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:
Feb. 21, 2023

Filed:

Feb. 13, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Bruno Alexandre Didier Jacon, Moissy-Cramayel, FR;

Baghdad Achbari, Moissy-Cramayel, FR;

Thomas Claude Broage, Moissy-Cramayel, FR;

Florent Robert André Godin, Moissy-Cramayel, FR;

Joël François Roudil, Moissy-Cramayel, FR;

Hervé Simonotti, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/80 (2006.01); B64D 27/10 (2006.01); F02C 7/28 (2006.01); F02K 3/02 (2006.01);
U.S. Cl.
CPC ...
F02K 1/80 (2013.01); B64D 27/10 (2013.01); F02C 7/28 (2013.01); F02K 3/025 (2013.01);
Abstract

An outer shroud of an intermediate casing for a dual flow turbine engine for an aircraft, the shroud including: an annular downstream portion provided with a shroud opening passing through an annular downstream edge of the shroud; a connecting member () attached to the annular downstream portion, and intended to attach an arm that passes through a secondary flow path; an air-sealing and fire-resistance device including: a portion including: a pad arranged in a hollow annular area of the annular downstream edge of the shroud; a blade protruding from the pad and clamped between a circumferential end and the radially outer end of the arm, a leaf spring (pressing the pad into the hollow annular area.


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