Supply system for the energy supply in an aircraft, aircraft...

Details Supply system for the energy supply in an aircraft, aircraft... Supply system for the energy supply in an aircraft, aircraft...

B - Operations, Transporting

64

D

B64D 41/00 (2006.01) B64D 11/02 (2006.01) B64D 13/06 (2006.01) B64D 15/02 (2006.01) B64D 37/04 (2006.01)

Patent

CA 2584889

A supply system (100) for the energy supply in an aircraft comprising an engine (101) for propelling an aircraft, a fuel cell (102) for supplying an aircraft with electric energy, a first fuel reservoir (103) for supplying the engine (101) with engine fuel and a second fuel reservoir (104) for supplying the fuel cell (102) with fuel cell fuel. The first fuel reservoir (103) is arranged separately of the second fuel reservoir (104).

L'invention porte sur un système (100) d'alimentation en énergie d'un aéronef comportant: un propulseur (101); une pille à combustible (102) fournissant l'électricité de bord; un premier réservoir (103) alimentant le propulseur en carburant; et un deuxième réservoir (104) alimentant la pile à combustible en combustible. Le premier réservoir (103) est indépendant du deuxième réservoir (104).

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