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. 19, 2021

Filed:

Apr. 24, 2017
Applicant:

Safran, Paris, FR;

Inventors:

Emilie Goncalves, Moissy-Cramayel, FR;

Nicolas Pierre Lanfant, Moissy-Cramayel, FR;

Robin Mandel, Moissy-Cramayel, FR;

Assignee:

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 23/00 (2006.01); F01D 25/02 (2006.01); F01D 5/14 (2006.01); F01D 9/02 (2006.01); B64D 15/22 (2006.01); B64D 15/16 (2006.01); B64D 15/00 (2006.01); B64D 15/20 (2006.01); B64D 15/12 (2006.01); F02C 7/047 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
B64C 23/005 (2013.01); B64D 15/00 (2013.01); B64D 15/12 (2013.01); B64D 15/16 (2013.01); B64D 15/163 (2013.01); B64D 15/20 (2013.01); B64D 15/22 (2013.01); F01D 5/141 (2013.01); F01D 5/143 (2013.01); F01D 9/02 (2013.01); F01D 25/02 (2013.01); F02C 7/047 (2013.01); F02K 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2250/61 (2013.01); F05D 2260/407 (2013.01); Y02T 50/60 (2013.01);
Abstract

The invention concerns an aircraft propulsion system comprising at least one member () in contact with a turbulent flow of a stream (F), characterised in that said member is covered, at least partially, by a piezoelectric structure (S) such as a piezoelectric film, said structure (S) comprising a grooved structure () comprising a series of grooves, in contact with the flow of the stream, the grooves extending in the direction of flow of the stream, the grooved structure comprising at least one geometric parameter (h, s, w) configured to adapt depending on at least one parameter of the flow of the stream and/or an operating point of the propulsion system and/or an engine speed of the propulsion system.


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