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:
Feb. 27, 2018

Filed:

Dec. 21, 2015
Applicant:

Airbus Operations (Sas), Toulouse, FR;

Inventors:

Julien Guillemaut, Toulouse, FR;

Guillaume Gallant, Lareole, FR;

Assignee:

Airbus Operations (SAS), Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); B64D 27/14 (2006.01); B64C 11/00 (2006.01); B64C 11/06 (2006.01); B64C 11/20 (2006.01);
U.S. Cl.
CPC ...
B64D 27/14 (2013.01); B64C 11/001 (2013.01); B64C 11/06 (2013.01); B64C 11/20 (2013.01); B64D 2027/005 (2013.01); Y02T 50/66 (2013.01);
Abstract

A propeller for a turbomachine intended to be driven in rotation about a propeller rotation axis and including variable pitch blades. The propeller further includes a structure for radial retention of the blades in the event of them breaking. The retaining structure extends around the propeller rotation axis and has the aerodynamic part of each blade of the propeller pass through it. Moreover, each aerodynamic part is equipped with an abutment configured to be retained radially by the retaining structure in the event of a blade fracture causing a fracture in the aerodynamic part radially inside the abutment.


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