Abstract: A method for the fabrication of large metal matrix composite structures comprising the continuous joining by brazing or welding of aluminum matrix tape using an infrared laser to melt the surface of the tape while applying pressure to the tape and simultaneously contacting it with previously applied tape layers on a rotating mandrel. The apparatus utilized to accomplish this fabrication process may include a variety of pre and post-contact heaters and preferably includes instruments for the continuous monitoring and control of the process.

Abstract: A selectively reinforced structure may be produced by embedding at least two metal matrix composite tapes in a non-planar relationship to one another and in a predetermined region of a structure to selectively reinforce the structure. Further, a method for selectively reinforcing a structure or part includes positioning at least two metal matrix composite tapes in a substantially fixed non-planar relationship in a predetermined location within a mold and filling the mold with a material such as a metal, metal alloy, polymer, foam, glass, or ceramic such that the MMC tapes are embedded within the material. A reinforced structure is produced that has at least two metal matrix composite tapes selectively positioned within the structure.

Abstract: The present invention provides for assemblies comprising metal matrix composite bars where the bars only intermittently have mutual contact. Minimally two bars of metal matrix composite are joined, for example by lap joints, or by the use of incorporated tabs and slots or over-lapping slots, at areas of mutual contact to form the assemblies. The metal matrix composite assemblies of the present invention may be readily assembled to provide structures, supports, or sub-assemblies, and the like, that may exhibit high strength and stiffness coupled with relatively low mass. Additionally, such assemblies may withstand exposure to elevated temperatures higher than can be tolerated by polymeric composites. Such assemblies are expected to be particularly suitable for lightweight, stiff support structures for space booms, satellite structures, mirror backings, solar panel supports, wall reinforcement, and the like.

Abstract: The present invention provides for assemblies comprising metal matrix composite bars where the bars only intermittently have mutual contact. Minimally two bars of metal matrix composite are joined, for example, by lap joints, or by the use of incorporated tabs and slots or over-lapping slots, at areas of mutual contact to form the assemblies. The metal matrix composite assemblies of the present invention may be readily assembled to provide structures, supports, or sub-assemblies, and the like, that may exhibit high strength and stiffness coupled with relatively low mass. Additionally, such assemblies may withstand exposure to elevated temperatures higher than can be tolerated by polymeric composites. Such assemblies are expected to be particularly suitable for lightweight, stiff support structures for space booms, satellite structures, mirror backings, solar panel supports, wall reinforcement, and the like.

Abstract: A glass fiber reinforced metal matrix composite is described. The composite includes glass fibers distributed in a metal matrix body. The fibers may be uniformly distributed in the metal matrix and may include continuous lengths of the glass fibers. The glass fibers may be glass fibers, S-glass, E-glass fibers, soda-lime-silica fibers, basalt fibers, quartz fibers, or other similar glassy fibers. The metal matrix may include aluminum or alloys of aluminum as well as other metals and alloys.