Materials and parts that can withstand high temperatures in an oxidizing medium, and method for manufacturing same

Patent metadata

Field	Value
Publication number	US-9382164-B2
Application number	US-201113992880-A
Country	US
Kind code	B2
Filing date	Dec 5, 2011
Priority date	Dec 10, 2010
Publication date	Jul 5, 2016
Grant date	Jul 5, 2016

Abstract

A refractory material that can withstand high temperatures in an oxidizing medium and containing at least:
a first constituent corresponding to hafnium, or to a non-oxide compound of hafnium, or circular in a or a non-oxide compound of zirconium, or corresponding to a mixture of at least two metals and/or compounds selected from hafnium a non-oxide compound of hafnium, zirconium, and a non-oxide compound of zirconium; a second constituent corresponding to the boron or to a non-oxide compound of boron, or corresponding to a mixture of boron and a non-oxide compound of boron; and a third constituent corresponding to a rare earth RE or to a non-oxide compound of the rare earth RE, or corresponding to a mixture of rare earth RE and a non-oxide compound of the rare earth RE, where RE is selected from scandium, yttrium, and the lanthanides.

The material contains neither silicon nor a compound of silicon.

First claim

The invention claimed is:

1. A composite material part constituted at least in part by carbon and having a protective coating providing protection at high temperatures in an oxidizing medium, wherein said protective coating is constituted by at least one refractory material that can withstand high temperatures in an oxidizing medium, the refractory material comprising:
hafnium, or a non-oxide compound of hafnium, or a mixture of hafnium and a non-oxide compound of hafnium;
boron or a non-oxide compound of boron, or a mixture of boron and a nonoxide compound of boron; and
a constituent corresponding to a rare earth element RE or a to non-oxide compound of the rare earth element RE, or corresponding to a mixture of rare earth element RE and a non-oxide compound of the rare earth element RE, where RE is selected from scandium, yttrium, and the lanthanides; and
said material containing neither silicon nor a compound of silicon.

2. A composite material part according claim 1 , wherein the refractory material contains a boride of said rare earth element RE and contains at least hafnium in metallic form, or hafnium in carbide or nitride or boride form.

3. A composite material part according to claim 1 , wherein the refractory material contains a nitride of said rare earth element RE, said material also containing at least one boride of hafnium and at least one non-oxide compound of hafnium.

4. A composite material part according to claim 1 , wherein the refractory material contains hafnium and a rare earth boride DyB4where Dy corresponds to dysprosium, which is a rare earth, or contains a carbide of hafnium and a rare earth boride DyB4 where Dy corresponds to dysprosium, which is a rare earth.

5. A composite material part according to claim 1 wherein the refractory material further comprises at least tantalum or a non-oxide compound of tantalum, or niobium or a non-oxide compound of niobium, or zirconium or a non-oxide compound of zirconium.

6. A composite material part according to claim 1 , constituting a rocket engine component made of thermostructural composite material and having at least its inside surface provided with said protective coating.

7. A method of making a part out of refractory material that can withstand high temperatures in an oxidizing medium, the method comprising the steps of:
making a composition comprising at least:
hafnium, or a non-oxide compound of hafnium, or a mixture of hafnium and a non-oxide compound of hafnium;
boron or a non-oxide compound of boron, or a mixture of boron and a nonoxide compound of boron; and
a constituent corresponding to a rare earth element RE or to a non-oxide compound of the rare earth element RE, or corresponding to a mixture of rare earth element RE and a non-oxide compound of rare earth element RE, where RE is selected from scandium, yttrium, and the lanthanides;
wherein the composition contains (i) a nitride of said rare earth element RE and at least one boride of hafnium and at least one non-oxide compound of hafnium, or (ii) hafnium and a boride of rare earth element RE, or (iii) a hafnium carbide and a boride of rare earth element RE;
said composition containing no silicon or compound silicon; and
shaping the composition and densifying said composition.

8. A method according to claim 7 , wherein the composition contains said nitride of said rare earth elemen RE, and said at least one boride of hafnium and said at least one non-oxide compound of hafnium.

9. A method according to claim 7 , wherein the composition contains hafnium and said boride of rare earth element RE or said hafnium carbide and said boride of rare earth element RE.

10. A method according to claim 7 , wherein the composition further comprises at least tantalum or a non-oxide compound of tantalum, or niobium or a non-oxide compound of niobium, or zirconium or a non-oxide compound of zirconium.

11. A method according to claim 7 , wherein said composition is densified by flash sintering.

12. A method of making a protective layer that can withstand high temperatures in an oxidizing medium, the layer being made on a composite material part constituted at least in part by carbon, said method comprising the steps of:
applying on the part a composition comprising at least:
hafnium, or a non-oxide compound of hafnium, or a mixture of hafnium and a non-oxide compound of hafnium;
boron or a non-oxide compound of boron, or a mixture of boron and a non-oxide compound of boron; and
a constituent corresponding to a rare earth element RE or to a non-oxide compound of a rare earth element RE, or corresponding to a mixture of rare earth element RE and a non-oxide compound of the rare earth element RE, where RE is selected from scandium, yttrium, and the lanthanides;
said composition containing no silicon or silicon compound; and
shaping the composition and densifying said composition.

13. A method according to claim 12 , wherein the composition contains a boride of said rare earth element RE and at least hafnium in metallic form or hafnium in carbide, or nitride, or boride form.

14. A method according to claim 12 , wherein the composition contains a nitride of said rare earth element RE, and at least one boride of hafnium and at least one non-oxide compound of hafnium.

15. A method according to claim 12 , wherein the composition contains hafnium and a rare earth boride DyB4, where Dy corresponds to dysprosium, which is a rare earth, or a carbide of hafnium and a rare earth boride DyB4 where Dy corresponds to dysprosium, which is a rare earth.

16. A method of using a part at a temperature higher than 2000° C. in an oxidizing medium, the method comprising:
providing the part, the part being a refractory part or a composite material part; and
using said refractory part or said composite material part under a temperature higher than 2000° C. in an oxidizing medium, wherein
said refractory part is constituted by a refractory material that can withstand high temperatures in the oxidizing medium, and
said composite material part constituted at least in part by carbon and having a protective coating providing protection at said high temperatures in the oxidizing medium, wherein said protective coating is constituted by at least the refractory material,
the refractory material comprising:
hafnium, or a non-oxide compound of hafnium, or a mixture of hafnium and a non-oxide compound of hafnium;
boron or a non-oxide compound of boron, or a mixture of boron and a nonoxide compound of boron; and
a constituent corresponding to a rare earth element RE or a to non-oxide compound of the rare earth element RE, or corresponding to a mixture of rare earth element RE and a non-oxide compound of the rare earth element RE, where RE is selected from scandium, yttrium, and the lanthanides; and
said material containing neither silicon nor a compound of silicon.

17. A method according to claim 16 , wherein the refractory material contains a boride of said rare earth element RE and at least hafnium in metallic form, or hafnium in carbide or nitride or boride form.

18. A method according to claim 16 , wherein the refractory material contains a nitride of said rare earth element RE, said material also containing at least one boride of hafnium and at least one non-oxide compound of hafnium.

19. A method according to claim 16 , wherein the refractory material contains hafnium and a rare earth boride DyB4, where Dy corresponds to dysprosium, which is a rare earth, or a carbide of hafnium and a rare earth boride DyB4 where Dy corresponds to

Assignees

• Andreani Anne-Sophie
• Rebillat Francis
• Poulon Angeline
• Thebault Jacques
• Sauveroche Anne
• Centre Nat Rech Scient
• Herakles

Inventors

• Andreani Anne-Sophie
• Rebillat Francis
• Poulon Angeline
• Thebault Jacques
• Sauveroche Anne

Classifications

• C04B35/83

  Carbon fibres in a carbon matrix · CPC title

• C04B2235/9684

  Oxidation resistance · CPC title

• C04B2235/3852

  Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride · CPC title

• C04B41/507

  Borides · CPC title

• C04B41/87

  Ceramics · CPC title