Military 200kg level cargo carrying square cabin

CN120171950BActive Publication Date: 2026-10-23SHANGHAI GEBANG AUTOMATION CO LTD
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Patent Information

Application Number
CN202510502921.6
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-04-22
Publication Date
2026-10-23
Estimated Expiration
2045-04-22

AI Technical Summary

Technical Problem

[0003]本申请提供一种军用200kg级载货方舱,用以解决现有技术中载货方舱在防护性能、空间利用、运输稳定性及运输工具适配性等方面存在的问题,以满足现代军事行动对物资高效运输与妥善存储的严格要求

Benefits of technology

1、增强其抗冲击、防腐蚀、防水、防尘、防弹以及防火等能力,确保内部物资安全,解决传统方舱外壳防护等级不足导致物资损坏的问题;

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Abstract

The application discloses a 200kg-level cargo carrying square cabin for military use, and provides an integrated innovative solution for the problems of low space utilization, poor transportation stability and weak transportation tool adaptability in the prior art. The core structure comprises the following: a bottom plate adopting a magnesium alloy light-weight bulletproof armor combined with a truss frame, an elastic support rod assembly built in the vertical pipe of the frame, a spiral groove-sliding sleeve type pull rope device for realizing quick hoisting self-adaptive buffering, a conical spring support foot and a multilayer spring-pad cylinder elastic assembly arranged at the two ends of the support rod, and a three-dimensional damping system formed by the conical spring support foot and the multilayer spring-pad cylinder elastic assembly. The cabin body is made of a lightweight magnesium alloy plate and a nanoscale waterproof cloth, and is provided with a gravity sensor, a positioning device and a cloud service monitoring system. The square cabin has multilevel impact resistance, corrosion resistance, waterproofness and bulletproof capability, can adapt to the damping requirements of complex transportation working conditions, solves the interface compatibility problem of various transportation tools, and realizes real-time monitoring and early warning of the state of the materials.
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Description

Technical Field

[0001] This invention relates to the field of military equipment technology, specifically to a military 200kg-class cargo container. Background Technology

[0002] As is well known, in modern military operations, the efficient transportation and proper storage of supplies are crucial to ensuring the successful execution of missions. Military missions often involve a variety of complex scenarios, from terrain-challenged areas such as mountains and jungles to harsh environments such as oceans and deserts, all requiring reliable cargo transport equipment for the transfer and temporary storage of supplies. As a core piece of military equipment undertaking this important task, the performance of cargo containers directly affects the efficiency and success of military operations. The need for a cargo capacity of 200kg or more is common in military operations. For example, resupplying small combat units at the front lines requires transporting various critical supplies, including weapons and ammunition, medical supplies, and communication equipment, with a total weight typically around 200kg. However, existing containerized units designed for this cargo capacity have many problems that urgently need to be addressed. From a protective performance perspective, existing containerized shelters are ill-equipped to withstand the complex and ever-changing battlefield environment and numerous threats. During field transport, they may encounter scratches from branches, impacts from rocks, etc. Ordinary containerized shelter shell materials cannot effectively resist such damage, leading to shelter breakage and threatening the safety of internal supplies. Furthermore, under extreme weather conditions, such as heavy rain and sandstorms, if the shelter lacks adequate waterproofing and dustproofing, internal supplies are prone to moisture and dust ingress, affecting their normal use. In addition, existing containerized shelter protective structures are insufficient to provide reliable protection against potential ignition sources and corrosive substances, failing to meet the stringent requirements for supply safety in military operations. In terms of space utilization, the existing 200kg-class cargo container's internal structural design lacks rationality. On the one hand, fixed cargo storage areas cannot flexibly adapt to goods of different shapes and sizes, resulting in serious space waste and low loading efficiency. For example, when transporting irregularly shaped medical equipment or large communication equipment, the unreasonable layout of the container often prevents full utilization of the space, leaving some space idle, while the actual amount of materials that can be loaded is far lower than the container's theoretical carrying capacity. On the other hand, the lack of an effective cargo classification and storage design within the container leads to various materials being mixed together, which not only increases the difficulty of loading and unloading but also makes them prone to damage due to collisions during transportation. Transportation stability is also a major shortcoming of existing containerized transport units. In military transport, road conditions are often extremely harsh, with bumpy and undulating terrain being commonplace. Existing containerized transport units are severely inadequate in terms of shock absorption and securing measures, lacking effective shock absorption devices and failing to effectively buffer vibrations during transport. This causes frequent shaking and collisions of cargo within the unit, easily leading to damage. Furthermore, the securing methods between the containerized unit and the transport vehicle are unreliable during transport, making it prone to displacement during sudden braking, turns, etc., potentially causing the containerized unit to fall off the transport vehicle and resulting in serious safety accidents. Additionally, when lifting the containerized unit by air, the ropes deform under tension; if the tension is too great or applied too quickly, it may exceed the rope's elastic limit, causing it to break. Furthermore, the diversity of modern military operations demands that cargo containers be highly adaptable to various transport vehicles. However, existing containers perform poorly in this regard. Different types of transport vehicles, such as military trucks, transport aircraft, and helicopters, have different loading interfaces and securing methods, while existing containers often only accommodate one or a few types of transport vehicles, failing to flexibly meet the needs of rapid switching between transport modes in military operations. This limits the flexibility of material transport, and in emergencies, the inability to find suitable transport vehicles in a timely manner may delay the delivery of materials, affecting the execution of military missions. Therefore, existing 200kg-class cargo containers have many shortcomings in terms of protection, space utilization, transport stability, and adaptability to transport vehicles, and can no longer meet the growing needs of modern military operations. Thus, developing a new type of military 200kg-class cargo container with superior performance is of paramount importance and is urgently needed. Summary of the Invention

[0003] This application provides a military 200kg-class cargo container to solve the problems existing in the prior art in terms of protective performance, space utilization, transportation stability and adaptability to transportation vehicles, so as to meet the strict requirements of modern military operations for efficient transportation and proper storage of materials.

[0004] To achieve the above objectives, the technical solution adopted by the present invention is as follows: A military-grade 200kg cargo container includes: a base plate and a frame mounted on the base plate. The frame includes: horizontal bars and vertical tubes. Each horizontal bar bears lateral load transmission and support within the frame, and each vertical tube bears vertical load transmission and support within the frame. The vertical tube has a hollow structure, with a through-hole top cover at the top end and a through-hole bottom cover at the bottom end. A support rod is provided within the hollow structure of the vertical tube, penetrating the vertical tube. A support rod retaining ring is provided on the outer side of the support rod, located in the hollow structure portion. Elastic components are provided between the support rod retaining ring and the through-hole top cover and the through-hole bottom cover, respectively. The top of the support rod protruding from the top cover of the through hole is provided with a pull rope assembly, and the bottom of the support rod protruding from the bottom cover of the through hole is provided with a support foot. The vertical tube with the built-in support rod is located on the side of the frame. The vertical tube with the built-in support rod elastically supports the frame. When the frame is lifted, the vertical tube with the built-in support rod can buffer the lifting speed and protect the pull rope assembly.

[0005] The aforementioned military 200kg-class cargo container includes a rope assembly comprising: a sliding sleeve and a rope body. The top of the support rod protruding from the outer side of the through-hole top cover is provided with a spiral groove. A spiral block is provided inside the sliding sleeve, and the spiral block matches the spiral groove. Both ends of the rope body are connected to the sliding sleeve.

[0006] The aforementioned military 200kg class cargo container, wherein the top of the support rod is also provided with a first retaining ring, the first retaining ring being located between the spiral groove and the through hole top cover; The bottom of the support rod is also provided with a second retaining ring, which is located between the support foot and the through hole bottom cover; Both the side of the first retaining ring facing the top cover of the through hole and the side of the second retaining ring facing the bottom plate of the through hole are provided with buffer pads.

[0007] The aforementioned military 200kg class cargo container, wherein the elastic component includes: a pad and a spring, the pad and the spring being sleeved on the outside of the support rod, and the pad and the spring being located in the upper space between the support rod retaining ring and the through hole top cover; The pad and the spring are located in the lower space between the support rod retaining ring and the through hole bottom cover; The number of the pads in the upper space is one or more; The number of springs in the upper space is one or more; The number of the pads in the lower space is one or more; The number of springs in the lower space is one or more; The support rod moves elastically within the vertical tube.

[0008] In the aforementioned military 200kg-class cargo container, the through-hole bottom cover is welded to the vertical pipe.

[0009] The aforementioned military 200kg-class cargo container, wherein the supporting legs include: a first plate, a conical spring, and a top head. The first plate has a circular hole in the middle, the large-diameter end of the conical spring is connected to the first plate, and the small-diameter end of the conical spring is connected to the top head; The bottom end of the support rod passes through the circular hole, passes through the middle of the conical spring, and is fixedly connected to the top head; The top head is conical, the tip of the top head is round, and the waist of the top head is curved inward to form an arc.

[0010] In the aforementioned military 200kg-class cargo container, the sum of the distance between the through-hole bottom cover and the first plate and the distance between the retractions of the conical springs is less than the distance between the retractions of the springs.

[0011] The aforementioned military 200kg-class cargo container includes a large cover plate inside the top surface of the frame. The large cover plate and the bottom plate are made of magnesium alloy lightweight bulletproof armor. The outside of the frame is covered with a waterproof cloth. The large cover plate is connected to one side of the frame by one or more hinges. The large cover plate is connected to the frame on the side away from the hinge by one or more latches.

[0012] The aforementioned military 200kg-class cargo container has three or more supporting legs evenly distributed on the lower side of the floor plate.

[0013] The aforementioned military 200kg-class cargo container includes two or more gravity sensors evenly distributed between the frame and the base plate, and a battery storage box and a positioning device for signal transmission and reception are also provided inside the frame. The signal transceiver positioning device transmits signals to mobile or fixed terminals via cloud services.

[0014] The present invention provides a military-grade 200kg cargo container, which, by adopting the above-mentioned solution, has the following advantages: 1. Enhance its impact resistance, corrosion resistance, waterproofing, dustproofing, bulletproofing, and fireproofing capabilities to ensure the safety of internal materials and solve the problem of insufficient protection levels of traditional container shells leading to material damage; 2. Overcome the shortcomings of single damping structures in adapting to complex transportation conditions, and construct a multi-dimensional damping system to adapt to complex transportation conditions; 3. Eliminates the drawbacks of incompatibility between existing modular shelters and various types of transport vehicles, enabling rapid hooking and lifting with ropes, and the rotation of the ropes creates a small-distance self-locking mechanism to reduce swaying; 4. To prevent component breakage due to impact overload during hoisting, a real-time monitoring and early warning mechanism for material status should be established. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of a military-grade 200kg cargo container. Figure 2 A schematic diagram of the frame of a military 200kg-class cargo container; Figure 3 A schematic diagram of the vertical tube of a military 200kg-class cargo container; Figure 4 A schematic diagram of the rope assembly for a military 200kg-class cargo container; Figure 5 A schematic diagram of the rope assembly of a 200kg-class military cargo container after being stretched and twisted. Figure 6 This is a schematic diagram of a 200kg-class military cargo container's cushioning.

[0016] The reference numerals in the accompanying drawings are as follows: 1. Base plate; 2. Frame; 3. Horizontal bar; 4. Vertical pipe; 5. Through-hole top cover; 6. Through-hole bottom cover; 7. Support rod; 8. Support rod retaining ring; 9. Elastic component; 10. Support foot; 11. Pull rope assembly; 12. Sliding sleeve; 13. Rope body; 14. Spiral groove; 15. Spiral block; 16. First retaining ring; 17. Second retaining ring; 18. Buffer pad; 19. Pad cylinder; 20. Spring; 21. First plate; 22. Top head; 23. Large cover plate; 24. Waterproof cloth; 25. Hinge; 26. Lock; 27. Gravity sensor; 28. Positioning device; 29. ​​Battery box; 30. Fixed terminal; 31. Conical spring; 32. Pull hook. Detailed Implementation

[0017] To make the technical means, inventive features, objectives and effects of the invention easier to understand, the invention will be further explained below with reference to specific illustrations.

[0018] like Figure 1-2 As shown, the present invention provides a military 200kg-class cargo container, comprising: a base plate 1 and a frame 2 mounted on the base plate 1, wherein the frame 2 includes: crossbars 3 and vertical tubes 4, each crossbar 3 mainly bears the lateral load transfer and support in the frame 2, and each vertical tube 4 mainly bears the vertical load transfer and support in the frame 2, the crossbars 3 and vertical tubes 4 are welded together, and the rigidity of the overall frame 2 is enhanced by the welding connection.

[0019] like Figure 3As shown, the vertical tube 4 has a hollow structure. A through-hole top cover 5 is located at the top of the vertical tube 4, and a through-hole bottom cover 6 is located at the bottom of the vertical tube 4. Either the through-hole top cover 5 or the through-hole bottom cover 6 is detachably connected to the vertical tube 4, so that when either the through-hole top cover 5 or the through-hole bottom cover 6 is detached from the vertical tube 4, the support rod 7 and its elastic component 9 can be installed inside the vertical tube 4. The support rod 7 is fixed inside the vertical tube 4 under the support of the elastic component 9. When both ends of the support rod are subjected to tension or thrust, the support rod 7 moves within the vertical tube 4. The extreme positions of the support rod 7's displacement within the vertical tube are constrained by the first retaining ring 16 and the second retaining ring 17, respectively.

[0020] Furthermore, a support rod retaining ring 8 is provided on the outer side of the support rod 7. The support rod retaining ring 8 is located in the hollow structure. Elastic components 9 are provided between the support rod retaining ring 8 and the through hole top cover 5 and the through hole bottom cover 6, respectively. The two elastic components 9 can abut against the support rod retaining ring 8, so that the support rod 7 can be reset after passive displacement.

[0021] like Figure 3 As shown, the top of the support rod 7, protruding from the through-hole cover 5, is equipped with a rope assembly 11, and the bottom of the support rod 7, protruding from the through-hole cover 6, is equipped with a support foot 10. When airlifting or transporting the container, the entire frame 2 can be lifted simply by inserting a hook into the rope assembly 11. Once the container is transported to the designated location, it can be lowered. After the support foot 10 lands, the support rod 7 moves upward within the vertical tube 4, while the elastic component 9 provides the initial buffer force. If the load inside the frame 2 is too heavy (exceeding 200 kg), the second retaining ring 17 presses tightly against the through-hole cover 6, limiting the upward displacement of the support rod 7 and thus eliminating the downward potential energy of the frame 2. The support rod 7 then resets within the vertical tube 4. In another embodiment, a hydraulic damping buffer (not shown in the figure) is installed between the first retaining ring 16 and the through-hole cover 5. The hydraulic damping buffer absorbs impact energy through a throttling effect, while allowing the hydraulic fluid to slowly return during reset, reducing the rebound speed and preventing severe vibration of the cargo inside the frame 2. Based on... Figure 3 The vertical tube 4 in the middle is to be replaced Figure 2 The internal vertical tube structure is 4.

[0022] The vertical tube 4, with its built-in support rod 7, is located on the side of the frame 2. This vertical tube 4 provides elastic support to the frame 2. When the frame 2 is lifted, the vertical tube 4 with its built-in support rod 7 cushions the lifting speed and protects the rope assembly 11. The initial acceleration of lifting the entire frame 2 by inserting the hook into the rope assembly 11 can reach 3-5 times the acceleration due to gravity. The support rod 7 moves upward a certain distance within the vertical tube 4, providing a certain amount of cushioning to the rope and preventing it from breaking.

[0023] like Figure 4-6In the specific embodiment of the present invention shown, the pull rope assembly 11 includes: a sliding sleeve 12 and a rope body 13. A spiral groove 14 is provided on the outer side of the portion of the support rod 7 protruding from the through-hole top cover 5. A spiral block 15 is provided inside the sliding sleeve 12, matching the spiral groove 14. Both ends of the rope body 13 are connected to the sliding sleeve 12. Here, as the sliding sleeve 12 is lifted by the rope body 13, it rotates along the trajectory of the spiral groove 14. At this time, the rope body 13 will wrap around the pull hook 32, thus stabilizing the frame 2 and preventing it from swaying.

[0024] In a specific embodiment of the present invention, a first retaining ring 16 is provided at the top of the support rod 7, and the first retaining ring 16 is located between the spiral groove 14 and the through hole top cover 5. A second retaining ring 17 is provided at the bottom of the support rod 7, and the second retaining ring 17 is located between the support foot 10 and the through hole bottom cover 6. Here, the first retaining ring 16 is used to limit the downward displacement space of the support rod 7 in the vertical tube 4, which not only prevents the elastic component 9 in the vertical tube 4 from being damaged due to excessive pressure, but also provides a hydraulic damping buffer between the first retaining ring 16 and the through hole top cover 5 to delay the reset time and improve the stability of the support rod 7 in the vertical tube 4. Here, the second retaining ring 17 is used to limit the upward displacement space of the support rod 7 in the vertical tube 4, which not only prevents the elastic component 9 in the vertical tube 4 from being damaged due to excessive pressure, but also supports the frame 2 when the second retaining ring 17 is in close contact with the through hole bottom cover 6.

[0025] Both the first retaining ring 16 facing the top cover 5 of the through hole and the second retaining ring 17 facing the bottom plate 1 of the through hole are provided with buffer pads 18.

[0026] In a specific embodiment of the present invention, the elastic component 9 includes: a pad 19 and a spring 20. The pad 19 and the spring 20 are sleeved on the outside of the support rod 7, and the pad 19 and the spring 20 are located in the upper space between the support rod retaining ring 8 and the through hole top cover 5. The pad 19 and the spring 20 are located in the lower space between the support rod retaining ring 8 and the through hole bottom cover 6; like Figure 6 As shown, there is one or more pads 19 in the upper space; there is one or more springs 20 in the upper space; there is one or more pads 19 in the lower space; and there is one or more springs 20 in the lower space. The function of the pads 19 is to shorten the length of the springs 20. In addition, the pads 19 can also guide the support rod 7, which moves elastically within the vertical tube 4.

[0027] In a specific embodiment of the present invention, the through-hole bottom cover 6 and the vertical tube 4 need to be rigidly connected. Therefore, the through-hole bottom cover 6 is welded to the vertical tube 4, and the through-hole bottom cover 6 will not be damaged after being impacted by the second retaining ring 17.

[0028] In a specific embodiment of the present invention, the support foot 10 includes: a first plate 21, a conical spring 31, and a top head 22. The first plate 21 has a circular hole in the middle. The large diameter end of the conical spring 31 is connected to the first plate 21, and the small diameter end of the conical spring 31 is connected to the top head 22. The bottom end of the support rod 7 passes through the circular hole and passes through the middle of the conical spring 31 to be fixedly connected to the top head 22. Its support foot 10 can provide secondary elastic buffer protection for the frame 2 after the second retaining ring 17 and the through hole bottom cover 6 are rigidly abutted.

[0029] The top part 22 is conical, with a rounded tip and an inwardly curved waist. Its unique structure allows it to be quickly inserted into the soil for positioning in soft soil.

[0030] In a specific embodiment of the present invention, the sum of the distance between the through hole bottom cover 6 and the first plate 21 and the distance between the retraction of the conical spring 31 is less than the distance between the retraction of the spring 20.

[0031] In a specific embodiment of the present invention, a large cover plate 23 is provided inside the top surface of the frame 2. The large cover plate 23 and the base plate 1 are made of lightweight magnesium alloy bulletproof armor. The outside of the frame 2 is covered with a waterproof cloth 24. The large cover plate 23 is connected to one side of the frame 2 by one or more hinges 25, and the large cover plate 23 is connected to the side of the frame 2 away from the hinges 25 by one or more latches 26. The edge of the large cover plate 23 is sealed with silicone foam (compression 30%). When the large cover plate 23 is placed on the frame 2, it has good sealing performance, a waterproof rating of IP68, and can withstand the pressure of 1m water for 72 hours.

[0032] In a specific embodiment of the present invention, three or more support feet 10 are evenly distributed on the lower side of the base plate 1.

[0033] In a specific embodiment of the present invention, two or more gravity sensors 27 are evenly distributed between the frame 2 and the base plate 1. The frame 2 is also equipped with a battery tank 29 and a positioning device 28 for signal transmission and reception. The positioning device 28 transmits signals to a mobile terminal or a fixed terminal 30 through a cloud service. The battery tank 29 provides power to the gravity sensors 27 and the positioning device 28, and can also serve as an emergency reserve point.

[0034] In a specific embodiment of the present invention, the supporting substrate is: The base plate (1) and frame (2) are made of 5083-H321 aluminum alloy (GB / T 3190) with a thickness of 6mm, or are made of lightweight magnesium alloy plate.

[0035] The top cover plate (3) is made of 20mm thick homogeneous armor steel (GB / T 2039). The waterproof fabric consists of an outer layer and an inner layer. The outer layer is made of aramid fiber reinforced waterproof canvas (600g / m², tear strength ≥500N). The inner layer is a 5mm thick EVA cushioning layer (Shore hardness 40A). Positioning device: Load monitoring: 4 HX711 gravity sensors (range 0-300kg, accuracy ±0.3%) The pull rope assembly 11 has a lead angle of 25° for the inner spiral block (241) of the sliding sleeve (24) and the rope body (242) is made of aramid 1414 fiber (diameter 10mm, breaking strength ≥28cN / dtex).

[0036] Support leg assembly: Conical spring 42 parameters: large end diameter: 100mm, small end diameter: 40mm, effective number of coils: 8, stiffness coefficient: 800N / mm, top head 43 surface overlaid with chromium carbide (thickness 0.3mm), top: lifting ring conforming to MIL-STD-129B (safe working load 100kN).

[0037] In summary, this invention provides a 200kg-class military cargo container that enhances its impact resistance, corrosion resistance, waterproofing, dustproofing, bulletproofing, and fireproofing capabilities, ensuring the safety of internal materials and solving the problem of insufficient protection levels in traditional container shells leading to material damage. It overcomes the shortcomings of single shock-absorbing structures in adapting to complex transportation conditions by constructing a multi-dimensional shock-absorbing system. It eliminates the incompatibility issues between existing containers and various types of transport vehicles, enabling rapid rope lifting, and the rope rotation creates a small-distance self-locking mechanism to reduce swaying. It prevents component breakage due to impact overload during hoisting and establishes a real-time monitoring and early warning mechanism for material status.

[0038] The specific embodiments of the invention have been described above. It should be understood that the invention is not limited to the specific embodiments described above, and the devices and structures not described in detail should be understood to be implemented in a manner common to the art; those skilled in the art can make various modifications or alterations within the scope of the claims, and make several simple deductions, variations or substitutions, which do not affect the substantive content of the invention.

Claims

1. A military-grade 200kg cargo container, comprising: The base plate and the frame provided on the base plate are characterized in that the frame includes: horizontal bars and vertical tubes, each of the horizontal bars bears the lateral load transmission and support in the frame, each of the vertical tubes bears the vertical load transmission and support in the frame, the vertical tubes are hollow structures, the top end of the vertical tubes is provided with a through-hole top cover, the bottom end of the vertical tubes is provided with a through-hole bottom cover, a support rod is provided in the hollow structure of the vertical tubes, the support rod passes through the vertical tubes, a support rod retaining ring is provided on the outside of the support rods, the support rod retaining ring is located in the hollow structure, and elastic components are provided between the support rod retaining ring and the through-hole top cover and the through-hole bottom cover respectively; The top of the support rod protruding from the top cover of the through hole is provided with a pull rope assembly, and the bottom of the support rod protruding from the bottom cover of the through hole is provided with a support foot. The vertical tube with the built-in support rod is located on the side of the frame. The vertical tube with the built-in support rod elastically supports the frame. When the frame is lifted, the vertical tube with the built-in support rod can buffer the lifting speed and protect the pull rope assembly. The pull rope assembly includes: a sliding sleeve and a rope body. The top end of the support rod protruding from the outer side of the through hole cover is provided with a spiral groove. A spiral block is provided inside the sliding sleeve. The spiral block matches the spiral groove. Both ends of the rope body are connected to the sliding sleeve. During lifting, the hook is located within the space formed by the rope and the sliding sleeve, and the rope is twisted and connected with the hook during the lifting process.

2. The military 200kg-class cargo container according to claim 1, characterized in that, The top of the support rod is also provided with a first retaining ring, which is located between the spiral groove and the through hole top cover; The bottom of the support rod is also provided with a second retaining ring, which is located between the support foot and the through hole bottom cover; The first retaining ring is provided on the side facing the top cover of the through hole, and the second retaining ring is provided on the side facing the bottom plate of the through hole.

3. The military 200kg-class cargo container according to claim 2, characterized in that, The elastic component includes: a pad and a spring, wherein the pad and the spring are sleeved on the outside of the support rod, and the pad and the spring are located in the upper space between the support rod retaining ring and the through hole top cover; The pad and the spring are located in the lower space between the support rod retaining ring and the through hole bottom cover; The number of the pads in the upper space is one or more; The number of springs in the upper space is one or more; The number of the pads in the lower space is one or more; The number of springs in the lower space is one or more; The support rod moves elastically within the vertical tube.

4. The military 200kg-class cargo container according to claim 3, characterized in that, The through-hole bottom cover is welded to the vertical pipe.

5. The military 200kg-class cargo container according to claim 4, characterized in that, The support leg includes: a first plate, a conical spring, and a top head. The first plate has a circular hole in the middle, the large-diameter end of the conical spring is connected to the first plate, and the small-diameter end of the conical spring is connected to the top head; The bottom end of the support rod passes through the circular hole, passes through the middle of the conical spring, and is fixedly connected to the top head; The top head is conical, the tip of the top head is round, and the waist of the top head is curved inward to form an arc.

6. The military 200kg-class cargo container according to claim 5, characterized in that, The sum of the distance between the through-hole bottom cover and the first plate and the distance between the retractions of the conical springs is less than the distance between the retractions of the springs.

7. The military 200kg-class cargo container according to claim 6, characterized in that, The top surface of the frame is equipped with a large cover plate, and the large cover plate and the bottom plate are made of magnesium alloy lightweight bulletproof armor. The outside of the frame is covered with waterproof cloth.

8. The military 200kg-class cargo container according to claim 7, characterized in that, The bottom plate is provided with three or more support feet evenly distributed on its lower side.

9. The military 200kg-class cargo container according to claim 8, characterized in that, Two or more gravity sensors are evenly distributed between the frame and the base plate. The frame also contains a battery box and a positioning device for signal transmission and reception. The signal transceiver positioning device transmits signals to mobile or fixed terminals via cloud services.

Citation Information

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