Claims
- 1. A ternary titanium aluminum iron alloy comprising titanium, aluminum, and iron in the following approximate atomic percent
- Ti-(50-55)Al-(9-20)Fe
- and including Ti(Fe,Al).sub.2 Laves phase.
- 2. A titanium aluminum iron alloy according to claim 1, wherein said alloy comprises one or more of Ti-53Al-11Fe and Ti-54Al-17Fe, compositions .+-.1 atomic percent.
- 3. A composite structural article comprising a substrate and a coating for protecting the substrate from oxidative attack and interstitial embrittlement at temperatures up to at least 1000.degree. C., and a diffusion barrier between said substrate and said coating, the diffusion barrier comprising titanium, aluminum, and iron in the following approximate atomic percent:
- Ti-(50-55)Al-(9-20)Fe.
- 4. The composite article of claim 3, wherein the substrate is a titanium aluminum-based alloy.
- 5. The composite article of claim 4, wherein the substrate alloy is selected from the group consisting of TiAl (gamma) titanium aluminide, Ti.sub.3 Al (.alpha..sub.2)-based titanium aluminide, orthorhombic-based (Ti.sub.2 AlNb) titanium aluminide, alumina-based fibers, and combinations of the above.
- 6. The composite article of claim 5, further comprising an exterior coating of MCrAlX, wherein M is iron, nickel, or cobalt, and X is optional and is yttrium, zirconium, hafnium, or ytterbium.
- 7. The composite article of claim 6, wherein said exterior coating comprises FeCrAlX.
- 8. An oxidation-resistant coating on a substrate, said coating comprising a multiphase alloy of titanium, aluminum, and iron in the following approximate atomic percent:
- Ti-(50-55)Al-(9-20)Fe
- wherein a phase of said alloy comprises a Laves phase.
- 9. The coating of claim 8, wherein the substrate comprises titanium or a titanium aluminide alloy.
- 10. The coating of claim 9, wherein the titanium aluminide alloy comprises TiAl (gamma) titanium aluminide.
- 11. The coating of claim 9, wherein the titanium aluminide alloy comprises Ti.sub.3 Al (.alpha..sub.2) titanium aluminide.
- 12. The coating of claim 9, wherein the titanium aluminide alloy comprises a titanium aluminide comprising TiAl (gamma)+Ti.sub.3 Al (.alpha..sub.2).
- 13. The coating of claim 9, wherein the titanium aluminide alloy comprises orthorhombic-based titanium aluminide.
- 14. The coating of claim 9, wherein said coating alloy comprises one or more of Ti-53Al-11Fe and Ti-54Al-17Fe, compositions .+-.1 atomic percent.
- 15. The coating according to claim 9, wherein the substrate comprises an alumina-based fiber.
- 16. The coating according to claim 15, wherein said alumina-based fiber is in a titanium aluminide matrix composite.
- 17. The coating according to claim 16, wherein said coating alloy comprises one or more of Ti-53Al-11Fe and Ti-54Al-17Fe, compositions .+-.1 atomic percent.
- 18. The coating according to claim 9, further comprising an exterior coating of MCrAlX wherein M is iron, nickel, or cobalt, and X is optional and is yttrium, zirconium, hafnium, or ytterbium.
- 19. The coating according to claim 18, wherein the titanium aluminide alloy comprises TiAl (gamma) titanium aluminide.
- 20. The coating according to claim 19, wherein the titanium aluminide alloy comprises Ti.sub.3 Al (.alpha..sub.2) titanium aluminide.
- 21. The coating according to claim 19, wherein said substrate is an orthorhombic-based titanium aluminide.
- 22. A method of protecting titanium substrates comprising the step of applying a layer of alloy comprising Ti-(50-55)Al-(9-20)Fe atomic percent on said substrate, said alloy including Ti(Fe, Al).sub.2 Laves phase.
- 23. A method of protecting titanium substrates according to claim 22, further comprising the step of applying an outer coating of FeCrAlX on said layer, wherein X is yttrium, zirconium, hafnium, or ytterbium.
- 24. An oxidation-resistant coating on a substrate, said coating comprising the first layer of a multi-phase ternary alloy of titanium, aluminum, and iron in the following approximate atomic ratio:
- Ti(50-55)-Al-(9-20)Fe
- and a second layer of MCrAlX on said layer wherein M is iron, nickel, or cobalt, and X is optional and is yttrium, zirconium, hafnium, or ytterbium.
ORIGIN OF INVENTION
The invention described herein was made in part by employees of the United States Government and may be manufactured and used by the Government for governmental purposes without the payment of any royalties thereon or therefor.
US Referenced Citations (14)
Non-Patent Literature Citations (1)
Entry |
Oxidation Mechanism of Gamma+LAVES Ti-Al-Cr Coating Alloys, Brady, Smialek, Humphrey and Smith, Oct. 1995, NASA Hi Temp Proceedings. |