Patent Number: 044977670
Section: claims

1. A compression hub for a fusion reactor system for purposes of providing resistance to the forces tending to draw the magnets in the fusion reactor system together toward a common point comprising a multiplicity of compression plates arranged in a layered assembly and interconnected so as to form a unitary structure, each of said compression plates being of a polygonal shape and having a first opening formed at the center thereof, each of said compression plates further having a second opening operative as a flow passage for coolant formed therein adjacent one of the corners defined by the polygonal shape of each of said compression plates, a first set and a second set of shear members associated with each of said compression plates, said first set of shear members including a first shear member supported on one side of said first opening of each of said compression plates and a second shear member supported on another side of said first opening of each of said compression plates, said second set of shear members including a third shear member supported on one side of said first opening of each of said compression plates and a fourth shear member supported on another side of said first opening of each of said compression plates, each of said compression plates having an interruption formed therein extending from said first opening formed therein to the circumference of said compression plate, said interruption having a piece of insulation positioned therein and dimensioned so as to completely fill said interruption, said insulation filled interruption of each of said compression plates being operative to impede the circulation through each of said compression plates as well as through the entire compression hub of eddy currents induced therein, said multiplicity of compression plates when arranged in a layered assembly being positioned relative to each other such that said first set of shear members of each of said compression plates lie in a first common plane that passes through said first opening of each of said compression plates and extends the length of the compression hub, said second set of shear members of each of said compression plates lie in a second common plane that extends the length of the compression hub and intersects said first common plane at the center of said first opening formed in each of said compression plates, said second opening of each adjacent pair of said multiplicity of compression plates lie in a third common plane that intersects both said first common plane and said second common plane at the center of said first opening formed in said adjacent pair of compression plates, said interruption formed in each of said compression plates defines a fourth common plane that extends the length of the compression hub and intersects said first common plane, said second common plane and said third common plane at the center of said first opening formed in each of said compression plates. 2. A compression hub as set forth in claim 1 wherein said interruption formed in each of said compression plates consists of a radial cut made in each of said compression plates. 3. A compression hub as set forth in claim 1 wherein each of said compression plates is formed of mating segments, and said interruption comprises the space existing between ends of the mating segments when the mating segments are in the mated state.