The present invention concerns a method for controlling an aircraft (1) comprising at least two engines (16, 17), each engine (16, 17) being arranged in its own engine compartment (21, 22), each engine (16, 17) being connected to a fuel supply circuit (31,...

The present invention relates to an inerting system for an aircraft and a method of inerting a hydrogen system, and in particular to an improved inerting system that reuses the inert gas already supplied to the hydrogen system through a fluid recirculation...

The invention relates to an assembly (50) comprising a mast (12) with two lateral walls (12b) provided with openings, an extinguishing agent reservoir, a support (111a) comprising two support elements (110a-b), where each presents a first bearing face (113...

L'invention concerne un ensemble (50) pour aéronef comportant un mât (12) avec un châssis (12a) et deux parois latérales (12b) percées d'une fenêtre (18), un réservoir (102a-b), un système d'accrochage (210) arrangé pour suspendre le réservoir (1...

An emergency supply system for a transportation means comprises at least one fuel cell, a hydrogen tank, an oxygen tank, an extinguishing agent container, an oxidant supply unit and an extinguishing-agent supply unit. The oxidant supply unit comprises an o...