Aircraft heater

Aeronautics and astronautics – Aircraft structure – Passenger or crew accommodation

Reexamination Certificate

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Reexamination Certificate

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06848652

ABSTRACT:
An aircraft heating system taps into a bleed air flowpath between a turbine engine and an external bleed air port on the aircraft. A system may be installed as a retrofit for heating the cabin of an aircraft already having a heating system for heating the cockpit.

REFERENCES:
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patent: 4978064 (1990-12-01), Steiner
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patent: 5479983 (1996-01-01), Fischer et al.
patent: 5897079 (1999-04-01), Specht et al.
patent: 6012515 (2000-01-01), Stubbendorff et al.
patent: 6139423 (2000-10-01), Wadey
patent: 6216981 (2001-04-01), Helm
patent: 6619589 (2003-09-01), Brasseur et al.

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