A fire suppression system (16) for an aircraft (cargo) compartment (8) comprises a source (18) of fire suppression agent and a supply line (20) for conducting the fire suppression agent to the compartment (8). The supply line comprises a pressure regulating device (26) arranged between the source (18) and the compartment (8) and a pressure relief valve (28) arranged downstream of the pressure regulating device (26). The pressure relief valve (28) has an outlet (30) which distributes the agent externally of the cargo compartment (8).
Fire supression systems
2015-12-02
Patent
Electronic Resource
English
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