IP Library Granted Patent US 8,801,384
Granted Patent B2
US 8,801,384 · App. 13/041,913 · Granted Aug 12, 2014

Airfoil attachment holding an airfoil root in a broach fitting

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Quick Facts
Patent No.
US 8,801,384
App. No.
13/041,913
Granted
Aug 12, 2014
Kind
B2
Abstract

An airfoil attachment including a support and flanks rising on it to delimit a broach compartment designed to receive and hold an airfoil root is provided. The flanks are machined so as to separate the portions and prevent a complete break of a flank and detachment of the airfoil when a crack develops because the crack is stopped by one of the notches.

Claims (15)

1. An attachment for an airfoil comprising:

a flat support that is perpendicular to a direction of the airfoil; and

two opposite flanks that rise up on the support delimiting a broach compartment in which a root of the airfoil is retained, the flanks being inclined towards each other from the support such that the compartment communicates to an exterior through a clamped opening and the flanks presenting overhanging regions which bear against the root of the airfoil when centrifugal force is applied on the airfoil,

wherein each of the flanks is divided into portions in a longitudinal direction of the compartment by at least one transverse notch from a free upper edge of the flank at a distance from the support, leading to a region adjacent to the support, the transverse notch extending through the free upper edge and the overhanging regions of both flanks and into a bottom of the compartment.

2. The airfoil attachment according to claim 1 , wherein the portions have different stiffnesses.

3. The airfoil attachment according to claim 2 , wherein one of the portions is bearing on an attachment rib of a platform covering the attachment.

4. The airfoil attachment according to claim 3 , wherein the rib is an attachment tab of a platform covering the attachment.

5. The airfoil attachment according to any one of claims 2 to 4 , wherein the portions have different thicknesses.

6. The airfoil attachment according to claim 1 , wherein the attachment is a pivot comprising a pivoting pin extending under the support.

7. An airfoil assembly, comprising:

an attachment according to claim 1 ; and

an airfoil comprising a root engaged in the compartment and an aerodynamic part rising from the root through an opening of the compartment.

8. The airfoil assembly according to claim 7 , wherein the attachment is metallic and the airfoil is made of a composite material.

9. A variable pitch propeller, comprising a circle of airfoil sets according to either of claim 7 or 8 , the airfoil attachments being pivots.

10. The airfoil attachment according to claim 1 , wherein the support is circular.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →