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:
Jan. 02, 2024

Filed:

Sep. 13, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Raphael Jean Philippe Dupeyre, Moissy-Cramayel, FR;

Josserand Jacques Andre Bassery, Moissy-Cramayel, FR;

Jeremy Jacques Attilio Fanelli, Moissy-Cramayel, FR;

Etienne Leon Francois, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/22 (2006.01); F01D 5/30 (2006.01); F01D 11/12 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); F01D 5/30 (2013.01); F01D 11/122 (2013.01); F05D 2240/127 (2013.01); F05D 2240/80 (2013.01); F05D 2250/182 (2013.01);
Abstract

A moving blade for a wheel of an aircraft turbine engine, including an aerodynamic aerofoil and an outer heel defining the aerofoil. The heel includes a platform and a first lip that projects from the platform. The first lip is inclined upstream and peripherally along an axis of elongation. The heel includes a row of ribs that are arranged at a distance from each other. The row of ribs extends along the axis of elongation and from the platform up to the first lip. The ribs are arranged upstream of the first lip in such a way as to generate turbulence upstream of first lip.


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