Importance

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Abstract

A system for extinguishing and suppressing a fire in an aircraft includes a precooler, a heat exchanger, a condenser, a gas separator, and an accumulator. The precooler is configured to receive a bleed air from an engine of the aircraft. The heat exchanger is fluidly coupled with the precooler. The condenser is configured to receive a cabin exhaust air from a passenger cabin of the aircraft. The gas separator is fluidly coupled with the condenser and is fluidly coupled with the heat exchanger. The gas separator is configured to generate a fire suppressing agent from the bleed air and the cabin exhaust air. The accumulator is fluidly coupled with the gas separator. The accumulator is configured to receive the fire suppressing agent.

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First Claim