Moon base energy system based on power generation-heat collection integrated assembly

Abstract

The invention provides a lunar base energy system based on a power generation-heat collection integrated assembly, and belongs to the field of lunar base energy supply, the lunar base energy system comprises a power generation-heat collection array, a heating module and a heat storage module, the power generation-heat collection array and the heat storage module are connected through a heat collection conveying pipeline to form a loop, the heating module comprises a cabin heat exchanger, a heat pump system and a lunar base cabin, the heat pump system is connected with the heat storage module through a pipeline to form a heat exchange loop, and the heat pump system exchanges heat with the lunar base cabin through a heat pump condenser; the lunar base cabin exchanges heat with the heat storage module through the heat conveying pipeline and the cabin heat exchanger. According to the system, output of heat energy and electric energy is achieved at the same time through the power generation-heat collection integrated assembly, various energy supplies can be provided for the lunar base, the generated heat can be directly used for heating lunar night equipment and personnel, and a sufficient guarantee is provided for reliable operation of the lunar base.

Description

Technical Field

[0001] The present invention belongs to the field of lunar base energy supply, and in particular relates to a lunar base energy system based on a power generation-heat collection integrated component. Background Art

[0002] As the closest extraterrestrial body to the Earth, the construction of a lunar base has become an important springboard for the development of human deep space exploration. An important prerequisite for all lunar activities such as lunar base construction and resource mining is to ensure the reliable operation of lunar-based equipment, and the special space environment on the lunar surface poses new challenges to this. First of all, the space distance between the moon and the Earth is 380,000 kilometers. Due to the existing space carrying capacity and cost factors, it is impossible to directly use energy on the Earth. Secondly, during the lunar night of 14 Earth days, the temperature on the lunar surface is as low as minus 180 ℃. Existing ground equipment and personnel cannot survive at this temperature. The heating and insulation of equipment and personnel in the long-term and extremely low-temperature space environment is also an urgent problem to be solved in the construction of the lunar base.

[0003] Since there is no atmosphere on the moon, the intensity of solar radiation during the lunar day is 1.5 times that of the earth, and a lunar day is about 14 earth days. Therefore, the lunar surface has abundant solar energy resources. How to efficiently use solar energy is crucial to the construction of the lunar base. At present, the energy supply system of the lunar base based on solar energy includes solar photovoltaic power generation system and solar thermal power generation system. The solar thermal power generation system has various functions. The solar energy collected by the circulating working fluid can be used for thermal cycle power generation and heating and insulation of equipment and personnel in the lunar base at the same time. However, the solar thermal power generation system has a complex structure and many components, resulting in high transportation costs between the earth and the moon. In addition, the system has a large number of complex moving parts such as turbines and compressors. In the harsh environment of extremely high and low temperatures on the lunar surface, the system life and reliability are severely challenged. These problems lead to certain disadvantages of solar thermal power generation system when it is applied on the lunar surface. Compared with the solar thermal system, the solar photovoltaic power generation system has the advantages of simple structure and high maturity, but there are also some problems when the solar photovoltaic power generation system is applied on the lunar surface. First, solar photovoltaic modules can only generate electricity using solar energy on the lunar surface, and the energy output form is single. For the lunar base, the single energy output form leads to a low risk resistance of the energy system. Secondly, solar photovoltaic power generation systems are equipped with batteries, and battery power heating is used during the lunar night to achieve heating and insulation of lunar base equipment and personnel. However, the energy density of batteries is low, and the charging and discharging efficiency is low in the extremely low temperature environment of the lunar night. Therefore, a larger placement space and resource ratio are required to meet the high-load energy demand of the lunar base, resulting in an increase in the cost of transportation from the earth to the moon. At the same time, the efficiency of solar photovoltaic power generation is low, generally 20% to 30%. If the large amount of heat and electricity needs of the lunar base are to be met at the same time, the area of ​​​​the photovoltaic panels must be increased, resulting in an increase in the cost of transportation from the earth to the moon.

[0004] Based on the above content, how to combine the advantages of solar thermal systems and photovoltaic power generation systems, design a multifunctional device with a simple and reliable structure that can generate electricity and heat at the same time, and design a lunar energy supply system based on the multifunctional device, which is of great significance for reducing the cost of Earth-Moon transportation, improving the utilization efficiency of lunar solar energy, and ensuring the reliable and long-life operation of the lunar base. Summary of the invention

[0005] In order to solve the above technical problems, the present invention proposes a lunar base energy system based on an integrated power generation and heat collection component. This energy system can use lunar solar energy to simultaneously achieve heat generation and power generation. The energy output is diverse in form and has high solar energy utilization efficiency. The heat produced can be directly used for heating equipment and personnel on the moon night, avoiding the application defects of low energy utilization efficiency and high resource allocation cost of battery-powered heating solutions, and reducing the transportation cost of the earth to the moon caused by energy storage devices such as batteries. At the same time, compared with the solar thermal power generation system, this energy system has a simple structure and fewer complex moving parts, which has certain advantages in ensuring the long-life reliability of the system and reducing the transportation cost of the earth to the moon.

[0006] To achieve the above object, the present invention adopts the following technical solution:

[0007] A lunar base energy system based on an integrated power generation and heat collection component comprises a power generation and heat collection array, a heat storage module and a heating module, wherein the power generation and heat collection array is composed of a certain number of power generation and heat collection integrated components connected in series and parallel, the heating module comprises a cabin heat exchanger, a lunar base cabin and a heat pump system, the power generation and heat collection array and the heat storage module are connected to form a loop through a solar thermal collector heat collection and transportation pipeline, the heat pump system is connected to the heat storage module through a pipeline to form a heat exchange loop, the heat pump system exchanges heat with the lunar base cabin through a condenser, and the lunar base cabin exchanges heat with the heat storage module through a heat transportation pipeline and a cabin heat exchanger.

[0008] Furthermore, the power generation-heat collection integrated assembly mainly includes photovoltaic cells, aerogel, solar thermal collector panels, heat collection pipelines and insulation layers, and the photovoltaic cells are arranged at certain intervals to ensure that the solar thermal collector panels can receive solar energy.

[0009] Furthermore, the solar transmittance of the aerogel is above 90%, which can fully ensure that the solar collector panel receives sufficient solar energy to generate heat.

[0010] Furthermore, the role of the aerogel is heat insulation. The thermal conductivity of the aerogel is lower than that of the air, and the transmittance in the infrared band is low, which can effectively reduce the heat loss caused by the thermal radiation of the solar collector panel, and at the same time avoid the adverse effect of the solar collector panel on the radiation heating of the photovoltaic cell, which leads to a decrease in the photoelectric conversion efficiency.

[0011] Furthermore, a heat collection pipeline is arranged on the back of the power generation-heat collection integrated assembly, and the heat collection pipeline and the solar heat collection panel are connected and heat exchanged by welding.

[0012] Furthermore, the power generation-heat collection array and the heat storage module transfer and exchange heat through heat collection pipelines and heat exchange medium, and the heat exchange medium can be heat transfer oil, antifreeze liquid, etc.

[0013] Furthermore, the heat storage module and the lunar base cabin directly transfer and exchange heat through connecting pipes and heat exchange media, or indirectly exchange heat through a heat pump system.

[0014] Furthermore, the heat storage module transfers the stored heat to the heat pump system through connecting pipelines, and then through the operation of the heat pump system, the heat is transferred to the lunar base cabin at the heat pump condenser.

[0015] Furthermore, the condenser and the cabin heat exchanger use circulating air to exchange heat with the cabin of the lunar base.

[0016] Furthermore, the heat storage module includes a heat storage box, sintered lunar soil and a heat storage box insulation assembly, and the heat storage box insulation assembly is used to reduce heat leakage from the heat storage box to the in-situ lunar soil.

[0017] Furthermore, the heat storage module is buried inside the in-situ lunar soil on the lunar surface, making full use of the low thermal conductivity characteristics of the in-situ lunar soil to achieve heat preservation of the heat storage module.

[0018] Furthermore, flow valve No. 1 and flow valve No. 2 are provided on the connecting pipeline between the power generation-heat collection array and the heat storage module, flow valve No. 3 and flow valve No. 6 are provided on the connecting pipeline between the heat storage module and the lunar base cabin, and flow valve No. 4 and flow valve No. 5 are provided on the connecting pipeline between the heat storage module and the heat supply heat exchanger.

[0019] Furthermore, a No. 1 working fluid pump is provided on the connecting pipeline between the power generation-heat collection array and the heat storage module, a No. 2 working fluid pump is provided on the connecting pipeline between the heat storage module and the heat supply heat exchanger, and a No. 3 working fluid pump is provided on the connecting pipeline between the heat storage module and the lunar base cabin.

[0020] Furthermore, a No. 1 temperature detection module is installed on the heat storage module to monitor the temperature of the sintered lunar soil inside the heat storage box in real time, and a No. 2 temperature detection module is installed on the lunar base cabin to monitor the temperature inside the lunar base cabin in real time.

[0021] Compared with the prior art, the present invention has the following beneficial technical effects:

[0022] 1. Compared with the lunar photovoltaic power generation system, the integrated power generation and heat collection assembly of the present invention can realize photovoltaic power generation and solar heat collection at the same time, with high solar energy utilization efficiency and various energy output forms, which can fully meet the various energy needs of the lunar base.

[0023] 2. The heat generated by the solar collector panels of the integrated power generation and heat collection assembly of the present invention can be directly used for heating equipment and personnel on moonlit nights, solving the practical application problems of low energy efficiency and high resource allocation costs of battery-powered heating solutions on moonlit nights, while reducing the Earth-Moon transportation costs of batteries and other energy storage devices.

[0024] 3. Compared with the solar thermal power generation system on the lunar surface, the present invention also achieves the energy output of heat and electrical energy. However, the system of the present invention has fewer complex moving parts, a simple and reliable structure, and is more in line with the design requirements of high reliability and long service life of the lunar base energy system. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] The accompanying drawings, which constitute part of the present invention, are used to provide a further understanding of the present invention. The exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute improper limitations of the present invention. In the accompanying drawings:

[0026] Figure 1 A lunar base energy system based on an integrated power generation and heat collection component according to an embodiment of the present invention;

[0027] Figure 2 This is the operation diagram of the lunar daytime power generation and heat storage system;

[0028] Figure 3 This is a schematic diagram of the operation of the direct heating mode of the heat storage module;

[0029] Figure 4 This is a schematic diagram of the operation of the heat storage module in indirect heating mode;

[0030] Figure 5 It is a schematic diagram of the structure of the heat storage module;

[0031] Figure 6 It is a structural schematic diagram of the integrated solar collector and power generation component; wherein a is the front view and b is the left view.

[0032] Among them, the figure numbers are as follows: 1-power generation-heat collection array, 2-power generation-heat collection array control module, 3-flow valve No. 1, 4-heat storage module, 5-temperature detection module No. 1, 6-working fluid pump No. 1, 7-flow valve No. 2, 8-flow valve No. 3, 9-flow valve No. 4, 10-working fluid pump No. 2, 11-heat supply heat exchanger, 12-compressor, 13-condenser, 14-cabin heat exchanger, 15-lunar base cabin, 16-temperature detection module No. 2, 17-throttle valve, 18-working fluid pump No. 3, 19-flow valve No. 5, 20-flow valve No. 6, 21-in-situ lunar soil, 22-heat storage box, 23-sintered lunar soil, 24-heat storage box insulation assembly, 25-photovoltaic cell, 26-aerogel, 27-solar collector, 28-heat collection pipeline, 29-insulation layer. DETAILED DESCRIPTION

[0033] The following will be combined with the drawings in the embodiments of the present invention to clearly explain the technical solutions in the embodiments of the present invention. It should be noted that the embodiments of the present invention and the features in the embodiments can be combined with each other without conflict, and the described embodiments are only part of the embodiments of the present invention, not all of the embodiments.

[0034] like Figure 1-Figure 4 As shown, a lunar base energy system based on an integrated power generation and heat collection component according to an embodiment of the present invention includes a power generation and heat collection array 1, a heat storage module 4 and a heating module. The power generation and heat collection array 1 and the heat storage module 4 are connected by a heat collection pipeline to form a loop.

[0035] The power generation and heat collection array 1 includes a heat exchange device, a lunar base cabin 15 and a heat pump system. The heat pump system includes a heat supply heat exchanger 11, a compressor 12, a condenser 13 and a throttle valve 17. The heat pump system exchanges heat with the heat storage module 4 through a connecting pipeline, the heat pump system exchanges heat with the lunar base cabin 15 through the condenser 13, and the lunar base cabin 15 exchanges heat with the heat storage module 4 through a heat transport pipeline and a cabin heat exchanger 14. At the same time, a No. 1 flow valve 3 and a No. 2 flow valve 7 are provided on the connecting pipeline between the power generation-heat collection array 1 and the heat storage module 4, a No. 3 flow valve 8 and a No. 6 flow valve 20 are provided on the connecting pipeline between the heat storage module 4 and the lunar base cabin 15, a No. 4 flow valve 9 and a No. 5 flow valve 19 are provided on the connecting pipeline between the heat storage module 4 and the heat supply heat exchanger 11, a No. 1 working fluid pump 6 is provided on the connecting pipeline between the power generation-heat collection array 1 and the heat storage module 4, a No. 2 working fluid pump 10 is provided on the connecting pipeline between the heat storage module 4 and the heat supply heat exchanger 11, a No. 3 working fluid pump 18 is provided on the connecting pipeline between the heat storage module 4 and the lunar base cabin 15, a No. 1 temperature detection module 5 is installed on the heat storage module 4, and a No. 2 temperature detection module 16 is installed in the lunar base cabin 15.

[0036] like Figure 5 As shown, the heat storage module 4 includes a heat storage box 22, sintered lunar soil 23, and a heat storage box insulation assembly 24. The heat storage box 22 is buried inside the in-situ lunar soil 21 on the lunar surface, making full use of the low thermal conductivity characteristics of the in-situ lunar soil 21 to achieve heat preservation of the heat storage module 4.

[0037] like Figure 6As shown, the power generation-heat collection array 1 includes a plurality of power generation-heat collection integrated components, which include photovoltaic cells 25, aerogel 26, solar heat collection panels 27, heat collection pipelines 28 and insulation layers 29, and the photovoltaic cells 25 are arranged at a certain interval to ensure that the solar heat collection panels 27 can receive solar energy. The photovoltaic cells 25 are arranged on the inner side of the upper surface of the shell, and the solar heat collection panels 27 are arranged thereunder. Aerogel 26 is arranged between the photovoltaic cells 25 and the solar heat collection panels 27. The insulation layer 29 is below the solar heat collection panels 27, and evenly spaced heat collection pipelines 28 are arranged in the insulation layer 29. The heat collection pipelines 28 are connected to the solar heat collection panels 27. The solar heat collection panels 27 absorb heat, convert it into electrical energy, and store it in the photovoltaic cells 25. At the same time, the heat absorbed by the solar heat collection panels 27 is transmitted to the outside of the shell through the heat collection pipelines 28 and sent to the heat storage module 4.

[0038] The embodiment of the present invention also provides a working method of a lunar base energy system based on a power generation-heat collection integrated assembly, including the following working modes:

[0039] Lunar day heat storage stage:

[0040] like Figure 2 As shown, in this embodiment, during the lunar day, the power generation-heat collection array 1 receives the radiation of solar energy, a part of the solar energy generates electricity through the photoelectric conversion effect of the photovoltaic cell, and a part of the solar energy is converted into heat energy through the solar thermal collector 27. When the solar radiation energy and the temperature of the solar thermal collector reach a certain standard, the No. 1 flow valve 3, the No. 2 flow valve 7 and the No. 1 working fluid pump 6 are opened, and the other valves are in a closed state. Under the driving action of the No. 1 working fluid pump 6, the heat exchange working fluid enters the power generation-heat collection array 1 through the No. 2 flow valve 7 to collect the heat energy generated by the solar thermal collector 27. After absorbing heat from the solar thermal collector 27, the heat exchange working fluid enters the heat storage module 4 through the No. 1 flow valve 3 and exchanges heat with the sintered lunar soil 23 therein, thereby storing the heat generated by the solar thermal collector 27 during the lunar day to meet the heating needs of the equipment and personnel of the lunar base during the lunar night.

[0041] Moon night heating stage:

[0042] Heat storage module 4 direct heating mode: Figure 3As shown, in this embodiment, during the moon night, flow valve No. 1 3, flow valve No. 2 7 and working fluid pump No. 1 are always in the closed state. At the initial stage of heating at moon night, the temperature inside the heat storage module is relatively high, and the lunar base cabin 15 can be directly heated. At this time, flow valve No. 3 8, flow valve No. 6 20 and working fluid pump No. 3 18 are opened, and the heat pump system, the remaining valves and working fluid pumps are all in the closed state. Driven by working fluid pump No. 3 18, the heat exchange working fluid enters the heat storage module 4 through flow valve No. 6 20. After absorbing the heat stored in the sintered lunar soil 23, the heat exchange working fluid flows through flow valve No. 3 8 along the connecting pipeline to the cabin heat exchanger 14, and the heat of the heat exchange working fluid is transferred to the lunar base cabin 15 by circulating air.

[0043] Heat storage module 4 indirect heating mode: Figure 4 As shown, in the direct heating mode of the heat storage module 4, as the heat inside the heat storage module 4 is continuously released, the temperature of the sintered lunar soil 23 continues to drop, and it is difficult to maintain the temperature requirements inside the lunar base cabin 15 in the later stage. At this time, the system adopts the indirect heating mode of the heat storage module 4, opens the No. 4 flow valve 9, the No. 5 flow valve 19, the No. 2 working fluid pump 10 and the heat pump system, and the remaining valves and working fluid pumps are in a closed state. The heat exchange working fluid enters the heat storage module 4 through the No. 5 flow valve 19 under the driving action of the No. 2 pump 10. After absorbing the heat of the heat storage module 4, the heat exchange working fluid enters the heat supply exchange module 4 through the No. 4 flow valve 9. Heat exchanger 11, in the heating heat exchanger 11, the heat exchange working medium exchanges heat with the refrigerant of the heat pump system. For the heat pump system, the low-temperature and low-pressure refrigerant absorbs the heat of the heat exchange working medium in the heating heat exchanger 11 and evaporates, then enters the compressor 12 for compression, and then becomes a high-temperature and high-pressure refrigerant gas. The high-temperature and high-pressure refrigerant gas comes out of the compressor 12 and enters the condenser 13, and then the heat of the refrigerant is transferred to the lunar base cabin 15 by circulating air. After that, the refrigerant enters the throttle valve and becomes a low-temperature and low-pressure refrigerant liquid, and then returns to the heating heat exchanger 11 for heat exchange with the heat exchange working medium.

[0044] In this embodiment, when heating on a moonlit night, the direct heating mode of the heat storage module 4 is adopted in the early stage of the moonlit night, and the indirect heating mode of the heat storage module 4 is adopted in the later stage of the moonlit night. This heating mode can fully release the heat stored in the sintered lunar soil storage 23, and the energy utilization efficiency is high.

[0045] In this embodiment, Figure 5 As shown, the sintered lunar soil 23 is processed into block-shaped cylinders or cubes and evenly placed in the heat storage box 22 for sensible heat storage. The thermal conductivity of the sintered lunar soil 23 can reach 2 W / (mk), which is more efficient in storing and releasing heat than the in-situ lunar soil 21 (the thermal conductivity is generally 0.001 W / (mk)).

[0046] In this embodiment, Figure 5As shown, since the thermal conductivity of the in-situ lunar soil 21 is very low, generally 0.001 W / (mk), the heat storage module 4 is buried inside the in-situ lunar soil 21 on the lunar surface for insulation. The heat storage module 4 is composed of sintered lunar soil 23, a heat storage box 22 and a heat storage box insulation assembly 24 from the inside to the outside. The heat storage box insulation assembly 24 is used to reduce the heat exchange between the low-temperature in-situ lunar soil 21 and the high-temperature heat storage module 4, thereby reducing heat storage losses.

[0047] The embodiments of the present invention disclosed above are only used to help illustrate the present invention. The embodiments do not describe all the details in detail, nor do they limit the application to the specific implementation methods described. According to the content of this specification, many modifications and changes can be made. This specification selects and specifically describes these embodiments in order to better explain the principles and practical applications of the present invention, so that those skilled in the art can understand and use the present invention well.

Claims

1. A lunar base energy system based on an integrated power generation and heat collection component, characterized in that: The invention comprises a power generation-heat collection array (1), a heat storage module (4) and a heating module. The power generation-heat collection array is composed of a certain number of power generation-heat collection integrated components connected in series and parallel. The heating module comprises a cabin heat exchanger (14), a lunar base cabin (15) and a heat pump system. The power generation-heat collection array (1) and the heat storage module (4) are connected via a solar heat collecting panel (27) heat collection and transmission pipeline to form a loop. The heat pump system is connected to the heat storage module (4) via a pipeline to form a heat exchange loop. The heat pump system exchanges heat with the lunar base cabin (15) via a condenser (13). The lunar base cabin (15) exchanges heat with the heat storage module (4) via a heat transmission pipeline and the cabin heat exchanger (14).

2. A lunar base energy system based on an integrated power generation and heat collection assembly according to claim 1, characterized in that: The power generation-heat collection integrated assembly mainly comprises a photovoltaic cell (25), an aerogel (26), a solar heat collection panel (27), a heat collection pipeline (28) and a thermal insulation layer (29), and the photovoltaic cells (25) are arranged at even intervals, thereby ensuring that the solar heat collection panel (27) can receive solar energy to generate heat.

3. A lunar base energy system based on an integrated power generation and heat collection assembly according to claim 1, characterized in that: The solar light transmittance of the aerogel (26) is above 90%, which can fully ensure that the solar collector plate (27) receives sufficient solar energy.

4. A lunar base energy system based on an integrated power generation and heat collection assembly according to claim 1, characterized in that: The aerogel (26) is used for heat insulation and thermal preservation. The thermal conductivity of the aerogel (26) is lower than that of air, and the transmittance in the infrared band is low, which effectively reduces the heat loss caused by the thermal radiation of the solar thermal collector (27), and at the same time avoids the adverse effect of the solar thermal collector (27) on the photovoltaic cell (25) due to radiation heating, which leads to a decrease in the photoelectric conversion efficiency.

5. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1 is characterized in that: A heat collection pipeline (28) is arranged on the back of the power generation and heat collection array (1), and the heat collection pipeline (28) and the solar heat collection plate (27) are connected and heat exchanged by welding.

6. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1 is characterized by: The power generation-heat collection array (1) and the heat storage module (4) transmit and exchange heat via a heat collection pipeline (28) and a heat exchange medium, wherein the heat exchange medium is heat transfer oil or antifreeze liquid.

7. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1 is characterized by: The heat storage module (4) and the lunar base cabin (15) directly transfer and exchange heat via connecting pipelines and heat exchange working fluids, or indirectly exchange heat via a heat pump system.

8. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1 is characterized by: The heat storage module (4) transfers the stored heat to the heat pump system via a connecting pipeline, and then the heat pump system operates to transfer the heat to the lunar base cabin (15) at the heat pump condenser (13).

9. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1 is characterized by: The condenser (13) and the cabin heat exchanger (14) use circulating air to perform heat exchange with the lunar base cabin (15).

10. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1, characterized in that: The heat storage module (4) comprises a heat storage box (22), sintered lunar soil (23) and a heat storage box insulation component (24), wherein the heat storage box insulation component (24) is used to reduce heat leakage from the heat storage box (22) to the in-situ lunar soil (21).

11. A lunar base energy system based on an integrated power generation and heat collection assembly according to claim 1, characterized in that: The heat storage module (4) is buried inside the in-situ lunar soil (21) on the lunar surface, and fully utilizes the low thermal conductivity characteristics of the in-situ lunar soil (21) to achieve heat preservation of the heat storage module.

12. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1, characterized in that: A No. 1 flow valve (3) and a No. 2 flow valve (7) are provided on the connecting pipeline between the power generation-heat collection array (1) and the heat storage module (4), a No. 3 flow valve (8) and a No. 6 flow valve (20) are provided on the connecting pipeline between the heat storage module (4) and the lunar base cabin (15), and a No. 4 flow valve (9) and a No. 5 flow valve (19) are provided on the connecting pipeline between the heat storage module (4) and the heat supply heat exchanger (11).

13. The lunar base energy system based on the integrated power generation and heat collection assembly according to claim 1, characterized in that: A first working fluid pump (6) is provided on the connecting pipeline between the power generation-heat collection array (1) and the heat storage module (4), a second working fluid pump (10) is provided on the connecting pipeline between the heat storage module (4) and the heat supply heat exchanger (11), and a third working fluid pump (18) is provided on the connecting pipeline between the heat storage module (4) and the lunar base cabin (15).

14. The solar photovoltaic and lunar soil heat storage-based lunar base power and heating energy system according to claim 1, characterized in that: A first temperature detection module (5) is installed on the heat storage module (4) for real-time monitoring of the temperature of the sintered lunar soil (23) inside the heat storage box (22); and a second temperature detection module (16) is installed on the lunar base cabin (15) for real-time monitoring of the temperature inside the lunar base cabin (15).

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