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:
Apr. 12, 2022

Filed:

May. 31, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Patrice André Commaret, Moissy-Cramayel, FR;

Haris Musaefendic, Moissy-Cramayel, FR;

Romain Nicolas Lunel, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/46 (2006.01); F02C 7/22 (2006.01); F02C 9/16 (2006.01); F23R 3/28 (2006.01);
U.S. Cl.
CPC ...
F23R 3/46 (2013.01); F02C 7/22 (2013.01); F02C 9/16 (2013.01); F23R 3/283 (2013.01); F05D 2220/32 (2013.01);
Abstract

An annular combustion chamber of a turbomachine is described. The combustion chamber has an axis of revolution and is delimited by coaxial internal and external annular walls joined upstream by a bottom of chamber substantially transverse to the walls. In some embodiments, the chamber includes at least one annular deflector placed in the chamber and substantially parallel to the bottom of chamber. The bottom of chamber may have openings adapted to be traversed by air for cooling the deflector. In some embodiments, the bottom of chamber and the deflector include mounting openings for mounting an annular row of injection devices for injecting a mixture of air and fuel into the chamber. At least a portion of the air for cooling the deflector is conveyed into the chamber through holes in the injection devices.


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