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:
Jun. 28, 2022

Filed:

Aug. 17, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Olivier Baptiste Bidart, Moissy-Cramayel, FR;

Galadriel Dancie, Moissy-Cramayel, FR;

Brice Marie Yves Emile Le Pannerer, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06T 7/00 (2017.01); F04C 28/28 (2006.01); F23M 5/00 (2006.01); G06T 11/60 (2006.01);
U.S. Cl.
CPC ...
G06T 7/001 (2013.01); F04C 28/28 (2013.01); F23M 5/00 (2013.01); G06T 11/60 (2013.01); G06T 2207/10068 (2013.01); G06T 2207/30164 (2013.01);
Abstract

The invention relates to a combustion chamber module for an aircraft turbine engine, comprising a combustion chamber defined by an internal annular wall and an external annular wall provided with air intake openings, the module further comprising an internal housing and an external housing. According to the invention, at least one of the internal and external housings has, on the surface thereof facing the combustion chamber, a marking system comprising a plurality of different marks angularly spaced apart from each other, each mark being produced facing one of the air intake openings in order to be visible from inside the combustion chamber and each indicating the angular position of a zone of the combustion chamber comprising the air intake opening.


Find Patent Forward Citations

Loading…