Space capsule framework structure

Abstract

The utility model discloses a space capsule skeleton structure, relates to the space capsule technical field, the space capsule skeleton structure comprises a frame main body, the outer side wall of the frame main body is provided with a shell assembly, the frame main body comprises a first frame and a second frame, the inner side of the first frame and the inner side of the second frame are fixedly provided with a plurality of cross beams, a first reinforcing rod is arranged on the inner side of the cross beam at the bottom in a penetrating mode, inserting holes are formed in the inner side of the cross beam at the top in a penetrating mode, second reinforcing rods are inserted into the inner sides of the two inserting holes located on the same side, and a supporting assembly is arranged at the bottom of the second frame. The whole framework has good stability in the vertical direction and the horizontal direction, the overall mechanical property is further enhanced, the strength and stability of the device are improved, all the assemblies are connected through bolts, and workers can maintain and adjust the device conveniently.

Description

Technical Field

[0001] This utility model relates to the field of space capsule technology, specifically a space capsule frame structure. Background Technology

[0002] Space capsules are a type of mobile home. Due to their ease of movement and low cost, they have gradually gained popularity in the market. Space capsules have a wide range of applications, including tourist attractions, high-end homestays, outdoor recreation, rooftop gardens, rural villas, forest villas, mountain forests, and private clubs.

[0003] The existing authorization announcement number CN220848029U discloses a metal frame for a space capsule that is easy to move. This device replaces the original single plate with multiple dispersed plates, which are fixed to the frame structure by connectors. When a plate is damaged, the corresponding plate can be replaced in time, and disassembly is convenient.

[0004] However, during the use of the space capsule's metal frame, replacing the original single plate with multiple separate plates will increase the pressure of the plates on the frame structure. Since it is only fixed by crossbeams, the crossbeams are prone to bending and deformation under long-term stress, resulting in a decrease in the overall stability of the frame structure. Utility Model Content

[0005] The purpose of this invention is to provide a space capsule frame structure to solve the problem that the crossbeams under long-term stress are prone to bending and deformation, which leads to a decrease in the overall frame structure stability.

[0006] To achieve the above objectives, this utility model provides the following technical solution:

[0007] A space capsule skeleton structure includes a frame body, an outer shell assembly is provided on the outer side wall of the frame body, the inner side wall of the outer shell assembly is fixedly connected to the surface of the frame body through a connector, and a support wheel is provided at the bottom of the outer shell assembly;

[0008] The main frame includes a first frame and a second frame. Multiple crossbeams are fixedly installed on the inner sides of the first frame and the second frame. A first reinforcing rod is provided through the inner side of the bottom crossbeam, and a plug hole is provided through the inner side of the top crossbeam. Two second reinforcing rods are inserted into the inner sides of the two plug holes on the same side. A support component is provided at the bottom of the second frame.

[0009] Based on the above technical solutions, this utility model also provides the following optional technical solutions:

[0010] In one alternative: a first mounting block is fixedly installed at both ends of the first reinforcing rod, and the inner side of the first mounting block is fixedly connected to the inner sidewall of the first frame by a first bolt.

[0011] In one alternative: two connected second reinforcing rods are alternately arranged one after the other, and the diameter of the second reinforcing rod is the same as the width of the crossbeam.

[0012] In one alternative: the support assembly includes a support frame, the bottom of which is provided with a support column, the bottom of which is fixedly connected to the top of the first frame by a second bolt, and the top of which is connected to the support frame has a threaded hole through it and is fixedly connected by a third bolt.

[0013] In one alternative: a second mounting block and a third mounting block are fixedly mounted on the surface of the support frame, the two second mounting blocks are fixedly connected to the second frame by a fourth bolt, and the third mounting block is fixedly connected to the crossbeam by a fifth bolt.

[0014] In one alternative: the support frame has the same width as the crossbeam, the support frame has mounting holes on its inner side, and the support column has reinforcing components on its surface.

[0015] In one alternative: the reinforcing component includes a first reinforcing block, two reinforcing ribs are fixedly mounted on the surface of the first reinforcing block, and a second reinforcing block is fixedly mounted on the other side of the reinforcing ribs. The first and second reinforcing blocks are fixedly connected to the connected support column by a sixth bolt.

[0016] In one alternative: the first reinforcing block, the two reinforcing ribs, and the second reinforcing block are integrated into one piece.

[0017] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0018] 1. In this utility model, the frame body and supporting components are arranged in a cooperative manner to make the entire skeleton have good stability in both vertical and horizontal directions, further enhancing the overall mechanical properties and improving the strength and stability of the device.

[0019] 2. In this utility model, bolts are used to connect the various components, which greatly facilitates the maintenance and adjustment of the device by the staff. When a certain part is damaged, the corresponding part can be quickly disassembled and replaced, which improves maintenance efficiency and reduces maintenance costs. Attached Figure Description

[0020] Figure 1 This is a schematic diagram of the overall structure of this utility model.

[0021] Figure 2 This is a schematic diagram of the connecting component structure of this utility model.

[0022] Figure 3 This is a schematic diagram of the main frame structure of this utility model.

[0023] Figure 4 This is a bottom view of the second frame structure of this utility model.

[0024] Figure 5 This is a side view of the reinforcing component of this utility model.

[0025] Figure reference numerals: 1. Frame body; 2. Shell assembly; 3. Connector; 4. Support wheel; 5. First frame; 6. Second frame; 7. Crossbeam; 8. First reinforcing rod; 9. Insertion hole; 10. Second reinforcing rod; 11. First mounting block; 12. First bolt; 13. Support frame; 14. Support column; 15. Second bolt; 16. Threaded hole; 17. Third bolt; 18. Second mounting block; 19. Third mounting block; 20. Fourth bolt; 21. Fifth bolt; 22. Mounting hole; 23. First reinforcing block; 24. Reinforcing rib; 25. Second reinforcing block; 26. Sixth bolt. Detailed Implementation

[0026] To make the objectives, technical solutions, and advantages of this utility model clearer, the present utility model will be further described in detail below with reference to the accompanying drawings and embodiments.

[0027] In one embodiment, such as Figures 1-5 As shown, the space capsule frame structure of this embodiment includes a frame body 1, an outer shell assembly 2 is provided on the outer side wall of the frame body 1, the inner side wall of the outer shell assembly 2 is fixedly connected to the surface of the frame body 1 through a connector 3, and a support wheel 4 is provided at the bottom of the outer shell assembly 2.

[0028] The main frame 1 includes a first frame 5 and a second frame 6. Multiple crossbeams 7 are fixedly installed on the inner side of the first frame 5 and the second frame 6. A first reinforcing rod 8 is provided through the inner side of the bottom crossbeam 7. An insertion hole 9 is provided through the inner side of the top crossbeam 7. A second reinforcing rod 10 is inserted into the inner side of the two insertion holes 9 located on the same side. A support component is provided at the bottom of the second frame 6.

[0029] In this embodiment, the frame body 1 provides a basic support frame for the entire device, ensuring the overall shape and stability. The outer shell assembly 2 and the connector 3 securely connect the outer shell assembly 2 to the frame body 1, ensuring that all parts work together and facilitating installation and disassembly by personnel. When a part is damaged, the corresponding part can be replaced in time, improving the flexibility and functionality of the device. The frame body 1 consists of a first frame 5 and a second frame 6. The fixed installation of multiple crossbeams 7 further enhances the stability of the frame. The first reinforcing rod 8 on the inner side of the bottom crossbeam 7 can improve the strength of the bottom of the frame and prevent deformation when subjected to large pressure or external force. The insertion hole 9 on the inner side of the top crossbeam 7, in conjunction with the second reinforcing rod 10, increases the lateral connection strength of the top of the frame. Together with the function of the support assembly, the entire frame has good mechanical properties in both vertical and horizontal directions.

[0030] In one embodiment, such as Figure 2 As shown, the first reinforcing rod 8 has a first mounting block 11 fixedly installed at both ends. The inner side of the first mounting block 11 is fixedly connected to the inner side wall of the first frame 5 by the first bolt 12. This installation method makes the installation and disassembly of the first reinforcing rod 8 more convenient and facilitates operation when maintaining the device or adjusting the structure.

[0031] In one embodiment, such as Figure 2 and Figure 3 As shown, two connected second reinforcing rods 10 are alternately arranged one after the other. The diameter of the second reinforcing rod 10 is the same as the width of the crossbeam 7. The alternating arrangement of the second reinforcing rods 10 can effectively strengthen the top of the frame in different directions, thereby avoiding weak areas under stress.

[0032] In one embodiment, such as Figure 2 and Figure 3 As shown, the support assembly includes a support frame 13, with a support column 14 at the bottom of the support frame 13. The bottom of the support column 14 is fixedly connected to the top of the first frame 5 by a second bolt 15. A threaded hole 16 is opened through the connection between the top of the support column 14 and the support frame 13, and is fixedly connected by a third bolt 17. This connection method makes the installation of the support assembly firm and reliable, and can better support the weight of the spacecraft and withstand various external forces.

[0033] In one embodiment, such as Figure 2As shown, a second mounting block 18 and a third mounting block 19 are fixedly installed on the surface of the support frame 13. The two second mounting blocks 18 are fixedly connected to the second frame 6 by a fourth bolt 20, and the third mounting block 19 is fixedly connected to the crossbeam 7 by a fifth bolt 21. The second mounting blocks 18 and the third mounting blocks 19 on the surface of the support frame 13 are fixedly connected to the second frame 6 and the crossbeam 7 by the fourth bolt 20 and the fifth bolt 21, respectively, which further enhances the connection stability between the support assembly and the frame body 1.

[0034] In one embodiment, such as Figure 3 and Figure 4 As shown, the support frame 13 has the same width as the crossbeam 7. The support frame 13 has mounting holes 22 on its inner side, and the support column 14 has reinforcing components on its surface. When the temperature is high, the mounting holes 22 facilitate the installation of the insulation board and increase the scalability of the structure.

[0035] In one embodiment, such as Figure 3 and Figure 4 As shown, the reinforcing component includes a first reinforcing block 23, two reinforcing ribs 24 are fixedly installed on the surface of the first reinforcing block 23, and a second reinforcing block 25 is fixedly installed on the other side of the reinforcing ribs 24. The first reinforcing block 23 and the second reinforcing block 25 are fixedly connected to the connected support column 14 by a sixth bolt 26, which can effectively disperse the pressure and tension borne by the support column 14, improve the load-bearing capacity of the support column 14, and thus enhance the stability of the entire support component.

[0036] In one embodiment, such as Figure 3 and Figure 4 As shown, the first reinforcing block 23, the two reinforcing ribs 24, and the second reinforcing block 25 are integrated into one piece. This integrated design enhances the strength and stability of the reinforcing component itself, and the reinforcing ribs 24 further improve the mechanical properties of the reinforcing component.

[0037] The above embodiment discloses a space capsule skeleton structure, wherein the frame body 1 is composed of a first frame 5 and a second frame 6. The fixed installation of multiple crossbeams 7 further enhances the stability of the frame. The inner side of the first mounting block 11 is fixedly connected to the inner side wall of the first frame 5 by the first bolt 12. This installation method makes the installation and disassembly of the first reinforcing rod 8 more convenient. It is easy to operate when maintaining the device or adjusting the structure. Moreover, the first reinforcing rod 8 can improve the strength of the bottom of the frame and prevent deformation when subjected to large pressure or external force. The insertion hole 9 on the inner side of the top crossbeam 7, in conjunction with the second reinforcing rod 10, increases the lateral connection strength of the top of the frame. The second mounting block 18 and the third mounting block 19 on the surface of the support frame 13 are fixedly connected to the second frame 6 and the crossbeam 7 by the fourth bolt 20 and the fifth bolt 21, respectively, further enhancing the connection stability between the support assembly and the frame body 1. This gives the entire frame good mechanical properties in both vertical and horizontal directions. The integrated design enhances the strength and stability of the reinforcing assembly itself. The reinforcing rib 24 further improves the mechanical properties of the reinforcing assembly, effectively dispersing the pressure and tension borne by the support column 14, improving the load-bearing capacity of the support column 14, and thus enhancing the stability of the entire support assembly. Most of the components are connected by bolts, which greatly facilitates the maintenance and adjustment of the device by the staff.

[0038] The above description is merely a specific embodiment of this application, but the scope of protection of this application is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this application should be included within the scope of protection of this application. Therefore, the scope of protection of this application should be determined by the scope of the claims.

Claims

1. A space capsule framework structure, comprising a frame body (1), the outer wall of the frame body (1) is provided with a shell assembly (2), the inner wall of the shell assembly (2) is fixedly connected with the surface of the frame body (1) through a connecting piece (3), and the bottom of the shell assembly (2) is provided with a supporting wheel (4). characterized in that The frame body (1) comprises a first frame (5) and a second frame (6), a plurality of cross beams (7) are fixedly installed in the inner side of the first frame (5) and the second frame (6), a first reinforcing rod (8) is penetratingly arranged in the inner side of the cross beam (7) at the bottom, a plug-in hole (9) is penetratingly arranged in the inner side of the cross beam (7) at the top, a second reinforcing rod (10) is plugged into the inner side of two plug-in holes (9) located at the same side, and the bottom of the second frame (6) is provided with a supporting assembly.

2. A space habitat structure according to claim 1, wherein, First mounting blocks (11) are fixedly installed at the front and rear ends of the first reinforcing rod (8), and the inner side of the first mounting block (11) is fixedly connected with the inner side wall of the first frame (5) through a first bolt (12).

3. A space habitat skeletal structure according to claim 1, wherein, Two second reinforcing rods (10) connected in series are alternately arranged at the front and rear, and the diameter of the second reinforcing rod (10) is the same as the width of the cross beam (7).

4. A space habitat skeletal structure according to claim 1, wherein, The supporting assembly comprises a supporting frame (13), the bottom of the supporting frame (13) is provided with a supporting column (14), the bottom of the supporting column (14) is fixedly connected with the top of the first frame (5) through a second bolt (15), a threaded hole (16) is penetratingly arranged at the position where the supporting column (14) top is connected with the supporting frame (13), and the supporting column (14) is fixedly connected through a third bolt (17).

5. A space habitat skeletal structure according to claim 4, wherein, Second mounting blocks (18) and third mounting blocks (19) are fixedly installed on the surface of the supporting frame (13), two second mounting blocks (18) are fixedly connected with the second frame (6) through a fourth bolt (20), and the third mounting block (19) is fixedly connected with the cross beam (7) through a fifth bolt (21).

6. A space habitat skeletal structure according to claim 4, wherein, The width of the supporting frame (13) is the same as that of the cross beam (7), mounting holes (22) are arranged in the inner side of the supporting frame (13), and the surface of the supporting column (14) is provided with a reinforcing assembly.

7. A space habitat skeletal structure according to claim 6, wherein, The reinforcing assembly comprises a first reinforcing block (23), two reinforcing ribs (24) are fixedly installed on the surface of the first reinforcing block (23), a second reinforcing block (25) is fixedly installed on the other side of the reinforcing rib (24), and the first reinforcing block (23) and the second reinforcing block (25) are fixedly connected with the connected supporting column (14) through a sixth bolt (26).

8. A space habitat skeletal structure according to claim 7, wherein, The first reinforcing block (23), the two reinforcing ribs (24) and the second reinforcing block (25) are integrally arranged.

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