Fuel cell system module

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 41/00 (2006.01)

Patent

CA 2710289

A fuel cell system module (10) for use in an aircraft (32) comprises at least one fuel cell system component (12, 22, 24). The fuel cell system module (10) is connectable modularly to a fuselage section (30) of the aircraft (32). A housing element (16, 26) of the fuel cell system module (10) is designed to form a section of an outer skin (34) of the aircraft (32) when the fuel cell system module (10) is in the state connected to the fuselage section (30) of the aircraft (32).

La présente invention concerne un module de système de pile à combustible (10) conçu pour être utilisé dans un aéronef (32), lequel module comprend au moins un composant de système de pile à combustible (12, 22, 24). Le module de système de pile à combustible (10) peut être raccordé de façon modulaire à une section de fuselage (30) de l'aéronef (32). Un élément boîtier (16, 26) du module de système de pile à combustible (10) est conçu de manière à former une partie d'un revêtement extérieur (34) de l'aéronef (32) lorsque le module de système de pile à combustible (10) est raccordé à la section de fuselage (30) de l'aéronef (32).

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