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:
Oct. 16, 2018

Filed:

Feb. 06, 2014
Applicant:

Snecma, Paris, FR;

Inventors:

Baptiste Jouy, Moissy-Cramayel, FR;

Bertrand Pellaton, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 5/22 (2006.01); F01D 5/02 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 5/02 (2013.01); F01D 5/141 (2013.01); F01D 5/225 (2013.01); F05D 2220/10 (2013.01); F05D 2220/36 (2013.01); F05D 2240/55 (2013.01); F05D 2250/00 (2013.01); F05D 2250/314 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01);
Abstract

An impeller for a turbine engine is disclosed, such as a turbojet engine or a turboprop engine of an aircraft, for rotating about an axis of rotation in a predetermined direction of rotation and for having a flow of gas passing therethrough, comprising a series of blades distributed circumferentially about the axis of rotation of the wheel, the radially external end of each blade comprising a heel supporting at least one radially external lip, extending circumferentially in an oblique direction relative to the radial plane perpendicular to the axis of rotation, the lip being angled circumferentially in the downstream direction in the aforementioned direction of rotation such as to enable a compression of the gases located upstream from the lip during the rotation of the impeller.


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