IP Library Granted Patent US 8,357,423
Granted Patent B2
US 8,357,423 · App. 12/747,275 · Granted Jan 22, 2013

Method for making a refractory carbide layer on a part made of C/C composite material

Inventors: Jacques Thebault (Bordeaux, FR); Christian Robin-Brosse (Le Haillan, FR); Aurélie Quet (Saint Medard en Jalles, FR); René Pailler (Cestas, FR)
Assignees: Snecma Propulsion Solide; Centre National de la Recherche Scientifique
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Quick Facts
Patent No.
US 8,357,423
App. No.
12/747,275
Granted
Jan 22, 2013
Kind
B2
Abstract

The invention relates to a method of making a refractory carbide layer on the accessible surface of a C/C composite material, the method including a step consisting in placing the composite material in contact with a reactive composition in solid form that contains an atomic proportion greater than or equal to one-third and less than or equal to 95% of a metal that is a precursor of a determined carbide having a melting temperature greater than 2000° C., and an atomic proportion of silicon that is greater than or equal to 5% and less than or equal to two-thirds. The method further includes a step consisting in impregnating the accessible surface of the C/C composite material with the reactive composition melted at a temperature that is greater than or equal to the melting temperature of the metal that is a precursor of a determined carbide.

Claims (18)

1. A method of making at least one layer of refractory carbide on a accessible surface of a carbon/carbon composite material, the method being characterized in that it comprises:

a step of placing the composite material in contact with a reactive composition in solid form containing an atomic proportion greater than or equal to one-third and less than or equal to 95% of a refractory metal that is a precursor of a determined carbide that has a melting temperature higher than 2000° C., together with an atomic proportion of silicon that is greater than or equal to 5% and less than or equal to two-thirds; and

a step of impregnating the accessible surface of the carbon/carbon composite material with the reactive composition melted by applying heat treatment at a temperature higher than or equal to the melting temperature of said refractory metal that is a precursor of a determined carbide so as to form a first phase of silicon carbide in contact with the carbon/carbon composite material, and a second phase of the determined carbide;

and wherein said first and second phases are formed solely by reaction with the carbon of the carbon/carbon composite material.

2. A method according to claim 1 , characterized in that the reactive composition comprises a metal selected from the group consisting of titanium, zirconium, niobium, hafnium, tantalum, and tungsten.

3. A method according to claim 1 , characterized in that the reactive composition comprises a metal disilicide selected from the group consisting of TiSi 2 , ZrSi 2 , NbSi 2 , HfSi 2 , TaSi 2 , and WSi 2 .

4. A method according to claim 1 , characterized in that the reactive composition further includes a third element.

5. A method according to claim 4 , characterized in that the reactive composition contains zirconium, and in that the third element is selected from the group consisting of aluminum, calcium, and yttrium.

6. A method according to claim 1 , characterized in that, prior to placing the carbon/carbon composite material in contact with the reactive composition, one or more external portions of the carbon/carbon composite material are covered in an anti-wetting agent.

7. A method according to claim 1 , characterized in that the reactive composition further contains a melting additive that does not react with carbon and that has a melting temperature that is lower than that of said refractory metal.

8. A method according to claim 7 , characterized in that the melting additive is selected from the group consisting of tin and copper.

9. A method according to claim 2 , characterized in that:

the reactive composition comprises a metal disilicide selected from the group consisting of TiSi 2 , ZrSi 2 , NbSi 2 , HfSi 2 , TaSi 2 , and WSi 2 ;

the reactive composition further includes a third element;

the reactive composition contains zirconium, and in that the third element is selected from the group consisting of aluminum, calcium, and yttrium;

prior to placing the carbon/carbon composite material in contact with the reactive composition, one or more external portions of the carbon/carbon composite material are covered in an anti-wetting agent;

the reactive composition further contains a melting additive that does not react with carbon and that has a melting temperature that is lower than that of said refractory metal; and

the melting additive is selected from the group consisting of tin and copper.

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 25, 2018
From: HERAKLES
To: ARIANEGROUP SAS
Reel/Frame 045151/0385 →
MERGER Recorded Jan 29, 2014
From: SNECMA PROPULSION SOLIDE
To: HERAKLES
Reel/Frame 032135/0709 →
CORRECTIVE ASSIGNMENT TO CORRECT THE APPLICANT OMITTED THE SECOND NAMED RECEIVING PARTIES DATA FROM THE COVER SHEET PREVIOUSLY RECORDED ON REEL 025079 FRAME 0543. ASSIGNOR(S) HEREBY CONFIRMS THE SECOND NAMED RECEIVING PARTIES DATA IS CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE, 3 RUE MICHEL-ANGE, 75016 PARIS FRANCE. Recorded Oct 15, 2010
From: THEBAULT, JACQUES; ROBIN-BROSSE, CHRISTIAN; QUET, AURELIE; PAILLER, RENE
To: SNECMA PROPULSION SOLIDE; CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE
Reel/Frame 025148/0182 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 1, 2010
From: THEBAULT, JACQUES; ROBIN-BROSSE, CHRISTIAN; QUET, AURELIE; PAILLER, RENE
To: SNECMA PROPULSION SOLIDE
Reel/Frame 025079/0543 →
Priority Claims (1)
FR 07 59802 · Dec 13, 2007 · national
Continuity (1)
Related Publication 20110017353A1 · Jan 27, 2011