IP Library Granted Patent US 9,315,927
Granted Patent B2
US 9,315,927 · App. 13/809,706 · Granted Apr 19, 2016

Method for producing a solid part

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Quick Facts
Patent No.
US 9,315,927
App. No.
13/809,706
Granted
Apr 19, 2016
Kind
B2
Abstract

A method for producing a solid part, including weaving a three-dimensional fibrous structure, the weaving being carried out with metal braids consisting of a plurality of metal strands mutually twisted about the longitudinal axis of the braid; and performing hot isostatic pressing on the fibrous structure causing the agglomeration of the metal braids of the fibrous structure so as to produce a solid part.

Claims (15)

1. A method of production of a solid part, said method comprising:

weaving a three-dimensional fibrous structure, said weaving being carried out with metal strands formed by a plurality of metal ends mutually twisted about the longitudinal axis of the strand;

performing hot isostatic pressing on said fibrous structure causing the agglomeration of the metal strands of said fibrous structure so as to produce a solid part.

2. The method of production according to claim 1 , wherein said weaving is carried out with metal strands formed by a plurality of metal ends, wherein the diameter of each end is less than 0.1 mm.

3. The method of production according to claim 1 , wherein said weaving is carried out with metal strands having a diameter equal to or greater than 0.5 mm.

4. The method of production according to claim 1 , wherein said weaving is carried out with metal strands having a diameter equal to or greater than 1 mm.

5. The method of production according to claim 1 , wherein said weaving is carried out with metal strands formed by a plurality of metal ends of titanium or by a plurality of metal ends of different materials.

6. The method of production according to claim 1 wherein said weaving is carried out with metal strands formed by a plurality of metal ends of different diameters.

7. The method of production according to claim 1 , wherein, prior to said hot isostatic pressing, said method comprises shaping said fibrous structure, said shaping being carried out manually.

8. The method of production according to claim 7 , wherein said shaping of said fibrous structure is carried out when said fibrous structure is put into place in a tool.

9. The method of production according to claim 1 , wherein, prior to said hot isostatic pressing, said method comprises cleaning said fibrous structure.

10. The method of production according to claim 1 , wherein said solid part is a metal reinforcement of the leading edge or trailing edge of the fan blade of a turbine engine or propeller.

11. The method of production according to claim 1 , wherein said method comprises:

weaving at least two three-dimensional fibrous structures, said weaving being carried out with metal strands formed by a plurality of metal ends mutually twisted about the longitudinal axis of the strand;

performing hot isostatic pressing on said at least two three-dimensional fibrous structures causing the agglomeration of the metal strands of said fibrous structures so as to produce a solid part.

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 Jan 11, 2013
From: DAMBRINE, BRUNO JACQUES GERARD; GODON, THIERRY; PERROUX, ALAIN ROBERT YVES
To: SNECMA
Reel/Frame 029614/0281 →