Method for making a metal part with a complex geometry with a thin wall

Patent metadata

Field	Value
Publication number	US-12330219-B2
Application number	US-202218082945-A
Country	US
Kind code	B2
Filing date	Dec 16, 2022
Priority date	Jun 13, 2017
Publication date	Jun 17, 2025
Grant date	Jun 17, 2025

Abstract

A metal part with a wall thickness less than 5 mm includes a preform made from a flexible composite sheet, a flexible composite sheet segment, and an appended insert including a fastening portion that is sandwiched between a rear end of the preform and the flexible composite sheet segment. The flexible composite sheet segment encloses the fastening portion of the appended insert.

First claim

What is claimed is:

1. A metal part with a wall thickness less than 5 mm, the metal part comprising:
a preform made from a flexible composite sheet;
a flexible composite sheet segment; and
an appended insert including a fastening portion that is sandwiched between a rear end of the preform and the flexible composite sheet segment,
wherein the flexible composite sheet segment encloses the fastening portion of the appended insert.

2. The metal part of claim 1 , wherein the composite sheet segment forms a bridge over the fastening portion, the bridge defining a gap between the composite sheet segment, the rear end of the preform, and the fastening portion prior to a debinding and sintering manufacturing step, and the composite sheet segment is configured to deform to fill the gap during the debinding and sintering manufacturing step.

3. The metal part of claim 1 , wherein the flexible composite sheet includes metal powder.

4. The metal part of claim 3 , wherein the metal powder has a particle size between 10 μm and 120 μm.

5. The metal part of claim 3 , wherein the metal powder has a particle size between 10 μm and 45 μm, with a median particle size of 30 μm.

6. The metal part of claim 1 , wherein the appended insert is a flange.

7. The metal part of claim 1 , wherein the preform is configured to be applied to a mold having a face defining a relief of the metal part.

8. The metal part of claim 1 , further comprising a plurality of stiffeners extending from an outer surface of the metal part.

9. The metal part of claim 1 , wherein the wall thickness is between 1 mm and 2 mm.

10. The metal part of claim 1 , wherein the preform is oversized prior to a debinding and sintering manufacturing step to compensate for a shrinkage of the preform.

11. The metal part of claim 1 , wherein the appended insert defines a hole.

12. The metal part of claim 11 , wherein a portion of the appended insert that defines the hole extends away from the rear end of the preform.

13. The metal part of claim 1 , wherein the flexible composite sheet segment is configured to shrink during one of a debinding and a sintering manufacturing step to enclose the fastening portion.

14. The metal part according to claim 1 , wherein the metal part is formed by a process comprising:
mixing a metal powder with a polymer binder to form a composite mixture, the metal powder being particles of an atomized metal alloy;
making a flexible composite sheet from the composite mixture;
cutting, in the flexible composite sheet, a preform of the metal part;
applying the preform in a mold having a face defining a relief of the metal part; and
debinding and sintering the preform to form the metal part;
wherein an appended insert has a fastening portion that is sandwiched between a rear end of the preform and a flexible composite sheet segment,
wherein, before the debinding and sintering step, the composite sheet segment forms a bridge over the fastening portion, the bridge defining a gap between the composite sheet segment, the rear end of the preform, and the fastening portion, and
wherein, during the debinding and sintering steps, the composite sheet segment deforms to fill the gap and to enclose the fastening portion of the appended insert.

15. The metal part of claim 14 , wherein the process further comprises a hot isostatic compaction after the debinding and sintering step.

16. The metal part of claim 14 , wherein the mold is a half-shell mold including a stop surface, and the mold is disposed during the debinding and sintering such that the preform is applied in the mold and against the stop surface by gravity.

17. The metal part of claim 14 , wherein the process further comprises fastening the appended insert by taking the fastening portion of the appended insert sandwiched between two segments of the flexible composite sheet prior to the debinding and sintering.

18. The metal part according to claim 1 ,
wherein the preform is cut from the flexible composite sheet,
the appended insert disposed on the preform and extending from the rear end of the preform.

19. The metal part of claim 18 , wherein the appended insert is sandwiched between the preform and the flexible composite sheet segment to form a continuous connection.

20. The metal part of claim 18 , wherein the flexible composite sheet is shrunk to the preform and the appended insert by a debinding and sintering process.

Assignees

• Safran
• Safran Nacelles

Inventors

• Soula Aurelie
• Sallot Pierre

Classifications

• B22F1/06

  Metallic powder characterised by the shape of the particles (nanosized particles B22F1/054) · CPC title

• B22F1/10

  Metallic powder containing lubricating or binding agents; Metallic powder containing organic material · CPC title

• B22F1/102

  Metallic powder coated with organic material · CPC title

• F05D2300/603

  Composites; e.g. fibre-reinforced · CPC title

• F05D2230/22

  by sintering · CPC title