| 摘要 |
<p>A method for managing an electric power network (1) of an aircraft, the power network (1) comprising at least one distribution bus arranged to supply electrical loads, at least one generator (G1, G2) of a propulsion engine of the aircraft, at least one main engine-class power unit (MPS1, MPS2), a plurality of contactors (C1-C18) designed to electrically connect the distribution buses with the propulsion engine generator (G1, G2) and/or the main power unit (MPS1, MPS2); and a management module designed to control the contactors (C1- C18), method in which, in normal operating conditions of the aircraft, the distribution bus is powered by the main engine-class power unit (MPS1, MPS2) and during the emergency operation of the aircraft, the distribution bus is powered by the propulsion engine generator (G1, G2).</p> |
