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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.

Patent No.:

US 10472074 B1

PDFFull Text
Date of Patent:
Nov. 12, 2019

Filed:

Jul. 27, 2016

Heating for an avionic equipment

Applicant:

Thales, Courbevoie, FR;

Inventors:

Adrien Desjardins, Vendome, FR;

Frederic Martin, Vendome, FR;

Claude Sarno, Valence, FR;

Romain Hodot, Valence, FR;

Jean-Philippe Pineau, Vendome, FR;

Assignee:

THALES, Courbevoie, FR;

Attorney:

Young & Thompson

Primary Examiner:

Philip J Bonzell

Assistant Examiner:

Tye William Abell

Int. Cl.
CPC ...
B64D 15/06 (2006.01); B64D 43/02 (2006.01); G01P 5/165 (2006.01); F28D 15/02 (2006.01); B33Y 10/00 (2015.01); B33Y 50/02 (2015.01); B33Y 80/00 (2015.01); B64F 5/00 (2017.01); F25B 39/00 (2006.01); B64D 15/12 (2006.01); F28D 21/00 (2006.01); F25B 39/02 (2006.01);
U.S. Cl.
CPC ...
B64D 15/06 (2013.01); B33Y 10/00 (2014.12); B33Y 50/02 (2014.12); B33Y 80/00 (2014.12); B64D 43/02 (2013.01); B64F 5/00 (2013.01); F25B 39/00 (2013.01); F28D 15/0266 (2013.01); G01P 5/165 (2013.01); B64D 15/12 (2013.01); F25B 39/02 (2013.01); F28D 15/02 (2013.01); F28D 2021/0021 (2013.01);
Abstract

The invention relates to an aircraft provided with at least one piece of aeronautic equipment fastened to the outside skin of the aircraft and a heater for heating the piece of aeronautic equipment. The heater is in the form of a thermodynamic closed circuit loop circulating heat-transfer fluid and including an evaporator and a heat source located inside the aircraft and a condenser located in the piece of aeronautic equipment or an appendage thereto. Fasteners in the form of tubular tabs include tubular channels for circulating the heat-transfer fluid.

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