Electric power and cooling system for an aircraft

Refrigeration – With internal-combustion engine – With electrical motor drive

Reexamination Certificate

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Details

C062S402000, C454S071000

Reexamination Certificate

active

06845630

ABSTRACT:
The present invention relates to an electrical power and cooling system for use in an aircraft having at least one engine. The electrical power and cooling system comprises a single shaft, a power turbine mounted on the shaft for receiving fresh pressurized air from the at least one engine, a cooling turbine mounted on the shaft and receiving the fresh pressurized air from the at least one engine, a generator mounted on the shaft, and a fan mounted on the shaft for creating a flow of cooling air. The system further has a condenser for removing moisture from the air exiting the cooling turbine and a mixing chamber for mixing the cooled dry air with recirculated cabin air. The electrical power and cooling system delivers conditioned air to a cabin and/or a flight deck onboard the aircraft and electrical power to the aircraft's electrical systems.

REFERENCES:
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patent: 5086622 (1992-02-01), Warner
patent: 5442905 (1995-08-01), Clasys et al.
patent: 5461882 (1995-10-01), Zywiak
patent: 5860283 (1999-01-01), Coleman et al.
patent: 5918472 (1999-07-01), Jonqueres
patent: 5956960 (1999-09-01), Niggeman
patent: 6124646 (2000-09-01), Artinian et al.
patent: 6189324 (2001-02-01), Williams et al.
patent: 6250097 (2001-06-01), Lui et al.
patent: 6408641 (2002-06-01), Skur, III
patent: 6615606 (2003-09-01), Zywiak
patent: WO 9848162 (1998-10-01), None

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