Fuel cell system, a fire fighting system, and an aircraft
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United States of America Patent
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Jan 30, 2018
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N/A
app pub date -
Aug 20, 2015
filing date -
Aug 26, 2014
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Abstract
A fuel cell system for an aircraft includes a fuel cell, wherein at the cathode side a cathode inlet and a cathode outlet is provided, and wherein at the anode side an anode inlet and an anode outlet is provided, and a cathode recirculation channel for passing the cathode product fluid from the cathode outlet to the cathode inlet. In the fuel cell system, the water content of the cathode product fluid in the cathode recirculation channel can be reduced or at least stabilized in a possibly effective way, because the cathode recirculation channel includes a water extraction device for extracting water from the cathode product fluid.
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