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:
Mar. 19, 2019

Filed:

Jul. 27, 2016
Applicant:

Thales, Courbevoie, FR;

Inventors:

Claude Sarno, Valence, FR;

Romain Hodot, Valence, FR;

Marc Duval-Destin, 27 rue Jules Vedrines, FR;

Assignee:

THALES, Courbevoie, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01P 5/165 (2006.01); B64D 15/12 (2006.01); B64D 43/02 (2006.01); F28D 15/02 (2006.01); B33Y 80/00 (2015.01); B33Y 10/00 (2015.01); B33Y 50/02 (2015.01); B22F 3/105 (2006.01); B22F 5/10 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
G01P 5/165 (2013.01); B22F 3/1055 (2013.01); B22F 5/10 (2013.01); B33Y 10/00 (2014.12); B33Y 50/02 (2014.12); B33Y 80/00 (2014.12); B64D 15/12 (2013.01); B64D 43/02 (2013.01); F28D 15/0266 (2013.01); F28D 2021/0021 (2013.01); Y02P 10/295 (2015.11);
Abstract

Manufacturing method by addition for at least one part of 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 of the aircraft and heating elements for that part, which include a thermodynamic loop including a closed circuit at least partially integrated, 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 being formed by a tubular channel with an empty section at least partially integral with the equipment piece, at least the part of the equipment piece arranged outside the aircraft is made by additive manufacturing and includes a base for fastening on the skin of the aircraft from which support elements for a Pitot tube extend.


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