Apparatuses and methods for fabricating metal matrix composite structures
A method for forming a metal matrix composite (MMC) structure includes forming an assembly including at least two blocks of a primary phase material sharing an interface at which a secondary phase material is disposed. The assembly has a length, a width, and a thickness. The method also includes clamping the assembly to at least one of urge the at least two blocks toward each other or maintain the at least two blocks at a predetermined position. Also, the method includes passing a rotating friction-stir pin along the interface from the front edge to the rear edge. The friction-stir pin has a mixing length extending at least the width of the assembly, and passing the friction-stir pin along the length of the assembly disperses the secondary phase material into the primary phase material and welds the at least two blocks together.
1. A method for forming a metal matrix composite (MMC) structure, the method comprising:
forming an assembly including at least two blocks of a primary phase material sharing an interface at which a secondary phase material is disposed, the assembly having a length extending from a front edge to a rear edge, a width extending perpendicular to the length, and a thickness;
clamping the assembly to at least one of urge the at least two blocks toward each other or maintain the at least two blocks at a predetermined position;
passing a rotating friction-stir pin along the interface from the front edge to the rear edge, wherein the friction-stir pin is supported at opposite ends as the friction-stir pin is passed along the interface, wherein the friction-stir pin has a mixing length extending at least the width of the assembly, wherein the passing the friction-stir pin disperses the secondary phase material into the primary phase material and welds the at least two blocks together.
2. The method of claim 1 , further comprising driving the friction-stir pin at the opposite ends as the friction-stir pin is passed alone the interface.
3. The method of claim 1 , wherein forming the assembly comprises disposing the secondary phase material within a cavity of at least one of the at least two blocks.
4. The method of claim 1 , wherein the at least two blocks comprise at least three blocks defining two interfaces.
5. The method of claim 4 , wherein the at least three blocks comprise three blocks comprised of different metals from each other.
6. The method of claim 4 , wherein the secondary phase material comprises a first secondary phase material disposed at a first interface and a second secondary phase material disposed at a second interface.
7. The method of claim 1 , wherein the primary phase material comprises Aluminum.
8. The method of claim 1 , wherein the secondary phase material comprises a ceramic powder.