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:
Jul. 21, 2020

Filed:

Oct. 21, 2016
Applicant:

Airbus Defence and Space S.a., Madrid, ES;

Inventors:
Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 15/02 (2006.01); F28D 15/06 (2006.01); B64D 15/06 (2006.01); B64C 3/00 (2006.01); B64D 29/00 (2006.01); F28D 15/02 (2006.01); F28F 23/00 (2006.01); F28F 13/00 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
B64D 15/02 (2013.01); B64C 3/00 (2013.01); B64D 15/06 (2013.01); B64D 29/00 (2013.01); F28D 15/0266 (2013.01); F28D 15/06 (2013.01); F28D 2021/0021 (2013.01); F28F 23/00 (2013.01); F28F 2013/006 (2013.01); F28F 2013/008 (2013.01);
Abstract

A two-phase type heat transfer device () for heat sources operating at a wide temperature range. The heat transfer device () includes an evaporator () collecting heat from a heat source, a condenser () providing heat to a cold sink by a first working fluid passing through liquid and vapor transport lines () that connect the evaporator () and the condenser (). The evaporator () is arranged inside a saddle () configured for avoiding that the temperature of the first working fluid in the evaporator () is greater than its critical point. The invention also refers to aircraft ice protection systems using the heat transfer device ().


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