Detachable non-metal high-strength fiber fireproof plate prefabricated cabin

Abstract

The present disclosure relates to the technical field of prefabricated cabins, and one embodiment of the present disclosure provides a detachable non-metal high-strength fiber fireproof plate prefabricated cabin, which comprises a main cabin plate, a pair of side cabin plates and a cabin door plate, the side cabin plates are connected between the main cabin plate and the cabin door plate, a splicing assembly is arranged between the main cabin plate, the side cabin plates and the cabin door plate, a sealing and ventilating assembly is arranged on the top of the main cabin plate, the splicing assembly comprises a pair of positioning grooves, the positioning grooves are arranged at both ends of the surface of the main cabin plate, the side cabin plates are inserted into the positioning grooves, a pair of splicing holes are arranged at both ends of the surface of the main cabin plate and in the side cabin plates, a splicing frame is inserted and connected in the splicing holes, and one side of the splicing frame is attached to the surface of the main cabin plate. Through the above technical scheme, the technical problem that the prefabricated cabins currently used in the prior art are mostly of integral structure, and large mechanical equipment needs to be used for hoisting and installation during installation, the process is complicated and time-consuming, and it is extremely difficult to disassemble if the prefabricated cabin needs to be moved later is solved.

Description

Technical Field

[0001] The embodiments disclosed herein relate to the technical field of prefabricated cabins, specifically to a detachable non-metallic high-strength fiber fireproof prefabricated cabin. Background Technology

[0002] Prefabricated modules are widely used as integrated equipment carriers in many fields such as modern industry, power, and communications. However, traditional prefabricated modules have significant shortcomings in terms of loading and unloading. Most prefabricated modules currently in use are integral structures, requiring large mechanical equipment for hoisting and installation. The process is cumbersome and time-consuming, placing high demands on the construction site and equipment. Once the installation location is determined, relocation later is extremely difficult, not only consuming a lot of manpower and resources but also easily damaging the prefabricated module.

[0003] With industry development and increasingly shorter project construction cycles, the demand for rapid loading and unloading of prefabricated modules is becoming increasingly urgent. For example, in some emergency or temporary projects, prefabricated modules need to be quickly installed and put into use, and then quickly disassembled and transferred to other locations after the task is completed. However, existing prefabricated modules cannot meet this requirement, leading to increased project costs and reduced efficiency. Therefore, developing a rapidly load-and-unloadable, detachable, non-metallic, high-strength fiber fireproof prefabricated module has become an urgent problem for the industry to solve. Utility Model Content

[0004] To overcome the above-mentioned defects, the embodiments of this disclosure provide a detachable non-metallic high-strength fiber fireproof prefabricated cabin, which solves the technical problem that the prefabricated cabins currently used in the prior art are mostly integral structures, which require large mechanical equipment for hoisting and installation during installation, making the process cumbersome and time-consuming, and making disassembly extremely difficult if relocation is required later.

[0005] According to one aspect, at least one embodiment of this disclosure provides a detachable non-metallic high-strength fiber fireproof prefabricated cabin, comprising: The main deck panel, a pair of side deck panels, and a door panel, wherein the side deck panels are connected between the main deck panel and the door panel; A splicing assembly is disposed between the main cabin panel, the side cabin panel, and the door panel; A top-sealing ventilation assembly is disposed on the top of the main compartment panel; The splicing assembly includes a pair of positioning slots, which are formed at both ends of the surface of the main cabin plate. The side cabin plate is inserted into the positioning slots. A pair of splicing holes are formed at both ends of the surface of the main cabin plate and inside the side cabin plate. A splicing frame is inserted into the splicing hole and connected thereto. One side of the splicing frame is attached to the surface of the main cabin plate.

[0006] As a further technical solution, a pair of sleeve holes are provided at both ends of the surface of the hatch panel, and the hatch panel is fitted onto one end of the splicing frame through the sleeve holes. The splicing frame has slots at both ends.

[0007] As a further technical solution, a connecting rod is inserted into a pair of opposing slots, the connecting rod is attached to the surface of the door panel, and the connecting rod is fixedly connected to the splicing frame by bolts.

[0008] As a further technical solution, the top ventilation assembly includes a top plate, a pair of slots are provided on the side surface of the side panel, and a pair of insert plates are provided at both ends of the bottom of the top plate, with the insert plates inserted into the slots.

[0009] As a further technical solution, the insert plate and the slot are fixedly connected by bolts, a cover is provided at the bottom of the top plate, an air intake mesh is opened at the bottom of the cover, and several air intake fans are installed on the surface of the top plate.

[0010] As a further technical solution, a shield is provided on the surface of the top plate. The shield has an open structure on both sides, and several baffles are provided inside both ends of the shield. A filter screen is installed inside both ends of the shield.

[0011] As a further technical solution, the baffle and the filter screen are connected by magnetic adsorption.

[0012] As a further technical solution, the splicing frame has an overall gate-shaped structure.

[0013] As a further technical solution, the top of the shield is an inclined slope structure, and both ends of the shield extend outward.

[0014] As a further technical solution, the bolts connecting the insert plate and the slot pass through the side panel and are simultaneously screwed into the splicing frame.

[0015] The beneficial effects of the embodiments disclosed herein are as follows: 1. The beneficial effects of the splicing components in this disclosure are that the positioning groove facilitates the quick positioning and installation of the side compartment panels, the splicing holes and splicing frames ensure a stable connection between the main compartment panels and the side compartment panels, and the portal-shaped splicing frame, together with the connecting rods and bolts, is tightly connected to the door panels to form a stable frame structure. The overall splicing method is simple to operate, facilitates quick loading and unloading, reduces installation difficulty, improves construction efficiency, and reduces reliance on large mechanical equipment.

[0016] 2. The beneficial effects of the top-sealing ventilation component in this disclosure are that the insert plate and slot are used in conjunction with bolts to fix the top plate, which is easy to disassemble and facilitates the relocation of the prefabricated cabin. The air intake fan and air intake mesh ensure air circulation in the cabin and maintain a good environment. The shield and filter can effectively filter air impurities and protect the equipment in the cabin. The shield with the inclined slope structure is waterproof, and the outward extension part expands the shielding range. Attached Figure Description

[0017] To more clearly illustrate the technical solutions in the embodiments of this disclosure, the accompanying drawings used in the description of the embodiments of this disclosure will be briefly introduced below. Obviously, the drawings described below are merely some exemplary embodiments of this disclosure. For those skilled in the art, other drawings can be obtained based on the content of the exemplary embodiments of this disclosure and these drawings without any creative effort.

[0018] Figure 1 This is a schematic diagram of a structure in one embodiment of the present disclosure; Figure 2 This is an isometric drawing of the present disclosure; Figure 3 This is an isometric sectional view of the present disclosure; Figure 4 This is another isometric sectional view of this disclosure; In the diagram: 1. Main compartment panel; 2. Side compartment panel; 3. Door panel; 4. Assembly assembly; 4-1. Positioning slot; 4-2. Assembly hole; 4-3. Assembly frame; 4-4. Sleeve hole; 4-5. Slot; 4-6. Connecting rod; 5. Top ventilation assembly; 5-1. Top plate; 5-2. Slot; 5-3. Insert plate; 5-4. Bulkhead; 5-5. Air intake mesh; 5-6. Air intake fan; 5-7. Shield; 5-8. Baffle; 5-9. Filter screen. Detailed Implementation

[0019] The present disclosure will now be described in further detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present disclosure and are not intended to limit the scope of the disclosure.

[0020] To keep the drawings concise, each drawing only schematically shows the parts relevant to the disclosure; these do not represent the actual structure of the product. Furthermore, for ease of understanding, in some drawings, only one of components with the same structure or function is schematically shown, or only one is labeled. In this document, "one" not only means "only one," but can also mean "more than one," and "several" includes "two" and "more than two."

[0021] In this document, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "linkage" should be interpreted broadly. For example, they can refer to fixed connections, detachable connections, or integral connections; they can refer to mechanical connections or electrical connections; they can refer to direct connections or indirect connections through an intermediate medium; and they can refer to the internal connection between two components. Those skilled in the art can understand the specific meaning of the above terms in this disclosure based on the specific circumstances.

[0022] In this disclosure, unless otherwise expressly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.

[0023] In the description of this embodiment, terms such as "upper," "lower," "left," and "right" are based on the orientation or positional relationship shown in the accompanying drawings. They are used only for the convenience of description and simplification of operation, and are not intended to indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this disclosure.

[0024] Furthermore, in the description of this application, the terms "first," "second," etc., are used only to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0025] like Figures 1-4 As shown, it illustrates a detachable non-metallic high-strength fiber fireproof prefabricated cabin according to an embodiment of the present disclosure, comprising: The main cabin panel 1, a pair of side cabin panels 2, and a door panel 3 are connected between the main cabin panel 1 and the door panel 3. The splicing component 4 is disposed between the main cabin panel 1, the side cabin panel 2, and the door panel 3; Top-sealing ventilation assembly 5 is installed on the top of the main cabin plate 1; The splicing assembly 4 includes a pair of positioning slots 4-1, which are formed at both ends of the surface of the main cabin plate 1. The side cabin plate 2 is inserted into the positioning slots 4-1. A pair of splicing holes 4-2 are formed at both ends of the surface of the main cabin plate 1 and in the side cabin plate 2. A splicing frame 4-3 is inserted into the splicing hole 4-2. One side of the splicing frame 4-3 is attached to the surface of the main cabin plate 1. A pair of sleeve holes 4-4 are formed at both ends of the surface of the hatch panel 3. The hatch panel 3 is fitted onto one end of the splicing frame 4-3 through the sleeve holes 4-4. A slot 4-5 is formed at both ends of the splicing frame 4-3. A connecting rod 4-6 is inserted into a pair of opposing slots 4-5. The connecting rod 4-6 is attached to the surface of the hatch panel 3. The connecting rod 4-6 is fixedly connected to the splicing frame 4-3 by bolts.

[0026] In some examples, during the assembly of the hull structure, a splicing assembly 4 is designed to achieve a stable connection between the main hull panel 1, side hull panels 2, and door panels 3. This assembly includes a pair of positioning slots 4-1 formed at both ends of the surface of the main hull panel 1, which serve to position the side hull panels 2 for installation, allowing them to be accurately inserted into the positioning slots 4-1. A pair of splicing holes 4-2 are formed at both ends of the surface of the main hull panel 1 and within the side hull panels 2. A splicing frame 4-3 is inserted into the splicing holes 4-2, with one side abutting against the surface of the main hull panel 1. The splicing frame 4-3 securely connects the main hull panel 1 and the side hull panels 2 together. A pair of sleeve holes 4-4 are opened at both ends of the surface of the hatch panel 3, which allows the hatch panel 3 to be fitted onto one end of the splicing frame 4-3 through the sleeve holes 4-4, realizing the initial connection between the hatch panel 3 and the splicing frame 4-3. The slots 4-5 opened at both ends of the splicing frame 4-3 cooperate with the connecting rods 4-6 inserted in a pair of opposite slots 4-5. The connecting rods 4-6 fit against the surface of the hatch panel 3, further enhancing the connection stability between the hatch panel 3 and the splicing frame 4-3. The connecting rods 4-6 are fixedly connected to the splicing frame 4-3 by bolts. This connection method is not only firm and reliable, but also easy to disassemble and maintain.

[0027] like Figures 1-4 As shown, this embodiment proposes a top-sealed ventilation assembly 5 including a top plate 5-1, a pair of slots 5-2 on the side surface of the side panel 2, a pair of insert plates 5-3 at both ends of the bottom of the top plate 5-1, the insert plates 5-3 being inserted into the slots 5-2, and the insert plates 5-3 being fixedly connected to the slots 5-2 by bolts, a cover 5-4 at the bottom of the top plate 5-1, an air inlet mesh 5-5 at the bottom of the cover 5-4, several air intake fans 5-6 installed on the surface of the top plate 5-1, a shield 5-7 on the surface of the top plate 5-1, the shield 5-7 having an open structure on both sides, several baffles 5-8 at both ends of the shield 5-7, and filters 5-9 installed at both ends of the shield 5-7.

[0028] In some examples, during the assembly and installation of the prefabricated cabin, a roof ventilation assembly 5 is designed to achieve a detachable roof and ensure ventilation within the cabin. This assembly includes a top plate 5-1 as the main component for the roof, and a pair of slots 5-2 on the side surface of the side cabin 2 that cooperate with a pair of insert plates 5-3 at both ends of the bottom of the top plate 5-1. The insert plates 5-3 can be accurately inserted into the slots 5-2, and are fixedly connected to the slots 5-2 by bolts, so that the top plate 5-1 is firmly installed on the side cabin 2, completing the roofing operation of the prefabricated cabin. When it is necessary to disassemble the top plate 5-1, simply unscrew the bolts to remove the top plate 5-1 from the side cabin 2, which is convenient and quick. A shroud 5-4 is provided at the bottom of the top plate 5-1. The air intake mesh 5-5 at the bottom is used for air intake. Several air intake fans 5-6 installed on the surface of the top plate 5-1 can draw outside air into the prefabricated cabin through the air intake mesh 5-5 to ensure air circulation inside the cabin. The shield 5-7 installed on the surface of the top plate 5-1 has an open structure on both sides, which can protect the air intake fans 5-6 and other components from external debris without affecting the air intake and exhaust. Several baffles 5-8 installed inside both ends of the shield 5-7 serve to support and fix the filter 5-9. The filter 5-9 installed inside both ends of the shield 5-7 can effectively filter dust, particles and other impurities in the air, ensuring that the air entering the prefabricated cabin is clean and preventing these impurities from damaging the equipment inside the cabin.

[0029] For example, such as Figure 4 As shown, the baffle 5-8 and the filter screen 5-9 are connected by magnetic adsorption.

[0030] In some examples, the baffle 5-8 and the filter screen 5-9 can be firmly attached together by magnetic adsorption, which can be easily disassembled and cleaned.

[0031] For example, such as Figure 3 As shown, the splicing frame 4-3 has an overall door-shaped structure.

[0032] In some examples, a rectangular frame structure is formed by connecting the gate-shaped structure with the connecting rods 4-6, which firmly connects the main cabin panel 1, a pair of side cabin panels 2 and the door panel 3 together.

[0033] For example, such as Figure 1 As shown, the top of the shield 5-7 is a sloping structure, and both ends of the shield 5-7 extend outward.

[0034] In some examples, the sloping structure serves as a waterproofing element, and by extending outwards, it increases the area of ​​coverage.

[0035] For example, such as Figure 1As shown, the bolts connecting the insert plate 5-3 and the slot 5-2 pass through the side compartment plate 2 and are simultaneously screwed into the splicing frame 4-3.

[0036] In some examples, the side panel 2 is connected to the connecting plate and the insert plate 5-3 to further improve structural stability.

[0037] In actual use: First, insert the side panel 2 into the positioning slot 4-1 of the main panel 1. Insert the splicing frame 4-3 into the splicing hole 4-2 of the main panel 1 and the side panel 2. Then, put the door panel 3 into one end of the splicing frame 4-3 through the sleeve hole 4-4. Then insert the connecting rod 4-6 and fix it with bolts to complete the splicing of the cabin. After that, insert the insert plate 5-3 of the top plate 5-1 into the slot 5-2 of the side panel 2. Use bolts to screw the side panel 2 into the splicing frame 4-3 to fix the top plate 5-1 to complete the installation. During use, the air intake fan 5-6 can be started. Air enters the prefabricated cabin through the air intake mesh 5-5. The filter screen 5-9 can be pulled out for cleaning.

[0038] It should be noted that the above embodiments are only used to illustrate the technical solutions of this disclosure and are not intended to limit it. Although this disclosure has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solutions of this disclosure without departing from the spirit and scope of the technical solutions of this disclosure, and all such modifications and substitutions should be covered within the scope of the claims of this disclosure.

Claims

1. A detachable non-metallic high-strength fiber fireproof prefabricated cabin, characterized in that, include: The main cabin panel (1), a pair of side cabin panels (2) and a door panel (3), wherein the side cabin panels (2) are connected between the main cabin panel (1) and the door panel (3); The splicing assembly (4) is disposed between the main cabin panel (1), the side cabin panel (2) and the door panel (3); A top-sealing ventilation assembly (5) is disposed on the top of the main cabin panel (1); The splicing assembly (4) includes a pair of positioning grooves (4-1), which are formed at both ends of the surface of the main cabin plate (1). The side cabin plate (2) is inserted into the positioning grooves (4-1). A pair of splicing holes (4-2) are formed at both ends of the surface of the main cabin plate (1) and in the side cabin plate (2). A splicing frame (4-3) is inserted into the splicing hole (4-2) and connected to it. One side of the splicing frame (4-3) is attached to the surface of the main cabin plate (1).

2. The detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 1, characterized in that, The hatch panel (3) has a pair of sleeve holes (4-4) at both ends of its surface. The hatch panel (3) is fitted onto one end of the splicing frame (4-3) through the sleeve holes (4-4). The splicing frame (4-3) has slots (4-5) at both ends of its surface.

3. A detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 2, characterized in that, A connecting rod (4-6) is inserted into a pair of opposing slots (4-5). The connecting rod (4-6) is attached to the surface of the door panel (3). The connecting rod (4-6) is fixedly connected to the splicing frame (4-3) by bolts.

4. The detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 1, characterized in that, The top ventilation assembly (5) includes a top plate (5-1), and a pair of slots (5-2) are provided on the side surface of the side panel (2). A pair of insert plates (5-3) are provided at both ends of the bottom of the top plate (5-1), and the insert plates (5-3) are inserted into the slots (5-2).

5. A detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 4, characterized in that, The insert plate (5-3) and the slot (5-2) are fixedly connected by bolts. A cover (5-4) is provided at the bottom of the top plate (5-1). An air inlet mesh (5-5) is opened at the bottom of the cover (5-4). Several air inlet fans (5-6) are installed on the surface of the top plate (5-1).

6. A detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 5, characterized in that, The top plate (5-1) is provided with a shield (5-7), the shield (5-7) has an open structure on both sides, a number of baffles (5-8) are provided inside both ends of the shield (5-7), and a filter screen (5-9) is installed inside both ends of the shield (5-7).

7. A detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 6, characterized in that, The baffle (5-8) and the filter screen (5-9) are connected by magnetic adsorption.

8. A detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 1, characterized in that, The splicing frame (4-3) has an overall door-shaped structure.

9. A detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 6, characterized in that, The top of the shield (5-7) is an inclined slope structure, and both ends of the shield (5-7) extend outward.

10. A detachable non-metallic high-strength fiber fireproof prefabricated cabin according to claim 4, characterized in that, The bolts connecting the insert plate (5-3) and the slot (5-2) pass through the side panel (2) and are simultaneously screwed into the splicing frame (4-3).

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