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:
Jul. 06, 2021

Filed:

Dec. 22, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Gilles Alain Charier, La Grande Paroisse, FR;

Thomas Julien Nguyen Van, Alfortville, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/30 (2006.01); F01D 7/00 (2006.01); F02C 3/067 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
B64C 11/306 (2013.01); F01D 7/00 (2013.01); F02C 3/067 (2013.01); F02C 7/36 (2013.01); F05D 2250/44 (2013.01); F05D 2260/40311 (2013.01);
Abstract

A turbine engine module including an upstream propulsive unit including a propellers doublet that are upstream and downstream, respectively mounted around an axis, a power turbine shaft with axis of rotation intended for rotating the propellers doublet, a speed reducer connected to the propellers doublet and driven by the shaft, and, a pitch-changing system including a cylinder that controls the pitch of the blades of the upstream propeller the rotational axis of the propellers doublet is shifted in relation to that of the shaft. The cylinder is placed downstream of the reducer, and the pitch-changing system includes a shaft for controlling the pitch of the blades that connect the cylinder to the blades of the upstream propeller.


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