NOMAD ELECTRIC ENERGY GENERATION SYSTEM FOR AN AIRCRAFT COMPRISING A FUEL CELL

摘要

A system for generating (S) nomadic electrical energy, in particular for an aircraft, said generation system (S) comprising a source of oxygen (RI), a source of hydrogen (R2), a fuel cell (2) generating electrical energy from dioxygen and dihydrogen. The generation system (S) comprises an aeronautical container (1) configured to be transported in an aircraft and in which the sources (R1, R2) and said fuel cell (2) are mounted, the generation system (S) comprising an electrical connection module (3) electrically connected to the fuel cell (2) and having an electrical outlet connection port (32) configured to be electrically connected to an aircraft for supplying electrical power thereto.