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:
Aug. 01, 2017

Filed:

Dec. 27, 2013
Applicants:

Rolls-royce Corporation, Indianapolis, IN (US);

Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);

Inventors:

Igor Vaisman, Carmel, IN (US);

Douglas J. Snyder, Carmel, IN (US);

Patrick C. Sweeney, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F25D 17/06 (2006.01); B64D 13/08 (2006.01); B64D 13/06 (2006.01); F25B 1/10 (2006.01); F25B 6/04 (2006.01); F25B 40/00 (2006.01); F25B 41/00 (2006.01); F25B 9/06 (2006.01);
U.S. Cl.
CPC ...
B64D 13/08 (2013.01); B64D 13/06 (2013.01); F25B 1/10 (2013.01); F25B 6/04 (2013.01); F25B 9/06 (2013.01); F25B 40/00 (2013.01); F25B 41/00 (2013.01); B64D 2013/064 (2013.01); B64D 2013/0614 (2013.01); B64D 2013/0674 (2013.01); F25B 2341/0011 (2013.01); F25B 2341/0661 (2013.01); F25B 2400/0401 (2013.01); F25B 2400/14 (2013.01); Y02T 50/56 (2013.01);
Abstract

A cooling system for an aircraft includes a first cooling circuit having a first evaporator and a second evaporator, and a second cooling circuit having a third evaporator and a fourth evaporator. One of the first and second cooling circuits includes a first set of valves arranged to direct refrigerant through a first cooling sub-circuit, a second cooling sub-circuit, or both the first and second cooling sub-circuits based on ambient conditions. Two of the evaporators are installed on a first side of the aircraft, and the other two of the four evaporators are installed on a second side of the aircraft opposite the first side, and the first and second cooling circuits reject heat, via a heat exchanger, from their respective cooling circuit to air passing into an engine of the aircraft.


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