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. 27, 2023

Filed:

May. 28, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

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

Jean-François Cabre, Moissy-Cramayel, FR;

Nicolas Camille Claude Curlier, Moissy-Cramayel, FR;

Lucas Arthur Pflieger, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/075 (2006.01); F02K 3/06 (2006.01); F02K 3/10 (2006.01);
U.S. Cl.
CPC ...
F02K 3/075 (2013.01); F02K 3/06 (2013.01); F02K 3/10 (2013.01); F05D 2220/323 (2013.01); F05D 2240/14 (2013.01); F05D 2260/52 (2013.01); F05D 2260/606 (2013.01);
Abstract

A confluence structure of an aircraft bypass turbine engine which includes a confluence plate with a downstream end supported by a portion that is movable in the direction of the axis by a control mechanism which can optionally be adjusted in flight. A mobile portion of a sleeve delimiting the secondary stream on the outside, and an inner projection of the outer casing can also slide axially in certain embodiments. This provides a wide range of options for modifying the gas dilution and operating conditions of the engine.


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