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:
Sep. 29, 2015

Filed:

Dec. 03, 2007
Applicants:

Wilson Willy Casas Noriega, Hamburg, DE;

Wolfgang Ebigt, Hamburg, DE;

Andreas Frey, Immenstaad, DE;

Inventors:

Wilson Willy Casas Noriega, Hamburg, DE;

Wolfgang Ebigt, Hamburg, DE;

Andreas Frey, Immenstaad, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F28D 15/00 (2006.01); F28F 7/00 (2006.01); B64D 13/00 (2006.01); B64D 13/06 (2006.01); F25B 25/00 (2006.01);
U.S. Cl.
CPC ...
B64D 13/00 (2013.01); B64D 13/06 (2013.01); B64D 2013/0614 (2013.01); B64D 2013/0674 (2013.01); F25B 25/005 (2013.01); F25B 2500/06 (2013.01); Y02T 50/56 (2013.01);
Abstract

An aircraft cooling system includes a first coolant stream which cools at least one first heat load and a second coolant stream which cools at least one second heat load. The aircraft cooling system is formed such that the first heat load and the second heat load are thermally coupled together. The first heat load and the second heat load can be formed by two mutually redundant aircraft components. A third coolant stream thermally couples the first heat load and the second heat load together. The third coolant stream can be cooled by a heat sink, such as the outer skin of the aircraft in a bilge region.


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