IP Library Granted Patent US 10,155,260
Granted Patent B2
US 10,155,260 · App. 14/913,050 · Granted Dec 18, 2018

Method for the high-temperature shaping of a metal blade reinforcement

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Quick Facts
Patent No.
US 10,155,260
App. No.
14/913,050
Granted
Dec 18, 2018
Kind
B2
Abstract

A shaping method making use of shaper tooling suitable for high-temperature shaping of a preformed metal part having two side fins extending from a nose, the method including putting the preformed metal part into place in a first bottom die of the tooling, holding the preformed metal part in a first determined position with a first movable central insert, forming one of the side fins of the preformed metal part into its final shape in alignment with the nose by moving with a first movable top die, turning over the preformed metal part, putting the preformed metal part into place in a second bottom die of the tooling, holding the preformed metal part in a second determined position with a second movable central insert, and shaping the other side fin into its final shape in alignment with the nose by moving with a second movable top die.

Claims (27)

1. A shaping method making use of shaper tooling suitable for high-temperature shaping of a preformed metal part having first and second side fins extending from a nose, the method comprising:

putting said preformed metal part into place in a first bottom die of said tooling;

holding said preformed metal part in a first determined position with a first movable central insert;

forming the first side fin of said preformed metal part into a final shape of the first side fin in alignment with said nose, said forming being preformed with a first movable top die;

turning over said preformed metal part having the first side fin that is shaped in the final shape of the first side fin;

putting said preformed metal part into place in a second bottom die of said tooling;

holding said preformed metal part in a second determined position with a second movable central insert; and

shaping the second side fin of said preformed metal part into a final shape of the second side fin in alignment with said nose, said shaping being performed with a second movable top die.

2. The shaping method according to claim 1 , wherein said holding in the first determined position is performed by moving said first movable central insert along a first axis.

3. The shaping method according to claim 1 , wherein said shaping the first side fin of said preformed metal part is performed by moving said performed metal part along a second axis.

4. The shaping method according to claim 3 , wherein said holding in the second determined position is performed by moving said second movable central insert along a third axis.

5. The shaping method according to claim 4 , wherein said axis in which said second movable central insert is moved corresponds substantially to a midplane between said first and second side fins.

6. The shaping method according to claim 4 , wherein said step of shaping the side fin of said preformed metal part is performed by moving said performed metal part along a fourth axis.

7. The shaping method according to claim 6 , wherein said second and fourth axes along which said first and second movable top dies are moved respectively are identical.

8. The shaping method according to claim 1 , wherein said second movable central insert is covered in a protective layer of boron nitride in order to facilitate withdrawal when extracting said preformed metal part from said shaper tooling.

9. A shaper tooling suitable for high-temperature shaping of a preformed metal part having first and second side fins extending from a nose, the tooling comprising:

a first bottom die in which said preformed metal part is put into place;

a first movable central insert for holding said preformed metal part in a first determined position;

a first movable top die for shaping the first side fin of said preformed metal part into a final shape of the first side fin in alignment with said nose;

a second bottom die in which said preformed metal part is put into place after being turned over;

a second movable central insert for holding said preformed metal part in a second determined position; and

a second movable top die for shaping the second side fin of said preformed metal part into a final shape of the second side fin in alignment with said nose.

10. The shaper tooling according to claim 9 , wherein said second movable central insert is covered in a protective layer of boron nitride.

11. The shaping method according to claim 1 , wherein the first movable central insert includes a first surface corresponding to the final shape of the first side fin, and a second surface corresponding to a non-final shape of the second side fin.

12. The shaping method according to claim 11 , wherein the second movable central insert includes a first surface corresponding to the final shape of the first side fin, and a second surface corresponding to the final shape of the second side fin.

13. The shaper tooling according to claim 9 , wherein the first movable central insert includes a first surface corresponding to the final shape of the first side fin, and a second surface corresponding to a non-final shape of the second side fin.

14. The shaper tooling according to claim 13 , wherein the second movable central insert includes a first surface corresponding to the final shape of the first side fin, and a second surface corresponding to the final shape of the second side fin.

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 Feb 19, 2016
From: ABOUSEFIAN, JACQUES; BOSSELUT, ANTOINE; KLEIN, GILLES CHARLES, CASIMIR
To: SNECMA
Reel/Frame 037776/0024 →