An aircraft with at least one propulsion assembly and its fire-fighting system, which includes two reservoirs of extinguishing agent, and, associated with each reservoir, a control that can be actuated by a pilot to open the reservoir, a detection assembly to detect a fire and emit, if appropriate, a fire alert signal, the propulsion assembly including a first and a second compartment each including at least one fire zone, the fire-fighting system including a bypass valve controlled by a localization unit, a set of pipes connecting each reservoir to each of the fire zones through the bypass valve, the localization unit configured to detect a fire in a fire zone in the first compartment, and, if appropriate, control the bypass valve so it adopts a first state where the extinguishing agent in a reservoir is expelled towards the one or more fire zones in the first compartment after activation of the control associated with a reservoir, the bypass valve otherwise being controlled to adopt a second state, in which the extinguishing agent in a reservoir is expelled towards the one or more fire zones in the second compartment.
AÉRONEF COMPRENANT UN ENSEMBLE PROPULSIF ET UN SYSTÈME ANTI-INCENDIE DE L'ENSEMBLE PROPULSIF
AIRCRAFT INCLUDING A PROPULSION ASSEMBLY AND A FIRE PROTECTION SYSTEM FOR THE PROPULSION ASSEMBLY
LUFTFAHRZEUG, DAS EINE ANTRIEBSEINHEIT UND EIN BRANDSCHUTZSYSTEM FÜR DIESE ANTRIEBSEINHEIT UMFASST
06.07.2022
Patent
Elektronische Ressource
Französisch
Aéronef comprenant un ensemble propulsif et un système anti-incendie de l’ensemble propulsif.
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