IP Library Granted Patent US 7,565,851
Granted Patent B2
US 7,565,851 · App. 11/176,318 · Granted Jul 28, 2009

Geometrical construction process for a flash land for the forging of a complex part

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Quick Facts
Patent No.
US 7,565,851
App. No.
11/176,318
Granted
Jul 28, 2009
Kind
B2
Abstract

A process for geometrical construction of a flash land is provided for a flash land that is to be provided in a die for forging of a turbomachine vane, in accordance with determined parameters, where the vane includes a blade. The process includes choosing at least three reference planes corresponding to a root, middle and tip of the blade. At least three reference sections of the blade in reference planes corresponding to the root, middle and tip of the blade are chosen in the reference planes. A length of the flash land and a shrinkage distance for the three reference sections are determined in the reference planes. Intermediate sections of the flash land and the corresponding flash gutter of the flash land from the reference sections are constructed by interpolation in the predetermined planes.

Claims (9)

1. A process for geometrical construction of a flash land, to be provided in a die for forging of a turbomachine vane, in accordance with determined parameters, where the vane includes a blade, the blade is defined by plane sections according to predetermined planes, and the flash land and a corresponding flash gutter of the flash land must be defined in accordance with said predetermined planes to obtain plane sections of the blade and of the flash land, said process comprising:

choosing at least three reference planes corresponding to a root, middle and tip of the blade,

choosing, in said reference planes, at least three reference sections of the blade in reference planes corresponding to the root, middle and tip of the blade,

determining, in said reference planes, a length of the flash land and a shrinkage distance for the three reference sections, and

constructing by interpolation, in said predetermined planes, intermediate sections of the flash land and the corresponding flash gutter of the flash land from said reference sections.

2. The process according to claim 1 , further comprising effecting different determinations of flash land parameters by varying said parameters in the reference sections before constructing the intermediate sections of the flash land and the corresponding gutter of the flash land.

3. The process according to claim 1 , wherein the sections of the flash land and the corresponding flash gutter at leading and trailing edges are calculated simultaneously.

4. The process according to claim 1 , wherein said constructing by interpolation the intermediate sections of the flash land and of the corresponding flash gutter of the flash land includes employing a polynomial interpolation technique.

5. The process according to claim 1 , further comprising rectifying, after said constructing by interpolation, an orientation of the sections of the flash gutter in order to remove any substantially vertical undercuts or walls.

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 Jun 22, 2009
From: LOUESDON, YVON; PLAZANET, JEAN-CLAUDE
To: SNECMA
Reel/Frame 022853/0087 →