Container with satellite communication function

By introducing structures such as fresh air circulation equipment, liquid cooling equipment and thermal insulation layer into the communication container, the temperature and humidity adjustment problems are solved, ensuring that the equipment is not damaged in harsh environments, and the stability and mobility of the container are improved.

CN223086708UActive Publication Date: 2025-07-11HAMI TIANCAO TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202422220758.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-09-10
Publication Date
2025-07-11
Estimated Expiration
2034-09-10

AI Technical Summary

Technical Problem

Existing communication containers are difficult to ensure temperature and humidity regulation, and satellite communication equipment is easily eroded by harsh environments, resulting in equipment damage.

Method used

A container with satellite communication is designed, including fresh air circulation equipment, liquid cooling equipment, heat insulation and moisture-proof layer, combined with sealed rings and flip motors, to achieve stable control of the internal environment and reliable storage of the equipment.

Benefits of technology

It realizes stable adjustment of the internal environment of the container, improves the stability and mobility of the equipment, and protects satellite communication equipment from external environment.

✦ Generated by Eureka AI based on patent content.

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  • Figure CN223086708U_ABST
    Figure CN223086708U_ABST
Patent Text Reader

Abstract

The utility model provides a container with a satellite communication function, and belongs to the technical field of containers. The container with the satellite communication function comprises a container body, an external hanging bin, a stacking groove, embedded supporting legs and an arc platform, the external hanging bin is fixedly connected to the exterior of the container body, the stacking groove is formed in the top of the container body, the embedded supporting legs are fixedly connected to the bottom of the container body, and subdivision partition plates are fixedly connected to the interior of the container body; the interior of the container body is divided into a cooling cabin, an equipment cabin and an operation cabin by the subdivision partition plates, a sealing ring is fixedly connected to the top of the operation cabin, a turnover motor is fixedly connected into the operation cabin, the arc platform is fixedly connected to the end of a transmission shaft of the turnover motor, and satellite communication equipment is fixedly connected to the outside of the arc platform. The satellite communication equipment storage device has the advantages of being capable of providing appropriate and stable humidity and air circulation for internal equipment of the device and facilitating storage of the satellite communication equipment.
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Description

Technical Field

[0001] The utility model relates to the technical field of containers, and particularly relates to a container with satellite communication. Background Art

[0002] A communication container is a standardized large container specially used for loading communication equipment. It is usually made of steel or other strong materials and has functions such as waterproof, dustproof, and moisture-proof, which can protect the internal communication equipment from the external environment. The communication container also has good mobility and can be quickly deployed to any place as needed. It is widely used in the fields of mobile communication, satellite communication, emergency communication, etc. However, most of the existing communication containers are modified based on ordinary containers, and it is difficult to ensure the internal temperature and humidity adjustment. Moreover, most of the equipment for satellite communication is directly installed outside the container, which is easily damaged under long-term exposure to wind, sun, and erosion by harsh environments. Therefore, this application provides a container with satellite communication. Summary of the Utility Model

[0003] To solve the above technical problems, the utility model proposes a satellite communication container that can provide a suitable and stable humidity and air circulation for the internal equipment of the device and facilitate the storage of satellite communication equipment.

[0004] The technical solution of the utility model is realized as follows:

[0005] A container with satellite communication includes a container main body, an external hanging bin, a stacking groove, fitting feet, and an arc platform. Among them, the external hanging bin is fixedly connected to the outside of the container main body, the stacking groove is opened at the top of the container main body, the fitting feet are fixedly connected to the bottom of the container main body, a partition board is fixedly connected inside the container main body, and the partition board divides the interior of the container main body into a cooling compartment, an equipment compartment, and an operation compartment. A sealing ring is fixedly connected to the top of the operation compartment, a flipping motor is fixedly connected inside the operation compartment, the arc platform is fixedly connected to the end of the transmission shaft of the flipping motor, and a satellite communication device is fixedly connected to the outside of the arc platform.

[0006] Furthermore, a top net is fixedly connected to the outside of the external hanging bin, side nets are fixedly connected to the sides of the external hanging bin, a stabilizing frame is fixedly connected to the outside of the side nets, a fresh air circulation device is fixedly connected to the inside of the external hanging bin. There are two groups of external hanging bins symmetrically distributed on the outside of the container main body, two groups of fresh air circulation devices symmetrically distributed inside the external hanging bins, and two groups of side nets symmetrically distributed on the outside of the external hanging bins.

[0007] Furthermore, a liquid cooling device is fixedly connected to the inside of the cooling compartment, and there are two groups of liquid cooling devices symmetrically distributed inside the cooling compartment.

[0008] Furthermore, an equipment rack is fixedly connected inside the equipment cabin. A communication device is movably connected to the outside of the equipment rack. The communication device is interconnected with the liquid cooling device. There are two groups of equipment racks symmetrically distributed inside the equipment cabin. There are multiple groups of communication devices evenly distributed inside the equipment rack.

[0009] Furthermore, one end of the arc platform far from the satellite communication device is fixedly connected with an anti-accumulation arc surface. The height of the satellite communication device is lower than the diameter of the sealing ring. The radian of the anti-accumulation arc surface is smaller than that of the sealing ring.

[0010] Furthermore, a bottom layer beam is fixedly connected to the bottom of the container main body. A moisture-proof layer is movably connected between the bottom layer beam and the container main body. The moisture-proof layer is laid on the bottoms of the cooling cabin, equipment cabin, and operation cabin as a whole. A heat-insulating layer is movably connected to the top and both sides inside the container main body. The heat-insulating layer wraps the periphery of the cooling cabin, equipment cabin, and operation cabin. A decorative layer is fixedly connected to the bottom of the container main body.

[0011] Furthermore, the fitting feet and the stacking grooves are mutually fitted and connected. Connecting grooves are opened on the outside of both the stacking grooves and the fitting feet. There are multiple groups of stacking grooves evenly distributed at the corners of the container main body and the external hanging bin.

[0012] Furthermore, hatch doors are fixedly connected to the outside of the cooling cabin and the operation cabin. A boarding ladder is detachably connected to the outside of the hatch doors.

[0013] The utility model has the following beneficial effects:

[0014] 1. By setting the fresh air circulation device, liquid cooling device, equipment rack, heat-insulating layer, and moisture-proof layer, the inside of the device simultaneously undergoes fresh air circulation and liquid cooling circulation, thereby adjusting and stabilizing the temperature inside the container main body in real time, providing a good environment for the equipment inside the device, and blocking external moisture and bad weather, greatly improving the stability of the device.

[0015] 2. By setting the sealing ring, flipping motor, arc platform, and satellite communication device, the device can perform accurate positioning and reliable satellite communication at any location, and can be stored when the weather is bad or it is idle, improving the mobility and adaptability of the equipment. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 is the overall structural schematic diagram of the utility model;

[0017] Figure 2 is the overall structural schematic diagram of the utility model;

[0018] Figure 3It is a schematic diagram of the overall structure of the present utility model;

[0019] Figure 4 It is an anatomical diagram of the internal structure of the present utility model;

[0020] Figure 5 It is a schematic diagram of a partial structure of the present utility model.

[0021] Wherein: 1. Container main body; 2. External hanging bin; 3. Top net; 4. Side net; 5. Stabilizing frame; 6. Fresh air circulation device; 7. Stacking groove; 8. Fitting support feet; 9. Connecting groove; 10. Compartment partition; 11. Cooling compartment; 12. Equipment compartment; 13. Operation compartment; 14. Liquid cooling equipment; 15. Equipment rack; 16. Communication equipment; 17. Sealing ring; 18. Tipping motor; 19. Arc platform; 20. Arc prevention surface; 21. Satellite communication equipment; 22. Heat insulation layer; 23. Bottom beam; 24. Moisture-proof layer; 25. Decorative layer; 26. Cabin door; 27. Embarkation ladder. Specific embodiments

[0022] Next, the technical solutions in the embodiments of the present utility model will be described clearly and completely. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the protection scope of the present utility model.

[0023] Please refer to Figures 1 to 5 As shown, a container with satellite communication provided by the present utility model includes a container main body 1, an external hanging bin 2, a stacking groove 7, fitting support feet 8, and an arc platform 19. Among them, the external hanging bin 2 is fixedly connected to the outside of the container main body 1, the stacking groove 7 is opened at the top of the container main body 1, the fitting support feet 8 are fixedly connected to the bottom of the container main body 1, a compartment partition 10 is fixedly connected inside the container main body 1, and the compartment partition 10 divides the inside of the container main body 1 into a cooling compartment 11, an equipment compartment 12, and an operation compartment 13. A sealing ring 17 is fixedly connected to the top of the operation compartment 13, a tipping motor 18 is fixedly connected inside the operation compartment 13, the arc platform 19 is fixedly connected to the end of the transmission shaft of the tipping motor 18, and a satellite communication equipment 21 is fixedly connected to the outside of the arc platform 19;

[0024] An external storage bin 2 is fixedly connected to a top-facing net 3 externally, a side net 4 is fixedly connected to the side of the external storage bin 2, a stabilizing frame 5 is fixedly connected to the outside of the side net 4, a fresh air circulation device 6 is fixedly connected to the inside of the external storage bin 2. There are two groups of external storage bins 2 and they are symmetrically distributed outside the container main body 1. There are two groups of fresh air circulation devices 6 and they are symmetrically distributed inside the external storage bin 2. There are two groups of side nets 4 and they are symmetrically distributed outside the external storage bin 2. A liquid cooling device 14 is fixedly connected to the inside of the cooling compartment 11. There are two groups of liquid cooling devices 14 and they are symmetrically distributed inside the cooling compartment 11. An equipment rack 15 is fixedly connected to the inside of the equipment compartment 12. A communication device 16 is movably connected to the outside of the equipment rack 15. The communication device 16 is connected to the liquid cooling device 14. There are two groups of equipment racks 15 and they are symmetrically distributed inside the equipment compartment 12. There are multiple groups of communication devices 16 and they are evenly distributed inside the equipment rack 15.

[0025] Specifically, after the container main body 1 is placed in the target area, the fresh air circulation device 6 circulates the air inside the cooling compartment 11, the equipment compartment 12, and the operation compartment 13 to ensure a healthy air environment inside the container main body 1. At the same time, the liquid cooling device 14 is connected to the communication device 16 to control the temperature inside the communication device 16. And in humid weather, the moisture-proof layer 24 separates the moisture from the inside of the container main body 1. In hot weather, the heat-insulating layer 22 isolates the high temperature from the inside of the container main body 1, greatly improving the stability of the device operation.

[0026] Furthermore, one end of the arc platform 19 away from the satellite communication device 21 is fixedly connected to an arc-preventing surface 20. The height of the satellite communication device 21 is lower than the diameter of the sealing ring 17. The radian of the arc-preventing surface 20 is smaller than that of the sealing ring 17. The bottom of the container main body 1 is fixedly connected to a bottom layer beam 23. A moisture-proof layer 24 is movably connected between the bottom layer beam 23 and the container main body 1. The moisture-proof layer 24 is laid on the bottoms of the cooling compartment 11, the equipment compartment 12, and the operation compartment 13 as a whole. A heat-insulating layer 22 is movably connected to the top and both sides inside the container main body 1. The heat-insulating layer 22 wraps the peripheries of the cooling compartment 11, the equipment compartment 12, and the operation compartment 13. The bottom of the container main body 1 is fixedly connected to a decorative layer 25. The fitting feet 8 and the stacking grooves 7 are fitted and connected to each other. Connection grooves 9 are provided on the outsides of both the stacking grooves 7 and the fitting feet 8. There are multiple groups of stacking grooves 7 and they are evenly distributed at the corners of the container main body 1 and the external storage bin 2. Hatches 26 are fixedly connected to the outsides of the cooling compartment 11 and the operation compartment 13. A boarding ladder 27 is detachably connected to the outside of the hatch 26.

[0027] By making the above settings, when the device needs to perform satellite positioning communication, the flipping motor 18 is turned on to drive the communication device 16 to rotate. After the satellite communication device 21 outside the arc platform 19 rotates out of the sealing ring 17, satellite communication operations can be carried out. When the satellite communication device 21 is idle, the flipping motor 18 is turned on again to store the satellite communication device 21 inside the operation cabin 13. At the same time, the satellite communication device 21 fits against the outer edge of the sealing ring 17, dispersing the accumulated water and debris outside it, preventing debris from accumulating outside the sealing ring 17, and greatly improving the mobility and adaptability of the device.

[0028] The above are only the preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent replacements, 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 container with satellite communication, characterized in that, It includes a container main body (1), an external hanging bin (2), a stacking groove (7), a fitting support leg (8), and an arc platform (19). Among them, the external hanging bin (2) is fixedly connected to the outside of the container main body (1), the stacking groove (7) is opened at the top of the container main body (1), the fitting support leg (8) is fixedly connected to the bottom of the container main body (1), a compartment partition board (10) is fixedly connected inside the container main body (1), and the compartment partition board (10) divides the inside of the container main body (1) into a cooling compartment (11), an equipment compartment (12), and an operation compartment (13). A sealing ring (17) is fixedly connected to the top of the operation compartment (13), a turning motor (18) is fixedly connected inside the operation compartment (13), the arc platform (19) is fixedly connected to the end of the transmission shaft of the turning motor (18), and a satellite communication device (21) is fixedly connected to the outside of the arc platform (19).

2. The container with satellite communication according to claim 1, characterized in that, A top net (3) is fixedly connected to the outside of the external hanging bin (2), a side net (4) is fixedly connected to the side of the external hanging bin (2), a stabilizing frame (5) is fixedly connected to the outside of the side net (4), a fresh air circulation device (6) is fixedly connected inside the external hanging bin (2), there are two groups of the external hanging bins (2) and they are symmetrically distributed on the outside of the container main body (1), there are two groups of the fresh air circulation devices (6) and they are symmetrically distributed inside the external hanging bins (2), and there are two groups of the side nets (4) and they are symmetrically distributed on the outside of the external hanging bins (2).

3. A container with satellite communication according to claim 1, characterized in that, A liquid cooling device (14) is fixedly connected inside the cooling compartment (11), and there are two groups of the liquid cooling devices (14) and they are symmetrically distributed inside the cooling compartment (11).

4. The container with satellite communication according to claim 3, characterized in that, An equipment rack (15) is fixedly connected inside the equipment compartment (12), a communication device (16) is movably connected to the outside of the equipment rack (15), the communication device (16) is connected to the liquid cooling device (14), there are two groups of the equipment racks (15) and they are symmetrically distributed inside the equipment compartment (12), and there are multiple groups of the communication devices (16) and they are evenly distributed inside the equipment racks (15).

5. A container with satellite communication according to claim 1, characterized in that, One end of the arc platform (19) away from the satellite communication device (21) is fixedly connected to an anti-accumulation arc surface (20), the height of the satellite communication device (21) is lower than the diameter of the sealing ring (17), and the radian of the anti-accumulation arc surface (20) is smaller than that of the sealing ring (17).

6. The container with satellite communication according to claim 1, characterized in that, A bottom layer beam (23) is fixedly connected to the bottom of the container main body (1), a moisture-proof layer (24) is movably connected between the bottom layer beam (23) and the container main body (1), the moisture-proof layer (24) is laid as a whole at the bottoms of the cooling compartment (11), the equipment compartment (12), and the operation compartment (13), a heat-insulating layer (22) is movably connected to the top and both sides inside the container main body (1), the heat-insulating layer (22) wraps the peripheries of the cooling compartment (11), the equipment compartment (12), and the operation compartment (13), and a decorative layer (25) is fixedly connected to the bottom of the container main body (1).

7. A container with satellite communication according to claim 1, characterized in that, The fitting foot (8) is fitted and connected with the stacking groove (7). Connecting grooves (9) are provided on the outer sides of both the stacking groove (7) and the fitting foot (8). There are multiple groups of stacking grooves (7) which are evenly distributed at the corners of the container body (1) and the external hanging bin (2).

8. A container with satellite communication according to claim 1, characterized in that, A hatch door (26) is fixedly connected to the outer sides of the cooling cabin (11) and the operation cabin (13). An embarkation ladder (27) is detachably connected to the outer side of the hatch door (26).