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Self-circulating heat management and power generation system for lunar base

A power generation system and heat management technology, applied in solar thermal power generation, solar heating systems, solar collectors in specific environments, etc., can solve problems such as low-temperature waste heat exceeding the working temperature range, inability to apply to space and aerospace, and heat transfer. To achieve the effect of saving electricity demand

Active Publication Date: 2019-04-12
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The existing technology is mainly applied to the ground state, and the cooling method is mainly water cooling, which cannot adapt to the heat exchange in the vacuum state of space, and the existing patent uses low-temperature waste heat exceeding the working temperature range of aerospace instruments and equipment, so it cannot be applied to space and aerospace fields such as lunar bases

Method used

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  • Self-circulating heat management and power generation system for lunar base

Examples

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Embodiment 1

[0026] In this example, a self-circulating thermal management and power generation system used in a lunar base, the working fluid is R600, and the circulation process is illustrated for daytime or extreme daytime conditions.

[0027] In daytime or extreme daytime conditions, the temperature of the cold plate is 30°C, the waste heat utilization is 6.3kW, after being heated by the directional solar collector 4, the temperature is 40°C, the evaporation pressure is 0.4MPa, and the expansion ratio of the turbine 5 is 2.5, The outlet pressure of the turbine 5 is 0.15MPa, the condensing temperature of the directional space radiator 10 is -10°C, the condensing pressure is 0.07MPa, the evaporation temperature of the refrigeration evaporator 13 is -15°C, and the space ambient temperature is 4K. The above parameters are taken as The working parameters illustrate the cycle flow, but the parameters involved in the implementation process do not limit the present invention.

[0028] 1. The l...

Embodiment 2

[0036] In this embodiment, a self-circulating heat management and power generation system used in a lunar base, the working fluid is R600, and the circulation process is illustrated for the night or polar night state.

[0037] During daytime or extreme daytime conditions, the temperature of the cold plate 2 is 30°C, the waste heat utilization is 6.3kW, the temperature is 40°C after being heated by the directional solar collector 4, the evaporation pressure is 0.4MPa, and the expansion ratio of the turbine 5 is 2.5 , the outlet pressure of the turbine 5 is 0.15MPa, the condensation temperature of the directional space radiator 10 is -10°C, the condensation pressure is 0.07MPa, the evaporation temperature of the refrigeration evaporator 13 is -15°C, and the space environment temperature is 4K, the above parameters As working parameters, the cycle flow is described, but the parameters involved in the implementation process do not limit the present invention.

[0038] 1. The liqui...

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Abstract

The invention discloses a self-circulating heat management and power generation system for a lunar base. Specifically, liquid saturated organic working media are sent to a cold plate or a directionalsolar collector by a working medium pump and are heated to a saturated or superheated steam state, then a turbine is pushed to rotate so as to drive generating load to generate power, gas working media flow into an ejector after going out of the turbine, gas on the outlet side of a refrigeration evaporator is injected into the ejector, the gas working media and the gas are mixed and diffused in the ejector and then enter a directional space radiator so as to release heat to the space and coagulate in a liquid state, a part of the liquid working media enter the working medium pump again so as to complete the power generating circulation, and the other part of the liquid working media are cooled and depressurized through a throttle valve and return to the refrigeration evaporator again so asto complete the refrigeration cycle. The self-circulating heat management and power generation system can be operated on the moon at daytime or polar day and at night or polar night, own power consumption is satisfied, additional power supply and cold supply are provided for the base, and the power demand of the lunar base is effectively saved.

Description

technical field [0001] The invention relates to a thermal management and power generation system in the aerospace field, in particular to a self-circulating thermal management and power generation system for a lunar base. Background technique [0002] Spacecraft thermal management is proposed along with the enlargement of space vehicles. It is a unified distribution and management of heat in large spacecraft from the perspective of the overall system, and completes the collection, transmission, utilization and dissipation of spacecraft heat. On the one hand, it ensures that its structural components, instruments and equipment are in a suitable temperature range in the space environment, so that they can work normally. On the other hand, ensure that the atmospheric environment in the cabin meets certain temperature conditions for the normal life of astronauts. In addition, the unified allocation and comprehensive utilization of the spacecraft's heat can reduce energy demand...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F24S20/00F25B9/08F28D20/02B64G1/50F01D15/10F01K27/00F03G6/06
CPCB64G1/50F01D15/10F01K27/00F03G6/067F25B9/08F28D20/02Y02E10/46Y02E60/14Y02E70/30
Inventor 孙培杰翁一武丁逸夫章恺王长焕包轶颖严立
Owner SHANGHAI AEROSPACE SYST ENG INST
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