Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon

1. An assembly between a titanium-based metal piece and a ceramic material piece based on silicon carbide and/or carbon, the assembly comprising a stack structure comprising the following elements assembled together by brazing, in the following order:

said metal piece;

a first intermediate piece that is suitable for deforming to accommodate differential expansion between said metal piece and said ceramic material piece;

a second intermediate piece that is rigid, that has a coefficient of expansion close to that of said ceramic material piece, and that is made of aluminum nitride (AlN) or of tungsten (W); and

said ceramic material piece,

wherein the brazing composition that assembles said second intermediate piece to the ceramic material piece is of the Ag—Mn type with a percentage by weight of manganese (Mn) that lies in the range 1% to 25%.

2. An assembly between a titanium-based metal piece and a ceramic material piece based on silicon carbide and/or carbon, the assembly comprising a stack structure comprising the following elements assembled together by brazing, in the following order:

said metal piece;

a first intermediate piece that is suitable for deforming to accommodate differential expansion between said metal piece and said ceramic material piece;

a second intermediate piece that is rigid, that has a coefficient of expansion close to that of said ceramic material piece, and that is made of aluminum nitride (AlN) or of tungsten (W); and

said ceramic material piece,

wherein the brazing composition that assembles said second intermediate piece and the ceramic material piece is of the Ag—Cu—Ti type with a percentage by weight of silver (Ag) not less than 50% and a percentage by weight of titanium (Ti) lying in the range 0.01% to 6%.

3. The assembly according to claim 2 , wherein said Ag—Cu—Ti brazing composition comprises the following percentages by weight: 63 of Ag; 35.25 of Cu; and 1.75 of Ti.

4. The assembly according to any one of claims 1 to 3 , wherein said ceramic material piece is made of solid silicon carbide.

5. The assembly according to any one of claims 1 to 3 , wherein said ceramic material piece comprises a ceramic matrix reinforced by silicon carbide or carbon fibers.

6. The assembly according to claim 5 , wherein said matrix includes at least one self-healing phase.

7. The assembly according to any one of claims 1 to, 3 wherein the metal piece is made of an alloy based on titanium, aluminum, and vanadium.

8. The assembly according to any one of claims 1 to 3 , wherein said first intermediate piece is made of a ductile solid material.

9. The assembly according to claim 8 , wherein said first intermediate piece is made of substantially pure titanium.

10. The assembly according to any one of claims 1 to 3 , wherein first intermediate piece is in the form of a deformable structure.

11. The assembly according to claim 10 , wherein said deformable structure includes at least one connecting intermediate element assembled by brazing to said metal piece and to said second intermediate piece, said connecting intermediate element being in the form of a deformable sheet presenting concentric undulations and brazed flat zones.

12. The assembly according to claim 11 , wherein said deformable structure includes at least one piece having the general shape of a concertina-folded tape defining curved portions facing alternately towards the metal piece and towards the second intermediate piece, said curved portions being separated by peaks, assembly by brazing between the metal piece and the first intermediate piece or the second intermediate piece as the case may be being performed via flat zones of at least some of said peaks.

13. A turbomachine nozzle including at least one assembly according to any one of claims 1 to 3 , wherein said metal piece is a casing of said nozzle and said ceramic material piece is a flap of said nozzle.

14. A turbomachine combustion chamber including at least one assembly according to any one of claims 1 to 3 , wherein said metal piece is a casing of said chamber and said ceramic material piece is a component part of said chamber.

15. A post-combustion equipment for a turbomachine, the equipment including at least one assembly according to any one of claims 1 to 3 , in which said metal piece is a post-combustion casing and said ceramic material piece is a flame-holder arm.

16. A turbomachine including at least one assembly according to any one of claims 1 to 3 .