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:
Mar. 31, 2020

Filed:

Nov. 27, 2017
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Steffen Golle, Dresden, DE;

Enrico Klausner, Dresden, DE;

Mario Raddatz, Coswig, DE;

Ullrich Hesse, Affalterabach, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/08 (2006.01); B64D 13/06 (2006.01); B64D 13/04 (2006.01); B64D 41/00 (2006.01); F25B 31/00 (2006.01); F25B 5/02 (2006.01);
U.S. Cl.
CPC ...
B64D 13/08 (2013.01); B64D 13/04 (2013.01); B64D 13/06 (2013.01); B64D 41/00 (2013.01); F25B 31/00 (2013.01); B64D 2013/0611 (2013.01); B64D 2013/0618 (2013.01); B64D 2013/0648 (2013.01); B64D 2013/0662 (2013.01); B64D 2013/0674 (2013.01); F25B 5/02 (2013.01); Y02T 50/56 (2013.01);
Abstract

An aircraft air conditioning system includes an ambient air line connected to an aircraft air conditioning system mixer to supply ambient air, and a cabin exhaust air line connectable to an aircraft cabin, and a bleed air line drawn off from an engine or auxiliary power unit. An ambient air compressor in the ambient air line compresses ambient air. A refrigerating apparatus includes a refrigerant circuit and a refrigerant compressor. The refrigerant circuit is thermally coupled to the air line to transfer heat from air line air to refrigerant circulating in the refrigerant circuit before the air is supplied to the mixer. A turbine is coupled to the air compressor. A control device controls the aircraft air conditioning system wherein in a first operating state the turbine receives air from the air line, and in a second operating state receives a mixture of bleed air and cabin exhaust air.


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