IP Library Granted Patent US 7,441,691
Granted Patent B2
US 7,441,691 · App. 10/504,638 · Granted Oct 28, 2008

Method for the production of parts by means of diffusion bonding and superplastic forming, and mold for carrying out said method

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Quick Facts
Patent No.
US 7,441,691
App. No.
10/504,638
Granted
Oct 28, 2008
Kind
B2
Abstract

A method for producing parts including at least one internal cavity. In the method at least two metal sheets are diffusion bonded; then the bonded metal sheets are bent; and then each of internal cavities is inflated by superplastic forming. The method is carried out by a mold allowing at least one first part to be diffusion bonded and then bent while inflating at least one second part by superplastic forming during a single operation, whereby the mold is heated. The method can be applied, e.g., to the field of aeronautics.

Claims (20)

1. A process for manufacturing parts that include at least one internal cavity, the process comprising:

providing, in a primary recessed portion of a mold, a first part comprising two metal sheets;

providing, in a secondary recessed portion of said mold, a second part comprising two metal sheets;

bonding said two metal sheets of said first part together by diffusion bonding thereby forming a first assembly of metal sheets;

deforming said first assembly of metal sheets; and

inflating a cavity between said two metal sheets of said second part by superplastic forming,

wherein said bonding, said deforming and said inflating are performed during a single heating operation performed on the mold.

2. The manufacturing process as claimed in claim 1 , wherein, for said first part, the diffusion bonding is carried out by providing, inside the primary recessed portion of the mold, a first injection of pressurized gas that presses the two metal sheets of said first part against a first plane surface of the primary recessed portion of the mold.

3. The manufacturing process as claimed in claim 2 , wherein, for said first part, the deforming of the first assembly formed by the two metal sheets of the first part bonded together is carried out while purging the pressurized gas introduced into the primary recessed portion during the first injection of gas, and then while providing a second injection of pressurized gas, which presses the two metal sheets of the first part bonded together against a second surface of the primary recessed portion of the mold.

4. The manufacturing process as claimed in claim 1 , wherein, for said second part, the inflating carried out on the internal cavity by superplastic forming is performed by providing an injection of pressurized gas into the internal cavity, the inflating being carried out such that a deformed second assembly of the metal sheets of the second part bonded together conforms to an internal wall of the secondary recessed portion of the mold.

5. The manufacturing process as claimed in claim 1 , wherein the single operation of heating the mold is carried out at a temperature of about 920° C.

6. The manufacturing process as claimed in claim 1 , wherein said inflating comprises inflating a plurality of cavities between said two metal sheets of said second part.

7. The manufacturing process as claimed in claim 1 , further comprising, during said single heating operation performed on the mold:

bonding said two metal sheets of said second part together by diffusion bonding thereby forming a second assembly of metal sheets;

deforming said second assembly of metal sheets.

8. The manufacturing process as claimed in claim 1 , wherein said providing of said first and second parts respectively in said primary and secondary recessed portions is performed such that said first and second parts are separated from each other by an intermediate block of said mold.

9. The manufacturing process as claimed in claim 8 , wherein said bonding of said two metal sheets of said first part is performed by pressing said first part against a planar surface of said intermediate block.

10. The manufacturing process as claimed in claim 9 , wherein said deforming of said first part is performed by pressing said first part against a surface of said primary recessed portion of said mold opposite to said planar surface of said intermediate block.

11. The manufacturing process as claimed in claim 1 , further comprising, after said step of providing said first and second parts respectively in said primary and secondary recessed portions of said mold, subjecting said mold to said single heating operation thereby heating said first and second parts above a predetermined temperature, and wherein said bonding, said deforming and said inflating are performed while said first and second parts are above said predetermined temperature.

12. The manufacturing process as claimed in claim 11 , wherein said bonding, said deforming and said inflating are performed while said first and second parts are maintained at a substantially constant temperature above said predetermined temperature.

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 Feb 8, 2005
From: FRANCHET, JEAN-MICHEL, PATRICK, MAURICE; KLEIN, GILLES, CHARLES, CASIMIR; LAMY, OLIVIER, DANIEL; SZKOLNIK, EDMOND, PAUL
To: SNECMA MOTEURS; HISPANO, HUREL
Reel/Frame 016247/0542 →