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. 07, 2026

Filed:

Jun. 12, 2023
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran Ceramics, Le Haillan, FR;

Inventors:

Fabrice Marcel Noël Garin, Moissy-Cramayel, FR;

Romain Claude Gabriel Bardon, Moissy-Cramayel, FR;

Fabrice Joël Luc Chevillot, Moissy-Cramayel, FR;

Lucien Henri Jacques Quennehen, Moissy-Cramayel, FR;

Simon Jean-Marie Bernard Cousseau, Moissy-Cramayel, FR;

Assignees:

SAFRAN AIRCRAFT ENGINES, Paris, FR;

SAFRAN CERAMICS, Le Haillan, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/22 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); F05D 2220/323 (2013.01); F05D 2240/80 (2013.01); F05D 2260/96 (2013.01);
Abstract

A bladed turbomachine assembly including at least two adjacent blades, each blade including a radial aerofoil and a platform located at a free radial end of the aerofoil, the platform of each blade of the bladed assembly being located circumferentially facing a platform of the other circumferentially adjacent blade of the bladed assembly, the bladed assembly including an insert arranged circumferentially between the platforms and which cooperates with the platforms, each platform including a circumferential bearing face against which a circumferential end of the insert is in contact, and the direction of the contact between each circumferential bearing face and the insert being oriented circumferentially with respect to the main axis (A).


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