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, 36) equipped with its own fuel supply…
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 system.
A multi-directional fire extinguishing nozzle (200; 300; 400; 500) is disclosed. The multi-directional fire extinguishing nozzle (200; 300; 400; 500) may comprise a pylon fitting (270; 470; 570) configured to receive a fire extinguishing agent. The multi-directional fire extinguishing nozzle (200…
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) oriented upward and onto which the…
The invention relates to an assembly (50) for an aircraft comprising a mast (12) with a frame (12a) and two side walls (12b) pierced with a window (18), a tank (102a-b), a hanging system (210) arranged to suspend the tank (102a-b) in front of the windows (18), a carriage (202) presenting a cradle…
L'invention concerne un ensemble propulsif avec un compartiment extérieur (112), un compartiment intérieur (140), une canalisation d'apport (266) et une canalisation de transfert (260) entre les deux compartiments, un système d'aspiration (252) entre les deux canalisations, un moyen de régulation…
L'invention concerne un ensemble propulsif comprenant une turbomachine accrochée à un mat, et un système anti-incendie, la turbomachine comprenant une pluralité de zones feu, le système anti-incendie comprenant deux réservoirs d'agent extincteur sous pression situés dans le mat et une ligne de…
L'invention concerne un aéronef comprenant au moins un ensemble propulsif (10) et son système anti-incendie (20) qui comprend deux réservoirs (R1, R2) d'agent extincteur, et associée à chaque réservoir, une commande (C1, C2) actionnable par un pilote pour l'ouverture du réservoir, un ensemble de…
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 oxygen inlet that is connectable to the…