IP Library Granted Patent US 7,370,688
Granted Patent B2
US 7,370,688 · App. 11/125,084 · Granted May 13, 2008

Lost wax moulding method with contact layer

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Quick Facts
Patent No.
US 7,370,688
App. No.
11/125,084
Granted
May 13, 2008
Kind
B2
Abstract

A method of manufacture of a multilayer ceramic shell mould whereof at least one contact layer out of a wax master pattern or a part to be manufactured, or other similar material, includes a step of preparing a first slip containing ceramic particles and a binder; a step of dipping the master pattern in a first slip; a step of forming the contact layer, and a step of depositing sand particles particles onto the layer and drying the contact layer. The ceramic particles of the slip are mullite particles and the slip includes a texturing agent.

Claims (28)

1. A method of manufacture of a multilayer ceramic shell out of a master pattern of a part to be manufactured, said method comprising the steps of:

preparing a first slip containing ceramic particles and a binder, wherein the first slip comprises mullite flour in an amount ranging between 65 and 80 in weight %,

dipping the master pattern in said slip and forming a contact layer, and

depositing sand particles on said contact layer and drying said contact layer,

wherein said sand particles are mullite grains having a grain size distribution range between 80-250 micron, wherein the first slip does not contain any zircon and the first slip comprises a wetting agent, a liquefier and a texturing agent,

forming additional layers on said contact layer thereby forming a ceramic shell;

disposing of said master pattern thereby forming a ceramic mould;

baking said ceramic mould;

casting a metal part in said ceramic mould;

wherein said contact layer forms an interface between said ceramic mould and said metal part, and

wherein said additional layers comprise a mixture of alumina and mullite flours in amounts ranging between 45 and 95% in weight, and mullite grains in amounts ranging between 0 and 25% in weight.

2. A method according to claim 1 , further comprising selecting the wetting agent among polyalkylene fat alcohols or alkoxylate alcohols.

3. A method according to claim 1 , further comprising selecting the liquefier among the amino acids, ammonium polyacrylates or carboxylic tri-acids with alcohol groups.

4. A method according to claim 1 , further comprising selecting the texturing agent among ethylene oxide polymers, xanthan gums or guar gums.

5. A method according to claim 1 , wherein the binder is based on water-based mineral colloïdal solutions.

6. A method according to claim 1 , wherein said depositing comprises sprinkling the sand particles.

7. A method of manufacturing said part, said method comprising the method of claim 1 , and further comprising a step of solidifying metal with columnar structure oriented solidification.

8. A method of manufacturing said part, said method comprising the method of claim 1 , and further comprising a step of solidifying metal with mono-crystalline structure oriented solidification.

9. A method according to claim 5 , wherein the binder is based on water-based colloïdal silica.

10. A method according to claim 1 , wherein said additional layers include zircon particles.

11. A method according to claim 1 , wherein said metal part is a part for a turbojet engine.

12. A method according to claim 2 , further comprising selecting the liquefier among the amino acids, ammonium polyacrylates or carboxylic tri-acids with alcohol groups.

13. A method according to claim 12 , further comprising selecting the texturing agent among ethylene oxide polymers, xanthan gums or guar gums.

14. A method according to claim 13 , wherein the binder is based on water-based mineral colloïdal solutions.

15. A method according to claim 1 , wherein said master pattern is made of wax.

16. The method according to claim 1 , wherein said depositing of said sand particles is performed so as to control said after-baking porosity thereby controlling the shell mould's sensitivity to thermal shock to comply with casting conditions meeting stresses of a solidification method selected from the group consisting of an equiaxed solidification (EX), a columnar structure oriented solidification (DS) and a mono-crystalline structure oriented solidification (SX).

17. The method according to claim 16 , wherein the binder is a water-based colloidal solution and not an alcohol-based binder.

18. The method according to claim 1 , wherein said method is free of a step of including a ceramic based mat of reinforcing material in said shell mould.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 10, 2005
From: BIRAMBEN, ARNAUD; MARTY, CHRISTIAN; RAGOT, PATRICE; HUSSON, JEAN-CHRISTOPHE; TRUELLE, FRANCK; CHEVALIER, PATRICK; FARGEAS, SERGE
To: SNECMA MOTEURS
Reel/Frame 016545/0478 →