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

US11534825B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11534825-B2
Application numberUS-201916714391-A
CountryUS
Kind codeB2
Filing dateDec 13, 2019
Priority dateJun 13, 2017
Publication dateDec 27, 2022
Grant dateDec 27, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A method for producing a thin-walled metal part with complex geometry includes mixing a metal powder with a polymer binder in order to obtain a composite mixture, producing a flexible composite sheet from the composite mixture, cutting, in the flexible composite sheet, a preform based on a contour of the metal part, applying the preform in a mold having a surface configured with a relief of the metal part, and debinding and sintering the preform in order to obtain the metal part.

First claim

Opening claim text (preview).

What is claimed is: 1. A method for making a metal part with a wall thickness less than 5 mm, the method 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 the sintering steps, 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. 2. The method according to claim 1 further comprising a hot isostatic compaction after the debinding and sintering step. 3. The method according to claim 1 , 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. 4. The method according to claim 1 , wherein the mold includes: a male mold portion and a female mold portion, the female mold portion including the face configured according to a relief of the metal part, and the male mold portion extending opposite the female mold portion at a distance larger than a thickness of the flexible composite sheet, and a stop surface extending transversely to the male mold portion and the female mold portion and disposed relative thereto such that during the debinding and sintering, the preform comes into contact with the stop surface by gravity. 5. The method according to claim 1 , wherein the preform is oversized to compensate for a shrinkage of the preform during the debinding and sintering. 6. The method according to claim 1 further comprising 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. 7. The method according to claim 1 , wherein the preform is glued prior to application in the mold. 8. The method according to claim 1 , wherein the metal powder has a particle size between 10 μm and 120 μm. 9. The method according to claim 1 , wherein the metal powder has a particle size between 10 μm and 45 μm, with a median particle size of 30 μm. 10. A method according to claim 1 , wherein at least one mold face opposite the preform includes contact pads separated by grooves. 11. The method according to claim 10 , wherein the contact pads and the grooves have dimensions which are related by a relationship: e/h<5, where e defines a dimension of the contact pads according to a direction perpendicular to the grooves, and h defines a width of the grooves. 12. The method according to claim 1 , wherein the debinding and sintering steps are carried out in the mold.

Assignees

Inventors

Classifications

  • Processes characterised by the sequence of their steps · CPC title

  • Removal of binder or filler (removal of binder from ceramics C04B35/638) · CPC title

  • Metallic powder coated with organic material · CPC title

  • Aspects linked to processes or compositions used in powder metallurgy · CPC title

  • by hot isostatic pressing · CPC title

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What does patent US11534825B2 cover?
A method for producing a thin-walled metal part with complex geometry includes mixing a metal powder with a polymer binder in order to obtain a composite mixture, producing a flexible composite sheet from the composite mixture, cutting, in the flexible composite sheet, a preform based on a contour of the metal part, applying the preform in a mold having a surface configured with a relief of the…
Who is the assignee on this patent?
Safran, Safran Nacelles
What technology area does this patent fall under?
Primary CPC classification B22F5/009. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 27 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).