Moon living cabin

Abstract

The invention discloses a lunar residential cabin, and relates to the technical field of spaceflight, the lunar residential cabin comprises a wall body, the wall body is connected with a heat supply system, the wall body is formed by splicing a plurality of heat supply modules end to end, and the heat supply temperature of the heat supply modules is adjustable; each heat supply module comprises a supporting wall, an internal heat dissipation unit is arranged on one side of the supporting wall, an external heat dissipation unit is arranged on the other side of the supporting wall, and a heat conduction assembly is arranged in the supporting wall. Every two adjacent heat conduction assemblies are connected end to end, the input end of the first heat conduction assembly communicates with the output end of the heat supply system, and the output end of the last heat conduction assembly communicates with the input end of the heat supply system. The internal heat dissipation unit and the external heat dissipation unit are both connected with the heat conduction assembly. According to the lunar living cabin, the technical problems of heat supply of the lunar living cabin, reduction of the carrying difficulty and the carrying cost of the lunar living cabin, improvement of the energy utilization rate and the like in the prior art are solved, and the lunar living cabin which is low in carrying cost and capable of automatically adjusting the heat supply requirement is provided.

Description

Technical Field

[0001] The present invention relates to the field of aerospace technology, and in particular to a lunar living cabin. Background Art

[0002] With the increasing demand for human space exploration and the gradual maturity of manned spaceflight technology, manned landing and the construction of lunar surface bases have become important directions at present. There is an extreme temperature difference between day and night on the lunar surface, from 150℃ during the day to -200℃ at night, and the night lasts as long as 14 days. Therefore, traditional solar energy and chemical energy cannot achieve long-term energy supply in this environment, while nuclear energy has the advantages of high energy density, long life and no dependence on sunlight. Therefore, space reactors have become the preferred option for lunar surface energy supply.

[0003] However, the surrounding environment of the lunar base is very different from that on Earth. In particular, the lunar living module needs to meet the work and life needs of scientific researchers, so heating the living module is a problem that needs to be solved. At the same time, since the lunar module is built, a rocket is needed to carry the lunar module to the moon. Based on the rocket's carrying volume, how to reduce the rocket's carrying cost is also a challenge facing mankind. At the same time, energy is not easy to obtain on the lunar surface, so how to improve energy utilization is also a problem that needs to be solved urgently. Summary of the invention

[0004] The purpose of the present invention is to solve the technical problems of heating the lunar living module in the prior art and reducing the difficulty and cost of transporting the lunar living module, while improving the energy utilization rate. The present invention proposes the following technical solutions:

[0005] A lunar living cabin comprises a wall body, wherein the wall body is connected to a heating system, the wall body is formed by splicing a plurality of heating modules connected end to end, and the heating temperature of the heating modules is adjustable.

[0006] Each of the heating modules comprises a supporting wall, one side of the supporting wall is provided with an internal heat dissipation unit, the other side is provided with an external heat dissipation unit, and a heat conduction component is provided inside; two adjacent heat conduction components are connected end to end, wherein the input end of the first heat conduction component is connected to the output end of the heating system, and the output end of the last heat conduction component is connected to the input end of the heating system; the internal heat dissipation unit and the external heat dissipation unit are both connected to the heat conduction component.

[0007] The heat-conducting component includes a heat-conducting block and a liquid metal pipe passing through the heat-conducting block. The liquid metal pipes of two adjacent heat-conducting components are connected end to end. Both sides of the heat-conducting block extend to both sides of the supporting wall. One side of the heat-conducting block is connected to the external heat dissipation unit, and the other side is connected to the internal heat dissipation unit.

[0008] The internal heat dissipation unit includes several heat dissipation components arranged side by side, each heat dissipation component includes an internal heat pipe, one end of the internal heat pipe is connected to the heat conduction component, and several heat dissipation fins are evenly arranged along the radial direction of the internal heat pipe. The heat dissipation fins are rotatably connected to the internal heat pipe, and a temperature adjustment component is provided at one end of the heat conduction component of each heat dissipation fin, and the temperature adjustment component is fixedly connected to the heat dissipation fin.

[0009] The outer periphery of the internal heat pipe is provided with arc-shaped slots having the same number as the heat dissipation fins, and one end of the heat dissipation fin is provided with a protrusion adapted to the arc-shaped slot, and the protrusion is inserted into the arc-shaped slot and rotates in the arc-shaped slot.

[0010] The temperature adjustment component comprises a temperature memory spring and a connecting rod, wherein the free end of the temperature memory spring is fixedly connected to one end of the connecting rod, and the other end of the connecting rod is fixedly connected to one end of the heat dissipation fin.

[0011] The external heat dissipation unit comprises a heat dissipation plate, a plurality of external heat pipes are arranged on the heat dissipation plate, and each of the external heat pipes is connected to the heat conduction component.

[0012] A mounting plate is provided at one end of the supporting wall, and a placement space for each temperature memory spring is reserved on the mounting plate. The temperature memory spring is placed in the space and a fixed end of the memory spring is fixedly connected to the mounting plate.

[0013] There are two internal heat dissipation units, which are distributed up and down, and both of them are connected to the heat conduction component.

[0014] The heating system comprises: a reactor;

[0015] A first circulation loop, wherein the first circulation loop is connected to the reactor after generating electricity and exchanging heat via a Stirling generator set to form a closed loop;

[0016] A second circulation loop, wherein the second circulation loop passes through the lunar living module and the heat exchange part of the Stirling generator set in sequence to form a closed loop, and the second circulation loop exchanges heat with the first circulation loop at the heat exchange part of the Stirling generator set;

[0017] The output end of the power generation part of the Stirling generator is connected to the lunar living module for supplying power to the lunar living module. A lunar soil shielding device is provided between the reactor and the lunar living module.

[0018] The present invention has the following advantages:

[0019] (1) The lunar living module provided by the present invention is a space formed by splicing a plurality of heating modules. This design modularizes the original living module walls, reduces the difficulty of rocket or carrier spacecraft transportation, reduces the transportation volume, and thus reduces the transportation cost.

[0020] (2) At the same time, based on the above-mentioned heating module, which is a component of the wall and has the function of heating, the wall and heating are combined, which reduces the work of the staff to install a separate heating device. At the same time, it also avoids the transportation space of the rocket or carrier spacecraft for the heating device, thereby reducing the load of the rocket launch and saving transportation costs.

[0021] (3) At the same time, the heating module provided by the present invention also has the function of temperature regulation. It can automatically reduce or increase the heat dissipation of heating according to the indoor temperature, so that the heating effect in the lunar living cabin can be properly adjusted according to the temperature of the lunar living cabin, so that the temperature of the entire living cabin is always at an appropriate temperature; at the same time, the heating module provided by the present invention adjusts the heat dissipation through mechanical adjustment, which reduces automatic control and directly avoids the energy loss required for automatic control.

[0022] (4) The heat source of the heating module provided by the present invention comes directly from the waste heat generated by the space reactor, which achieves waste heat utilization and saves energy compared to simple electric heating. At the same time, the utilization of nuclear reaction energy is optimized.

[0023] (5) Based on the characteristics of the lunar thermal environment, the present invention allows the waste heat generated by the space reactor to be dissipated and at the same time provide heating for the lunar base living cabin. The temperature in the living cabin can be adaptively adjusted, while taking into account the waste heat discharge function of the space reactor, simplifying the system structure and reducing the weight, thereby reducing the load of the rocket launch. In addition, the system does not require external electricity and can operate independently, thereby improving the overall energy utilization rate. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 It is a structural schematic diagram of the heating module;

[0025] Figure 2 This is an enlarged view of point B;

[0026] Figure 3 This is a schematic diagram of the structure of the lunar living module;

[0027] Figure 4 It is a schematic diagram of the heat dissipation component structure;

[0028] Figure 5 This is the enlarged view of point A;

[0029] Figure 6 Schematic diagram of the internal heat pipe structure;

[0030] Figure 7 This is the enlarged view of point C;

[0031] Figure 8 Schematic diagram of the heating system.

[0032] In the figure: 00. Wall, 1. Heating module, 11. Support wall, 12. Internal heat dissipation unit, 121. Heat dissipation assembly, 1211. Internal heat pipe, 1212. Heat dissipation fins, 1213. Temperature control assembly, 12131. Memory spring, 12131. Connecting rod, 1214. Arc slot, 1215. Protrusion, 13. External heat dissipation unit, 131. Heat dissipation plate, 14. Heat conduction assembly, 141. Heat conduction block, 142. Liquid metal conduit, 15. Mounting plate, 2. Reactor, 3. First circulation loop, 4. Stirling generator set, 6. Second circulation loop, 7. Lunar soil shielding device, 8. Circulation pump, 9. Control valve. DETAILED DESCRIPTION

[0033] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments.

[0034] Therefore, the following detailed description of the embodiments of the present invention is not intended to limit the scope of the invention claimed for protection, but merely represents some embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.

[0035] It should be noted that, in the absence of conflict, the embodiments of the present invention and the features and technical solutions in the embodiments may be combined with each other.

[0036] It should be noted that similar numbers and letters represent similar items in the following figures, so once an item is defined in one figure, it does not need to be further defined and explained in the subsequent figures. In the description of the present invention, it should be noted that the orientation or position relationship indicated by the terms "upper", "lower", etc. is based on the orientation or position relationship shown in the drawings, or the orientation or position relationship in which the product of the invention is usually placed when in use, or the orientation or position relationship commonly understood by those skilled in the art. Such terms are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention. In addition, the terms "first", "second", etc. are only used to distinguish the description, and cannot be understood as indicating or implying relative importance.

[0037] See also Figure 3: A lunar living module, comprising a wall 00, the wall 00 is connected to a heating system, the heating system is used to heat the wall 00; the wall 00 is formed by connecting a plurality of heating modules 1 end to end, and the heating temperature of the heating modules 1 is adjustable. The output end of the heating system is connected to the input end of the first heating module 1; the input end of the heating system is connected to the output end of the last heating module 1, so as to form a closed heating loop with the heating system so that the heat provided by the heating system is transferred to the wall 00.

[0038] See also Figure 1 and Figure 2 Each of the heating modules 1 comprises a supporting wall 11, wherein one side of the supporting wall 11 is provided with an internal heat dissipation unit 12, the other side is provided with an external heat dissipation unit 13, and a heat conduction component 14 is provided inside; two adjacent heat conduction components 14 are connected end to end, wherein the input end of the first heat conduction component 14 is connected to the output end of the heating system, and the output end of the last heat conduction component 14 is connected to the input end of the heating system; the internal heat dissipation unit 12 and the external heat dissipation unit 13 are both connected to the heat conduction component 14. The heat conduction component 14 is used to conduct the heat provided by the conduction heating system to the internal heat dissipation unit 12 and the external heat dissipation unit 13, the internal heat dissipation unit 12 diffuses the heat to the inside of the lunar living cabin, and the external heat dissipation unit 13 is used to balance the heat and dissipate the excess heat to the environment outside the lunar living cabin.

[0039] The heat-conducting assembly 14 includes a heat-conducting block 141 and a liquid metal pipe 142 passing through the heat-conducting block 141. The liquid metal pipes 142 of two adjacent heat-conducting assemblies 14 are connected end to end. Both sides of the heat-conducting block 141 extend to both sides of the supporting wall 11. One side of the heat-conducting block 141 is connected to the external heat dissipation unit 13, and the other side is connected to the internal heat dissipation unit 12. The input end of the first liquid metal pipe 142 is connected to the output end of the pipe of the heating system, and the output end of the last liquid metal pipe 142 is connected to the input end of the pipe of the heating system, forming a closed loop. The liquid metal pipe 142 is filled with high-temperature liquid metal liquid transported from the heating system. The temperature of the high-temperature liquid metal liquid is transferred to the internal heat dissipation unit 12 and the external heat dissipation unit 13 through the heat-conducting block 141. The external heat dissipation unit 13 dissipates heat, and the heat emitted by the internal heat dissipation unit 12 provides heat for the internal environment of the lunar living cabin.

[0040] See also Figure 4 and Figure 5The internal heat dissipation unit 12 includes several heat dissipation components 121 arranged side by side, each heat dissipation component 121 includes an internal heat pipe 1211, one end of the internal heat pipe 1211 is connected to the heat conduction component 14, and several heat dissipation fins 1212 are evenly arranged along the radial direction of the internal heat pipe 1211. The heat dissipation fins 1212 are rotatably connected to the internal heat pipe 1211. A temperature adjustment component 1213 is arranged at one end of each heat dissipation fin 1212 away from the heat conduction component 14, and the temperature adjustment component 1213 is fixedly connected to the heat dissipation fin 1212. The heat conduction block 141 is provided with a circular hole adapted to the internal heat pipe 1211, and one end of the internal heat pipe 1211 is inserted into the circular hole to achieve connection with the heat conduction block 141. The temperature adjustment component 1213 controls the heat dissipation area of ​​the heat dissipation fin 1212 by controlling the heat dissipation fin 1212, so as to achieve regulation of the heat dissipation temperature.

[0041] The temperature adjustment component 1213 includes a temperature memory spring 12131 and a connecting rod 12132. The free end of the temperature memory spring 12131 is fixedly connected to one end of the connecting rod 12132, and the other end of the connecting rod 12132 is fixedly connected to one end of the heat dissipation fin 1212. The free ends of two adjacent temperature memory springs 12131 are arranged in opposite directions. The connecting rod 12132 is generally made of heat insulating material to prevent the temperature on the heat dissipation fin 1212 from being transferred to the temperature memory spring 12131 through the connecting rod 12132, thereby affecting the performance of the temperature memory spring 12131.

[0042] See also Figure 6 and Figure 7 The outer periphery of the internal heat pipe 1211 is provided with arc-shaped slots 1214 having the same number as the heat dissipation fins 1212, and one end of the heat dissipation fin 1212 is provided with a protrusion 1215 adapted to the arc-shaped slot 1214, and the protrusion 1215 is inserted into the arc-shaped slot 1214 and rotates in the arc-shaped slot 1214. The installation directions of two adjacent arc-shaped slots 1214 are opposite.

[0043] The temperature memory spring 12131 can be extended and retracted according to the temperature conditions. The free end of the temperature memory spring 12131 is fixedly connected to the heat dissipation fin 1212 through the connecting rod 12132. When the temperature in the living cabin is too high, the temperature memory spring 12131 contracts, driving the heat dissipation fin 1212 to rotate and fold, thereby reducing the heat dissipation area of ​​the heat dissipation fin 1212. Moreover, since the free ends of two adjacent temperature memory springs 12131 are arranged in opposite directions, the rotation and folding directions of the two adjacent heat dissipation fins 1212 are opposite, and the heat dissipation area of ​​the heat dissipation fin 1212 is reduced. When the temperature in the living cabin is too low, the temperature memory spring 12131 extends, driving the heat dissipation fin 1212 to rotate and unfold, increasing the heat dissipation area of ​​the heat dissipation fin 1212, thereby increasing the indoor temperature of the living cabin. Furthermore, since the free ends of two adjacent temperature memory springs 12131 are arranged in opposite directions, the rotation and unfolding directions of the two adjacent heat dissipation fins 1212 are opposite, and the heat dissipation area of ​​the heat dissipation fin 1212 is increased.

[0044] The external heat dissipation unit 13 includes a heat dissipation plate 131, on which a plurality of external heat pipes are disposed, each of which is connected to the heat conducting component 14. The external heat pipe is used to conduct the heat of the heat conducting component 14 to the heat dissipation plate 131 for diffusion.

[0045] One end of the supporting wall 11 is provided with a mounting plate 15, on which a placement space for each of the temperature memory springs 12131 is reserved, and the temperature memory springs 12131 are placed in the space and the fixed ends of the temperature memory springs 12131 are fixedly connected to the mounting plate 15. The mounting plate 15 is used to install the temperature memory springs 12131, so that the temperature memory springs 12131 are placed in the space position reserved by the mounting plate 15, so that the temperature memory springs 12131 will not fall; and the fixed ends of the temperature memory springs 12131 are fixedly connected to the mounting plate 15.

[0046] On each heating module 1, two internal heat dissipation units 12 are provided, the two internal heat dissipation units 12 are distributed up and down, and the two internal heat dissipation units 12 are connected to the heat conduction component 14. This design is for better heat conduction and ensures the heat conduction performance of the internal heat pipe 1211.

[0047] The working principle of the above scheme is:

[0048] The liquid metal pipes 142 of each heating module 1 are connected end to end to form a heating pipeline, and the input end of the first liquid metal pipe 142 is connected to the output end of the pipe of the heating system, and the output end of the last liquid metal pipe 142 is connected to the input end of the pipe of the heating system, forming a closed loop. The heating system inputs high-temperature liquid metal to the liquid metal pipe 142, and the heat of the high-temperature liquid metal is transmitted to the internal heat pipe 1211 and the external heat pipe through the heat conduction block 141, and the internal heat pipe 1211 then conducts the heat to the heat dissipation fins 1212 rotatably connected to the internal heat pipe 1211. Since the heat dissipation fin 1212 is connected to the free end of the temperature memory spring 12131, when the temperature in the living cabin is too high, the temperature memory spring 12131 contracts, driving the heat dissipation fin 1212 to rotate and fold, thereby reducing the heat dissipation area of ​​the heat dissipation fin 1212; and since the free ends of two adjacent temperature memory springs 12131 are arranged in opposite directions, the rotation and folding directions of the two adjacent heat dissipation fins 1212 are opposite, and the heat dissipation area of ​​the heat dissipation fin 1212 is reduced. When the temperature in the living cabin is too low, the temperature memory spring 12131 extends, driving the heat dissipation fin 1212 to rotate and expand, increasing the heat dissipation area of ​​the heat dissipation fin 1212, thereby increasing the indoor temperature of the living cabin. Furthermore, since the free ends of two adjacent temperature memory springs 12131 are arranged in opposite directions, the rotation and expansion directions of the two adjacent heat dissipation fins 1212 are opposite, and the heat dissipation area of ​​the heat dissipation fin 1212 is increased. By adjusting the heat dissipation area, the purpose of adjusting the indoor temperature is achieved. The heat of the external heat pipe is transferred to the heat sink 131, and the heat sink 131 diffuses the excess heat to the external environment. The high-temperature liquid metal providing heat then flows into the heating system from the output end of the last liquid metal pipe 142 to perform a heat cycle.

[0049] The heating system comprises: a reactor 2;

[0050] A first circulation loop 3, wherein the first circulation loop 3 is connected to the reactor 2 after generating electricity and exchanging heat via a Stirling generator set 4 to form a closed loop;

[0051] The second circulation loop 6, the second circulation loop 6 passes through the heat exchange part of the lunar living module and the Stirling generator set (4) in sequence to form a closed loop, the second circulation loop 6 performs heat exchange with the first circulation loop 3 in the heat exchange part of the Stirling generator set (4); the Stirling generator set includes a heat exchange part and a power generation part, the heat exchange part is used for heat exchange, and the power generation part is used to convert the heat energy of the first circulation loop into electric energy and output electric power; one loop of the heat exchange part of the Stirling generator set is connected to the first circulation loop, and the other loop is connected to the second circulation loop, so that the first circulation loop and the second circulation loop perform heat exchange in the heat exchange part of the Stirling generator set, and the second circulation loop uses the residual heat of the first circulation loop after the power generation part of the Stirling generator set generates electricity to heat the lunar living module. The power generation part of the Stirling generator 4 outputs electric energy, and the output electric energy is connected to the lunar living module to supply power to the lunar living module, and a lunar soil shielding device 7 is provided between the reactor 2 and the lunar living module. The first circulation loop 3 and the second circulation loop 6 are both provided with a circulation pump 8 and a control valve 9. The second circulation loop 6 is connected to the pipeline inlet reserved in the lunar living module (i.e., the input end of the liquid metal pipeline of the first heating module 1), so that the high-temperature liquid metal in the first circulation pipeline flows into the wall 00 of the lunar living module, and flows out from the pipeline outlet reserved in the lunar living module (and the output end of the liquid metal pipeline of the last heating module 1) and then continues to flow into the second circulation pipeline to form a closed loop.

[0052] The working principle of the above-mentioned heating system is: the reactor 2 undergoes a nuclear reaction and releases a large amount of heat at the same time. The cooling liquid in the first circulation loop 3 flows through the reactor 2, the cooling liquid heats up, and takes away the excess heat of the reactor 2. The heated cooling liquid in the first circulation loop 3 flows through the Stirling generator set 4. The power generation part of the Stirling generator 4 converts the heat energy carried in the first circulation loop 3 into electrical energy and outputs electricity. At the same time, after the cooling liquid in the first circulation loop 3 is cooled to a certain extent, it exchanges heat with the second circulation loop 6 at the heat exchange part of the Stirling generator set 4. The cooling liquid (generally liquid metal) in the second circulation loop 6 heats up. After the cooling liquid in the first circulation loop 3 is further cooled, it flows through the reactor 2 again to cool the reactor 2, and the cycle repeats. After the cooling liquid in the second circulation loop 6 heats up, it enters the wall 00 of the lunar living module, and heat exchange occurs in the lunar living module. The lunar living module exchanges the heat provided by the heated cooling liquid in the second circulation loop 6 to the inside of the lunar living module for heating the inside of the lunar living module. After the cooling liquid in the second circulation loop 6 flows through the lunar living module to cool down, the cooling liquid in the second circulation loop 6 flows through the heat exchanger 5 again to exchange heat with the first circulation pipeline to heat up the cooling liquid in the second circulation loop 6, and the cycle repeats. The electricity generated by the Stirling generator 4 is connected to the power supply system of the lunar living module to supply power to the lunar living module, and is also connected to other work uses where it is needed.

[0053] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical scheme and inventive concept of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A lunar living module, characterized in that: The invention comprises a wall body (00), wherein the wall body (00) is connected to a heating system, and the wall body (00) is formed by splicing a plurality of heating modules (1) connected end to end, and the heating temperature of the heating modules (1) is adjustable.

2. A lunar living module as claimed in claim 1, characterized in that: Each of the heating modules (1) comprises a supporting wall (11), one side of the supporting wall (11) is provided with an internal heat dissipation unit (12), the other side of the supporting wall (11) is provided with an external heat dissipation unit (13), and a heat conduction component (14) is provided inside; two adjacent heat conduction components (14) are connected end to end, wherein the input end of the first heat conduction component (14) is connected to the output end of the heating system, and the output end of the last heat conduction component (14) is connected to the input end of the heating system; the internal heat dissipation unit (12) and the external heat dissipation unit (13) are both connected to the heat conduction component (14).

3. A lunar living module as claimed in claim 2, characterized in that: The heat-conducting component (14) comprises a heat-conducting block (141) and a liquid metal pipe (142) passing through the heat-conducting block (141); the liquid metal pipes (142) of two adjacent heat-conducting components (14) are connected end to end; two sides of the heat-conducting block (141) extend to two sides of the supporting wall (11); one side of the heat-conducting block (141) is connected to the external heat dissipation unit (13), and the other side is connected to the internal heat dissipation unit (12).

4. A lunar living module as claimed in claim 2, characterized in that: The internal heat dissipation unit (12) comprises a plurality of heat dissipation components (121) arranged side by side, each heat dissipation component (121) comprises an internal heat pipe (1211), one end of the internal heat pipe (1211) is connected to the heat conduction component (14), a plurality of heat dissipation fins (1212) are evenly arranged along the radial direction of the internal heat pipe (1211), the heat dissipation fins (1212) are rotatably connected to the internal heat pipe (1211), and a temperature adjustment component (1213) is arranged at one end of each heat dissipation fin (1212) away from the heat conduction component (14), and the temperature adjustment component (1213) is fixedly connected to the heat dissipation fin (1212).

5. A lunar living module as claimed in claim 4, characterized in that: The outer periphery of the internal heat pipe (1211) is provided with arc-shaped slots (1214) whose number is the same as the number of the heat dissipation fins (1212); one end of the heat dissipation fin (1212) is provided with a protrusion (1215) adapted to the arc-shaped slot (1214); the protrusion (1215) is inserted into the arc-shaped slot (1214) and rotates in the arc-shaped slot (1214).

6. A lunar living module as claimed in claim 4, characterized in that: The temperature control component (1213) comprises a temperature memory spring (12131) and a connecting rod (12132), wherein the free end of the temperature memory spring (12131) is fixedly connected to one end of the connecting rod (12132), and the other end of the connecting rod (12132) is fixedly connected to one end of the heat dissipation fin (1212).

7. A lunar living module as claimed in claim 2, characterized in that: The external heat dissipation unit (13) comprises a heat dissipation plate (131), on which a plurality of external heat pipes are arranged, and each of the external heat pipes is connected to the heat conduction component (14).

8. A lunar living module as claimed in claim 5, characterized in that: A mounting plate (15) is provided at one end of the supporting wall (11), and a placement space for each of the temperature memory springs (12131) is reserved on the mounting plate (15); the temperature memory spring (12131) is placed on the space and a fixed end of the memory spring is fixedly connected to the mounting plate (15).

9. A lunar living module as claimed in claim 2, characterized in that: Two internal heat dissipation units (12) are provided, the two internal heat dissipation units (12) are distributed vertically, and the two internal heat dissipation units (12) are both connected to the heat conduction component (14).

10. A lunar living module as claimed in claim 2, characterized in that: The heating system comprises: a reactor (2), A first circulation loop (3), wherein the first circulation loop (3) is connected to the reactor (2) after generating electricity and exchanging heat via a Stirling generator set (4) to form a closed loop; A second circulation loop (6), wherein the second circulation loop (6) passes through the lunar living module and the heat exchange part of the Stirling generator set (4) in sequence to form a closed loop, and the second circulation loop (6) performs heat exchange with the first circulation loop (3) at the heat exchange part of the Stirling generator set (4); The output end of the power generation part of the Stirling generator (4) is connected to the lunar living module for supplying power to the lunar living module. A lunar soil shielding device (7) is provided between the reactor (2) and the lunar living module.

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