IP Library Granted Patent US 7,318,466
Granted Patent B2
US 7,318,466 · App. 11/127,092 · Granted Jan 15, 2008

Lost wax casting method

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Quick Facts
Patent No.
US 7,318,466
App. No.
11/127,092
Granted
Jan 15, 2008
Kind
B2
Abstract

A method of manufacture of a multilayer ceramic shell mould out of a master pattern includes the steps of dipping the master pattern in a first slip containing ceramic particles and a binder, depositing sand particles to form a contact layer, dipping the master pattern in a second slip containing ceramic particles and a binder, depositing sand particles to form an intermediate layer, dipping the master pattern in at least a third slip containing ceramic particles to form a reinforcing layer. The ceramic particles of the slips includes mullite, alumina, or a mixture of the two, whereas no layer contains any zircon.

Claims (47)

1. A method of manufacturing a multilayer ceramic shell mould with at least one contact layer, one intermediate layer and several reinforcing layers, out of a master pattern, said method comprising the following steps:

dipping said master pattern in a first slip containing ceramic particles and a binder to form a first layer, depositing sand particles onto the first layer and drying said first layer, in order to form said contact layer,

dipping said master pattern in a second slip containing ceramic particles and a binder to form a second layer, depositing sand particles onto said second layer and drying said second layer, in order to form said intermediate layer,

dipping said master pattern in at least a third slip containing ceramic particles and a binder to form a third layer, depositing sand particles onto said third layer, drying said third layer, in order to form a reinforcing layer, forming reinforcing layers being repeated until obtaining a shell mould of a set thickness, and

baking the shell mould by heating up the shell mould to a temperature ranging between 1000 and 1150° C.,

wherein the ceramic particles of the slips comprise mullite or alumina, or a mixture of mullite and alumina, whereas no layer contains any zircon, and

wherein said second slip comprises in weight percentage:

a 50-75% mixture of alumina flour,

a 5-20% mullite flour,

a 20-30% colloïdal silica binder,

0-5% water, and

a wetting agent, a liquefier and a texturing agent,

wherein said sand particles are composed of mullite grains,

wherein the sand particles are applied so that the shell mould exhibits an after-baking porosity ranging between 20 and 35%, and

wherein the second and third slips comprise a mixture of alumina and mullite flours and mullite grains.

2. The method according to claim 1 , wherein the particles of the slips comprise one of mullite or alumina.

3. The method according to claim 1 , wherein the binders for the different slips are based on mineral colloïdal solutions.

4. The method according to claim 1 , wherein the grains have a size distribution ranging between 80 and 1000 microns.

5. The method according to claim 1 , wherein for the first three layers, the sand particles are applied by sprinkling.

6. The method according to claim 1 , wherein the sand particles are applied by fluidised bed.

7. The method according to claim 1 , wherein the first slip for oriented solidification contains mullite flour, in an amount ranging from 40 and 80% in weight, alumina flour, a colloïdal silica-based binder, and organic admixtures.

8. The method according to claim 1 , wherein the first slip for equiaxed solidification, comprises a mixture of alumina and mullite flours in amounts ranging respectively between 40 and 80% in weight of alumina and between 2 and 30% in weight of mullite flow, a colloïdal silica-based binder, a germinative and organic admixtures.

9. The method according to claim 1 , wherein the second and third slips 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.

10. The method according to claim 1 , further comprising a baking cycle of the finished shell mould, wherein the baking cycle comprises heating up to a temperature ranging between 1030 and 1170° C.

11. The method according to claim 1 , wherein said third slip comprises in weight percentage:

a 30-45% mixture of alumina flour,

a 15-30% mullite flour,

14-24% mullite grains,

a 10-20% colloidal silica binder,

5-15% water, and

a wetting agent, a liquefier, a texturing agent and a sintering agent.

12. The method according to claim 11 , wherein said first slip comprises in weight percentage:

a 40-80% mixture of alumina flour,

a 2-30% mullite flour,

a 0-10% germinative, cobalt aluminate,

a 18-30% colloidal silica binder,

0-5% water, and

a wetting agent, a liquefier and a texturing agent.

13. The method according to claim 11 , wherein said first slip comprises in weight percentage:

a 2-30% mixture of alumina flour,

a 40-80% mullite flour,

a 18-30% colloïdal silica binder,

0-5% water, and

a wetting agent, a liquefier and a texturing agent.

14. 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).

15. The method according to claim 1 , wherein the step of baking the shell mould consists of heating up the shell mould to a temperature ranging between 1000 and 1150° C. such that said method is free of any heating of said shell mould to a temperature greater than 1150° C.

16. 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 12, 2005
From: BIRAMBEN, ARNAUD; CALERO, PATRICK; CHEVALIER, PATRICK; HUSSON, JEAN-CHRISTOPHE; MARTHY, CHRISTIAN; RAGOT, PATRICE; RICHARD, JEAN-PIERRE; TRUELLE, FRANCK; VALENTE, ISABELLE
To: SNECMA MOTEURS
Reel/Frame 016564/0241 →