IP Library Granted Patent US 7,370,506
Granted Patent B2
US 7,370,506 · App. 11/091,764 · Granted May 13, 2008

Forging die with marking means

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Quick Facts
Patent No.
US 7,370,506
App. No.
11/091,764
Granted
May 13, 2008
Kind
B2
Abstract

A forging die includes on one face, a half-imprint of a part to be forged such as a turbine engine blade. The die also includes on the face, a device for forming a marking along two directions relatively to which the position of the imprint is defined, the device including two pads protruding relatively to the face and each including two notches defining the two directions. This device preferably includes two pads machined on the die at the same time as the imprint, and each including two notches in the form of a cross.

Claims (38)

1. A method of mounting dies in a forging press, said method comprising the steps of:

checking alignment of two pads of a forging die upon mounting said forging die in the forging press, wherein said forging die includes on a face, a half-imprint of a part to be forged and a marker on said face, said marker providing a marking along two directions relatively to which a position of said imprint is defined, said marker including said two pads protruding relatively to said face, each pad including two notches defining said two directions,

positioning a stud in malleable material on each of the pads,

crushing the studs between the pads of both dies and

checking the markings provided by the notches on the studs.

2. A die for forging a blade of a turbine engine, said die comprising:

a block with an imprint of a half-blade, said block having a top face, a bottom face, a first side face and a second side face opposite said first side face, said imprint extending between said first and second side faces along a main axis of said imprint;

wherein said block includes a first notch that is closer to said first side face than to said second side face and a second notch that is closer to said second side face than to said first side face;

wherein said first and second notches are parallel to each other and to said main axis of said imprint,

wherein said first and second notches are at a same distance from said main axis of said imprint and are on a same side of said main axis of said imprint so as to be aligned with each other.

3. The die according to claim 2 , wherein said half-imprint is of a blade of a turbine engine.

4. The die of claim 2 , wherein said first and second notches are perpendicular to said first and second side faces.

5. The die of claim 2 , wherein said first and second notches are not continuous with each other such that said block is free of any notch between said first and second notches.

6. The die of claim 2 , wherein said block includes a third notch and a fourth notch, said third and fourth notches being perpendicular to said first and second notches.

7. The die of claim 6 , wherein said third notch is at a predetermined distance from a reference point for said imprint and said fourth notch is at another predetermined distance from said reference point.

8. The die of claim 6 , further comprising another block with another imprint having a shape complementary to the half-blade, wherein said another block includes notches, each notch of said another block being positioned so as to be aligned with one of said first, second, third and fourth notches when said block and said another block are pressed against each other.

9. The die of claim 6 , wherein:

said first and second notches are perpendicular to said first and second side faces,

said block has a third side face extending from said first side face to said second side face and a fourth side face opposite said third side face and extending from said first side face to said second side face, and

said third and fourth notches are perpendicular to said third and fourth side faces.

10. The die of claim 9 , wherein said third and fourth notches are not continuous with each other such that said block is free of any notch between said third and fourth notches.

11. A for forging a blade of a turbine engine, said die comprising:

a block with an imprint of a half-blade, said block having a top face, a bottom face, a first side face and a second side face opposite said first side face, said imprint extending between said first and second side faces along a main axis of said imprint;

wherein said block includes a first notch that is closer to said first side face than to said second side face and a second notch that is closer to said second side face than to said first side face;

wherein said first and second notches are parallel to each other and to said main axis of said imprint,

wherein said first and second notches are at a same distance from said main axis of said imprint,

wherein said block includes a third notch and a fourth notch, said third and fourth notches being perpendicular to said first and second notches, and

wherein said third notch crosses said first notch and said fourth notch crosses said second notch.

12. The die of claim 11 , wherein said third notch crosses said first notch at midpoints of said first and third notches and said fourth notch crosses said second notch at midpoints of said second and fourth notches.

13. The die of claim 12 , wherein said block comprises a first and a second pad, said first pad protruding from a surface of said block and defining said first and third notches, and said second pad protruding from the surface of said block and defining said second and fourth notches.

14. The die of claim 13 , wherein said first and second pads are disc-shaped.

15. A die for forging a blade of a turbine engine, said die comprising:

a first block with an imprint of a half-blade, said block having a top face, a bottom face, a first side face and a second side face opposite said first side face, said imprint extending between said first and second side faces along a main axis of said imprint; and

another block with another imprint having a shape complementary to the half-blades,

wherein said first block includes a first notch that is closer to said first side face than to said second side face and a second notch that is closer to said second side face than to said first side face;

wherein said first and second notches are parallel to each other and to said main axis of said imprint,

wherein said first and second notches are at a same distance from said main axis of said imprint.

16. The die of claim 15 , wherein said another block includes notches, each notch of said another block being positioned so as to be aligned with one of said first and second notches when said block and said another block are pressed against each other.

Assignments (4)
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 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 21, 2005
From: LORIEUX, ALAIN; LEVY, JEAN-JACQUES; LHOMME, DANIEL; PLAZANET, CLAUDE; GEORGE, PIERRE; COUGNAUD, CAMILLE; BOURGEOIS, ALAIN
To: SNECMA MOTEURS
Reel/Frame 016794/0731 →