Method of casting monocrystalline metal parts

Patent metadata

Field	Value
Publication number	US-9731350-B2
Application number	US-201214237982-A
Country	US
Kind code	B2
Filing date	Aug 6, 2012
Priority date	Aug 9, 2011
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

A foundry method of casting monocrystalline metal parts, the method including at least casting a molten alloy into a cavity of a mold through at least one casting channel in the mold, subjecting the alloy to heat treatment, and removing the mold, and wherein the heat treatment is performed before an end of mold removal.

First claim

The invention claimed is:

1. A foundry method of casting monocrystalline metal parts, the method comprising:
casting a molten alloy into a cavity of a mold through at least one casting channel in the mold, wherein the cavity is shaped for molding a final metal part;
subjecting the alloy to heat treatment; and
removing the mold;
wherein the heat treatment is performed after the alloy has solidified in the mold and before an end of mold removal,
wherein the casting channel includes at least one transition zone adjacent to the cavity, and presents, in the transition zone, relative to an upstream section of the casting channel in a flow direction of the molten alloy, a cross-section that is enlarged in a direction of a main axis of a section of the cavity in a plane that is perpendicular to the casting channel,
wherein, after the casting, the transition zone forms, adjacent to the final metal part formed by the cavity, an enlarged section, a central rod formed by the casting channel upstream from the enlarged section, and at least one metal web connected to the central rod and the enlarged section, the at least one metal web being thinner than the central rod,
wherein the metal part is a turbine engine blade, and
wherein the enlarged section is adjacent to a blade tip of the turbine blade.

2. A foundry method according to claim 1 , wherein the removal of the mold comprises a first removal by hammering and a subsequent removal by water jet, the heat treatment being performed at least before the removal by water jet.

3. A foundry method according to claim 1 , wherein the transition zone has a rounded portion of radius not less than 0.3 mm between the casting channel and the cavity.

4. A foundry method according to claim 1 , wherein, after the casting, the transition zone forms at least one metal web on each of two opposite sides of the central rod, which at least one metal web is thinner than the central rod.

5. A foundry method according to claim 1 , wherein the mold includes at least one core penetrating into and protruding from the cavity and occupying a space adjacent to the casting channel to form a cavity in the final metal part.

6. A foundry method according to claim 5 , wherein, after casting, the transition zone forms at least one metal web adjacent to the core on each of two opposite sides of the core.

7. A foundry method according to claim 1 , wherein the mold includes a plurality of cavities arranged as a bunch to mold a plurality of metal parts simultaneously.

8. A monocrystalline metal part produced by a foundry method according to claim 1 .

9. A foundry method of casting monocrystalline metal parts, the method comprising:
casting a molten alloy into a cavity of a mold through at least one casting channel in the mold, wherein the cavity is shaped for molding a final metal part;
subjecting the alloy to heat treatment; and
removing the mold;
wherein the casting channel includes at least one transition zone adjacent to the cavity, and presents, in the transition zone, relative to an upstream section of the casting channel in a flow direction of the molten alloy, a cross-section that is enlarged in a direction of a main axis of a section of the cavity in a plane that is perpendicular to the casting channel,
wherein, after the casting, the transition zone forms, adjacent to the final metal part formed by the cavity, an enlarged section, a central rod formed by the casting channel upstream from the enlarged section, and at least one metal web connected to the central rod and the enlarged section, the at least one metal web being thinner than the central rod,
wherein the metal part is a turbine engine blade, and
wherein the enlarged section is adjacent to a blade tip of the turbine blade.

10. A foundry method of casting monocrystalline parts according to claim 9 , wherein, after the casting, the transition zone forms at least one metal web on each of two opposite sides of the central rod, which at least one metal web is thinner than the central rod.

11. A foundry method of casting monocrystalline metal parts according to claim 9 , wherein the mold includes at least one core penetrating into and protruding from the cavity and occupying a space adjacent to the casting channel to form a cavity in the final metal part.

12. A foundry method of casting monocrystalline metal parts according to claim 11 , wherein the metal web adjacent to the core presents an outer edge following a substantially concave line adjacent on a surface of the core.

13. A foundry method of casting monocrystalline metal parts according to claim 11 , wherein, alter casting, the transition zone forms at least one metal web adjacent to the core on each of two opposite sides of the core.

14. A foundry method of casting monocrystalline metal parts according to claim 13 , wherein the metal webs adjacent to the core present outer edges that join together at ends to surround the core.

15. A foundry method of casting monocrystalline metal parts according to claim 9 , wherein the transition zone has a rounded portion of radius not less than 0.3 mm between the casting channel and the cavity.

Assignees

• Chan Celine Yanxi
• Marie Benoit Georges Jocelyn
• Locatelli David
• Snecma

Inventors

• Chan Celine Yanxi
• Marie Benoit Georges Jocelyn
• Locatelli David

Classifications

• B22D29/00

  Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots {(B22D13/10, B22D11/124, B22D17/00 take precedence)} · CPC title

• B22D27/04 Primary

  Influencing the temperature of the metal, e.g. by heating or cooling the mould · CPC title

• B22C9/04

  Use of lost patterns · CPC title

• B22D27/00

  Treating the metal in the mould while it is molten or ductile (B22D7/12, B22D11/10, B22D43/00 take precedence); {Pressure or vacuum casting (B22D17/00 takes precedence)} · CPC title