Air contamination detection in an aircraft air system

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 13/00 (2006.01)

Patent

CA 2731593

An aircraft air system includes a gas turbine engine, a bleed air duct directing compressed air bled from a compressor to an inner compartment within the aircraft, and an air contamination detector located downstream of the gas turbine engine compressor. The air contamination detector includes a visual indicator which detects the presence of a fluid contaminant within the bleed air.

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