Casting pattern

Patent metadata

Field	Value
Publication number	US-9616489-B2
Application number	US-201314427485-A
Country	US
Kind code	B2
Filing date	Sep 6, 2013
Priority date	Sep 11, 2012
Publication date	Apr 11, 2017
Grant date	Apr 11, 2017

Abstract

A casting pattern for a lost-pattern casting, the pattern being in a shape of a turbine engine blade with a root and a body on either side of a platform that is substantially perpendicular to a main axis of the blade, and a method of producing a shell mold from the pattern, and a casting method using the shell mold. The blade body presents a pressure side, a suction side, a leading edge, and a trailing edge. The pattern also includes an expansion strip adjacent to the trailing edge, and a refractory core embedded in the pattern but presenting, both on the pressure side and on the suction side, a respective flush varnished surface between the trailing edge and the expansion strip. A web extends between the platform and the expansion strip and presents a free edge between them.

First claim

The invention claimed is:

1. A pattern for lost-pattern casting, the pattern being in a shape of a turbine engine blade with a root and a body on either side of a platform that is substantially perpendicular to a main axis of the blade, the blade body presenting a pressure side, a suction side, a leading edge, and a trailing edge, the pattern comprising:
an expansion strip adjacent to the trailing edge, and a refractory core embedded in the pattern but presenting, both on the pressure side and on the suction side, a respective flush varnished surface between the trailing edge and the expansion strip; and
a web extending between the platform and the expansion strip and presenting a free edge between them.

2. The pattern according to claim 1 , wherein the free edge of the web extends from one edge of the platform to the expansion strip.

3. The pattern according to claim 1 , further presenting a progressive transition between a free edge of the expansion strip and the free edge of the web.

4. The pattern according to claim 1 , wherein the web has a thickness that is less than or equal to a thickness of the expansion strip.

5. The pattern according to claim 1 , wherein the free edge of the web is rounded in a transverse plane.

6. The pattern according to claim 1 , further comprising an out-of-part segment extending the body at an end opposite from the root of the blade, and wherein the web presents a height that is not greater than half the height of the body including the out-of-part segment.

7. The pattern according to claim 1 , wherein a junction between the web and the platform extends a junction between the suction side and the platform.

8. The pattern according to claim 1 , further comprising a selector channel pattern that is connected to an end of the blade body that is opposite from the blade root.

9. An assembly comprising:
a plurality of patterns that are connected together by a tree,
wherein each pattern of the plurality is in a shape of a turbine engine blade with a root and a body on either side of a platform that is substantially perpendicular to a main axis of the blade, the blade body presenting a pressure side, a suction side, a leading edge, and a trailing edge, and
the pattern comprising an expansion strip adjacent to the trailing edge, a refractory core embedded in the pattern but presenting, both on the pressure side and on the suction side, a respective flush varnished surface between the trailing edge and the expansion strip, and a web extending between the platform and the expansion strip and presenting a free edge between them.

10. A method of fabricating a shell mold, the method comprising:
dipping in a slip at least one casting pattern in a shape of a turbine engine blade with a root and a body on either side of a platform that is substantially perpendicular to a main axis of the blade, the blade body presenting a pressure side, a suction side, a leading edge, and a trailing edge, the pattern comprising an expansion strip adjacent to the trailing edge, a refractory core embedded in the pattern but presenting, both on the pressure side and on the suction side, a respective flush varnished surface between the trailing edge and the expansion strip, and a web extending between the platform and the expansion strip and presenting a free edge between them;
powdering the at least one slip-coated pattern with refractory sand to form a shell around the at least one pattern;
removing the at least one pattern; and
baking the shell.

11. A casting method comprising:
dipping in a slip at least one casting pattern in a shape of a turbine engine blade with a root and a body on either side of a platform that is substantially perpendicular to a main axis of the blade, the blade body presenting a pressure side, a suction side, a leading edge, and a trailing edge, the pattern comprising an expansion strip adjacent to the trailing edge, a refractory core embedded in the pattern but presenting, both on the pressure side and on the suction side, a respective flush varnished surface between the trailing edge and the expansion strip, and a web extending between the platform and the expansion strip and presenting a free edge between them;
powdering the at least one slip-coated pattern with refractory sand to form a shell around the at least one pattern;
removing the at least one pattern;
baking the shell to fabricate a shell mold;
casting molten metal into the shell mold;
cooling the metal with directional solidification thereof;
knocking out the shell mold to recover a raw metal casting; and
finishing the raw casting.

Assignees

• Snecma

Inventors

• Coyez Dominique
• Fargeas Serge

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

• C30B29/52

  Alloys · CPC title

• B22D27/045

  Directionally solidified castings · CPC title

• B22C7/02 Primary

  Lost patterns · CPC title

• B22C9/04

  Use of lost patterns · CPC title