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:
Jul. 20, 2021

Filed:

Jan. 26, 2016
Applicant:

Safran, Paris, FR;

Inventor:

Matthieu Leyko, Orsay, FR;

Assignee:

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 5/12 (2006.01); F23R 7/00 (2006.01); F23R 3/48 (2006.01); F23R 3/26 (2006.01); F23R 3/46 (2006.01); F02K 7/06 (2006.01); F02C 7/264 (2006.01);
U.S. Cl.
CPC ...
F02C 5/12 (2013.01); F23R 3/26 (2013.01); F23R 3/46 (2013.01); F23R 3/48 (2013.01); F23R 7/00 (2013.01); F02C 7/264 (2013.01); F02K 7/06 (2013.01); F05D 2240/35 (2013.01);
Abstract

The invention relates to a turbine engine combustion module (), in particular for an aircraft turbine engine, designed to carry out constant-volume combustion, comprising: at least two combustion chambers (A,B) arranged about an axis, each chamber (A,B,C) comprising a compressed gas intake port () and a burnt gas exhaust port (); and an ignition means that triggers combustion in the combustion chambers (A,B,C). The module () comprises at least one duct () which establishes a communication between a first combustion chamber (A) and at least one second combustion chamber (B) in order to inject burnt gases from the first combustion chamber (A) into the second combustion chamber (B) so as to trigger combustion in the second combustion chamber (B).


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