Space hybrid propulsion system based on technology of photocatalytic water splitting for hydrogen production

A technology of photo-splitting water for hydrogen production and space mixing, which is applied in jet propulsion, electrolysis process, electrolysis components, etc., can solve the problems of large size of solar panels, complex structure of propulsion system, and high power loss, etc., to simplify the system. Good structure, good stability, and the effect of improving utilization efficiency

Pending Publication Date: 2021-05-28
XIAN AEROSPACE PROPULSION INST
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Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that in the existing water-based propulsion system, the solar battery sails are bulky, the proton exchange membrane water electrolysis cell has high requirements for electric energy, the loss of electric energy is large, the efficiency of hydrogen production is low, and the structure of the propulsion system is complicated. problems, and provides a space hybrid propulsion system based on photo-splitting water hydrogen production technology

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  • Space hybrid propulsion system based on technology of photocatalytic water splitting for hydrogen production
  • Space hybrid propulsion system based on technology of photocatalytic water splitting for hydrogen production
  • Space hybrid propulsion system based on technology of photocatalytic water splitting for hydrogen production

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[0038]In order to make the objects, advantages and features of the present invention, the spatial hybrid propulsion system proposed by the present invention will be further described in detail below with reference to the accompanying drawings and the specific embodiments.

[0039]Photo hydrogen hydrogen hydrogen hydrogen production uses photocatalytic materials and solar energy to solve water into hydrogen and oxygen to solve a chemical technique of green production of solar storage and hydrogen production, mainly photocatalytic and photoelectric catalysis. The optoelectronic catalysis is advantageous with respect to photocatalysis, which can effectively separate and collect hydrogen and oxygen. In such a manner, the photoelectric catalysis is employed, and the catalyst is deposited on the conductive substrate, and the photode electrode is formed into a two-electrode system, and the two optic electrodes are immersed in the electrode. In the electrolyte, oxygen and hydrogen gas, hydrogen,

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Abstract

The invention relates to a space hybrid propulsion system based on the technology of photocatalytic water splitting for hydrogen production, and aims to solve the problem that in an existing water-based propulsion system, solar arrays are large in size, a proton exchange membrane water electrolytic cell is high in requirements for electrical energy, large in loss of electrical energy and low in hydrogen production efficiency, and the propulsion system is complicated in structure. The space hybrid propulsion system comprises a water storage tank, a photocatalytic water splitting module, a hydrogen and oxygen storage module, a hydrogen and oxygen flow control module, a hydrogen and oxygen engine module and an oxygen cold gas engine module, wherein the photocatalytic water splitting module comprises an electrolytic cell, a proton exchange membrane, a hydrogen production electrode, an oxygen production electrode and a condenser; the proton exchange membrane is arranged in the electrolytic cell; the electrolytic cell is divided into a hydrogen production chamber and an oxygen production chamber by the proton exchange membrane; the hydrogen production electrode and the oxygen production electrode are separately arranged in the hydrogen production chamber and the oxygen production chamber; the condenser is arranged on the oxygen production chamber; the water storage tank is used for supplying water to the photocatalytic water splitting module; the hydrogen and oxygen storage module is used for storing hydrogen and oxygen; and the hydrogen and oxygen are supplied to the hydrogen and oxygen engine module and the oxygen cold gas engine module through the hydrogen and oxygen flow control module.

Description

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Claims

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Application Information

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Owner XIAN AEROSPACE PROPULSION INST
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