Aluminized metallic scaffold for high temperature applications and method of making an aluminized metallic scaffold
An aluminized metallic scaffold for high temperature applications comprises a porous non-refractory alloy structure including a network of interconnected pores extending therethrough. The porous non-refractory alloy structure comprises a transition metal phase and an aluminide phase, and portions of the porous non-refractory alloy structure between interconnected pores have a thickness no greater than about 500 nm. A method of making an aluminized metallic scaffold for high-temperature applications comprises introducing aluminum into a surface of a porous metallic structure at an elevated temperature. The porous metallic structure comprises a transition metal and has a network of interconnected pores extending therethrough, where portions of the porous metallic structure between interconnected pores have a thickness no greater than about 500 nm. As the aluminum is introduced into the surface and diffusion occurs, an aluminide phase is formed, resulting in a porous non-refractory alloy structure comprising the aluminide phase and a transition metal phase.
1. An aluminized metallic scaffold for high temperature applications, the aluminized metallic scaffold comprising:
a porous alloy structure including a network of interconnected pores extending therethrough, the porous alloy structure comprising a transition metal phase and an aluminide phase, the porous alley structure not including niobium, molybdenum, tantalum, tungsten or rhenium,
wherein portions of the porous refractory alloy structure between the interconnected pores have a thickness no greater than about 500 nm, and
wherein the porous alloy structure has an inverse opal morphology.
2. The aluminized metallic scaffold of claim 1 , wherein the transition metal phase is selected from the group consisting of: a nickel phase, a titanium phase, an iron phase, a vanadium phase, a chromium phase, and a cobalt phase.
3. The aluminized metallic scaffold of claim 1 , wherein the aluminide phase is selected from the group consisting of: a nickel aluminide, a titanium aluminide, an iron aluminide, a vanadium aluminide, a chromium aluminide, and a cobalt aluminide.
4. The aluminized metallic scaffold of claim 1 , wherein the porous alloy structure comprises a porous nickel-base alloy structure,
wherein the transition metal phase comprises a nickel phase, and
wherein the aluminide phase comprises a Ni 3 Al phase.
5. The aluminized metallic scaffold of claim 4 , wherein the porous nickel-base alloy structure does not comprise a Ni 2 Al 3 phase.
6. The aluminized metallic scaffold of claim 1 , wherein each of the interconnected pores is about 1 μm or less in lateral size, and wherein the interconnected pores comprise a periodic arrangement.
7. The aluminized metallic scaffold of claim 1 , wherein the interconnected pores exhibit a size variation of about 5% or less.
8. The aluminized metallic scaffold of claim 1 , wherein the porous alloy structure includes aluminum at a concentration from about 8 at. % to about 25 at. %.
9. The aluminized metallic scaffold of claim 1 , wherein the aluminide phase is distributed throughout the porous alloy structure.
10. The aluminized metallic scaffold of claim 1 , wherein a distribution of the aluminide phase in the porous alloy structure does not exhibit a stepwise gradient as a function of thickness.
11. The aluminized metallic scaffold of claim 1 , wherein the porous alloy structure comprises a hardness at least 80% higher than that of a porous metallic structure consisting essentially of the transition metal phase.
12. The aluminized metallic scaffold of claim 11 , wherein the hardness is at least about 250 MPa.
13. An aluminized metallic scaffold for high temperature applications, the aluminized metallic scaffold comprising:
a porous alloy structure including a network of interconnected pores extending therethrough, the porous alloy structure comprising a transition metal phase and an aluminide phase the porous alloy structure not including niobium, molybdenum, tantalum, tungsten or rhenium,
wherein portions of the porous alloy structure between interconnected pores have a thickness no greater than about 500 nm, and
wherein the interconnected pores exhibit a size variation of about 5% or less.