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Distributed air-cooled fuel cell system and spacecraft

A fuel cell system and fuel cell technology, used in fuel cells, fuel cell additives, fuel cell heat exchange, etc., can solve the problems affecting the stable output of the system, differences in power generation efficiency, etc., to improve reliability, assist heat dissipation, The effect of improving the efficiency of hydrogen-to-electricity conversion

Active Publication Date: 2022-01-07
国家电投集团氢能科技发展有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The system combines the installation environment characteristics of the internal fuel cell sub-modules and the thermal management requirements of the battery itself, and performs multi-objective closed-loop speed control on the fan to achieve high-efficiency output of the fuel cell system as a whole. The monitoring and control of fan steering realizes the comprehensive management of the overall temperature of the power system, which solves the problem that the power generation efficiency of each subunit is too large due to environmental differences in the actual operation of the distributed air-cooled fuel cell power system, which affects the overall stable output of the system.

Method used

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  • Distributed air-cooled fuel cell system and spacecraft
  • Distributed air-cooled fuel cell system and spacecraft
  • Distributed air-cooled fuel cell system and spacecraft

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Embodiment Construction

[0035] Embodiments of the present application are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application.

[0036] The following describes the distributed air-cooled fuel cell system of the embodiment of the present application with reference to the accompanying drawings.

[0037] figure 1 A schematic structural diagram of a distributed air-cooled fuel cell system proposed in the embodiment of the present application, as shown in figure 1 As shown, the system includes: a hydrogen storage module 10 , a fuel cell module 20 , an electronic control module 30 and a first temperature sensor 40 . Wherein, the hydrogen storage module 10...

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Abstract

The invention discloses a distributed air-cooled fuel cell system and a spacecraft. The system comprises a hydrogen storage module, a fuel cell module, an electric control module and a first temperature sensor, wherein the first temperature sensor is used for monitoring the environment temperature of the system; the hydrogen storage module is used for supplying low-pressure hydrogen to the fuel cell module; the fuel cell module comprises at least three air-cooled hydrogen fuel cells which are connected in a series-parallel mode, and each cell comprises a second temperature sensor and a rotating speed and rotating direction adjustable fan; and the electric control module comprises a controller located in the center of the system, and the controller is used for adjusting the rotating direction of each fan according to the environment temperature and conducting closed-loop control over the rotating speed of the fan according to the running temperature and the generated power of each battery. According to the system, multi-target closed-loop rotating speed control is conducted on the fan by combining the environmental characteristics of the inner battery and the thermal management requirement of the system, the fan is controlled to rotate according to the environmental temperature, and the overall power generation output efficiency of the system is improved.

Description

technical field [0001] The present application relates to the technical field of proton exchange membrane fuel cells, in particular to a distributed air-cooled fuel cell system and spacecraft. Background technique [0002] At present, air-cooled hydrogen fuel cell systems are increasingly widely used in aerospace and other fields due to their advantages of high-quality power density, zero pollution and long battery life. In spacecraft such as UAVs, since the layout of the air-cooled fuel cell power system must match the cabin of the spacecraft, it is often restricted by the space layout and gas flow characteristics. The thermal management system of the air-cooled fuel cell monitors the ambient temperature and the stack temperature, and controls the heat dissipation of the air-cooled fuel cell in combination with factors such as solid-state hydrogen storage heat dissipation and power regulation. [0003] In related technologies, the thermal management system of air-cooled fu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01M8/04014H01M8/0432H01M8/0438H01M8/0444H01M8/04701H01M8/2465
CPCH01M8/04014H01M8/04388H01M8/04447H01M8/0432H01M8/04701H01M8/2465H01M2250/20Y02E60/50
Inventor 孙振兴韩立勇吕希曹博凯胡黎花杨子骁高博一李欢曾琪钊陈平李从心
Owner 国家电投集团氢能科技发展有限公司
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