Fabricated modular passive intelligent energy storage type space capsule house

By improving the design of the lifting device, the storage and displacement adjustment of the lifting ring are realized, the problems of easy corrosion and space occupation of the lifting support device are solved, the lifting and adaptability of the space capsule are improved, and the needs of multiple scenarios are met.

CN120759466APending Publication Date: 2025-10-10BEIJING HONGLIANZHONG LIGHT STEEL STRUCTURE HOUSING
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Patent Information

Application Number
CN202510916166.6
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-07-03
Publication Date
2025-10-10

AI Technical Summary

Technical Problem

Existing space capsule lifting support devices are prone to corrosion and damage, affecting the overall structural integrity and floor space. They also have a single function and are unable to meet the lifting needs of multiple scenarios.

Method used

A lifting device is designed, including a hollow seat, a movable seat and a lifting ring body. The storage and expansion of the lifting ring are achieved through the combination of a composite limit rod and a torsion spring. Combined with a composite slide rail and a limit component, displacement adjustment is provided. It is equipped with a water pipe and a travel wheel to meet the lifting, traction and cooling requirements.

Benefits of technology

The lifting device can be stored to reduce the floor space, maintain the integrity of the overall appearance, provide multi-scenario lifting and displacement adjustment, improve adaptability, and meet the lifting, traction and cooling functions.

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Abstract

The invention relates to the technical field of space capsules, and discloses an assembly type modular passive intelligent energy storage space capsule house which comprises a space capsule and a base installed in the space capsule, a plurality of hoisting devices are transversely installed at the top of the space capsule along the structure of the space capsule, and each hoisting device comprises a hollow base and a movable base. The bottom of the hollow base is installed on the top of the space capsule. According to the assembly type modular energy storage space capsule, a hoisting main body structure formed by a movable seat, a composite limiting rod piece and a hoisting ring body in the hoisting device can be contained in a corresponding hollow seat in a reciprocating sleeving mode or expanded to be vertically used, and the requirement that existing hoisting equipment is matched to hoist the space capsule and related structures is met; overall storage and adjustment of the hoisting device can also reduce the occupied space of the space capsule and maintain the appearance integrity of the space capsule, and can also facilitate stacking, conveying and transferring of a plurality of space capsules.
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Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of space capsules, in particular to an assembled modular passive intelligent energy storage space capsule house. BACKGROUND

[0002] The assembled modular energy storage space capsule is a new type of living space combining passive house technology, modular technology, intelligent system and energy storage system, aiming to minimize energy consumption and improve living comfort, and combining modular rapid construction and scene adaptation design, and can realize terrain adaptive layout of desert, forest, coastal and other scenes through intelligent splicing algorithm, meeting the needs of multi-industry such as camping ground and luxury hotel.

[0003] At present, in order to facilitate the transfer of space capsules, the existing technology usually sets a lifting support device on the top of the space capsule to cooperate with the existing lifting equipment to meet the lifting and transfer requirements of the space capsule. However, the lifting support device used at present is a single auxiliary device composed of a lifting ring and a base, which can meet the lifting and transportation requirements, but the protruding lifting ring structure is exposed to the use environment for a long time, which greatly increases the risk of corrosion and damage. In addition, the protruding lifting ring structure will cause certain adverse effects on the integrity of the overall structure of the space capsule and the occupied space. Therefore, in view of the above existing problems, the applicant will provide an assembled modular passive intelligent energy storage space capsule house to solve them. SUMMARY

[0004] Technical problems to be solved In view of the deficiencies of the prior art, the present application provides an assembled modular passive intelligent energy storage space capsule house to solve the problems raised in the background art.

[0005] Technical scheme To achieve the above purpose, the present application provides the following technical scheme: an assembled modular passive intelligent energy storage space capsule house, comprising a space capsule, a base installed on the space capsule, a plurality of lifting devices installed on the top of the space capsule along the structure thereof, the lifting device comprising a hollow seat and a movable seat, the bottom of the hollow seat being installed on the top of the space capsule; A composite limiting rod is arranged between the inner side of the movable seat and the hollow seat, and a lifting ring body is fixed to the surface of the movable seat, the combination of the movable seat and the lifting ring body being capable of being accommodated in the hollow seat under the adjustment of the composite limiting rod.

[0006] Preferably, the composite limiting rod comprises a support shaft, the middle part of the support shaft being fixedly sleeved on the inner side of the bottom of the movable seat, and the bottom of the lifting ring body being fixed to the top of the movable seat. The two ends of the support shaft respectively pass through the front and rear ends of one side of the hollow seat and extend to the outside of the hollow seat. The outside of the end head of the support shaft is provided with an internal threaded sleeve connected to the inner wall of the hollow seat. The end surface of the support shaft is provided with an external thread and is threadedly connected to a torsion spring through the external thread. The torsion spring in a relative position can clamp and limit the support shaft after being threadedly connected to the support shaft. The support shaft is an I-shaped structure, and the end surface of the torsion spring that can contact the hollow seat is provided with a plurality of friction grooves.

[0007] Preferably, a first rubber sheet, a second rubber sheet and a support tube are installed in the other side of the hollow seat, and the support tube is installed between the bottom surface of the first rubber sheet and the inner wall of the other side of the hollow seat. The second rubber sheet is fixedly sleeved inside the other side of the hollow seat and forms a clearance gap with the surface of the first rubber sheet.

[0008] Preferably, a composite slide rail is slidably installed at the bottom of the lifting device arranged in the middle of the space capsule, and the composite slide rail is fixed on the surface of the middle of the space capsule. A superior arc groove is opened on the surface of the composite slide rail, and a spherical rod fixed to the bottom of the corresponding hollow seat is clamped inside the superior arc groove.

[0009] Preferably, the surface of the composite slide rail is provided with a plurality of limiting grooves communicating with the superior arc groove space, and a limiting component is provided between the limiting grooves and the corresponding bottom of the hollow seat; The limiting component includes an internal threaded sleeve, an I-shaped screw, a limiting block, and a guide rod. The internal threaded sleeve is fixed on the side of the hollow seat, and the two ends of the guide rod respectively pass through the internal threaded sleeve and are fixedly connected to the surface of the limiting block. One end of the I-shaped screw is threadedly connected to the internal threaded sleeve and can apply pressure to the limiting block so that the limiting block is clamped in the corresponding limiting groove.

[0010] Preferably, the limit block is specifically a T-shaped structure, and the end of the limit block away from the guide rod is an arc-shaped end. A spring is mounted on the outer side of the end of the guide rod away from the limit block, and the two ends of the spring are respectively fixed on the surface of the internal threaded sleeve and the surface of the end of the guide rod away from the limit block.

[0011] Preferably, a hexagonal groove is provided in the end of the I-shaped screw away from the internal threaded sleeve, and there is a space between the I-shaped screw and the guide rod.

[0012] Preferably, the bottom of the base is provided with a running wheel, the top structure of the running wheel is provided with a threaded hole, the bottom of the base is provided with a clearance hole aligned with the threaded hole, and the bottom of the base and the top of the running wheel can be detachably installed by means of screws fitted into the clearance hole and then threadedly connected to the threaded hole; Two hoisting devices are provided in the middle of the space capsule, and the two hoisting devices can be respectively located outside the front and rear ends of the middle of the space capsule under the sliding adjustment of the corresponding composite slide rails, and form a traction clearance space between them and one side of the space capsule, and a traction component is provided in the traction clearance space; The traction component consists of a traction ring and two traction ropes fixed on the surface of the traction ring. One end of the traction rope away from the traction ring is tied and fixed on the corresponding lifting ring body.

[0013] Preferably, two lifting devices are provided in the middle of the space capsule, and the two lifting devices can be respectively located outside the front and rear ends of the middle part of the space capsule under the sliding adjustment of the corresponding composite slide rails. A guiding and making way space is formed between the lifting devices arranged outside the front and rear ends of the middle part of the space capsule and the lifting devices arranged on both sides of the top of the space capsule. A water pipe is installed in the guiding and making way space, one end of the water pipe is tied and fixed to the lifting ring body in the lifting device on either side of the top of the space capsule, and the other end of the water pipe passes through the lifting ring bodies in the remaining lifting devices in sequence and surrounds along the surface of the space capsule, and a water outlet facing the space capsule is provided on the surface of the water pipe.

[0014] Preferably, the space capsule is composed of a modular assembly of a living room assembly capsule, a bathroom assembly capsule, a bedroom assembly capsule and a balcony assembly capsule, and the splicing structures of two adjacent capsules can be installed by screws; and the frame structures of the living room assembly capsule, the bathroom assembly capsule, the bedroom assembly capsule and the balcony assembly capsule are all integrated with a composite insulation layer, a broken bridge structure, an airtight layer, a water and electricity system, an electrical system and an outer decorative layer from the inside to the outside, and glass components are nested in the bedroom assembly capsule and the balcony assembly capsule.

[0015] Beneficial effects The present invention provides an assembled modular passive intelligent energy storage space capsule house, which has the following beneficial effects: 1. The hoisting device of the assembled modular energy storage space capsule is provided. The main hoisting structure formed by the movable seat, composite limit rod and lifting ring body inside it can be reciprocated and stored or expanded vertically for use inside the corresponding hollow seat. In addition to meeting the needs of cooperating with existing lifting equipment to lift the space capsule and related structures, the overall storage and adjustment of the hoisting device can also reduce the space occupied by the space capsule and maintain the integrity of the space capsule's appearance. It can also facilitate the stacking, transportation and transfer of multiple space capsules.

[0016] 2. The assembled modular energy storage space capsule has a displacement adjustment structure composed of a composite slide rail, a limit component, and a spherical rod. After further combination and use with a lifting device, it can provide displacement adjustment conditions for the lifting device in a relative state, thereby meeting other usage requirements of the space capsule during actual use.

[0017] 3. The assembled modular energy storage space cabin, the water pipe, the walking wheel and the traction component are combined with the displacement adjusting structure and the two hoisting devices in the middle of the space cabin, which can provide traction displacement, water spraying cooling and other extended use conditions for the space cabin, and further improve the self adaptability of the space cabin in complex environment. BRIEF DESCRIPTION OF DRAWINGS

[0018] Figure 1 is a front view of the structure of the present application; Figure 2 is a top view of the structure of the present application; Figure 3 is a sectional view of the space cabin of the structure of the present application; Figure 4 is a sectional view of the hollow seat of the structure of the present application; Figure 5 is a sectional view of the movable seat of the structure of the present application; Figure 6 is a storage diagram of the lifting ring body of the structure of the present application; Figure 7 is a top view of the first rubber sheet of the structure of the present application; Figure 8 is an enlarged diagram of the composite slide rail of the structure of the present application; Figure 9 is an enlarged diagram of the limiting part of the structure of the present application; Figure 10 is an enlarged diagram of the spherical rod of the structure of the present application; Figure 11 is a sectional view of the spherical rod of the structure of the present application; Figure 12 is an enlarged diagram of the structure of the present application Figure 9 at A; Figure 13 is an enlarged diagram of the traction component of the structure of the present application; Figure 14 is a layout diagram of the water pipe of the structure of the present application; Figure 15 is a whole assembly diagram of the space cabin.

[0019] In the figure: 1. Space capsule; 2. Hoisting device; 21. Hollow seat; 22. Movable seat; 23. Composite limiting rod; 231. Support shaft; 232. Torsion spring; 233. Internal threaded sleeve; 24. Lifting ring body; 25. First rubber sheet; 26. Second rubber sheet; 27. Support cylinder; 3. Living room assembly cabin; 4. Bathroom assembly cabin; 5. Bedroom assembly cabin; 6. Composite slide rail; 7. Limiting component; 71. Internal threaded sleeve; 72. I-shaped screw; 73. Limiting block; 74. Guide rod; 75. Spring; 8. Limiting groove; 9. Spherical rod; 10. Traction component; 11. Base; 12. Travel wheel; 13. Water pipe; 14. Balcony assembly cabin. DETAILED DESCRIPTION

[0020] Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making any creative work shall fall within the scope of protection of the present invention.

[0021] Reference Figure 1 An assembled modular passive intelligent energy storage space capsule house includes a passive space capsule 1, which uses the capillary radiation system or heat pump technology in the existing technology to stably control the indoor temperature within the range of 20-26℃, achieving uniform and windless physical comfort.

[0022] The passive Space Capsule 1 is equipped with humidification and dehumidification modules to regulate humidity, maintaining an optimal range of 40-60% 6RH to avoid excessive dryness or dampness. Furthermore, the fresh air system continuously introduces filtered outdoor air to ensure sufficient oxygen content while filtering out pollutants such as PM2.5 and pollen, allowing for hourly indoor air circulation and refreshment.

[0023] The air is kept clean by removing bacteria, volatile organic compounds and other pollutants through a high-efficiency filtration system. The heat transfer coefficient of the passive space capsule 1's outer protective structure does not exceed 0.15w / (m 2 K), the heat loss caused by unit temperature difference per square meter of external surface does not exceed 0.15W.

[0024] The passive capsule 1 is wrapped in insulation material throughout the building, with the insulation structure located inside the exterior envelope. This reduces thermal bridging, eliminates structural thermal bridging risks through thermal break designs or special joint treatments, and eliminates thermal bridging paths.

[0025] Passive houses primarily utilize triple-glazed insulated windows. Counting from the outside in, the second and fifth windows have a Low-E coating. Warm-edge spacers are used, and the glass extends as far as 2-3 cm into the frame. The glass is filled with an inert gas, such as argon or krypton, to reduce the window's thermal conductivity. These triple-glazed, dual-chamber passive windows maximize energy capture while minimizing energy loss. They also offer superior sound insulation and triple sealing for exceptional airtightness.

[0026] Doors, windows, and joints are sealed with highly airtight materials such as rubber and silicone to ensure the building's overall airtightness meets standards. During the construction phase, airtightness checks are strictly enforced, and exhaust heat is recovered during ventilation to maintain a constant indoor temperature and oxygen level (CO2 concentration ≤ 1000ppm).

[0027] See also Figure 1-Figure 7 An assembled modular passive intelligent energy storage space capsule house includes a space capsule 1 and a base 11 installed on the space capsule 1. Several lifting devices 2 are installed on the top of the space capsule 1 along its own structure. The lifting devices 2 include a hollow seat 21 and a movable seat 22. The bottom of the hollow seat 21 is installed on the top of the space capsule 1.

[0028] A composite limiting rod 23 is provided between the movable seat 22 and the inner side of the hollow seat 21, and a lifting ring body 24 is fixed to the surface of the movable seat 22. The assembly of the movable seat 22 and the lifting ring body 24 can be fitted into the interior of the hollow seat 21 for storage under the adjustment of the composite limiting rod 23. The composite limiting rod 23 includes a support shaft 231. The middle part of the support shaft 231 is fixedly fitted into the inner side of the bottom of the movable seat 22. The bottom of the lifting ring body 24 is fixed to the top of the movable seat 22. The two ends of the support shaft 231 respectively pass through the front and rear ends of one side of the hollow seat 21 and extend to the outside of the hollow seat 21. The outer side of the end of the support shaft 231 is provided with an internal threaded sleeve 233 connected to the inner wall of the hollow seat 21. The end surface of the support shaft 231 is provided with an external thread and is threadedly connected to a torsion spring 232 through the external thread. The torsion spring 232 in the relative position can clamp and limit the support shaft 231 after being threadedly connected to the support shaft 231, thereby ensuring the stability of the lifting ring body 24 during vertical lifting and providing a convenient installation environment for the lifting ring body 24. The support shaft 231 is an I-shaped structure, and the end surface of the torsion spring 232 that can contact the hollow seat 21 is provided with a plurality of friction grooves. The plurality of friction grooves can increase the friction force of the torsion spring 232 after contacting the hollow seat 21 and then moving, thereby indirectly improving the structural strength of the torsion spring 232 after being connected to the hollow seat 21.

[0029] During use, the space capsule 1 and the various structures and bases 11 installed therein can be hoisted and transported by tying and fixing the multiple slings of the existing hoisting equipment to the lifting ring bodies 24 of the hoisting device 2 installed on both sides of the top and the middle of the space capsule 1. After completion, the hoisting equipment can use its own multiple slings and the corresponding number of lifting ring bodies 24 to lift them to the appropriate position. After the space capsule 1 is stably installed at the designated location, the multiple hoisting devices 2 in the idle state are stored and adjusted. The specific operations are as follows: By twisting the two torsion springs 232 inside the lifting device 2, the two torsion springs 232 are caused to move spirally away from the hollow seat 21 on the end of the support shaft 231, thereby restoring the freedom of movement of the assembly formed by the movable seat 22 and the lifting ring body 24. At the same time, the internal threaded sleeve 233 will enter the rotational reset automatic reset state from the rotational deformation yielding state of the lifting ring body 24 used vertically, and then drive the lifting ring body 24 and the movable seat 22 to automatically flip to the inside of the hollow seat 21, and be integrated with the hollow seat 21, thereby reducing its own footprint, maintaining the integrity of the overall appearance of the space capsule 1, and optimizing the appearance effect.

[0030] See also Figure 6-Figure 7 The other side of the hollow seat 21 is equipped with a first rubber sheet 25, a second rubber sheet 26 and a support tube 27. The support tube 27 is installed between the bottom surface of the first rubber sheet 25 and the inner wall of the other side of the hollow seat 21. The second rubber sheet 26 is fixedly sleeved inside the other side of the hollow seat 21 and forms a clearance between it and the surface of the first rubber sheet 25.

[0031] During use, considering the objective phenomenon that most of the structure of the lifting ring body 24 is still exposed in the use environment, the first rubber sheet 25, the second rubber sheet 26 and the support tube 27 are provided to cover the lifting ring body 24 for auxiliary protection. The specific principle is as follows: During the process of flipping and storing the lifting ring body 24 into the hollow seat 21, the lifting ring body 24 is first inserted and merged with the first rubber sheet 25, so that the first rubber sheet 25 and the second rubber sheet 26 are deformed and give way. After the lifting ring body 24 is forced through the gap between the first rubber sheet 25 and the second rubber sheet 26, the lifting ring body 24 is inserted and restrained by the support tube 27, and the first rubber sheet 25 and the second rubber sheet 26 are restored to their original position by utilizing their own elastic structure, thereby covering and protecting the lifting ring body 24 and maintaining the long service life of the lifting ring body 24.

[0032] See also Figures 8-12, a composite slide rail 6 is slidably installed at the bottom of the hoisting device 2 arranged in the middle of the space capsule 1, and the composite slide rail 6 is fixed on the surface of the middle part of the space capsule 1. A superior arc groove is provided on the surface of the composite slide rail 6, and a spherical rod 9 fixed to the bottom of the corresponding hollow seat 21 is clamped inside the superior arc groove. The composite slide rail 6 cooperates with the spherical rod 9 to provide displacement adjustment conditions for the corresponding hoisting device 2. A plurality of limiting grooves 8 communicating with the superior arc groove space are provided on the surface of the composite slide rail 6. A limiting component 7 is provided between the limiting groove 8 and the bottom of the corresponding hollow seat 21. The matching set of the limiting component 7 and the limiting groove 8 can limit the hoisting device 2 after displacement; The limiting component 7 includes an internal threaded sleeve 71, an I-shaped screw 72, a limiting block 73, and a guide rod 74. The internal threaded sleeve 71 is fixed to the side of the hollow seat 21. The two ends of the guide rod 74 respectively pass through the internal threaded sleeve 71 and are fixedly connected to the surface of the limiting block 73. One end of the I-shaped screw 72 is threadedly connected to the internal threaded sleeve 71 and can apply pressure to the limiting block 73, so that the limiting block 73 is clamped in the corresponding limiting groove 8. The stop block 73 is specifically a T-shaped structure, and the end of the stop block 73 away from the guide rod 74 is an arc-shaped end, thereby optimizing the smooth effect of the insertion of the corresponding limit groove 8. A spring 75 is sleeved on the outer side of the end of the guide rod 74 away from the stop block 73. The two ends of the spring 75 are respectively fixed to the surface of the internal threaded sleeve 71 and the surface of the end of the guide rod 74 away from the stop block 73. The spring 75 serves as an auxiliary structure and can provide auxiliary power for the automatic reset of the limit block 73 and the guide rod 74 after movement, thereby improving the use effect of the relevant structure. An inner hexagonal groove is provided in the end of the I-shaped screw 72 away from the internal threaded sleeve 71, which facilitates subsequent twisting and force application, improving the convenience of using the structure. There is also a space between the I-shaped screw 72 and the guide rod 74 to avoid structural interference when adjacent structures cooperate.

[0033] During use, in order to meet different usage requirements, the composite slide rail 6 can be used as a mobile support to adjust the displacement of the hoisting device 2 set in the middle of the space capsule 1. The specific operation is as follows: The spherical rod 9 is used to engage and guide the composite slide rail 6 to make the lifting device 2 move to the specified position along the surface of the composite slide rail 6. After completion, the I-shaped screw 72 is turned, and the I-shaped screw 72 is spirally engaged with the internal threaded sleeve 71 and gradually presses the limit block 73 until the limit block 73 is engaged with the preset corresponding limit groove 8. In this way, the overall limit requirement of the moved lifting device 2 is completed, and in the process of engaging and fitting the limit block 73 with the limit groove 8, the guide rod 74 is engaged with the internal threaded sleeve 71 to provide displacement guidance for the limit block 73, and the spring 75 is deformed to make way.

[0034] See also Figure 13The bottom of the base 11 is provided with a running wheel 12, and the top structure of the running wheel 12 is provided with a threaded hole. The bottom of the base 11 is provided with a clearance hole aligned with the threaded hole, and the bottom of the base 11 and the top of the running wheel 12 can be detachably installed by screws and the clearance hole set and then threadedly connected with the threaded hole; Two hoisting devices 2 are provided in the middle of the space capsule 1. The two hoisting devices 2 can be respectively positioned outside the front and rear ends of the middle of the space capsule 1 under the sliding adjustment of the corresponding composite slide rails 6, and form a traction clearance space between them and one side of the space capsule 1. A traction component 10 is provided in the traction clearance space. The traction component 10 is composed of a traction ring and two traction ropes fixed on the surface of the traction ring. The ends of the traction ropes away from the traction ring are tied and fixed to the corresponding lifting ring body 24.

[0035] When in use, when it is necessary to move a short to medium distance and the moving space cannot accommodate large equipment such as lifting equipment, the existing jack is first used to lift the space capsule 1 so that there is enough clearance between the base 11 and the ground. Then, multiple running wheels 12 are sequentially installed on the bottom of the base 11 on both sides of the bottom of the space capsule 1. After completion, the jack is removed, and the multiple running wheels 12 are used in conjunction with the corresponding number of bases 11 to support the space capsule 1 and its associated structures and provide conditions for movement; Next, the two lifting devices 2 are moved along the surface of the composite slide rail 6 to the designated positions outside the front and rear ends of the space capsule 1. After completion, the I-shaped screw 72 is turned, and the I-shaped screw 72 is spirally engaged with the internal threaded sleeve 71 and gradually presses the limit block 73 until the limit block 73 is engaged with the preset corresponding limit groove 8, thereby completing the overall limit requirement of the moved lifting device 2. Subsequently, the two traction ropes inside the traction component 10 are respectively tied and fixed to the lifting ring bodies 24 in the two lifting devices 2, and then a small mobile device is used to drive the traction component 10, so that the space capsule 1 and the related structures of the space capsule 1 can be automatically moved over medium and short distances.

[0036] See also Figure 14 Two lifting devices 2 are provided in the middle of the space capsule 1, and the two lifting devices 2 can be respectively located outside the front and rear ends of the middle part of the space capsule 1 under the sliding adjustment of the corresponding composite slide rails 6. A guiding and making way space is formed between the lifting devices 2 arranged outside the front and rear ends of the middle part of the space capsule 1 and the lifting devices 2 arranged on both sides of the top of the space capsule 1. A water pipe 13 is installed in the guiding and making way space. One end of the water pipe 13 is tied and fixed to the lifting ring body 24 in the lifting device 2 on either side of the top of the space capsule 1, and the other end of the water pipe 13 passes through the lifting ring bodies 24 in the remaining lifting devices 2 in sequence and surrounds along the surface of the space capsule 1. A water outlet facing the space capsule 1 is provided on the surface of the water pipe 13.

[0037] During use, considering the problem of failure of the cooling system of the space capsule 1 under high-temperature use, the two lifting devices 2 can be moved along the surface of the composite slide rail 6 to the designated positions outside the front and rear ends of the space capsule 1. After completion, the I-shaped screw 72 is screwed, and the I-shaped screw 72 is spirally engaged with the internal threaded sleeve 71 and gradually presses the limit block 73 until the limit block 73 is engaged with the preset corresponding limit groove 8, thereby completing the overall limit requirement of the moved lifting device 2. Subsequently, one end of the water pipe 13 is tied and fixed to the lifting ring body 24 in the lifting device 2 on either side of the top of the space capsule 1, and the other end of the water pipe 13 passes through the lifting ring body 24 in the remaining lifting devices 2 in turn and surrounds the surface of the space capsule 1, and the other end port of the water pipe 13 cooperates with the small water pump carried, which can automatically spray water on the surface of the space capsule 1 through the water pipe 13 for water cooling.

[0038] See also Figure 15 The space capsule 1 is composed of a modular assembly of a living room assembly capsule 3, a bathroom assembly capsule 4, a bedroom assembly capsule 5 and a balcony assembly capsule 14, and the splicing structures of two adjacent capsules can be installed by screws; and the frame structures of the living room assembly capsule 3, the bathroom assembly capsule 4, the bedroom assembly capsule 5 and the balcony assembly capsule 14 are integrated with a composite insulation layer, a thermal break structure, an airtight layer, a water and electricity system, an electrical system and an external decorative layer from the inside to the outside, and glass components are nested in the bedroom assembly capsule 5 and the balcony assembly capsule 14.

[0039] When in use, the modular assembly of the living room assembly cabin 3, the bathroom assembly cabin 4, the bedroom assembly cabin 5 and the balcony assembly cabin 14 forms a space capsule 1, which can achieve the effect of a space capsule plus a passive house in terms of the specific setting and use of the overall structure, and on this basis forms a passive space capsule, and the main structure of each cabin is bolted together and then insulated, thermally insulated, water and electricity, and internal and external decorative lights are installed; Furthermore, the living room assembly cabin 3, the bathroom assembly cabin 4, the bedroom assembly cabin 5 and the balcony assembly cabin 14 are modularly assembled in the process of forming the space capsule 1, just like building blocks, and the finished product is obtained after the assembly is completed.

[0040] It should be noted that, in this document, relational terms such as first and second, etc., are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that includes a list of elements includes not only those elements but also other elements not explicitly listed, or elements inherent to such process, method, article, or apparatus.

[0041] While embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions, and variations may be made to these embodiments without departing from the principles and spirit of the invention, and that the scope of the invention is defined by the appended claims and their equivalents.

Claims

1. An assembled modular passive intelligent energy storage space capsule house, comprising a space capsule (1) and a base (11) mounted on the space capsule (1), characterized in that: The top of the space capsule (1) is laterally mounted with a plurality of lifting devices (2), the lifting devices (2) comprising a hollow seat (21) and a movable seat (22), the bottom of the hollow seat (21) being mounted on the top of the space capsule (1); A composite limiting rod (23) is provided between the movable seat (22) and the inner side of the hollow seat (21), and a hanging ring body (24) is fixed to the surface of the movable seat (22). The assembly of the movable seat (22) and the hanging ring body (24) can be fitted into the interior of the hollow seat (21) for storage under the adjustment of the composite limiting rod (23).

2. The assembled modular passive intelligent energy storage space capsule house according to claim 1, characterized in that: The composite limiting rod (23) includes a support shaft (231), the middle portion of the support shaft (231) is fixedly sleeved on the inner side of the bottom of the movable seat (22), and the bottom of the lifting ring body (24) is fixed on the top of the movable seat (22); The two ends of the support shaft (231) respectively pass through the front and rear ends of one side of the hollow seat (21) and extend to the outside of the hollow seat (21); the outer side of the end of the support shaft (231) is provided with an internal thread sleeve (233) connected to the inner wall of the hollow seat (21); the end surface of the support shaft (231) is provided with an external thread and is threadedly connected to a torsion spring (232) through the external thread; and the torsion spring (232) in a relative position can clamp and limit the support shaft (231) after being threadedly connected to the support shaft (231); The support shaft (231) is an I-shaped structure, and a plurality of friction grooves are provided on the end surface of the torsion spring (232) that is in contact with the hollow seat (21).

3. The assembled modular passive intelligent energy storage space capsule house according to claim 1, characterized in that: The other side of the hollow seat (21) is internally sleeved with a first rubber sheet (25), a second rubber sheet (26) and a support tube (27). The support tube (27) is installed between the bottom surface of the first rubber sheet (25) and the inner wall of the other side of the hollow seat (21). The second rubber sheet (26) is fixedly sleeved inside the other side of the hollow seat (21) and forms a clearance gap with the surface of the first rubber sheet (25).

4. The assembled modular passive intelligent energy storage space capsule house according to claim 1, characterized in that: A composite slide rail (6) is slidably mounted on the bottom of the hoisting device (2) provided in the middle of the space capsule (1). The composite slide rail (6) is fixed on the surface of the middle of the space capsule (1). A superior arc groove is provided on the surface of the composite slide rail (6), and a spherical rod (9) fixed to the bottom of the corresponding hollow seat (21) is clamped inside the superior arc groove.

5. The assembled modular passive intelligent energy storage space capsule house according to claim 4, characterized in that: The surface of the composite slide rail (6) is provided with a plurality of limiting grooves (8) communicating with the superior arc groove space, and a limiting component (7) is provided between the limiting grooves (8) and the bottom of the corresponding hollow seat (21); The limiting component (7) includes an internal threaded sleeve (71), an I-shaped screw (72), a limiting block (73), and a guide rod (74). The internal threaded sleeve (71) is fixed on the side of the hollow seat (21). Both ends of the guide rod (74) respectively pass through the internal threaded sleeve (71) and are fixedly connected to the surface of the limiting block (73). One end of the I-shaped screw (72) is threadedly connected to the internal threaded sleeve (71) and can apply pressure to the limiting block (73) so that the limiting block (73) is clamped in the corresponding limiting groove (8).

6. The assembled modular passive intelligent energy storage space capsule house according to claim 5, characterized in that: The limit block (73) is specifically a T-shaped structure, and the end of the limit block (73) away from the guide rod (74) is an arc-shaped end. A spring (75) is sleeved on the outer side of one end of the guide rod (74) away from the limit block (73), and the two ends of the spring (75) are respectively fixed on the surface of the internal thread sleeve (71) and the surface of one end of the guide rod (74).

7. The assembled modular passive intelligent energy storage space capsule house according to claim 5, characterized in that: An inner hexagonal groove is provided in the end of the I-shaped screw (72) away from the internal thread sleeve (71), and a space is provided between the I-shaped screw (72) and the guide rod (74).

8. The assembled modular passive intelligent energy storage space capsule house according to claim 1, characterized in that: The bottom of the base (11) is provided with a running wheel (12), the top structure of the running wheel (12) is provided with a threaded hole, the bottom of the base (11) is provided with a clearance hole aligned with the threaded hole, and the bottom of the base (11) and the top of the running wheel (12) can be detachably installed by screws fitted into the clearance hole and then threadedly connected to the threaded hole; Two hoisting devices (2) are provided in the middle of the space capsule (1), and under the sliding adjustment of the corresponding composite slide rail (6), the two hoisting devices (2) can be respectively located outside the front and rear ends of the middle of the space capsule (1) and form a traction clearance space between the space capsule (1) and one side, and a traction component (10) is provided in the traction clearance space; The traction component (10) consists of a traction ring and two traction ropes fixed on the surface of the traction ring, and one end of the traction rope away from the traction ring is tied and fixed to the corresponding lifting ring body (24).

9. The assembled modular passive intelligent energy storage space capsule house according to claim 1, characterized in that: Two hoisting devices (2) are provided in the middle of the space capsule (1), and the two hoisting devices (2) can be respectively located outside the front and rear ends of the middle of the space capsule (1) under the sliding adjustment of the corresponding composite slide rail (6). A guiding space is formed between the hoisting devices (2) provided outside the front and rear ends of the middle of the space capsule (1) and the hoisting devices (2) provided on both sides of the top of the space capsule (1). A water pipe (13) is provided in the guiding space. One end of the water pipe (13) is tied and fixed to a hoisting ring body (24) in a hoisting device (2) on either side of the top of the space capsule (1), and the other end of the water pipe (13) passes through the hoisting ring bodies (24) in the remaining hoisting devices (2) in sequence and surrounds along the surface of the space capsule (1). A water outlet facing the space capsule (1) is provided on the surface of the water pipe (13).

10. The assembled modular passive intelligent energy storage space capsule house according to claim 1, characterized in that: The space capsule (1) is composed of a living room assembly capsule (3), a bathroom assembly capsule (4), a bedroom assembly capsule (5), and a balcony assembly capsule (14) in a modular assembly manner, and the splicing structure of two adjacent capsules can be installed by screws; Furthermore, the frame structures of the living room assembly cabin (3), the bathroom assembly cabin (4), the bedroom assembly cabin (5) and the balcony assembly cabin (14) are all integrated with a composite insulation layer, a broken bridge structure, an airtight layer, a water and electricity system, an electrical system and an outer decorative layer from the inside out, forming a use effect similar to a passive house. Glass components are nested and installed in the bedroom assembly cabin (5) and the balcony assembly cabin (14).