Process and system for dealing with fire in an aircraft...

A - Human Necessities – 62 – C

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A62C 3/08 (2006.01) A62C 99/00 (2010.01) B64D 25/00 (2006.01)

Patent

CA 2378826

Ce procédé comprend une phase de.détection (par 26) de la présence du feu, ainai qu'une phase d'extinction de ce feu, comprenant une phase de projection (par 24), dans le compartiment (16), d'un fluide d'extinction, en particulier de l'eau, ainsi qu'une phase de génération (par 2) d'air enrichi en gaz inerte, à partir d'une source d'air comprimé (5) interne à l'avion, et une phase d'admission (par 10 et 12) d'au moins une partie de cet air enrichi dans le compartiment (16).

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