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. 06, 2020

Filed:

Feb. 20, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Paul Antoine Foresto, Fontainbleau, FR;

Vivien Mickaël Courtier, Yerres, FR;

Christophe Paul Jacquemard, Hericy, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/32 (2006.01); B64C 11/06 (2006.01); F01D 5/14 (2006.01); B64C 11/02 (2006.01); F01D 5/02 (2006.01); F01D 5/30 (2006.01); F01D 7/00 (2006.01); F04D 29/36 (2006.01);
U.S. Cl.
CPC ...
F04D 29/329 (2013.01); B64C 11/02 (2013.01); B64C 11/06 (2013.01); F01D 5/02 (2013.01); F01D 5/143 (2013.01); F01D 5/30 (2013.01); F01D 7/00 (2013.01); F04D 29/323 (2013.01); F04D 29/362 (2013.01); F05D 2220/36 (2013.01); F05D 2250/184 (2013.01); F05D 2250/713 (2013.01); F05D 2260/74 (2013.01); Y02T 50/673 (2013.01);
Abstract

A hub for a propeller having variable-pitch blades for a turbomachine with longitudinal rotation axis, including a plurality of blade platforms, each one being designed to receive a blade root, the platforms being distributed around the annular outer periphery of the hub concentrically with the longitudinal rotation axis, wherein each blade platform has the general geometric shape of a spherical cap, and wherein, between two adjacent blade platforms around the longitudinal rotation axis, the transverse dimension, in particular the diameter, of the hub can vary axially and radially.


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