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:
Sep. 19, 2017

Filed:

Aug. 22, 2014
Applicant:

Snecma, Paris, FR;

Inventors:

Damien Merlot, Vaux le Penil, FR;

Remi Sers, Paris, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F01D 5/12 (2006.01); F01D 5/14 (2006.01); F01D 11/00 (2006.01); F01D 5/34 (2006.01); F01D 5/02 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3069 (2013.01); F01D 5/021 (2013.01); F01D 5/12 (2013.01); F01D 5/3038 (2013.01); F01D 5/3061 (2013.01); F01D 5/34 (2013.01); F01D 11/008 (2013.01); F01D 5/143 (2013.01); F05D 2220/323 (2013.01); F05D 2240/24 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01);
Abstract

An assembly for an aircraft turbine engine including an integral element including a disk and a plurality of blades is provided. Each blade has a connection zone connecting the blade to the disk, the connection zone including a first part arranged at the external flowpath delimitation surface provided on the disk, and at least one second end part arranged at a recess formed in the disk along the axial extension of the external surface, the average fillet radius defined by the second end part being larger than the fillet radius defined by the first part. The assembly further includes a flowpath reconstruction part formed in the aerodynamic continuity of the external surface, so as to cover the recess.


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