Modular soundproofing structure for space capsules
By using splicing and soundproofing installation components on the frame surface in the modular soundproofing structure of the space capsule, the problems of low modular splicing and difficulty in upgrading the soundproofing effect are solved, achieving efficient installation and enhanced soundproofing effect.
Patent Information
- Application Number
- CN202522155378.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-11
- Publication Date
- 2026-08-25
- Estimated Expiration
- 2035-10-11
AI Technical Summary
Existing modular soundproofing structures for space capsules have low modularity, low installation efficiency, and difficulty in upgrading soundproofing performance.
The system employs splicing and soundproofing mounting components on the frame surface, including snap-fit grooves and snap-fit blocks, arc-shaped blocks and arc-shaped plates, combined with magnetic and bolt connections to enhance module splicing and soundproofing performance.
It improves the installation efficiency and sound insulation of modular sound insulation structures, enhances the compactness and overall strength of modules, and improves the adaptability of sound insulation effects.
Smart Images

Figure CN224678915U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of space capsule equipment technology, specifically a modular sound insulation structure for a space capsule. Background Technology
[0002] With the improvement of living standards, more and more people are traveling. The supply of hotel rooms and inns in scenic areas is often insufficient, and the prices are very expensive, frequently accounting for a large portion of people's short-distance travel costs, increasing travel expenses. Coupled with the formation of an overtime work culture, this has spurred the emergence of capsule hotels. These hotels consist of dozens of neatly stacked capsules, each accommodating one customer. Some say they resemble spaceship capsules. Besides operating independently, capsule hotels often share facilities with saunas and bathhouses.
[0003] A publicly available patent (publication number CN219365553U) discloses a heat insulation and sound reduction structure for a space capsule. Sound-absorbing cotton is placed inside the outer explosion-proof layer, a sound-absorbing panel is placed outside the cotton, a fixing plate is placed outside the panel, and a vacuum chamber is placed inside the fixing plate. A conduit is connected to the side of the vacuum chamber, and the conduit is connected to a valve. Reinforcing steel bars are placed inside the outer explosion-proof layer, and these bars are connected to insulating cement. This heat insulation and sound reduction structure utilizes a vacuum pump to evacuate the vacuum chamber through the conduit, then closes the valve. The external sound insulation is achieved through the dual absorption of sound-absorbing cotton and panels, as well as the isolation provided by the vacuum chamber, thus blocking external noise and ensuring comfort for those inside the capsule. Simultaneously, the reinforcing steel bars and insulating cement provide heat insulation, preventing the cabin from becoming stuffy. A protective cover protects the inner conduit and valve, preventing accidental contact by users and protecting these components.
[0004] However, there are some problems in the use of existing modular soundproofing structures for space capsules: 1. The modular soundproofing structures for space capsules on the market have low overall modular splicing, making them inconvenient to replace and install, thus reducing the overall installation efficiency; 2. The overall soundproofing effect of the modular soundproofing structures for space capsules on the market cannot be effectively upgraded and adapted, thus reducing the overall soundproofing performance. Utility Model Content
[0005] The purpose of this invention is to provide a modular soundproof structure for a space capsule to solve the problems mentioned in the background art.
[0006] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a modular sound insulation structure for a space capsule, including a frame, splicing and installation components disposed on the surface of the frame, and sound insulation installation components disposed on the surface of the frame;
[0007] The splicing and installation assembly includes a snap-fit groove on one side of the frame surface, and a snap-fit block fixedly connected to the other side of the frame surface. The snap-fit block is fitted into the snap-fit groove, and multiple frames are spliced together by means of the snap-fit block.
[0008] The sound insulation installation assembly includes arc-shaped blocks fixedly connected to the four corners inside the frame. The arc-shaped blocks are concave, and an arc-shaped plate is connected to the surface of the arc-shaped blocks. The arc-shaped plate is convex, and a sound insulation plate is fixedly connected to one end of the arc-shaped plate. The sound insulation plate is installed through the arc-shaped plate.
[0009] As a further improvement of this utility model: the surface of the snap-fit plate is provided with a first connection hole, and a bolt is fitted inside the first connection hole.
[0010] As a further improvement of this utility model: a second connecting hole is provided inside the snap-fit groove, and a bolt is fitted inside the second connecting hole, with the first connecting hole and the second connecting hole aligned inside.
[0011] As a further embodiment of this utility model: the sound insulation installation component further includes a first magnetic block embedded and connected to both sides inside the frame, and a second magnetic block is embedded and connected inside the sound insulation plate.
[0012] As a further embodiment of this utility model: the first magnetic block and the second magnetic block are magnetically connected, and the surface of the frame is provided with an inner groove, and there are multiple inner grooves.
[0013] As a further improvement of this utility model: the bottom of the inner groove is provided with an injection port, and an external plate is connected to the surface of the injection port.
[0014] As a further embodiment of this utility model: the frame has an inner cavity, and a sound insulation board is connected inside the inner cavity; the frame, the arc-shaped board, and the arc-shaped block are all made of sound insulation material.
[0015] Compared with the prior art, the beneficial effects of this utility model are:
[0016] 1. In the modular installation of this utility model, multiple frames are installed on the inner side wall surface of the space capsule. The frames are connected by snap-fit blocks and snap-fit slots. The snap-fit blocks are inserted into the snap-fit slots, aligning the first connecting hole on the surface of the snap-fit block with the second connecting hole in the snap-fit slot. Bolts are then tightened to splice the two frames together. Different numbers of frames can be installed according to different lengths. As a result, the modular sound insulation structure of the space capsule has high modular splicing capability, making it easy to replace and install, thereby improving the overall installation efficiency.
[0017] 2. When this utility model enhances sound insulation, its arc-shaped plate is installed against the inner wall of the frame. The two corners of the arc-shaped plate are fitted with the arc-shaped blocks in the frame to increase the tightness of the installation and enhance the sound insulation effect. One end of the arc-shaped plate is installed with the sound insulation board to enhance the sound insulation effect inside the frame. Multiple internal grooves on the surface of the frame facilitate the installation of multiple external plates, increasing the overall strength and reducing the problem of deformation under stress. As a result, when the modular sound insulation structure of the space capsule is used, the overall sound insulation effect can be effectively upgraded and adapted, thereby improving the overall sound insulation performance. Attached Figure Description
[0018] Figure 1 This is a schematic diagram of the overall structure of an embodiment of the present utility model;
[0019] Figure 2 This is a schematic diagram of the arc-shaped block structure according to an embodiment of the present utility model;
[0020] Figure 3 This is a schematic diagram of the arc-shaped plate structure according to an embodiment of the present utility model;
[0021] Figure 4 This is a schematic diagram of the inner groove structure of an embodiment of the present utility model.
[0022] In the diagram: 1. Frame; 2. Inner cavity; 301. Snap-fit plate; 302. First connecting hole; 303. Snap-fit groove; 304. Second connecting hole; 305. Bolt; 401. Arc-shaped block; 402. First magnetic block; 403. Arc-shaped plate; 404. Sound insulation plate; 405. Second magnetic block; 406. Inner groove; 407. Glue injection port; 408. Outer plate. Detailed Implementation
[0023] To facilitate the solution of the problem, this utility model provides a modular soundproof structure for a space capsule. The technical solutions of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only a part of the embodiments of this utility model, and not all of them. All other embodiments obtained by those skilled in the art based on the embodiments of this utility model without creative effort are within the scope of protection of this utility model.
[0024] Example 1
[0025] like Figures 1 to 4As shown, this embodiment provides a modular soundproofing structure for a space capsule, including a frame 1, a splicing and installation assembly disposed on the surface of the frame 1, and a soundproofing installation assembly disposed on the surface of the frame 1. The splicing and installation assembly includes a snap-fit groove 303 formed on one side of the surface of the frame 1, and a snap-fit block fixedly connected to the other side of the surface of the frame 1. The snap-fit block is fitted inside the snap-fit groove 303, and multiple frames 1 are spliced together by the snap-fit block. The soundproofing installation assembly includes arc-shaped blocks 401 fixedly connected to the four corners of the inner side of the frame 1. The arc-shaped blocks 401 are concave, and an arc-shaped plate 403 is fitted to the surface of the arc-shaped blocks 401. The arc-shaped plate 403 is convex, and a soundproofing plate 404 is fixedly connected to one end of the arc-shaped plate 403, and the soundproofing plate 404 is installed by the arc-shaped plate 403.
[0026] Example 2
[0027] In addition to all the technical features in Embodiment 1, this embodiment also includes: the sound insulation installation assembly further includes a first magnetic block 402 embedded and connected to both sides inside the frame 1, and a second magnetic block 405 embedded and connected inside the sound insulation plate 404. The first magnetic block 402 and the second magnetic block 405 are magnetically connected. The surface of the frame 1 is provided with an inner groove 406, and there are multiple inner grooves 406. The first magnetic block 402 and the second magnetic block 405 facilitate the overall splicing and installation, and also facilitate replacement and use, thus increasing its usability.
[0028] Furthermore, the bottom of the inner groove 406 is provided with an injection port 407, and an outer plate 408 is connected to the surface of the injection port 407. The frame 1 is provided with an inner cavity 2, and a sound insulation plate 404 is connected to the inner cavity 2. The frame 1, the arc plate 403 and the arc block 401 are all made of sound insulation material. The injection port 407 facilitates the addition of glue, making it easy to install and use the outer plate 408.
[0029] Furthermore, the snap-fit plate 301 has a first connecting hole 302 on its surface, and a bolt 305 is fitted inside the first connecting hole 302. The snap-fit groove 303 has a second connecting hole 304 inside, and a bolt 305 is fitted inside the second connecting hole 304. The first connecting hole 302 and the second connecting hole 304 are aligned inside, and the first connecting hole 302 and the second connecting hole 304 increase the connection points, making it easier to disassemble and use.
[0030] Working principle: During the modular installation of the entire assembly, multiple frames 1 are installed on the inner wall surface of the spacecraft. Frames 1 are connected by snap-fit blocks and snap-fit slots 303. The snap-fit blocks are inserted into the snap-fit slots 303, aligning the first connecting hole 302 on the surface of the snap-fit block with the second connecting hole 304 in the snap-fit slot 303. Bolts 305 are then tightened to splice and install two frames 1 together. Different numbers of frames 1 can be installed according to different lengths. The curved plate 403 is attached to the inner wall of the frame 1. During installation, the two corners of the arc-shaped plate 403 are fitted with the arc-shaped block 401 in the frame 1 to increase the tightness of the installation and improve the sound insulation effect. One end of the arc-shaped plate 403 is installed with the sound insulation plate 404 to increase the sound insulation effect inside the frame 1. The surface of the frame 1 has multiple inner grooves 406 to facilitate the installation of multiple outer plates 408, which increases the overall strength and reduces the problem of deformation under stress. As a result, when the modular sound insulation structure of the space capsule is used, the overall sound insulation effect can be effectively upgraded and adapted, thereby improving the overall sound insulation performance.
[0031] It will be apparent to those skilled in the art that this invention is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or essential characteristics of this invention. Therefore, the embodiments should be considered illustrative and non-limiting in all respects, and the scope of this invention is defined by the appended claims rather than the foregoing description. Thus, it is intended that all variations falling within the meaning and scope of equivalents of the claims be included within this invention. No reference numerals in the claims should be construed as limiting the scope of the claims.
[0032] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.
Claims
1. A modular sound insulation structure for a space capsule, characterized in that: Includes a frame (1), splicing and mounting components disposed on the surface of the frame (1), and sound insulation mounting components disposed on the surface of the frame (1); The splicing and installation assembly includes a snap-fit groove (303) opened on one side of the surface of the frame (1), and a snap-fit block is fixedly connected to the other side of the surface of the frame (1). The snap-fit block is fitted inside the snap-fit groove (303) and multiple frames (1) are spliced together through the snap-fit block. The sound insulation installation assembly includes arc-shaped blocks (401) fixedly connected to the four corners of the inner side of the frame (1). The arc-shaped blocks (401) are concave in shape, and an arc-shaped plate (403) is connected to the surface of the arc-shaped blocks (401). The arc-shaped plate (403) is convex in shape, and a sound insulation plate (404) is fixedly connected to one end of the arc-shaped plate (403). The sound insulation plate (404) is installed through the arc-shaped plate (403).
2. The modular sound insulation structure for a space capsule according to claim 1, characterized in that: The snap-fit plate (301) has a first connection hole (302) on its surface, and a bolt (305) is fitted inside the first connection hole (302).
3. The modular sound insulation structure for a space capsule according to claim 2, characterized in that: The snap-fit groove (303) has a second connecting hole (304) inside, and a bolt (305) is fitted inside the second connecting hole (304). The first connecting hole (302) and the second connecting hole (304) are aligned inside.
4. The modular sound insulation structure for a space capsule according to claim 1, characterized in that: The sound insulation installation assembly also includes a first magnetic block (402) embedded in both sides of the inside of the frame (1), and a second magnetic block (405) embedded in the inside of the sound insulation panel (404).
5. The modular sound insulation structure for a space capsule according to claim 4, characterized in that: The first magnetic block (402) and the second magnetic block (405) are magnetically connected, and the frame (1) has an inner groove (406) on its surface, and there are multiple inner grooves (406).
6. The modular sound insulation structure for a space capsule according to claim 5, characterized in that: The bottom of the inner groove (406) is provided with a glue injection port (407), and an outer plate (408) is connected to the surface of the glue injection port (407).
7. The modular sound insulation structure for a space capsule according to claim 1, characterized in that: The frame (1) has an inner cavity (2) inside, and a sound insulation board (404) is connected inside the inner cavity (2). The frame (1), the arc plate (403) and the arc block (401) are all made of sound insulation material.
Citation Information
Patent Citations
Heat insulation and sound reduction structure of space capsule
CN219365553U