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. 03, 2015

Filed:

Jul. 23, 2010
Applicants:

Eric Jacques Boston, Cesson, FR;

Michel André Bouru, Montereau sur le Jard, FR;

Laurent Jablonski, Melun, FR;

Philippe Gérard Edmond Joly, Vaux le Penil, FR;

Inventors:

Eric Jacques Boston, Cesson, FR;

Michel André Bouru, Montereau sur le Jard, FR;

Laurent Jablonski, Melun, FR;

Philippe Gérard Edmond Joly, Vaux le Penil, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/32 (2006.01); F01D 5/02 (2006.01); F01D 21/04 (2006.01); B64C 11/02 (2006.01); B64C 11/48 (2006.01); F01D 1/26 (2006.01); F01D 5/30 (2006.01); F01D 7/00 (2006.01); F01D 7/02 (2006.01); F02C 6/20 (2006.01); F02C 9/58 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
F04D 29/321 (2013.01); B64C 11/02 (2013.01); B64C 11/48 (2013.01); F01D 1/26 (2013.01); F01D 5/025 (2013.01); F01D 5/3007 (2013.01); F01D 7/00 (2013.01); F01D 7/02 (2013.01); F02C 6/206 (2013.01); F02C 9/58 (2013.01); B64D 2027/026 (2013.01); Y02T 50/66 (2013.01); F05D 2220/325 (2013.01); F05D 2260/74 (2013.01); F05D 2260/79 (2013.01); Y02T 50/671 (2013.01);
Abstract

A hub for a propeller having variable pitch blades for a turbine engine, for example for a propfan turbine engine. The propeller hub includes: a polygonal ring having substantially radial cylindrical housings distributed about a central axis of the ring for receiving the blades; a rotor element for the turbine of the turbine engine; a supporting flange attached to the ring so as to connect the ring to the rotor element; and a plurality of backup retaining members linked to the rotor element, and each of which includes at least one bearing surface opposite an outer surface of the ring with a radial spacing.


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