X-ray target assembly and methods for manufacturing same

1. An x-ray target assembly for use in a rotating anode assembly, comprising:

a substrate comprising a refractory metal and one or more oxide compounds dispersed in the refractory metal;

a heat sink comprising carbon;

a barrier layer positioned between the substrate and heat sink, wherein the barrier layer is substantially free of the one or more oxide compounds that are dispersed in the refractory metal;

a braze layer positioned between the heat sink and the barrier layer,

wherein the barrier layer has a thickness that substantially prevents the one or more oxide compounds from reacting with the carbon in the heat sink, thereby reducing the formation of oxide gasses in an interface region between the substrate and the heat sink.

2. An x-ray target assembly as in claim 1 , wherein the refractory metal is molybdenum or a molybdenum alloy.

3. An x-ray target assembly as in claim 1 , wherein the barrier layer comprises a substantially pure metal, a boride, a silicide, a nitride, or a carbide of Mo, Ta, Re, W, Ti, Nb, V, Hf, or Zr, or a combination thereof.

4. An x-ray target assembly as in claim 1 , wherein the barrier layer has a thickness in a range from about 0.01 mm to about 2.5 mm.

5. An x-ray target assembly as in claim 1 , wherein the braze layer comprises Zr, Ti, V, Cr, Fe, Co, Ni, Pt, Rd, or Pd.

6. An x-ray target assembly as in claim 1 , wherein the oxide compound comprises lanthana, yttria, ceria, thoria, or a combination thereof.

7. An x-ray target assembly as in claim 1 , wherein the substrate is disk-shaped and further comprises a circular target track about a periphery of the substrate.

8. An x-ray target assembly as in claim 1 , wherein the barrier layer and the substrate are directly bonded together and the barrier layer and the heat sink are bonded together by the braze.

9. An x-ray tube assembly comprising the x-ray target assembly of claim 1 .

10. A high performance CT-scanner comprising the x-ray tube of claim 9 .

11. A method for manufacturing an x-ray target assembly, comprising:

providing a substrate comprising a refractory metal and one or more oxide compounds dispersed in the refractory metal;

forming a target track on the substrate;

forming a barrier layer on at least a portion of the substrate, the barrier layer comprising a material that is substantially free of the one or more oxide compounds that are dispersed in the refractory metal; and

brazing a carbon-based heat sink to the barrier layer such that the barrier layer substantially prevents the one or more oxide compounds from reacting with the carbon in the heat sink during the brazing step, thereby reducing the formation of oxide gasses in an interface region between the substrate and the heat sink.

12. A method as in claim 11 , wherein the refractory metal is Mo.

13. A method as in claim 11 , wherein the barrier material is deposited on the substrate using a technique selected from the group consisting of plasma spray coating, salt-bath electrodeposition, electroplating, vacuum sputtering, melt evaporation, chemical vapor deposition, physical vapor deposition, or a combination thereof.

14. A method as in claim 11 , wherein the barrier material is metullurgically bonded to the substrate using a technique selected from the group consisting of hot rolling, cold rolling, upset forging, hot isostatic pressing, cold isostatic pressing, and combinations thereof.

15. A method as in claim 11 , wherein the oxide compound comprises lanthana, yttria, ceria, thoria, or a combination thereof.

16. A method as in claim 11 , wherein the heat sink comprises graphite or a carbon composite.

17. A method as in claim 11 , wherein the barrier layer comprises Mo, Ta, Re, W, Ti, Nb, V, Hf, Zr, or combinations thereof.

18. An x-ray tube comprising an x-ray target manufactured according to the method of claim 11 .

19. A method for manufacturing a x-ray target assembly, comprising:

providing a substrate comprising an oxide dispersion strengthened (ODS) Mo alloy;

forming a target track on the substrate;

coating at least a portion of the substrate with a layer of a substantially pure metal or metal alloy selected from the group consisting of Mo, Ta, Re, W, Ti, Nb, V, Hf, Zr, or a Mo alloy thereof;

outgas sing the coated substrate; and

brazing a graphite disk to the outgassed coated substrate using a braze comprising Zr, Ti, V, Cr, Fe, Co, Ni, Pt, Rd, or Pd, wherein the coating has a thickness that substantially prevents oxides present within the oxide dispersion strengthened (ODS) Mo alloy from reacting with carbon in the graphite disk, thereby reducing the formation of oxide gasses in an interface region between the substrate and the heat sink.

20. A method as in claim 19 , wherein the oxide-free barrier layer is deposited on the substrate using a technique selected from the group consisting of plasma spray coating, salt-bath electrodeposition, electroplating, vacuum sputtering, melt evaporation, chemical vapor deposition, physical vapor deposition, or a combination thereof.

21. A method as in claim 19 , wherein the oxide-free barrier layer is mechanically adhered to the substrate using a technique selected from the group consisting of hot rolling, cold rolling, upset forging, hot isostatic pressing, cold isostatic pressing, and combinations thereof.

22. A method as in claim 19 , wherein the ODS Mo alloy comprises an oxide of lanthana, yttria, ceria, thoria, or a combination thereof.

23. An x-ray tube comprising an x-ray target manufactured according to the method of claim 19 .