A hybrid power distribution system for an aircraft includes a first and second set of electrically-powered devices, such as inverters, motors and so forth. A first battery system is coupled to one or more of the first set of electrically-powered devices an...

La présente invention concerne un système et un procédé (20) d'aide au pilotage d'un aéronef, ledit procédé (20) comportant lors d'une phase de vol dudit aéronef au moins deux étapes de mesure (21, 21') d'au moins deux valeurs courantes respective...

A distributed electronic control system (100) for an aircraft includes an engine data controller (103) arranged on an airframe of the aircraft and a plurality of engine data concentrators (104-106) arranged proximate an engine of the aircraft in signal com...

The power plant (2) has a control unit (5) with a memory (6), where the memory containing information enabling the engine to be operated in accordance with two distinct utilization envelopes during a maximum number of flying hours. An envelope enables take...