IP Library › Granted Patent US 12,343,790
Granted Patent B2
US 12,343,790 · App. 18/728,789 · Granted Jul 1, 2025

Assembly for producing a molding made of removable material of a turbomachine

Inventors: Hervé Bruno Marc Osmont (Moissy-Cramayel, FR); Ramzi Bohli (Moissy-Cramayel, FR); Alexis Lourette (Moissy-Cramayel, FR); Joseph Toussaint Tami Lizuzu (Moissy-Cramayel, FR)
Assignees: SAFRAN; SAFRAN AIRCRAFT ENGINES
B22D17/24B22D25/02
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Quick Facts
Patent No.
US 12,343,790
App. No.
18/728,789
Granted
Jul 1, 2025
Kind
B2
Abstract

An assembly for producing a molding, made of removable material, of a turbomachine blade, includes an injection mold for the removable material in which a first core element and a second core element are mounted in a predetermined molding position, wherein the first and second core elements extend in a first direction. The mold includes a first face for molding a pressure-side face of the blade and a second face for molding a suction-side face of the blade and arranged facing the first face in a second direction perpendicular to the first direction. Retaining members hold the cores in position in the injection mold.

Claims (19)

1. An assembly for producing a molding, made of removable material, of a turbomachine blade, comprising an injection mold for said removable material in which a first core element and a second core element are configured to be mounted in a predetermined molding position, the first and second core elements extending in a first direction, the mold comprising:

a first molding face configured to mold a pressure-side face of the blade and a second molding face configured to mold a suction-side face of the blade and arranged facing the first face in a second direction perpendicular to the first direction, and

retaining members configured to hold the cores in position in the injection mold,

wherein at least a first retaining member extends from the first face of the mold in the second direction and extends at least partially through the first and second core elements, the first retaining member comprising a first support point at which the first retaining member bears against the first core element and a second support point at which the first retaining member bears against the second core element.

2. The assembly according to claim 1 , wherein the first core element and the second core element are shaped so that the first support point of the first retaining member blocks movement of the first core element in a first directional orientation along a third direction perpendicular to the first and second directions, and the second support point of the first retaining member blocks movement of the second core element in a second directional orientation that is opposite to the first directional orientation along the third direction.

3. The assembly according to claim 1 , wherein a second retaining member extends from the first molding face in the second direction, the second retaining member comprising a first support point at which the second retaining member bears against the first core element and a second support point at which the second retaining member bears against the second core element, said first support point and second point of support of the second retaining member being different from the first support point and the second support point of the first retaining member.

4. The assembly according to claim 3 , wherein the first core element and the second core element are shaped so that the first support point of the second retaining member blocks movement of the first core element in the first directional orientation along a third direction perpendicular to the first and second directions and the second support point of the second retaining member blocks movement of the second core element in a second directional orientation that is opposite to the first directional orientation along the third direction.

5. The assembly according to claim 4 , wherein the second retaining member comprises a spacing means between the first support point of the second retaining member and the second support point of the second retaining member, the spacing means ensuring, during production of the molding made of removable material, a spacing of a constant distance between said support points along the third direction.

6. The assembly according to claim 1 , wherein the first retaining member comprises a spacing means between the first support point of the first retaining member and the second support point of the first retaining member, the spacing means ensuring, during production of the molding made of removable material, a spacing of constant distance between said support points along at least one among the first direction, the second direction, or the third direction.

7. The assembly according to claim 1 , wherein the first retaining member and/or the second retaining member is movable between a retaining position, in which the second retaining member holds at least one core element, and a retracted position, the retaining member comprising a retraction mechanism configured to position the retaining member in the retaining position or in the retracted position.

8. The assembly according to claim 1 , wherein the first retaining member and/or the second retaining member comprises an axis of rotation and a head that is eccentric relative to the axis of rotation and that cooperates with the first core element and the second core element.

9. A method for producing a molding, made of removable material, of a turbomachine blade, the method comprising:

providing a first core element and a second core element, said core elements extending in a first direction; and

providing an injection mold for said removable material,

wherein the mold comprises:

a first molding face configured to mold a pressure-side face of the blade and a second molding face configured to mold a suction-side face of the blade and arranged facing the first face in a second direction perpendicular to the first direction; and

retaining members configured to hold the cores in position in the injection mold, among which at least a first retaining member extends from the first molding face in the second direction,

the method further comprising the step of positioning the first core element and the second core element on the first molding face such that the first retaining member extends at least partially through the first and second core elements and comprises a first support point at which the first retaining member bears against the first core element and a second support point at which the first retaining member bears against the second core element.

10. The method according to claim 9 , the mold further comprising a second retaining member extending from the first molding face in the second direction, the method further comprising the step of positioning the first core element and the second core element on the first molding face such that the second retaining member comprises a first support point at which the second retaining member bears against the first core element and a second support point at which the second retaining member bears against the second core element.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 12, 2024
From: OSMONT, HERVÉ BRUNO MARC; BOHLI, RAMZI; LOURETTE, ALEXIS; TAMI LIZUZU, JOSEPH TOUSSAINT
To: SAFRAN; SAFRAN AIRCRAFT ENGINES
Reel/Frame 067980/0324 →
Priority Claims (1)
FR 2200251 · Jan 13, 2022 · national
Continuity (1)
Related Publication 20250083221A1 · Mar 13, 2025
References Cited (7)
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