Prefabricated passive intelligent energy storage space cabin house

Abstract

The application relates to an assembled passive intelligent energy storage space cabin house, and relates to the technical field of residential facilities, which comprises a space cabin house, the space cabin house comprises a main body unit, the surface of the main body unit is provided with an energy supply unit, and the surface of the main body unit is also provided with an expansion unit. The application has the following remarkable technical effects: efficient dynamic lighting and space saving are realized through the foldable energy supply unit; the expansion unit adopts a rigid structure to enhance stability and expandability; the shell adopts an aviation aluminum plate combined with a multilayer composite structure, which can guarantee high strength and light weight to resist extreme environments, realize intelligent temperature control through an insulation layer and a carbon crystal plate, optimize lighting and ventilation through a motorized skylight, and comprehensively improve the environmental adaptability, energy efficiency, structural reliability and living comfort of the house, so that the application can meet the application requirements in multiple scenes.

Description

TECHNICAL FIELD

[0001] The present application relates to a residential facility, in particular to a prefabricated passive intelligent energy storage space cabin house. BACKGROUND

[0002] At present, with the increasing demand for temporary or long-term residential facilities in the fields of field scientific research, disaster emergency, remote area residence and space exploration, prefabricated modular houses have been widely used due to their advantages of rapid assembly and strong mobility. However, the adaptability of the prefabricated houses in the prior art in complex environments still has significant deficiencies: in terms of energy supply, the traditional energy supply system mostly uses fixed solar panels or independent power generation equipment. The former cannot be dynamically adjusted according to the light angle, resulting in low energy conversion efficiency, and the external structure occupies a large amount of external space, affecting personnel activities and equipment deployment. The latter has problems such as low integration, complex cable connection and large energy loss, and is difficult to meet the continuous power supply demand in off-grid environments. In terms of space utilization, the existing expansion structure generally relies on movable connections such as sliding or hinging, which can achieve space expansion, but has defects such as insufficient support stability, limited expansion range and decreasing structural strength with expansion distance, especially in extreme environments such as strong wind and high-low temperature difference, which is prone to connection rupture or deformation, and cannot guarantee the safety of long-term use. The completely fixed expansion design faces the problems of large transportation volume and complex on-site assembly, and it is difficult to balance the transportation convenience and space demand in use. In terms of structural integration and reliability, the functional modules of the traditional prefabricated house, such as the energy supply system, the main frame and the expansion structure, are independently designed, and the connection parts are prone to stress concentration points. In addition, the energy collection, storage and distribution system lacks collaborative control, resulting in low overall energy efficiency. Furthermore, the design of the support structure in the prior art does not fully consider the adaptability to complex terrain, and the single-point or four-point support method has insufficient anti-overturning capacity in soft ground and slope scenes, limiting its application in extreme environments.

[0003] In view of the above related technologies, the present application provides a prefabricated passive intelligent energy storage space cabin house, which realizes efficient energy utilization and space saving through a foldable energy supply unit, solves the contradiction between stability and transportation convenience of the existing expansion structure through a modular expansion unit, and forms an integrated support system through the rigid connection design of the main unit and each functional module, significantly improving the adaptability and reliability in complex environments, and meeting the urgent demand for high-performance residential facilities in field operations, emergency resettlement, space exploration and other scenarios. SUMMARY

[0004] The purpose of the present application is to provide a prefabricated passive intelligent energy storage space cabin house.

[0005] The application provides an assembled passive intelligent energy storage space cabin house which adopts the technical scheme as follows: the space cabin house comprises a main unit, the surface of the main unit is provided with an energy supply unit, the surface of the main unit is also provided with an expansion unit, and the surface of the main unit is fixedly connected with an outer shell unit;

[0006] The expansion unit is used for expanding the space cabin house, the expansion unit comprises an expansion frame, the top end of the expansion frame is fixedly connected with a support frame four, the bottom end of the expansion frame is fixedly connected with a support frame five, the bottom end of the expansion frame is also fixedly connected with a support frame six, one end of the support frame six away from the expansion frame is fixedly connected with a support foot two, the top end of the expansion frame is fixedly connected with a support column three, the inner wall of the expansion frame is fixedly connected with a support column four, the inner wall of the expansion frame is also fixedly connected with a support column five, the surface of the expansion frame is sleeved with a connecting frame three, the surface of the expansion frame is also sleeved with a connecting frame four, and the inner side surface of the connecting frame four is fixedly connected with a support frame seven.

[0007] Preferably, the energy supply unit is used for supplying energy to the space cabin house and can be folded to save space, the energy supply unit comprises a connecting frame one, the surface of the connecting frame one is fixedly connected with a support plate, the surface of the connecting frame one is also fixedly connected with a support block one, the surface of the support plate is fixedly connected with a mounting frame, the surface of the mounting frame is fixedly connected with a first motor, the output end of the first motor is fixedly connected with a lead screw, the surface of the lead screw is threadedly connected with a sliding block, the inner wall of the sliding block is rotatably connected with a rotating block one, the inner wall of the rotating block one is rotatably connected with a transmission rod, the two ends of the transmission rod are provided with the same rotating block one, one end of the rotating block one away from the transmission rod is rotatably connected with a rotating seat, and the bottom end of the rotating seat is fixedly connected with a solar panel.

[0008] Preferably, the surface of the solar panel is rotatably connected with a rotating block two, the surface of the rotating block two is rotatably connected with a connecting frame two, and the surface of the connecting frame two is fixedly connected with a support block two.

[0009] Preferably, the main unit comprises a main frame, the inner wall of the main frame is fixedly connected with a support column one, the top end of the main frame is fixedly connected with a support frame one, the support frame one is provided with two groups, the two groups of support frames one are linearly arranged along the inner wall of the main frame, the bottom end of the main frame is fixedly connected with a support frame two, the bottom end of the main frame is fixedly connected with a support frame three, the bottom end of the support frame three is fixedly connected with a support foot one, and the inner wall of the main frame is also fixedly connected with a support column two.

[0010] Preferably, the surface of the main frame is fixedly connected with the connecting frame two, the surface of the main frame is slidingly connected with the connecting frame three, and the surface of the main frame is slidingly connected with the connecting frame four.

[0011] Preferably, the inner wall of the connecting frame one is fixedly connected with the connecting frame three, the inner side surface of the supporting block one is fixedly connected with the main frame, and the inner side surface of the supporting block one is further fixedly connected with the inner wall of the expansion frame.

[0012] Preferably, the inner side surface of the supporting block two is fixedly connected with the supporting column two, and the inner side surface of the supporting block two is further fixedly connected with the surface of the supporting column one.

[0013] Preferably, the mounting frame is provided with two, the two mounting frames are linearly arranged and distributed along the surface of the supporting plate, and the two ends of the lead screw are rotationally connected with the inner wall of the mounting frame.

[0014] Preferably, the shell unit comprises an aviation aluminum plate, the inner wall of the aviation aluminum plate is fixedly connected with an electric sunroof, the surface of the aviation aluminum plate is provided with a hatch, the inner wall of the aviation aluminum plate is fixedly connected with foamed polyurethane, the inner wall of the foamed polyurethane is fixedly connected with a rot-resistant wooden keel, the inner wall of the rot-resistant wooden keel is fixedly connected with a European pine board, the inner wall of the European pine board is fixedly connected with a carbon crystal plate, the inner wall of the carbon crystal plate is fixedly connected with a glass window, the inner wall of the foamed polyurethane is fixedly connected with the surface of a supporting frame one, and the inner wall of the rot-resistant wooden keel is fixedly connected with the surface of the supporting frame one.

[0015] In summary, the present application has at least one of the following beneficial technical effects:

[0016] 1. The innovative foldable energy supply unit realizes efficient energy acquisition and flexible space adaptation. The cooperation of the double rotary pair linkage mechanism rotating block one, rotating block two and the lead screw transmission system enables the solar panel to realize multi-angle dynamic adjustment and complete folding storage, breaking through the limitations of traditional fixed or single-axis adjustment energy supply devices. The transmission rod drives the solar panel to rotate around the rotating block two as a fulcrum, and combined with the vertical swing of the rotating seat, it can realize ±90° pitch angle and ±45° horizontal angle adjustment. Based on the geometric relationship between the structural degrees of freedom and the light incidence angle, the power generation efficiency at different latitudes and seasons is improved compared with the traditional fixed inclination angle solar panel. When not in use, the solar panel can be folded along the surface of the main frame to a state close to the wall surface, with a thickness increase of only 15-20 cm. Compared with the traditional external fixed design, it saves a large external activity space, effectively solves the conflict between energy acquisition and personnel activity space in a small area, and is especially suitable for scenes with strict space utilization requirements such as space cabin exterior, field workstation, etc.

[0017] 2. The body fixed expansion unit realizes modular space expansion and structural stability enhancement. Unlike the instability of existing assembly type houses relying on sliding or hinged structure to realize expansion, the application is designed by fixed connection of expansion frame and main unit, to support frame four, five, six and support column three, four, five to form a rigid expansion structure, while maintaining the integrity of the main frame, realizing space extension: the expansion frame is independently contacted with the ground through the support foot two, and cooperates with the support foot one of the main unit to form a six-point support system, which improves the overturning moment compared with the traditional four-point support, and significantly enhances the adaptability to complex terrain; the inside is rigidly connected with the support column one and two of the main frame through the support column four and five, so that the structural strength of the expanded space is consistent with that of the main unit, avoiding the weak connection problem of existing sliding expansion structure, and keeping compact state during transportation, quickly assembling on site through fixed bolts, realizing stable expansion of use area, based on the geometric size ratio of the expansion frame and the main frame, suitable for scenes requiring long-term fixed deployment and high structural safety requirements such as polar scientific research station and disaster permanent settlement point;

[0018] 3. Integrated assembly type design realizes efficient transportation and multi-module function cooperation The application modularly integrates the main unit, the energy supply unit and the expansion unit, solves the pain points of existing assembly type buildings, such as large transportation volume, complicated assembly and independent operation of functional modules, the energy supply unit and the expansion unit are closely attached to the main frame, the overall packaging volume is reduced compared with traditional houses with the same function, a single standard container can transport 2-3 complete sets of equipment, greatly reducing transportation cost and space occupation; the support block one simultaneously fixes the inner walls of the main frame and the expansion frame, the support block two connects the support column of the main unit, so that the three modules form a rigid whole, avoiding the weak problem of the connection of traditional assembly type structure, at the same time, the electric energy of the energy supply unit can be directly input into the energy storage system of the main unit, realizing closed-loop management of energy collection-storage-distribution through intelligent control, reducing energy loss by more than 15% compared with existing independent energy supply equipment, through deep cooperation of mechanical structure and functional system, the reliability and energy efficiency ratio of the overall equipment are improved. BRIEF DESCRIPTION OF DRAWINGS

[0019] Figure 1 It is a whole structure schematic diagram of the application;

[0020] Figure 2 It is an internal filling structure schematic diagram of the application;

[0021] Figure 3 It is a part of the filling structure schematic diagram of the application;

[0022] Figure 4 It is a whole frame structure schematic diagram of the application;

[0023] Figure 5 It is a whole frame structure split schematic diagram of the application;

[0024] Figure 6 Part structure schematic diagram of the present application;

[0025] Figure 7 Energy supply unit structure schematic diagram of the present application;

[0026] Figure 8 Part structure schematic diagram of the present application.

[0027] Mark explanation: 1, space cabin house; 10, main unit; 1001, main frame; 1002, support column one; 1003, support frame one; 1004, support frame two; 1005, support frame three; 1006, support foot one; 1007, support column two; 20, energy supply unit; 2001, connecting frame one; 2002, support plate; 2003, support block one; 2004, mounting frame; 2005, first motor; 2006, lead screw; 2007, sliding block; 2008, rotating block one; 2009, rotating seat; 2010, solar panel; 2011, rotating block two; 2012, connecting frame two; 2013, support block two; 2014, transmission rod; 30, expansion unit; 3001, expansion frame; 3002, support frame four; 3003, support frame five; 3004, support frame six; 3005, support foot two; 3006, support column three; 3007, support column four; 3008, support column five; 3009, connecting frame three; 3010, connecting frame four; 3011, support frame seven; 40, shell unit; 4001, aviation aluminum plate; 4002, electric sunroof; 4003, cabin door; 4004, foamed polyurethane; 4005, anti-corrosion wood keel; 4006, osb board; 4007, carbon crystal plate; 4008, glass window. DETAILED DESCRIPTION

[0028] The present application is further described in detail below in combination with 1-8.

[0029] A prefabricated passive intelligent energy storage space cabin house, referring to Figures 1-6, including a space cabin house 1, through the capillary radiation system or heat pump technology in the prior art, the indoor temperature is stably controlled in the range of 20-26℃, the uniform and windless comfortable feeling is realized, the passive space cabin house 1 is also provided with a humidification and dehumidification module to adjust humidity and keep in the range of 40-etc: avoid excessive dryness or humidity. Above and it can rely on the fresh air system to continuously introduce 60% RH to ensure sufficient oxygen content, while filtering PM2.5, pollen and other pollutants, the filtered outdoor air realizes indoor air circulation update per hour. Through the high-efficiency filtration system to remove bacteria, volatile organic compounds and other pollutants, maintain air cleanliness. The heat transfer coefficient of the passive space house 1 is not more than 0.15 W / (m'K), the heat loss per square meter of the outer surface caused by unit temperature difference is not more than 0.15 W. The passive space cabin house 1 is wrapped by the thermal insulation material outside the building and the passive space cabin house 1 is located inside the thermal insulation structure of the outer envelope. Thus reduce the "thermal bridge" phenomenon, eliminate the risk of structural thermal bridge by bridge design or special node treatment, eliminate the thermal bridge path. The passive house mainly adopts three glass thermal insulation windows, from outside to inside, the second and fifth surfaces have 1ow-e coating edge spacing strips, the glass extends into the window frame by 2-3cm, the glass is filled with argon or the glass adopts inert gas such as warm, krypton gas to reduce the thermal conductivity of the window body. The passive window with two cavities can obtain more energy while reducing energy loss; superior sound insulation effect; three seals, air tightness is extremely reasonable. The door and window, joint and other parts are provided with high air tightness material such as rubber and silicone seal to ensure that the overall air tightness of the building meets the standard. The air tightness node needs to be strictly checked during the construction stage, and the exhaust heat is recovered while ventilating to maintain the indoor constant temperature and constant air (C0: concentration ≤1000ppm). The space cabin house 1 comprises a main unit 10, a power supply unit 20 is arranged on the surface of the main unit 10, an expansion unit 30 is also arranged on the surface of the main unit 10, and an outer shell unit 40 is fixedly connected to the surface of the main unit 10;

[0030] The expansion unit 30 is used for expanding the space cabin house 1, and the expansion unit 30 comprises an expansion frame 3001, a support frame four 3002 is fixedly connected to the top end of the expansion frame 3001, a support frame five 3003 is fixedly connected to the bottom end of the expansion frame 3001, a support frame six 3004 is also fixedly connected to the bottom end of the expansion frame 3001, a support foot two 3005 is fixedly connected to the end, away from the expansion frame 3001, of the support frame six 3004, a support column three 3006 is fixedly connected to the top end of the expansion frame 3001, a support column four 3007 is fixedly connected to the inner wall of the expansion frame 3001, a support column five 3008 is also fixedly connected to the inner wall of the expansion frame 3001, a connecting frame three 3009 is sleeved on the surface of the expansion frame 3001, a connecting frame four 3010 is also sleeved on the surface of the expansion frame 3001, and a support frame seven 3011 is fixedly connected to the inner side surface of the connecting frame four 3010.

[0031] The expansion unit 30 is used for expanding the space capsule house 1, which includes an expansion frame 3001 as a main support structure, a support frame four 3002 fixedly connected at the top end and a support frame five 3003, a support frame six 3004 fixedly connected at the bottom end, which together constitute the upper and lower end support system of the frame, wherein the support frame six 3004 is fixedly connected with a support foot two 3005 at the end away from the expansion frame 3001, for stably transmitting the weight of the expansion unit to the ground, and forming a multi-point support with the support foot one 1006 of the main unit 10 to enhance the overall stability; the support column three 3006 at the top end of the expansion frame 3001 is fixedly connected with a support column four 3007 and a support column five 3008 fixedly connected with the inner wall, which respectively reinforce the structure of the expansion frame 3001 from the top and the inside, improve the anti-deformation and load-bearing capacity of the frame, and ensure the strength of the space structure after expansion; the connection frame three 3009 and the connection frame four 3010 on the surface of the expansion frame 3001 serve as interface components for connecting the frame with the outside or other units, wherein the support frame seven 3011 fixedly connected to the inner surface of the connection frame four 3010 can further assist the connection frame four 3010 in supporting the expansion frame 3001, while providing a mounting fulcrum for possible external equipment or structures, so that the expansion unit 30 not only expands the space, but also forms a stable and reliable support structure through the coordinated action of various components, meeting the strength and safety requirements of the space capsule house in the expanded state.

[0032] The energy supply unit 20 is used for supplying energy to the space capsule house 1, which can be folded to save space. The energy supply unit 20 includes a connection frame one 2001, a support plate 2002 fixedly connected to the surface of the connection frame one 2001, a support block one 2003 fixedly connected to the surface of the connection frame one 2001, an installation frame 2004 fixedly connected to the surface of the support plate 2002, a first motor 2005 fixedly connected to the surface of the installation frame 2004, a lead screw 2006 fixedly connected to the output end of the first motor 2005, a sliding block 2007 threadedly connected to the surface of the lead screw 2006, a rotating block one 2008 rotatably connected to the inner wall of the sliding block 2007, a transmission rod 2014 rotatably connected to the inner wall of the rotating block one 2008, the same rotating block one 2008 provided at both ends of the transmission rod 2014, a rotating seat 2009 rotatably connected to one end of the rotating block one 2008 away from the transmission rod 2014, and a solar panel 2010 fixedly connected to the bottom end of the rotating seat 2009.

[0033] The energy supply unit 20 is an energy supply module of the space cabin house 1, which realizes space saving while meeting efficient energy supply through a foldable structure design. The specific structure and functions are as follows: the connecting frame one 2001 serves as a basic installation carrier, and the support plate 2002 and the support block one 2003 fixed on the surface bear different functions respectively. The support plate 2002 is used for installing the power transmission assembly, and the support block one 2003 is fixed on the inner side of the main body frame 1001 and the inner wall of the expansion frame 3001, realizing the rigid connection of the energy supply unit and the main body structure. The mounting bracket 2004 on the surface of the support plate 2002 fixes the first motor 2005, and the lead screw 2006 at the output end of the motor rotates under the drive of the motor. The sliding block 2007 connected by threads converts the rotary motion into linear motion, and the rotating block one 2008 on the inner wall of the sliding block 2007 forms a rotating pair with the rotating block one 2008 at both ends of the transmission rod 2014, so that the linear motion of the sliding block can drive the transmission rod 2014 to translate. The rotating block one 2008 at the other end of the transmission rod 2014 is rotationally connected with the rotating seat 2009, and the solar panel 2010 fixed at the bottom end of the rotating seat 2009 can rotate around the rotating seat 2009. At the same time, the solar panel 2010 is rotationally connected with the connecting frame two 2012 through the rotating block two 2011, forming a double rotating pair linkage mechanism. When the first motor 2005 rotates forward, the sliding block 2007 is driven to move by the lead screw 2006, and the solar panel 2010 is unfolded to the working angle by the transmission rod 2014, and the rotation of the rotating seat 2009 is used for pitch adjustment to align with the sunlight, so as to improve the light energy absorption efficiency. When it is necessary to save space, the motor is reversed to drive the sliding block 2007 to move reversely, and the transmission rod 2014 is pulled to make the solar panel 2010 fold around the rotating seat 2009 to be close to the surface of the main body frame 1001. At this time, the support block one 2003 and the connecting frame one 2001 jointly bear the structural support function, ensuring the stability of the folded state. The whole system realizes the foldability and intelligent control of the energy supply module through the coordinated operation of the components with the same reference numerals, meets the energy demand of the space cabin house, solves the problem of space occupation through structural design optimization, eliminates the risk of structural thermal bridge through broken bridge design, completely eliminates the thermal bridge path, avoids energy loss and condensation problems caused by local temperature difference, and realizes zero leakage under extreme temperature and humidity through high-weather-resistant sealing strips and silicone weather-resistant glue. The air tightness n50 is less than or equal to 0.6, water-tightness ≥ 1500Pa, its cabin drinking water with a complete set of water supply system, water supply system is prior art, set up in the warehouse outside the decorative lamp, decorative lamp for power saving lamp, and the internal circuit connection is prior art, space cabin house has five designs: constant temperature, constant humidity, constant oxygen, constant clean and constant static, in the constant temperature aspect through capillary tube radiation system or heat pump technology, the indoor temperature is stably controlled in 20-26℃ range, realize uniform and no wind feel of body comfort, these slender pipes are densely distributed in the ceiling, wall or floor in the form of network, form high efficient heat exchange network. When the system runs, low temperature hot water or cold water circulates in the capillary tube, exchanges heat with indoor environment through radiation heat exchange, for example, through low temperature hot water radiation heating in winter, through high temperature cold water radiation cooling in summer, in the constant humidity aspect, adjust humidity through humidification and dehumidification module, keep in 40-60%RH etc. Suitable range, avoid excessive dry or humid, in the constant oxygen aspect, rely on fresh air system to continuously introduce filtered outdoor air, ensure sufficient oxygen content, at the same time, filter PM2.5, pollen and other pollutants, realize indoor air circulation update every hour, in the whole system realizes the effect of high efficiency, energy saving and low carbon environmental protection, in the constant clean aspect, remove bacteria, volatile organic compounds (VOC) and other pollutants through high efficiency filtration system, maintain air cleanliness, in the constant static aspect, the space cabin adopts multi-layer sound insulation material, so that the environment in the cabin remains quiet, and the noise outside can be greatly reduced.

[0034] The surface of the solar panel 2010 is rotatably connected with a rotating block two 2011, the surface of the rotating block two 2011 is rotatably connected with a connecting frame two 2012, and the surface of the connecting frame two 2012 is fixedly connected with a supporting block two 2013.

[0035] The surface of the solar panel 2010 is rotatably connected with a rotating block two 2011, the surface of the rotating block two 2011 is rotatably connected with a connecting frame two 2012, and the surface of the connecting frame two 2012 is fixedly connected with a supporting block two 2013.

[0036] The main body unit 10 comprises a main body frame 1001, the inner wall of the main body frame 1001 is fixedly connected with a support column one 1002, the top end of the main body frame 1001 is fixedly connected with a support frame one 1003, the support frame one 1003 is provided with two groups, the two groups of support frame one 1003 are distributed in linear array along the inner wall of the main body frame 1001, the bottom end of the main body frame 1001 is fixedly connected with a support frame two 1004, the bottom end of the main body frame 1001 is fixedly connected with a support frame three 1005, the bottom end of the support frame three 1005 is fixedly connected with a support leg one 1006, and the inner wall of the main body frame 1001 is also fixedly connected with a support column two 1007.

[0037] The main body frame 1001 of the main body unit 10 serves as the core bearing structure of the space cabin house 1, the support column one 1002 and the support column two 1007 fixedly connected with the inner wall of the main body frame 1001 enhance the frame rigidity from the inside, the support column one 1002 is distributed along the longitudinal direction to improve the bending resistance, and the support column two 1007 assists in strengthening the local structure; the two groups of support frame one 1003 distributed in linear array at the top end provide a mounting base for the top equipment and disperse the load, and the support frame two 1004 and the support frame three 1005 at the bottom end jointly bear the vertical load, wherein the support frame three 1005 is in contact with the ground through the support leg one 1006 at the bottom end to form a stable support point, and the distribution of the support leg one 1006 is optimized in cooperation with the position of the support column to optimize the stress transmission path; each support structure is formed into a rigid whole through welding or bolt connection, so that the main body frame 1001 can bear external environmental loads such as wind load, snow load and the weight of internal functional modules, and ensure the structural stability of the space cabin during transportation, installation and long-term use, thereby providing a reliable mounting carrier for the energy supply unit 20 and the expansion unit 30.

[0038] The surface of the main body frame 1001 is fixedly connected with the connecting frame two 2012, the surface of the main body frame 1001 is slidably connected with the connecting frame three 3009, and the surface of the main body frame 1001 is slidably connected with the connecting frame four 3010.

[0039] The main body frame 1001 is the core load-bearing structure of the space cabin house 1, and its surface is functionally coordinated with the energy supply unit 20 and the expansion unit 30 through different connection methods: fixed connection with the connecting frame two 2012, rigid fixing of the solar panel support structure of the energy supply unit 20 to the surface of the main body frame through the rotating block two 2011, the connecting frame two 2012 and the supporting block two 2013, to ensure the stability of the solar panel 2010 during the unfolding of the power generation or folding, and at the same time, through the supporting block two 2013, the support column one 1002 and the support column two 1007 of the inner wall of the main body frame, a multi-point load-bearing structure is formed to disperse the load; sliding connection with the connecting frame three 3009 and the connecting frame four 3010 provides a movable mounting interface for the expansion frame 3001 of the expansion unit 30, so that the expansion frame 3001 can slide along the surface of the main body frame 1001, cooperate with the support frame four 3002, the support frame five 3003, the support frame six 3004 and the support foot two 3005 to realize space expansion, and the sliding connection design not only ensures the guidance of the expansion frame during movement, but also allows it to adjust the position according to the use demand, and at the same time, through the support frame seven 3011 inside the connecting frame four 3010, the structural rigidity during sliding is enhanced, so that the main unit 10 and the expansion unit 30 form a whole structure of "core stability and flexible expansion" under the double action of fixed connection and sliding connection, and the structural strength and space adaptability are considered.

[0040] The inner wall of the connecting frame one 2001 is fixedly connected with the connecting frame three 3009, and the inner side surface of the supporting block one 2003 is fixedly connected with the main body frame 1001 and the inner wall of the expansion frame 3001.

[0041] The connecting frame one 2001 is a basic installation frame of the energy supply unit 20, and the inner wall thereof is fixedly connected with the connecting frame three 3009 of the capacity expansion unit 30, so that the energy supply unit 20 and the capacity expansion unit 30 are preliminarily rigidly connected in structure, and the force is ensured to be borne by the two units in cooperation during the operation of the space cabin house 1; the inner side surface of the support block one 2003 is fixedly connected with the inner wall of the main frame 1001 and the capacity expansion frame 3001 respectively, and plays a “double anchoring” role, that is, on one hand, the energy supply unit 20 is stably connected to the main frame 1001 through the support block one 2003, and on the other hand, the capacity expansion frame 3001 and the main frame 1001 are directly connected through the support block one 2003, so as to form a triangular stable structure of “main body-support block-capacity expansion”, effectively disperse the load at the connection position of the main unit 10 and the capacity expansion unit 30, and avoid stress concentration; the mechanical force generated by the support plate 2002, the installation frame 2004 and other components of the energy supply unit 20 when the solar panel 2010 is unfolded or folded can be synchronously transmitted to the main frame 1001 and the capacity expansion frame 3001 through the connecting frame one 2001 and the support block one 2003, so as to ensure that the whole space cabin house 1 remains stable in structure during the operation of the energy supply unit, and at the same time, the connection stiffness of the capacity expansion frame 3001 relative to the main frame 1001 is enhanced, so that the three units form an organic whole, and the anti-deformation ability and reliability of the space cabin house in a complex environment are improved.

[0042] The inner side surface of the support block two 2013 is fixedly connected with the support column two 1007, and the inner side surface of the support block two 2013 is also fixedly connected with the surface of the support column one 1002.

[0043] The support block two 2013 is a key connecting component of the energy supply unit 20 and the main body unit 10. The inner side surfaces of the support block two 2013 are fixedly connected with the support column one 1002 and the support column two 1007 of the inner wall of the main body frame 1001 respectively, forming a "double-column anchoring" structure. On the one hand, the mechanical load generated during the rotation of the solar panel 2010, such as the thrust in the unfolding process and the tension in the folding process, is evenly dispersed to the support column one 1002 and the support column two 1007 through the support block two 2013, avoiding deformation or fracture caused by local stress concentration of the main body frame 1001. On the other hand, by utilizing the structural characteristics of the longitudinal distribution of the support column one 1002 and the support column two 1007 along the inner wall of the main body frame 1001, the vertical stiffness and the torsional resistance of the connection between the energy supply unit 20 and the main body unit 10 are enhanced. When the solar panel 2010 is adjusted at ± 90° pitch angle or folded, the support block two 2013 can form a stable mechanical transmission path through the bidirectional fixed support column, ensuring the structural stability of the main body frame during the operation of the energy supply unit. In addition, this connection mode also strengthens the integrity of the internal support system of the main body unit 10. The support column one 1002 and the support column two 1007 are transversely connected through the support block two 2013, further improving the ability of the main body frame 1001 to resist external environmental loads such as strong wind and temperature deformation. The energy supply unit 20 and the main body unit 10 form a rigid whole in structure, ensuring the reliable operation of the space cabin house 1 under complex working conditions.

[0044] The mounting bracket 2004 is provided with two, and the two mounting brackets 2004 are linearly arranged along the surface of the support plate 2002. The two ends of the lead screw 2006 are rotationally connected with the inner wall of the mounting bracket 2004.

[0045] The mounting frame 2004 is provided with two and is distributed in linear arrangement along the surface of the support plate 2002, the inner wall of which is rotationally connected with the two ends of the lead screw 2006, and both of them constitute the core support structure of the transmission system in the energy supply unit 20: the two mounting frames 2004 position the two ends of the lead screw 2006 through linear arrangement, ensuring that the lead screw 2006 rotates stably under the drive of the first motor 2005, avoiding axial deviation or radial shaking caused by single-point support, so as to ensure that the sliding block 2007 connected by threads can move accurately and linearly along the axis direction of the lead screw 2006; the rotation connection of the two ends of the lead screw 2006 with the inner wall of the mounting frame 2004 allows it to rotate freely, and through the fixed connection of the mounting frame 2004 with the support plate 2002, the support plate 2002 is fixed on the surface of the connecting frame one 2001, the torque and axial force generated in the transmission process are transmitted to the base frame of the energy supply unit 20, ensuring the movement stability of the rotating block one 2008 driven by the sliding block 2007, the transmission rod 2014 and the solar panel 2010 when being unfolded or folded; this double-mounting frame supported lead screw structure design optimizes the mechanical distribution through symmetrical layout, improves the stiffness and fatigue resistance of the transmission system, so that the solar panel 2010 can obtain stable power input during angle adjustment or folding storage, ensuring the long-term reliable operation of the energy supply unit 20, and providing a mechanical basis for the accurate displacement control of the sliding block 2007, indirectly improving the tracking accuracy of the solar panel to the light angle and the efficiency of spatial folding.

[0046] The shell unit 40 comprises an aviation aluminum plate 4001, the inner wall of the aviation aluminum plate 4001 is fixedly connected with an electric sunroof 4002, the surface of the aviation aluminum plate 4001 is provided with a hatch 4003, the inner wall of the aviation aluminum plate 4001 is fixedly connected with a foamed polyurethane 4004, the inner wall of the foamed polyurethane 4004 is fixedly connected with a corrosion-resistant wooden keel 4005, the inner wall of the corrosion-resistant wooden keel 4005 is fixedly connected with a European pine plate 4006, the inner wall of the European pine plate 4006 is fixedly connected with a carbon crystal plate 4007, the inner wall of the carbon crystal plate 4007 is fixedly connected with a glass window 4008, the inner wall of the foamed polyurethane 4004 is fixedly connected with the surface of the support frame one 1003, and the inner wall of the corrosion-resistant wooden keel 4005 is fixedly connected with the surface of the support frame one 1003.

[0047] The shell unit 40 provides multiple functions such as protection, heat preservation, and lighting for the space cabin house 1 through a multi-layer composite structure design. The outermost layer is an aviation aluminum plate 4001, which has the characteristics of light weight and high strength to resist external impact, radiation, and harsh weather. The cabin door 4003 is provided on the surface of the aviation aluminum plate 4001 for personnel access and material transportation. The electric skylight 4002 fixed on the inner wall of the aviation aluminum plate 4001 realizes intelligent lighting and ventilation. The foamed polyurethane 4004 fixed on the inner wall of the aviation aluminum plate 4001 serves as a heat preservation layer, effectively isolating heat exchange between the inside and outside of the cabin, improving the energy-saving performance of the house, and being fixed with the support frame 1003 to enhance the structural stability. The rot-resistant wooden keel 4005 inside the foamed polyurethane 4004 not only provides support as an internal framework but also further strengthens the overall rigidity through fixed connection with the support frame 1003. The osier board 4006 fixed on the inner wall of the rot-resistant wooden keel 4005 provides a flat base for the decoration and functional layer. The carbon crystal plate 4007 inside the osier board 4006 has a heating function to adjust the temperature in the cabin. The glass window 4008 on the inner wall of the carbon crystal plate 4007 is used for light transmission and field of view expansion, and also plays a role in heat insulation. Through layer-by-layer fixing and connection, the shell unit 40 and the main unit 10 are tightly combined to form a whole that has protection, comfort, and structural strength, meeting the use requirements of the space cabin house in various complex environments.

[0048] The embodiments of the specific implementation are the preferred embodiments of the present application, and are not intended to limit the protection scope of the present application. The same components are represented by the same reference numerals. Therefore, any equivalent changes made according to the structure, shape, and principle of the present application should be covered by the protection scope of the present application.

Claims

1. A prefabricated passive intelligent energy storage space cabin house, comprising a space cabin house (1), characterized in that, The space cabin house (1) includes a main unit (10), the surface of the main unit (10) is provided with a power supply unit (20), and the surface of the main unit (10) is also provided with an expansion unit (30); the surface of the main unit (10) is fixedly connected with a shell unit (40); The expansion unit (30) is used for expanding the space cabin house (1), and the expansion unit (30) includes an expansion frame (3001), the top end of the expansion frame (3001) is fixedly connected with a support frame four (3002), the bottom end of the expansion frame (3001) is fixedly connected with a support frame five (3003), the bottom end of the expansion frame (3001) is also fixedly connected with a support frame six (3004), one end of the support frame six (3004) away from the expansion frame (3001) is fixedly connected with a support foot two (3005), the top end of the expansion frame (3001) is fixedly connected with a support column three (3006), the inner wall of the expansion frame (3001) is fixedly connected with a support column four (3007), the inner wall of the expansion frame (3001) is also fixedly connected with a support column five (3008), the surface of the expansion frame (3001) is sleeved with a connecting frame three (3009), and the surface of the expansion frame (3001) is also sleeved with a connecting frame four (3010); the inner side surface of the connecting frame four (3010) is fixedly connected with a support frame seven (3011); The power supply unit (20) is used for supplying energy to the space cabin house (1), and can be folded to save space, the power supply unit (20) includes a connecting frame one (2001), the surface of the connecting frame one (2001) is fixedly connected with a support plate (2002), the surface of the connecting frame one (2001) is also fixedly connected with a support block one (2003), the surface of the support plate (2002) is fixedly connected with a mounting frame (2004), the surface of the mounting frame (2004) is fixedly connected with a first motor (2005), the output end of the first motor (2005) is fixedly connected with a lead screw (2006), the surface of the lead screw (2006) is threadedly connected with a sliding block (2007), the inner wall of the sliding block (2007) is rotatably connected with a rotating block one (2008), the inner wall of the rotating block one (2008) is rotatably connected with a transmission rod (2014), the two ends of the transmission rod (2014) are provided with the same rotating block one (2008), one end of the rotating block one (2008) away from the transmission rod (2014) is rotatably connected with a rotating seat (2009), and the bottom end of the rotating seat (2009) is fixedly connected with a solar panel (2010); The surface of the solar panel (2010) is rotatably connected with a rotating block two (2011), the surface of the rotating block two (2011) is rotatably connected with a connecting frame two (2012), and the surface of the connecting frame two (2012) is fixedly connected with a support block two (2013).

2. The prefabricated passive intelligent energy storage space cabin house according to claim 1, characterized in that, The main body unit (10) comprises a main body frame (1001), the inner wall of the main body frame (1001) is fixedly connected with a support column one (1002), the top end of the main body frame (1001) is fixedly connected with a support frame one (1003), the support frame one (1003) is provided with two groups, two groups of the support frame one (1003) are linearly arrayed along the inner wall of the main body frame (1001), the bottom end of the main body frame (1001) is fixedly connected with a support frame two (1004), the bottom end of the main body frame (1001) is fixedly connected with a support frame three (1005), the bottom end of the support frame three (1005) is fixedly connected with a support foot one (1006), and the inner wall of the main body frame (1001) is further fixedly connected with a support column two (1007).

3. The prefabricated passive intelligent energy storage space cabin house according to claim 2, characterized in that, The surface of the main body frame (1001) is fixedly connected with a connecting frame two (2012), the surface of the main body frame (1001) is slidably connected with a connecting frame three (3009), and the surface of the main body frame (1001) is slidably connected with a connecting frame four (3010).

4. The prefabricated passive intelligent energy storage space cabin house according to claim 1, characterized in that, The inner wall of the connecting frame one (2001) is fixedly connected with the connecting frame three (3009), the inner side surface of the support block one (2003) is fixedly connected with the main body frame (1001), and the inner side surface of the support block one (2003) is further fixedly connected with the inner wall of the expansion frame (3001).

5. The prefabricated passive intelligent energy storage space cabin house according to claim 1, characterized in that, The inner side surface of the support block two (2013) is fixedly connected with the support column two (1007), and the inner side surface of the support block two (2013) is further fixedly connected with the surface of the support column one (1002).

6. The prefabricated passive intelligent energy storage space cabin house according to claim 1, characterized in that, The mounting frame (2004) is provided with two, two mounting frames (2004) are linearly arranged along the surface of the support plate (2002), and the two ends of the lead screw (2006) are rotatably connected with the inner wall of the mounting frame (2004).

7. The prefabricated passive intelligent energy storage space cabin house according to claim 1, characterized in that, The shell unit (40) comprises an aviation aluminum plate (4001), the inner wall of the aviation aluminum plate (4001) is fixedly connected with an electric sunroof (4002), the surface of the aviation aluminum plate (4001) is provided with a hatch (4003), the inner wall of the aviation aluminum plate (4001) is fixedly connected with a foamed polyurethane (4004), the inner wall of the foamed polyurethane (4004) is fixedly connected with a preservative wood keel (4005), the inner wall of the preservative wood keel (4005) is fixedly connected with a European pine board (4006), the inner wall of the European pine board (4006) is fixedly connected with a carbon crystal plate (4007), the inner wall of the carbon crystal plate (4007) is fixedly connected with a glass window (4008), the inner wall of the foamed polyurethane (4004) is fixedly connected with the surface of the support frame one (1003), and the inner wall of the preservative wood keel (4005) is fixedly connected with the surface of the support frame one (1003).

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