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:
Mar. 15, 2022

Filed:

Dec. 22, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Serge René Morreale, Moissy-Cramayel, FR;

Yanis Benslama, Moissy-Cramayel, FR;

Jérémy Dievart, Moissy-Cramayel, FR;

Dominik Igel, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/36 (2006.01); F01D 7/00 (2006.01); F04D 29/059 (2006.01); B64C 11/38 (2006.01); F04D 29/32 (2006.01); F04D 29/056 (2006.01); F01D 25/16 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F04D 29/362 (2013.01); B64C 11/385 (2013.01); F01D 7/00 (2013.01); F01D 25/16 (2013.01); F02K 3/06 (2013.01); F04D 29/056 (2013.01); F04D 29/059 (2013.01); F04D 29/323 (2013.01); F04D 29/325 (2013.01); F05D 2220/36 (2013.01); F05D 2260/79 (2013.01); F05D 2270/64 (2013.01); Y02T 50/60 (2013.01);
Abstract

A ducted fan module with variable-pitch blades for a turbo engine includes a rotor carrying a plurality of blades, a stationary casing, and a blade pitch changing and control system. The rotor includes a central shaft and a surrounding blade support ring. A front end of the blade support ring is connected to a front end of the central shaft, creating a rearward-opening annular space between the blade support ring and the central shaft. A tubular part is connected to the stationary casing and extends into the annular space.


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