IP Library Granted Patent US 10,132,177
Granted Patent B2
US 10,132,177 · App. 14/893,332 · Granted Nov 20, 2018

Hollow vane, and associated production method

Inventors: Guillaume Fribourg (Puteaux, FR); Pierre Delaleau (La Garenne Colombes, FR); Florian Tellier (Yerres, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F01D9/041B23P11/025B23P15/04F01D5/147F05D2230/60F05D2240/12F05D2300/43F05D2300/502F16B4/008
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Quick Facts
Patent No.
US 10,132,177
App. No.
14/893,332
Granted
Nov 20, 2018
Kind
B2
Abstract

A hollow vane, includes a main portion, of which the cavity is closed by a cover, that is produced by expanding the main portion relative to the cover, for example by means of differential thermal expansion, then by placing the cover at the bottom of the opening of the cavity, before allowing the main portion to close again, closing a nesting between a protrusion at the bottom of the cover and a widening at the bottom of the opening. The disadvantages linked to the use of welding, glue or even assembly parts are as such avoided.

Claims (21)

1. A hollow vane comprising:

a main portion; and

a cover, the cover being mounted in an opening of the main portion in such a way as to close the opening and to form with the main portion an external, substantially continuous face of the vane,

wherein the main portion comprises a cavity that communicates with the external face via the opening,

wherein the cover comprises a protrusion, extending over a portion of a thickness of the cover at a distance from the external face, and over an edge of the cover,

wherein the main portion comprises a widening of the opening, located at a distance from the external face and in which the protrusion of the cover penetrates, and

wherein the opening of the main portion comprises a bottom face which is a bearing face for an internal face of the cover.

2. The hollow vane according to claim 1 , wherein the cover is mounted without clearance in the opening of the main portion between the protrusion and the external face, and the protrusion is housed in the widening with clearance.

3. The hollow vane according to claim 1 , wherein the cover is attached to the main portion without any intermediate material.

4. The hollow vane according to claim 1 , wherein the protrusion and the widening extend either over complete edges of the opening and of the cover, or over portions that can be superimposed of said edges.

5. The hollow vane according to claim 1 , wherein the protrusion and the widening extend in front of leading and trailing edges of the vane, the cover protruding outside of the main portion in front of the leading edge and retracting in the main portion in front of the leading edge, by a decreasing thickness from the cover from the leading edge to the trailing edge, or by a decreasing depth of the widening from the leading edge to the trailing edge.

6. The hollow vane according to claim 1 , wherein the opening and the cover are limited, at the protrusion and at the widening, by oblique edges which have sections that continuously widen from the external face of the vane.

7. The hollow vane according to claim 6 , wherein said oblique edges form lower angles with directions perpendicular to the external face of the vane.

8. The hollow vane according to claim 7 , wherein said oblique edges form lower angles 5° with the directions perpendicular to the external face of the vane.

9. The hollow vane according to claim 6 , wherein said oblique edges of the opening and of the cover form different angles with directions perpendicular to the external face of the vane, at least to one of the sides of the opening.

10. The hollow vane according to claim 1 , wherein the cover fully occupies the opening of the main portion, is connected to the main portion by nested anchoring, and is produced by molding in the opening.

11. A method of producing a hollow vane, the vane comprising a main portion and a cover, the cover being mounted in an opening of the main portion in such a way as to close the opening and to form with the main portion an external, substantially continuous face of the vane, the main portion further comprising a cavity that communicates with the external face via the opening, and the cover comprises a protrusion, extending over a portion of a thickness of the cover at a distance from the external face, and over an edge of the cover, and the main portion comprises a widening of the opening, located at a distance from the external face and in which the protrusion of the cover penetrates,

the method comprising:

dilating the main portion of the vane relative to the cover due to a difference in temperature between the main portion and the cover, the difference in temperature being created by at least one of a heating of the main portion and a cooling of the cover;

introducing the cover into the opening without the protrusion penetrating into the widening; and

stopping the dilating of the main portion of the vane in order to allow the main portion of the vane to retract on the cover and to allow the widening to adjust around the protrusion.

Assignments (3)
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 23, 2015
From: FRIBOURG, GUILLAUME; DELALEAU, PIERRE; TELLIER, FLORIAN
To: SNECMA
Reel/Frame 037120/0212 →
Priority Claims (1)
FR 13 54805 · May 28, 2013 · national
Continuity (1)
Related Publication 20160123167A1 · May 5, 2016