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. 17, 2018

Filed:

May. 20, 2015
Applicant:

Snecma, Paris, FR;

Inventors:

Sebastien Emile Philippe Tajan, Sucy en Brie, FR;

Denis Louis Bocquet, Bois le Roi, FR;

Gilles Alain Charier, La Grande Paroisse, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 35/06 (2006.01); B64C 11/30 (2006.01); F01D 7/00 (2006.01); B64C 11/38 (2006.01); B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
B64D 35/06 (2013.01); B64C 11/306 (2013.01); B64C 11/38 (2013.01); B64D 2027/005 (2013.01); Y02T 50/66 (2013.01);
Abstract

The present invention relates to a propulsion unit comprising a pair of contra-rotating coaxial propellers, that are referred to as upstream () and downstream (), the downstream propeller, forming a rotating reference frame, being mounted for rotation about a central member forming a stationary reference frame, and being provided with a device for changing the pitch of the blades, characterized in that the downstream propeller is supported by bearings arranged externally on the cylindrical central support, an upstream bearing () of which is arranged downstream of a device for changing the pitch of the blades of the upstream propeller, and in that said device for changing the pitch of the downstream propeller comprises a linear actuator () in the stationary reference frame with an element () that is able to move axially along the axis of the downstream propeller, the upstream bearing comprising an inner ring that is rigidly connected to the linear actuator and an outer ring that is rigidly connected to a rotating casing () of the downstream propeller, and a movement-transmission mechanism () connecting said movable element of the linear actuator to the blades, comprising a load-transfer bearing arranged to transmit the axial forces from the linear actuator to the rotating reference frame of the downstream propeller.


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