Space capsule with heating plate function

By employing a combination of heating components, heat-conducting plates, and insulation panels in the space capsule, the problem of heat loss was solved, achieving efficient heating and energy-saving effects, and improving the heating efficiency and safety of the space capsule.

CN223724247UActive Publication Date: 2025-12-26HEBEI XINSHUN HONGYUAN ASSEMBLED HOUSING CO LTD
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Patent Information

Application Number
CN202423259230.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-12-28
Publication Date
2025-12-26
Estimated Expiration
2034-12-28

AI Technical Summary

Technical Problem

During the heating process, heat is easily lost through the cabin, resulting in energy waste.

Method used

Heating components are used to heat the base plate, and heat is quickly transferred to the side walls using heat-conducting plates. Insulation plates are installed on the side walls to reduce heat loss. At the same time, electric heating rods and heat dissipation plates extend the contact time between air and heat to improve heating efficiency, and connecting plates are used to enhance the stability of the insulation plates to reduce heat leakage.

Benefits of technology

It improves the heating efficiency of spacecraft, reduces energy waste due to heat loss, enhances safety and stability, and optimizes energy utilization.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to a space capsule with a heating plate function, and belongs to the technical field of space cabins, the space capsule comprises a bottom plate, a top plate and a side wall connecting the bottom plate and the top plate, a metal heat conduction plate is inserted and fixedly connected in the side wall, one end of the bottom plate is provided with a cavity, a heating assembly for heating the interior of the space capsule is arranged in the cavity, and the heating assembly is connected with the top plate. And an insulation board is arranged on the outer side of the side wall. The device has the effect of reducing energy waste caused by heat loss.
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Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of space cabins, and particularly relates to a space cabin with a heating plate function. BACKGROUND

[0002] The space cabin is a kind of mobile house, which is usually assembled in a factory and then transported to a destination for fixing, and is widely used due to its convenience. The space cabin is divided into several rooms by wallboards, and side wall windows and skylights are installed in the rooms. Curtains, central air conditioners, lamps and smart home systems are also installed in the house.

[0003] In the process of heating the interior of the space cabin, heat is easily lost through the space cabin body. Therefore, a large amount of heat needs to be provided to maintain the temperature inside the space cabin, which causes waste of energy. CONTENT OF THE UTILITY MODEL

[0004] In order to reduce the waste of energy caused by heat loss, the present application provides a space cabin with a heating plate function.

[0005] The space cabin with a heating plate function provided by the present application adopts the following technical solution:

[0006] The space cabin with a heating plate function comprises a bottom plate, a top plate and a side wall connected therebetween, a heat-conducting plate made of metal is inserted and fixedly connected in the side wall, one end of the bottom plate is provided with a cavity, a heating assembly for heating the interior of the space cabin is arranged in the cavity, and a heat-insulating plate is arranged outside the side wall.

[0007] By using the above technical solution, the space cabin is heated by the heating assembly. At this time, the bottom plate is rapidly heated under the action of the heating assembly, and the heat-conducting plate in the side wall rapidly conducts the heat generated by the heating assembly to the side wall, thereby improving the heating efficiency of the space cabin. The heat-insulating plate on the side wall prevents the heat in the space cabin from being lost through the side wall, thereby reducing the waste of energy caused by heat loss.

[0008] Optionally, the cavity is arranged along the width direction of the bottom plate and located at one end of the bottom plate. The heating assembly comprises an electric heating rod arranged in the cavity and parallel to the width direction of the bottom plate. A battery for electrifying the electric heating rod is mounted on the bottom plate. An air inlet pipe in communication with one end of the cavity is inserted and fixedly connected to one side of the bottom plate. An air suction pump is mounted on the air inlet pipe. A heating pipe is laid on the bottom plate, and both ends of the heating pipe are in communication with the end portions of the cavity.

[0009] By adopting the technical scheme, the battery supplies power to the electric heating rod, at this time, the electric heating rod generates heat, air is drawn into the cavity through the air inlet pipe by the air pump, so that the air contacts the electric heating rod and generates hot air, at this time, the hot air in the cavity enters the heating pipe and heats the bottom plate along the length direction of the heating pipe, and the heat-conducting plate on the side wall conducts the heat on the bottom plate to the side wall, when the hot air moves to the other end of the heating pipe, it enters the cavity again to heat, so that the space cabin room is heated quickly, and the waste of energy caused by heat loss is further reduced.

[0010] Optionally, a heat releasing plate is arranged on the side wall of the electric heating rod and extends along the length direction of the electric heating rod.

[0011] By adopting the technical scheme, the heat generated by the electric heating rod is conducted to the heat releasing plate, at this time, the air entering the cavity through the air inlet pipe contacts the electric heating rod, and at the same time, moves along the length direction of the heat releasing plate to the heating pipe, at this time, the heat releasing plate prolongs the contact time of the air and the electric heating rod, and the air is also heated in the process of contacting the heat releasing plate, so that the air is further heated, the heating efficiency of the space cabin room is improved, and the waste of energy caused by heat loss is further reduced.

[0012] Optionally, the heat insulation plates are evenly laid outside the side wall and fixedly connected with the outside of the side wall, and a connecting assembly connecting the adjacent heat insulation plates is arranged between the adjacent heat insulation plates.

[0013] By adopting the technical scheme, the heat insulation plates are fixed on the side wall and connected with each other through the connecting assembly, so that the stability of the heat insulation plates installed on the side wall is improved, the possibility of heat loss through the side wall is reduced, the possibility of heat loss through the joint of the heat insulation plates is reduced, and the waste of energy caused by heat loss is further reduced.

[0014] Optionally, the connecting assembly comprises connecting rods fixedly connected with one side of the adjacent two heat insulation plates and parallel to each other, and a connecting plate is sleeved on the outside of the oppositely arranged connecting rods, and the connecting plate is fixedly connected with the corresponding connecting rod through bolts.

[0015] By adopting the technical scheme, the connecting plate is sleeved on the oppositely arranged connecting rods and fixed with the corresponding connecting rod through bolts, so that the stability of the connection between the adjacent two heat insulation plates is improved, and part of the gap between the adjacent two heat insulation plates is blocked by the connecting plate, so that the possibility of heat loss is further reduced, and the waste of energy caused by heat loss is further reduced.

[0016] Optionally, an insulating layer is sleeved and fixedly connected with the two ends of the electric heating rod.

[0017] By adopting the technical scheme, the insulating layer is wrapped outside the electric heating rod, thereby reducing the adverse effect of electric leakage of the electric heating rod on the safety of the personnel in the space cabin and improving the safety of temperature rise of the space cabin.

[0018] Optionally, a temperature sensor is mounted on the side of the side wall away from the heat preservation plate, and the temperature sensor is wirelessly connected with a control host, and the control host is wirelessly connected with the battery.

[0019] By adopting the technical scheme, the temperature sensor detects the temperature inside the space cabin, when the temperature inside the space cabin is higher than the comfortable temperature of human body, the temperature sensor transmits an electric signal to the control host, and the control host drives the battery to power off the electric heating rod, thereby reducing the possibility that the electric heating rod continuously heats the inside of the space cabin and affects the living experience of the personnel, when the temperature inside the space cabin is lower than the comfortable temperature of human body, the temperature sensor transmits an electric signal to the control host, and the control host drives the battery to power on the electric heating rod, thereby facilitating heating of the inside of the space cabin, and further reducing the waste of energy caused by heat loss.

[0020] Optionally, a solar panel is mounted on the top side of the top plate, the solar panel is electrically connected with an energy storage battery, and the energy storage battery is electrically connected with the electric heating rod.

[0021] By adopting the technical scheme, the solar panel is mounted on the top plate and absorbs solar energy when the weather is good, at this time, the absorbed solar energy is converted into electric energy and stored in the energy storage battery for standby, when the electric quantity in the battery is insufficient, the energy storage battery continues to supply power to the electric heating rod, thereby not affecting the heating of the space cabin by the electric heating rod, and the solar energy is utilized, further reducing the waste of energy.

[0022] In summary, the present application has at least one of the following beneficial technical effects:

[0023] 1. The space cabin is heated by the heating assembly, at this time, the bottom plate is rapidly heated under the action of the heating assembly, the heat conduction plate in the side wall rapidly conducts the heat generated by the heating assembly to the side wall, thereby improving the heating efficiency of the space cabin, and the heat preservation plate on the side wall makes the heat in the space cabin not easy to be lost by conduction of the side wall, thereby reducing the waste of energy caused by heat loss;

[0024] 2. The heat generated by the electric heating rod is conducted to the heat releasing plate, at this time, the air entering the cavity through the air inlet pipe contacts the electric heating rod and spirally moves along the length direction of the heat releasing plate to the heating pipe, at this time, the heat releasing plate prolongs the contact time of the air with the electric heating rod, and the air is also heated in the process of contacting the heat releasing plate, thereby further facilitating heating of the air, improving the heating efficiency of the space cabin, and further reducing the waste of energy caused by heat loss;

[0025] 3. The connecting plate is sleeved on the oppositely arranged connecting rods and is fixed with the corresponding connecting rods through bolts, so that the stability of the connection between the two adjacent thermal insulation plates is increased, and the part of the gap between the two adjacent thermal insulation plates is blocked by the connecting plate, so that the possibility of heat loss is further reduced, and the waste of energy caused by heat loss is reduced. BRIEF DESCRIPTION OF DRAWINGS

[0026] Figure 1 is the overall structure schematic diagram of the space cabin with a heating plate function in the embodiment of the application.

[0027] Figure 2 is the structure schematic diagram of the position relationship between the heat conducting plate and the thermal insulation plate in the embodiment of the application.

[0028] Figure 3 is the structure schematic diagram of the position relationship between the heating pipe and the heat releasing plate in the embodiment of the application.

[0029] Mark explanation: 1, bottom plate; 11, cavity; 2, top plate; 21, skylight; 22, solar panel; 3, side wall; 31, heat conducting plate; 32, thermal insulation plate; 4, connecting assembly; 41, connecting rod; 42, connecting plate; 5, heating assembly; 51, electric heating rod; 52, insulation layer; 53, air inlet pipe; 54, air pump; 55, heating pipe; 56, heat releasing plate; 6, control host. DETAILED DESCRIPTION

[0030] The application will be further described in detail below with reference to the drawings.

[0031] The embodiment of the application discloses a space cabin with a heating plate function. Figure 1 and Figure 2 The space cabin with a heating plate function comprises a horizontal bottom plate 1, one end of the bottom plate 1 is arranged in a circular arc shape which rises from both ends to the middle to the direction away from the other end of the bottom plate 1. A top plate 2 corresponding to the bottom plate 1 and opposite to the bottom plate 1 is arranged above the bottom plate 1, a skylight 21 is installed in the middle of the top plate 2, and a vertical side wall 3 connecting the two is fixedly connected between the bottom plate 1 and the top plate 2.

[0032] Referring to Figure 1 and Figure 2 A vertical heat conducting plate 31 made of metal material is inserted and fixed in the side wall 3, which is arranged as a steel plate in the embodiment of the application. A plurality of uniformly distributed thermal insulation plates 32 are fixedly connected to the outer side of the side wall 3, and a connecting assembly 4 connecting the two is arranged between the adjacent thermal insulation plates 32. The circular arc-shaped end of the bottom plate 1 is provided with a cavity 11 arranged along the width direction of the bottom plate 1, and a heating assembly 5 for heating the bottom plate 1 is arranged in the cavity 11.

[0033] The space cabin is heated by the heating assembly 5, at this time the bottom plate 1 is rapidly heated under the action of the heating assembly 5, the heat conduction plate 31 in the side wall 3 makes the heat generated by the heating assembly 5 rapidly conduct to the side wall 3, and the heat preservation plate 32 on the side wall 3 makes the heat in the space cabin not easy to dissipate under the conduction of the side wall 3, so as to facilitate the heating of the space cabin.

[0034] The heat preservation plate 32 is fixed on the side wall 3 and connected by the connecting assembly 4, which increases the stability of the heat preservation plate 32 installed on the side wall 3, reduces the possibility of heat loss in the space cabin through the side wall 3, and reduces the possibility of heat loss through the joint of the heat preservation plate 32.

[0035] Referring to Figure 1 and Figure 3 The heating assembly 5 includes an electric heating rod 51 arranged in the cavity 11 and along the width direction of the bottom plate 1, the end of the electric heating rod 51 penetrates through the bottom plate 1 and is fixedly connected with the bottom plate 1. The electric heating rod 51 is horizontal, and the two ends of the electric heating rod 51 are sleeved and fixedly connected with an insulating layer 52. One end of the cavity 11 is communicated with a horizontal air inlet pipe 53 inserted into the bottom plate 1, and the air inlet pipe 53 is provided with a gas suction pump 54.

[0036] The heating pipe 55 is laid in the bottom plate 1, the air inlet end of the heating pipe 55 is communicated with the end of the cavity 11 away from the air inlet pipe 53 and the side of the cavity 11 away from the air inlet pipe 53, and the other end of the heating pipe 55 is communicated with the end of the cavity 11 close to the air inlet pipe 53 and the side of the cavity 11 opposite to the air inlet pipe 53. The electric heating rod 51 is electrically connected with a battery (not shown in the figure), and the outer side of the electric heating rod 51 is provided with a heat releasing plate 56 spirally arranged along the length direction of the electric heating rod 51, and the side of the heat releasing plate 56 close to the electric heating rod 51 is fixedly connected with the side wall 3 of the electric heating rod 51.

[0037] Referring to Figure 1 The upper side of the top plate 2 is provided with two solar panels 22 at both ends, the solar panels 22 are wirelessly connected with an energy storage battery (not shown in the figure), and the energy storage battery is electrically connected with the electric heating rod 51.

[0038] Referring to Figure 1 The temperature sensor (not shown in the figure) is installed in the side wall 3, the temperature sensor is wirelessly connected with the control host 6, and the energy storage battery and the battery are wirelessly connected with the control host 6.

[0039] The battery supplies power to the electric heating rod 51, at this time the electric heating rod 51 generates heat, the air is sucked into the cavity 11 through the air inlet pipe 53 and contacts the electric heating rod 51 to generate hot air, the heat generated by the electric heating rod 51 is conducted to the heat releasing plate 56, at this time the air entering the cavity 11 through the air inlet pipe 53 contacts the electric heating rod 51, and at the same time moves along the length direction of the heat releasing plate 56 to the heating pipe 55, at this time the heat releasing plate 56 prolongs the contact time of the air with the electric heating rod 51, and the air is also heated in the process of contacting the heat releasing plate 56, until entering the heating pipe 55 and heating the bottom plate 1 along the length direction of the heating pipe 55, at the same time the heat conduction plate 31 on the side wall 3 conducts the heat on the bottom plate 1 to the side wall 3, when the hot air moves to the other end of the heating pipe 55, it enters the cavity 11 again to heat, which facilitates the rapid heating of the space cabin room.

[0040] The temperature sensor detects the temperature inside the space cabin room, when the temperature inside the space cabin room is higher than the comfortable temperature of the human body, the temperature sensor transmits an electric signal to the control host 6, the control host 6 drives the battery to cut off the power supply of the electric heating rod 51, so as to reduce the possibility that the electric heating rod 51 continuously heats the inside of the space cabin room and affects the living experience of the personnel, when the temperature inside the space cabin room is lower than the comfortable temperature of the human body, the temperature sensor transmits an electric signal to the control host 6, and the control host 6 drives the battery to supply power to the electric heating rod 51, so as to control the temperature of the space cabin room.

[0041] The insulating layer 52 is wrapped outside the electric heating rod 51, which reduces the adverse effect of the electric heating rod 51 on the safety of the personnel in the space cabin room when the electric heating rod 51 leaks, and improves the safety of the space cabin room heating; the solar panel 22 is installed on the top plate 2 and absorbs solar energy when the weather is good, at this time the absorbed solar energy is converted into electric energy and stored in the energy storage battery for standby use, when the electric quantity in the battery is insufficient, the energy storage battery continues to supply power to the electric heating rod 51, which does not affect the heating of the electric heating rod 51 to the space cabin room.

[0042] Referring to Figure 2 The connecting assembly 4 includes a plurality of connecting rods 41 which are adapted to the thermal insulation plates 32 and are uniformly distributed along the edges of the thermal insulation plates 32 away from the side wall 3, in the embodiment of the application, four connecting rods 41 are provided and are parallel to the edges of the thermal insulation plates 32. The connecting rods 41 on the sides of the adjacent two thermal insulation plates 32 close to each other are provided with the same connecting plate 42, and the length direction of the connecting plate 42 is parallel to the connecting line between the corresponding connecting rods 41.

[0043] The two ends of the connecting plate 42 are bent at right angles to the direction close to the side wall 3, and the sides of the corresponding connecting rods 41 away from each other are abutted with the bent ends of the connecting plate 42 and are fixedly connected with the connecting plate 42 through bolts.

[0044] The connecting plate 42 is sleeved on the oppositely arranged connecting rod 41 and is fixed with the corresponding connecting rod 41 through bolts, so that the stability of the connection of the two adjacent heat preservation plates 32 is increased, and the part of the gap between the two adjacent heat preservation plates 32 is blocked by the connecting plate 42, so that the heat loss is reduced.

[0045] The implementation principle of the space cabin with the heating plate function is that the air is heated by the electric heating rod 51 and is delivered into the heating pipe 55, so that the space cabin room is heated; at this time, the bottom plate 1 is rapidly heated under the action of the heating pipe 55, the heat conduction plate 31 in the side wall 3 makes the heat in the heating pipe 55 rapidly conduct to the side wall 3, and the heat preservation plate 32 on the side wall 3 makes the heat in the space cabin room not easy to be lost under the conduction of the side wall 3, so that the space cabin room is heated.

[0046] The above are the preferred embodiments of the present application, and are not limited to the protection scope of the present application, so that: all equivalent changes made according to the structure, shape, principle of the present application should be covered in the protection scope of the present application.

Claims

1. A space capsule having a hot plate function, characterized by: The utility model provides a space capsule room, including bottom plate (1), top plate (2) and the side wall (3) of connecting both, the side wall (3) is inserted and fixedly connected with the heat conduction plate (31) of metal material, one end of bottom plate (1) is equipped with cavity (11), be equipped with heating assembly (5) in the cavity (11) and carry out heating to the inside of space capsule room, and the outer side of side wall (3) is equipped with insulating board (32).

2. The space capsule with the heating plate function according to claim 1, characterized in that: The cavity (11) is arranged along the width direction of the bottom plate (1) and located at one end of the bottom plate (1), the heating assembly (5) includes an electric heating rod (51) located in the cavity (11) and parallel to the width direction of the bottom plate (1), a battery is installed on the bottom plate (1) to supply power to the electric heating rod (51), an air inlet pipe (53) is inserted and fixedly connected to one end of the cavity (11) on one side of the bottom plate (1), a suction pump (54) is installed on the air inlet pipe (53), and a heating pipe (55) is laid on the bottom plate (1), both ends of the heating pipe (55) are communicated with the end of the cavity (11).

3. The space capsule with the function of the hot plate according to claim 2, characterized in that: The side wall (3) of the electric heating rod (51) is provided with a heat dissipation plate (56) arranged along the length direction of the electric heating rod (51), and the heat dissipation plate (56) is spirally arranged along the length direction of the electric heating rod (51).

4. The space capsule with the function of the hot plate according to claim 3, characterized in that: The insulating board (32) is uniformly laid on the outer side of the side wall (3) and fixedly connected with the outer side of the side wall (3), and a connecting assembly (4) is arranged between adjacent insulating boards (32).

5. The space capsule with the function of the hot plate according to claim 4, characterized in that: The connecting assembly (4) includes connecting rods (41) fixedly connected on the sides of adjacent two insulating boards (32) and parallel to each other, and the outer sides of the connecting rods (41) arranged opposite to each other are sleeved with the same connecting plate (42), and the connecting plate (42) is fixedly connected with the corresponding connecting rod (41) by bolts.

6. The space capsule with the function of the hot plate according to claim 5, characterized in that: Both ends of the outer side of the electric heating rod (51) are sleeved and fixedly connected with an insulating layer (52).

7. The space capsule with the function of the hot plate according to claim 6, characterized in that: A temperature sensor is installed on the side of the side wall (3) away from the insulating board (32), the temperature sensor is wirelessly connected with a control host (6), and the control host (6) is wirelessly connected with the battery.

8. The space capsule with the function of the hot plate according to claim 7, characterized in that: A solar panel (22) is installed on the upper side of the top plate (2), the solar panel (22) is electrically connected with an energy storage battery, and the energy storage battery is electrically connected with the electric heating rod (51).