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:
Sep. 13, 2016

Filed:

May. 04, 2012
Applicants:

Francois Marie Paul Marlin, Villiers sous Grez, FR;

Frederic Imbourg, Orly, FR;

Didier Queant, Saint Fargeau Ponthierry, FR;

Inventors:

Francois Marie Paul Marlin, Villiers sous Grez, FR;

Frederic Imbourg, Orly, FR;

Didier Queant, Saint Fargeau Ponthierry, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F01D 5/32 (2006.01); F01D 11/00 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3038 (2013.01); F01D 5/323 (2013.01); F01D 11/008 (2013.01); F04D 29/322 (2013.01); F05D 2220/36 (2013.01);
Abstract

A rotor of a turbomachine, such as a multi-flow turbojet engine fan, has a disc including, on the rim thereof, substantially axial slots with a dovetailed cross-section, and blades mounted individually in the slots, an axial wedge positioned between the root of the blades and the bottom of the slots, and a transverse lock providing upstream axial immobilization of the blades in the slot thereof. The lock is guided in radial notches formed in the flanks of the slots and radially supported against the wedge. The axial wedge is immobilised in the upstream direction, butting up against a transverse annular component secured to the disc.


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