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:
May. 22, 2018

Filed:

Jul. 27, 2016
Applicant:

Thales, Courbevoie, FR;

Inventors:

Romain Hodot, Valence, FR;

Claude Sarno, Valence, FR;

Frederic Martin, Vendome, FR;

Adrien Desjardins, Vendome, FR;

Jean-Philippe Pineau, Vendome, FR;

Assignee:

THALES, Courbevoie, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01F 1/46 (2006.01); B64D 15/06 (2006.01); B64D 15/12 (2006.01); B64D 43/02 (2006.01); G01P 5/165 (2006.01); B33Y 80/00 (2015.01); F28D 15/04 (2006.01); B33Y 50/02 (2015.01); B22F 3/105 (2006.01); B22F 5/10 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
B64D 15/06 (2013.01); B22F 3/1055 (2013.01); B22F 5/10 (2013.01); B33Y 50/02 (2014.12); B33Y 80/00 (2014.12); B64D 15/12 (2013.01); B64D 43/02 (2013.01); F28D 15/043 (2013.01); G01F 1/46 (2013.01); G01P 5/165 (2013.01); B22F 2202/13 (2013.01); B22F 2203/00 (2013.01); F28D 2021/0021 (2013.01);
Abstract

A piece of aeronautic equipment intended to equip an aircraft, the equipment piece () including at least one part intended to be arranged at a skin () outside of the aircraft and heating elements for that part, which include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including an evaporator and a zone in which condensation of the heat transfer fluid can occur in the appendage to heat it, outside the evaporator, the circuit in which the fluid circulates is formed by a tubular channel with an empty section, at least the part of the piece of equipment arranged outside the aircraft is made by additive manufacturing and includes a fastening base () for fastening on the skin of the aircraft from which support elements () for a Pitot tube () provided with lateral static pressure taps () extend.


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