embodiments can be combined with each other.

[0041] 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.

[0042] 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.

[0043] 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.

[0044] The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0045] This embodiment relates to a communication triple-tube tower, which can solve the problem of installing UAV airports on towers without affecting the load-bearing capacity of the communication antenna, enabling the communication triple-tube tower to have the function of a UAV airport, thereby empowering existing communication triple-tube towers, while the take-off and landing platform structure has high stability.

[0046] In terms of overall structure, such as Figures 1 to 7 As shown, the communication single-tube tower of this embodiment includes a tower body 1 with three tower columns 11, a transverse beam assembly 12 disposed on the tower body 1, and a drone airport 2 disposed on one side of the tower body 1.

[0047] The transverse beam assembly 12 includes a transverse reinforcing beam 121 disposed between two adjacent tower columns 11. The UAV airport 2 includes a take-off and landing platform 21 disposed on one of its transverse reinforcing beams 121, and a support beam assembly 22 or a cable tie beam assembly 23 disposed between the take-off and landing platform 21 and the main body of the tower 1. Alternatively, the take-off and landing platform 21 and the main body of the tower 1 are provided with a support beam assembly 22 and a cable tie beam assembly 23. The take-off and landing platform 21 is located on one side of the main body of the tower 1, the support beam assembly 22 is located below the take-off and landing platform 21, and the cable tie beam assembly 23 is located above the take-off and landing platform 21.

[0048] At this point, the above configuration solves the problem of installing the UAV airport on the tower without affecting the load-bearing capacity of the communication antenna, enabling the three-tube communication tower to function as a UAV airport and improving the utilization rate of the communication tower. Furthermore, the transverse beam assembly 12 strengthens the structural strength of the tower body 1, and a supporting beam assembly 22 or a diagonal beam assembly 23 is provided between the main body of the tower and the take-off and landing platform 21 of the UAV airport 2, which strengthens the structural strength of the take-off and landing platform 21, giving the UAV airport 2 structure higher stability. Based on the above overall description, in detail, the three-tube communication tower of this embodiment also has an antenna frame 15 at the top of the tower for installing communication antennas, realizing the communication function of the communication tower. In this embodiment, the antenna installed on the antenna frame 15 can adopt various structures of antenna equipment well known to those skilled in the art, which will not be elaborated further.

[0049] In this embodiment, as a preferred implementation, such as Figure 2 , Figure 4 and Figure 5 As shown, the multiple tower columns 11 include a first tower column 111, a second tower column 112, and a third tower column 113. Multiple transverse reinforcing beams 121 are located in the same horizontal plane and include a first transverse reinforcing beam 1211 located between the first tower column 111 and the second tower column 112, a second transverse reinforcing beam 1212 located between the first tower column 111 and the third tower column 113, and a third transverse reinforcing beam 1213 located between the second tower column 112 and the third tower column 113. The lifting platform 21 is located on the third transverse reinforcing beam 1213.

[0050] By using multiple tower columns 11 and arranging the first transverse reinforcing beam 1211, the second transverse reinforcing beam 1212, and the third transverse reinforcing beam 1213 in the same horizontal plane, the communication three-tube tower can achieve greater rigidity in the plane, effectively resisting external loads. At the same time, this design can reduce the number of reinforcing beams used while ensuring the structural reliability of the communication three-tube tower, thus helping to reduce costs.

[0051] In this embodiment of the communication three-tube tower, the line connecting the first tower column 111, the second tower column 112 and the third tower column 113 forms an equilateral triangle on any horizontal plane. By utilizing the stability characteristics of the triangle, the structural stability of the tower body 1 can be improved, giving the three-tube tower good load-bearing capacity and stability.

[0052] Furthermore, it is worth mentioning that in the specific implementation of this embodiment of the three-tube communication tower, reinforcing diagonal beams 13 are connected between each of the two adjacent tower columns 11. Some of the reinforcing diagonal beams 13 and the transverse reinforcing beams share connection points with the main body of the tower 1. Moreover, the reinforcing diagonal beams 13, the main body of the tower 1, and the reinforcing transverse beams can form multiple triangular structures to strengthen the structural strength of the tower 1 and further enhance the structural stability of the three-tube tower.

[0053] In addition, it should be noted that the design of the communication tower body and the division of tower sections 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.

[0054] In this embodiment, as a preferred implementation, such as Figure 7 As shown, the take-off and landing platform 21 includes a first platform longitudinal beam 211 and a second platform longitudinal beam 212 spaced apart on the third transverse reinforcing beam 1213, and multiple platform crossbeams 213 located between the first platform longitudinal beam 211 and the second platform longitudinal beam 212. The first platform longitudinal beam 211 and the second platform longitudinal beam 212 both extend horizontally away from the first tower column 111. A support net 214 is provided on the frame formed by the first platform longitudinal beam 211, the second platform longitudinal beam 212 and each platform crossbeam 213. The unmanned aerial vehicle (UAV) cabin 4 is provided on the support net 214.

[0055] Secondly, the first platform longitudinal beam 211 and the second platform longitudinal beam 212 are spaced apart on the third transverse reinforcing beam 1213, and multiple platform crossbeams 213 are provided between the first platform longitudinal beam 211 and the second platform longitudinal beam 212. The first platform longitudinal beam 211 and the second platform longitudinal beam 212 extend horizontally away from the first tower column 111. A support net 214 is provided on the frame formed by each longitudinal beam and each crossbeam, which makes the entire frame structure simple, easy to assemble, and conducive to reducing the overall cost. The setting of the support net 214 can also reduce the weight while ensuring the support.

[0056] In this embodiment, the take-off and landing platform 21 should be between 3.1m and 3.3m long and between 1.1m and 1.3m wide to ensure sufficient installation space for the drone bay 4. Furthermore, the drone bay 4 can adopt structures such as storage sheds or warehouses known to those skilled in the art for parking drones, which will not be elaborated upon here.

[0057] In this embodiment, as a preferred implementation, such as Figure 2 and Figure 3 As shown, the support beam assembly 22 includes a first support unit 221 disposed between the second tower column 112 and the first platform longitudinal beam 211, and a second support unit 222 disposed between the third tower column 113 and the second platform longitudinal beam 212. Specifically, the first support unit 221 disposed between the second tower column 112 and the first platform longitudinal beam 211, and the second support unit 222 disposed between the third tower column 113 and the second platform longitudinal beam 212, can form a reliable force transmission path between the support unit, the tower column 11, and the platform longitudinal beam, which can further enhance the support effect and improve the stability of the lifting platform 21.

[0058] In this embodiment, as a preferred implementation, see [reference needed]. Figure 2 and Figure 3 As shown, the first support unit 221 includes a first support beam 2211 and a second support beam 2212 disposed between the second tower column 112 and the first platform longitudinal beam 211, and multiple first reinforcing beams 2213 disposed between the first support beam 2211 and the second support beam 2212. The second support beam 2212 is located below the first support beam 2211. The second support unit 222 includes a third support beam 2221 and a fourth support beam 2222 disposed between the third tower column 113 and the second platform longitudinal beam 212, and multiple second reinforcing beams 2223 disposed between the third support beam 2221 and the fourth support beam 2222. The fourth support beam 2222 is located below the third support beam 2221.

[0059] Thus, by setting multiple support beams in a support unit and adding multiple reinforcing beams between the multiple support beams, the structural strength of the support beam assembly 22 can be effectively increased, and the support effect of the support beam assembly 22 can be enhanced. In addition, the multiple support beam assemblies 2 arranged can enhance the overall structural stability of the take-off and landing platform 21.

[0060] In this embodiment, as a preferred implementation, such as Figure 2 , Figure 3 and Figure 5As shown, the first support beam 2211, the second support beam 2212, and multiple first reinforcing beams 2213 form multiple triangular structures, and the third support beam 2221, the fourth support beam 2222, and multiple second reinforcing beams 2223 also form multiple triangular structures. It can be understood that by forming multiple triangular structures between the first support beam 2211, the second support beam 2212, and the multiple first reinforcing beams 2213, and similarly between the third support beam 2221, the fourth support beam 2222, and the multiple second reinforcing beams 2223, the high strength of the triangular structures can be utilized to enhance the structural strength of the support beam assembly 22.

[0061] Furthermore, the end of the second support beam 2212 furthest from the second tower column 112 is connected to the connection point between the first support beam 2211 and the second tower column 112, and the end of the fourth support beam 2222 furthest from the third tower column 113 is connected to the connection point between the third support beam 2221 and the third tower column 113. This arrangement allows for the construction of multiple triangular structures. For example, the first support beam 2211, the second support beam 2212, and the support of the first platform longitudinal beam 211 can form a triangular structure; the first support beam 2211, the second support beam 2212, and the support of the first platform longitudinal beam 211 can also form a triangular structure; and the first support beam 2211, the second support beam 2212, and the second tower column 112 can also form a triangular structure. By setting multiple triangular structures, the structural strength of the support beam assembly 22 can be strengthened, thereby enhancing the overall structural strength and improving the load-bearing capacity of the landing platform 21.

[0062] In this embodiment, as a preferred implementation, such as Figure 2 As shown, the cable-stayed beam assembly 23 includes a first cable-stayed beam assembly 231 disposed between the second tower column 112 and the first platform longitudinal beam 211, and a second cable-stayed beam assembly 232 disposed between the third tower column 113 and the second platform longitudinal beam 212.

[0063] By utilizing the first inclined beam assembly 231 and the second inclined beam assembly 232, with the first inclined beam assembly 231 positioned between the second tower column 112 and the first platform longitudinal beam 211, and the second inclined beam assembly 232 positioned between the third tower column 113 and the second platform longitudinal beam 212, the first and second inclined beam assemblies 231 and 232 can cooperate with the first support unit 221 and the second support unit 222 to transfer and distribute the gravity of the lifting platform 21, thereby enhancing the pulling effect of the inclined beams and improving the structural stability of the lifting platform 21.

[0064] In this embodiment, as a preferred implementation, such as Figure 2 and Figure 3As shown, the connection point between the first cable-stayed beam assembly 231 and the first platform longitudinal beam 211 is located between the connection point between the second tower column 112 and the first support unit 221 and the first platform longitudinal beam 211. The connection point between the second cable-stayed beam assembly 232 and the second platform longitudinal beam 212 is located between the connection point between the third tower column 113 and the second support unit 222 and the second platform longitudinal beam 212.

[0065] The connection point between the first cable-stayed beam assembly 231 and the first platform longitudinal beam 211 is located between the connection point between the second tower column 112 and the first support unit 221 and the first platform longitudinal beam 211. The connection point between the second cable-stayed beam assembly 232 and the second platform longitudinal beam 212 is located between the connection point between the third tower column 113 and the second support unit 222 and the second platform longitudinal beam 212. By staggering the connection points, multiple force transmission channels can be built, which is more conducive to the transmission and distribution of the load-bearing force of the lifting platform 21 and improves the pulling effect of the cable-stayed beam assembly 22.

[0066] In this embodiment, as a preferred implementation, such as Figure 2 and Figure 4 As shown, the main body of the tower 1 includes a third inclined beam assembly 233 located between the first tower column 111 and the third transverse reinforcing beam 1213, with the third inclined beam assembly 233 situated above the transverse beam assembly 12. Furthermore, the third inclined beam assembly 233, which connects the first tower column 111 and the third transverse beam, further enhances the tensile strength of the inclined beam assembly 22, disperses the gravity of the landing platform 21, and improves the structural stability of the landing platform 21.

[0067] Specifically, the connection point between the third cable-stayed beam assembly 233 and the third transverse reinforcing beam 1213 is located at the midpoint of the third transverse reinforcing beam 1213, making the force more uniform and avoiding deformation or breakage of the third transverse reinforcing beam 1213 due to uneven force, which would cause instability of the lifting platform 21.

[0068] Furthermore, in this embodiment, the crossbeams and diagonal beams or the crossbeams and crossbeams are all connected by a detachable method, which facilitates the assembly and maintenance of the communication tower and UAV airport 2, effectively reduces the construction difficulty of the communication tower and UAV airport 2, increases the construction speed of the communication tower, and also helps to reduce manufacturing costs.

[0069] In addition, a ladder 14 is provided on the main body of the tower 1, and an opening 215 is provided on the support net 214 near the third transverse reinforcing beam 1213, with the opening 215 corresponding to the ladder 14. This facilitates the maintenance of the communication tower and the UAV airport 2 by staff, improves the convenience of equipment maintenance, and also helps to reduce maintenance risks and improve maintenance safety.

[0070] In this embodiment, as a preferred implementation, the height h of the take-off and landing platform 21 on the main body of the tower 1 is between 4 and 6 meters. Setting the take-off and landing platform 21 between 4 and 6 meters can avoid the disadvantages of the take-off and landing being inconvenient due to excessive high-altitude wind force affecting the stability of the UAV during landing, interference between the UAV rotor and antenna during take-off and landing, etc., caused by the take-off and landing platform 21 being too high. 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 installation height of the take-off and landing platform 21 being too high.

[0071] In addition, it is worth mentioning that if the altitude 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 altitude of the take-off and landing platform 21 should not be set too low.

[0072] Similarly, in practice, the drone cabin 4 should be at least 2 meters away from the tower 1 during installation to avoid interference between the airflow generated by the drone during takeoff and landing and the tower 1, which would affect flight safety.

[0073] In detail, the tower body 1 has a total height of 35m and a total weight of 5.72 tons. The lifting platform 21 is located 5m above the ground, and connecting plates are welded to the tower column 11 of the tower body 1 at 3m, 4m, 5m, and 7m. At the 4m and 5m installation connecting plates, two layers of support beam assemblies 22 made of angle steel are installed, and the two layers of angle steel diagonal braces are reinforced by four reinforcing beams made of angle steel. The lifting platform 21 is installed on the installation connecting plate at 6m. At the 7.5m installation connecting plate, two layers of diagonal tie beam assemblies 23 made of angle steel are installed to reinforce the lifting platform 21. All longitudinal and transverse beams constituting the lifting platform 21 are made of angle steel. The lifting platform 21 is approximately 3.2m long and 1.2m wide.

[0074] The communication triple-tube tower described in this utility model can solve the problem of installing UAVs on towers without affecting the load-bearing capacity of the communication antenna, enabling the communication triple-tube tower to have the function of a UAV airport, thereby empowering the existing communication triple-tube tower. At the same time, the take-off and landing platform 21 structure has high stability.

[0075] 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 three-tube communication tower, characterized in that: It includes a tower body (1) with three tower columns (11), a transverse beam assembly (12) on the tower body (1), and a drone airport (2) on one side of the tower body (1); The transverse beam assembly (12) includes a transverse reinforcing beam (121) disposed between two adjacent tower columns (11); The unmanned aerial vehicle airport (2) includes a take-off and landing platform (21) mounted on one of its transverse reinforcing beams (121), and a support beam assembly (22) and / or a cable tie beam assembly (23) disposed between the take-off and landing platform (21) and the main body of the tower (1). The take-off and landing platform (21) is located on one side of the main body of the tower, the support beam assembly (22) is located below the take-off and landing platform (21), and the cable tie beam assembly (23) is located above the take-off and landing platform (21).

2. The communication triplex tower according to claim 1, characterized in that: The multiple tower columns (11) include a first tower column (111), a second tower column (112), and a third tower column (113); Multiple transverse reinforcing beams (121) are located in the same horizontal plane and include a first transverse reinforcing beam (1211) between the first tower column (111) and the second tower column (112), a second transverse reinforcing beam (1212) between the first tower column (111) and the third tower column (113), and a third transverse reinforcing beam (1213) between the second tower column (112) and the third tower column (113), and the lifting platform (21) is located on the third transverse reinforcing beam (1213).

3. The communication three-tube tower according to claim 2, characterized in that: The take-off and landing platform (21) includes a first platform longitudinal beam (211) and a second platform longitudinal beam (212) spaced apart on the third transverse reinforcing beam (1213), and multiple platform crossbeams (213) between the first platform longitudinal beam (211) and the second platform longitudinal beam (212). The first platform longitudinal beam (211) and the second platform longitudinal beam (212) both extend horizontally away from the first tower column (111), and a support net (214) is provided on the frame formed by the first platform longitudinal beam (211), the second platform longitudinal beam (212) and each of the platform crossbeams (213). The unmanned aerial vehicle (UAV) cabin (4) is provided on the support net (214).

4. The communication three-tube tower according to claim 3, characterized in that: The support beam assembly (22) includes a first support unit (221) disposed between the second tower column (112) and the first platform longitudinal beam (211), and a second support unit (222) disposed between the third tower column (113) and the second platform longitudinal beam (212).

5. The communication three-tube tower according to claim 4, characterized in that: The first support unit (221) includes a first support beam (2211) and a second support beam (2212) disposed between the second tower column (112) and the first platform longitudinal beam (211), and multiple first reinforcing beams (2213) disposed between the first support beam (2211) and the second support beam (2212), wherein the second support beam (2212) is located below the first support beam (2211); and / or, The second support unit (222) includes a third support beam (2221) and a fourth support beam (2222) disposed between the third tower column (113) and the second platform longitudinal beam (212), and multiple second reinforcing beams (2223) disposed between the third support beam (2221) and the fourth support beam (2222), wherein the fourth support beam (2222) is located below the third support beam (2221).

6. The communication triplex tower according to claim 5, characterized in that: The first support beam (2211), the second support beam (2212), and multiple first reinforcing beams (2213) form multiple triangular structures, and the third support beam (2221), the fourth support beam (2222), and multiple second reinforcing beams (2223) also form multiple triangular structures; and / or, The end of the second support beam (2212) away from the second tower column (112) is connected to the connection point between the first support beam (2211) and the second tower column (112), and the end of the fourth support beam (2222) away from the third tower column (113) is connected to the connection point between the third support beam (2221) and the third tower column (113).

7. The communication three-tube tower according to claim 4, characterized in that: The cable-stayed beam assembly (23) includes a first cable-stayed beam (231) disposed between the second tower column (112) and the first platform longitudinal beam (211), and a second cable-stayed beam (232) disposed between the third tower column (113) and the second platform longitudinal beam (212).

8. The communication three-tube tower according to claim 7, characterized in that: The connection point between the first cable-stayed beam (231) and the first platform longitudinal beam (211) is located between the second tower column (112) and the connection point between the first support unit (221) and the first platform longitudinal beam (211); The connection point between the second inclined beam (232) and the second platform longitudinal beam (212) is located between the connection point between the third tower column (113) and the second support unit (222) and the second platform longitudinal beam (212).

9. The communication three-tube tower according to claim 3, characterized in that: The main body of the tower (1) includes a third diagonal bracing beam (233) disposed between the first tower column (111) and the third transverse reinforcing beam (1213), the third diagonal bracing beam (233) being located above the transverse beam assembly (12); and / or, The tower body (1) is provided with a ladder (14), and the support net (214) is provided with an opening (215) arranged near the third transverse reinforcing beam (1213), and the opening (215) is provided corresponding to the ladder (14).

10. The communication triplex tower according to any one of claims 1 to 9, characterized in that: The height h of the lifting platform (21) on the main body of the tower (1) is between 4 and 6 m.

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