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:
Nov. 10, 2020

Filed:

Jan. 05, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Romain Guillaume Cuvillier, Moissy-Cramayel, FR;

Nils Edouard Romain Bordoni, Moissy-Cramayel, FR;

Michel Gilbert Roland Brault, Moissy-Cramayel, FR;

Guillaume Patrice Kubiak, Moissy-Cramayel, FR;

Arnaud Nicolas Negri, Moissy-Cramayel, FR;

Nathalie Nowakowski, Moissy-Cramayel, FR;

Emmanuel Pierre Dimitri Patsouris, Moissy-Cramayel, FR;

Sebastien Emile Philippe Tajan, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 7/00 (2006.01); F02K 3/06 (2006.01); F04D 29/36 (2006.01);
U.S. Cl.
CPC ...
F01D 7/00 (2013.01); F02K 3/06 (2013.01); F04D 29/362 (2013.01); F05D 2220/36 (2013.01); F05D 2260/74 (2013.01); F05D 2260/79 (2013.01);
Abstract

A fan of a turbine engine includes a disc provided with blades at the periphery thereof, the blades being mounted so as to pivot on the disc about a pivot axis, and a mechanism for changing the pitch of the blades. The mechanism is configured to adjust an angular position of each blade around the pivot axis. The angular position is in an angular setting range no greater than 20°.


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