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US09072921B2 Thermodynamically-optimized advanced fire suppression system 有权
热力学优化的先进灭火系统

Thermodynamically-optimized advanced fire suppression system
Abstract:
A fire suppression system for an aircraft includes an air separation module configured to receive exhaust air and ram air, conditioned compressor bleed air, and any combination thereof. The air separation module is also configured to provide nitrogen-enriched air and inert gas. The nitrogen-enriched air flows into a nitrogen-enriched air distribution network for fuel tank inerting. The inert gas flows into an inert gas distribution network for fire suppression in areas of the aircraft other than fuel tanks.
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