Cluster model and shell for obtaining an accessory for the independent handling of formed parts and associated method

Patent metadata

Field	Value
Publication number	US-10875084-B2
Application number	US-201716473150-A
Country	US
Kind code	B2
Filing date	Dec 22, 2017
Priority date	Dec 26, 2016
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

A cluster model and a shell for the production, by lost wax casting, of a plurality of turbomachine elements, are provided. The shell includes a central sprue that is fluidly connected to a casting cup for receiving molten metal; a plurality of shell elements; a plurality of bottom feed conduits for the shell elements; and a handling accessory shell that is independent of the plurality of shell elements and of their metal supply circuit, such that there is no fluid connection to the shell elements. The handling accessory shell is fluidly connected to the central sprue so as to allow top-pour casting of the handling accessory shell.

First claim

The invention claimed is:

1. A cluster model, about which is intended to be formed a shell for production, by lost wax casting, of a plurality of turbomachine elements, said model having a longitudinal axis and comprising:
a replica of a casting cup suitable for the injection of molten metal into the shell;
a replica of a central sprue extending along the longitudinal axis, suitable for being fluidically connected to the casting cup for receiving the molten metal;
a plurality of replicas of shell elements each intended for obtaining one of the turbomachine elements, each shell element including a first bottom end portion and a second top end portion;
a plurality of replicas of bottom feed conduits for the shell elements, suitable for being fluidically connected to the central sprue and the second bottom end portions of the shell elements so as to allow bottom-pour casting of the shell elements; and
a replica of a handling accessory shell that is independent of the plurality of shell elements and of a metal supply circuit thereof, such that there is no fluidic connection to the shell elements, the handling accessory shell being suitable for being fluidically connected to the central sprue so as to allow top-pour casting of the handling accessory shell.

2. A shell for production, by lost wax casting, of a plurality of turbomachine elements, said shell having a longitudinal axis and comprising:
a casting cup suitable for the injection of molten metal into the shell;
a central sprue extending along the longitudinal axis, of the shell that is fluidically connected to the casting cup for receiving the molten metal;
a plurality of shell elements each intended for obtaining one of the turbomachine elements, each shell element including a first bottom end portion and a second top end portion;
a plurality of bottom feed conduits for the shell elements that are fluidically connected to the central sprue and the second bottom end portions of the shell elements so as to allow bottom-pour casting of the shell elements; and
a handling accessory shell that is independent of the plurality of shell elements and of a metal supply circuit thereof, such that there is no fluidic connection to the shell elements, the handling accessory shell being fluidically connected to the central sprue so as to allow top-pour casting of the handling accessory shell.

3. The shell according to claim 2 , wherein the handling accessory shell comprises radial arms fluidically connecting a handling ring shell, centered about the longitudinal axis, to the central sprue.

4. The shell according to claim 3 , wherein the handling accessory shell comprises a central element of central axis coinciding with the longitudinal axis of the shell, attached to the central sprue or to the casting cup, the radial arms fluidically connecting the handling ring shell to the central element.

5. The shell according to claim 2 , wherein the shell elements arranged about the longitudinal axis, being spaced circumferentially apart from one another, and defining an inner space centered about the longitudinal axis wherein the central sprue is located.

6. The shell according to claim 2 , wherein each shell element is fluidically connected, at the level of the second top end portion thereof, to a single wax discharge conduit connected to the casting cup.

7. The shell according to claim 2 , wherein each shell element is fluidically connected, at a level of the second top end portion thereof, to a single wax discharge conduit, and wherein the shell comprises at least one first assembly and one second assembly of a plurality of wax discharge conduits respectively connected to one another by at least one first lateral conduit and one second lateral conduit, said at least one first lateral conduit and one second lateral conduit being respectively fluidically connected to the casting cup via at least one first and one second main wax discharge conduits extending respectively between the casting cup and said at least one first and one second lateral conduits.

8. The shell according to claim 2 , wherein the shell turbomachine elements are shell bladed elements, each designed for obtaining a single movable blade.

9. A method for producing, by lost wax casting, a plurality of turbomachine elements, using the shell according to claim 2 , the method comprising:
casting the metal in the shell for forming at least the turbomachine elements.

10. The method according to claim 9 , further comprising producing a material other than metal for forming the handling accessory.

Assignees

• Safran
• Safran Aircraft Engines

Inventors

• Niane Ngadia Taha
• Bohli Ramzi
• Galvin Loic
• Boukerma Said

Classifications

• B22C9/04 Primary

  Use of lost patterns · CPC title

• B22C7/02

  Lost patterns · CPC title

• B22D27/045

  Directionally solidified castings · CPC title

• B22C9/082

  Sprues, pouring cups · CPC title

• B22C9/043 Primary

  Removing the consumable pattern · CPC title