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. 04, 2024

Filed:

Nov. 03, 2021
Applicant:

Safran Nacelles, Gonfreville-l'Orcher, FR;

Inventors:

Jean-Philippe Joret, Moissy-Cramayel, FR;

Vincent Devanlay, Moissy-Cramayel, FR;

Marine Ollivier, Moissy-Cramayel, FR;

Guillaume Levieux, Moissy-Cramayel, FR;

Assignee:

SAFRAN NACELLES, Gonfreville-l'Orcher, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); F05D 2260/30 (2013.01);
Abstract

The invention relates to an assembly for a turbomachine, comprising an exhaust cone () and an exhaust case having an annular inner shell, the exhaust cone () and the exhaust case extending about an axis (X), the exhaust cone () having a radially outer skin () extending in the projection of said inner shell and a radially inner skin () defining a chamber () with the outer skin (), the upstream end () of the cone () being fastened to the inner shell () via connecting lugs (), the assembly comprising an annular fairing () located radially outside said lugs () and extending axially between the inner shell () of the exhaust case () and the outer skin () of the exhaust cone (), said fairing () extending in the projection of said inner shell () and of the outer skin (), the assembly being characterized in that the fairing () is segmented and consists of multiple angular segments () arranged circumferentially end to end.


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