FUEL CELL ELECTROTHERMAL COGENERATION SYSTEM

PROBLEM TO BE SOLVED: To provide a methods for transferring heat produced by a fuel cell module positioned onboard an aircraft.SOLUTION: A power generation system onboard an aircraft includes a fuel cell module configured to produce heat. A loop heat pipe module 218 is coupled to the fuel cell modul...

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Bibliographische Detailangaben
Hauptverfasser:	MOCHIZUKI MASATAKA, MASUKO KOICHI, GUO ZHEN, STEVEN E HAHN, JOSEPH SHERMAN BREIT, SINGH RANDEEP
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY TRANSPORTING
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a methods for transferring heat produced by a fuel cell module positioned onboard an aircraft.SOLUTION: A power generation system onboard an aircraft includes a fuel cell module configured to produce heat. A loop heat pipe module 218 is coupled to the fuel cell module 202. The loop heat pipe module 218 includes a first fluid that absorbs the heat from the fuel cell module 202 and is channeled through the loop heat pipe module 218.