An aircraft including a fuselage defining a cabin and baggage bay, engine compartments for receiving engines, an auxiliary power unit compartment for receiving an auxiliary power unit, and a fire suppression system including first and second reservoirs containing a fire suppressant. The reservoirs are each connected to all of the engine compartments for distribution of the fire suppressant thereto. The first reservoir is connected to only one of the auxiliary power unit compartment and baggage bay, and the second reservoir is connected to only the other of the auxiliary power unit compartment and baggage bay. A fire suppression system for an aircraft and a method of connecting a fire suppression system of an aircraft are also discussed.
AIRCRAFT FIRE SUPPRESSION SYSTEM
BRANDUNTERDRÜCKUNGSSYSTEM FÜR FLUGZEUG
SYSTÈME D'EXTINCTION D'INCENDIE POUR AÉRONEF
2021-08-11
Patent
Electronic Resource
English