The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 05, 2016

Filed:

Nov. 09, 2012
Applicant:

Turbomeca, Bordes, FR;

Inventor:

Laurent Houssaye, Saint Faust, FR;

Assignee:

TURBOMECA, Bordes, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/06 (2006.01); B64D 13/06 (2006.01); B64D 41/00 (2006.01);
U.S. Cl.
CPC ...
B64D 13/06 (2013.01); B64D 41/00 (2013.01); B64D 2013/0611 (2013.01); B64D 2013/0648 (2013.01); Y02T 50/53 (2013.01); Y02T 50/56 (2013.01);
Abstract

A method and architecture for recovery of energy in an aircraft, both at altitude and on the ground, and recovering thermal energy from an exhaust. An architecture for recovery of energy includes an auxiliary power unit APU including an exhaust nozzle and a gas generator including a shaft transmitting power to a load compressor. The compressor supplies compressed air via a supply duct to an ECS air conditioning system of a passenger cabin. A recovery turbocharger is connected, directly or via a transmission case, to the shaft of the APU. The turbocharger includes a recovery turbine powered by a downstream branch of a conduit mounted on a heat exchanger fitted to the nozzle. The conduit includes an upstream branch connected to channels connecting air outlets of the cabin and the compressor. A second exchanger can be mounted between the supply duct and the cabin outlet channel.


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