Patent Number: 046541829
Section: description

DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings, apparatus for containing plasma in a high energy plasma device 20 includes a vacuum tight liner wall generally indicated by reference numeral 22 in FIG. 1. The liner wall 22, which is preferably made of stainless steel, is part of a primary confinement vessel. The liner wall may be disposed within and supported by a shell (not shown) formed of a relatively thick copper wall forming a secondary chamber. Such an arrangement is shown in commonly-assigned U.S. Pat. No. 4,302,284, the teachings of which are incorporated herein by reference. While the wall 22 is exemplarily shown as a torus, it will be appreciated that it can be formed in any desired shape. The device includes a frame 24 for supporting the liner and a magnet system 26 which could be made up of toroidal, poloidal, helical and other coils or windings which may be either of superconductive or normal material. The purposes of the magnet system are to produce and confine the plasma inside the liner wall. The liner wall is preferably made up of a number of sections 28 with each section 28 having a closed peripheral wall defining an interior 30 with open ends. Adjacent interiors of adjacent sections form a plasma path 32. The sections 28 preferably have a relatively thin wall and have sufficient loop resistance that the penetration times for the magnetic field provided by the magnet system, are acceptably short. Certain of the sections are provided with ports 34 and associated piping for passage of the constituents of the plasma and for applying a vacuum. As shown in FIG. 2, each section 28 includes an inside surface 36 and an outside surface 38 with its interior being generally circular in cross section. Theoretically, a properly designed magnet system would provide sufficiently homogeneous magnetic fields that the plasma is contained in the liner wall out of contact with the liner wall inner surface. However, available magnet systems do not provide such ideal fields and the plasma contacts the liner wall inner surface. When the plasma contacts the inner surface of a section 28, energetic particles from the plasma impinge on the wall resulting in localized heating and causing melting and loss of vacuum integrity. Additionally metal ions from the sections enter and contaminate the plasma. The introduction of the metal ions into the plasma causes increased radiation resulting in power loss in the plasma. In order to protect the liner wall from damage due to contact by the plasma, the apparatus of the present invention includes a plurality of armature rings 40 disposed at spaced locations inside the liner wall. Each ring 40 includes means for entering into rolling engagement with the inside surface 36 of one of the segments 28 and each ring includes current-carrying armature conductors extending at an angle to lines of force extending inside the section and provided by the helical coil portion of the magnetic system 26. More specifically, as shown in FIG. 2, the magnetic system includes a plurality of spaced conductors 42 helically wound about the outer surface of the liner wall 22. For purposes of illustration, four conductors 42 are shown which carry direct current with adjacent conductors carrying current in opposite directions. As suggested in FIG. 3, the conductors 42 provide magnetic lines of flux which extend inside each section, generally normal to the plasma path. Referring to FIG. 4, the armature ring 40 is made of electrically conductive material and includes a first annular end 44, a second annular end 46 and a plurality of spaced bars 48, extending in the direction of the plasma path and constituting the armature conductors, interconnecting the annular ends 44 and 46. Positioned between adjacent bars 48 are rollers 50 having oppositely extending lugs 52 received in cavities 54 formed by channel-shaped sections of the annular ends between the bars 48. A spring 55 is positioned inwardly of its corresponding lug to bias the rollers outwardly into engagement with the inside surface 36 of the section 28 in which the armature ring is positioned. Accordingly, the armature uses the section inside surface as a race on which to rotate. The rollers are preferably formed of an electrically insulative material such as a ceramic. In the event the inner surface 36 is not circular in cross section, a track which did provide a circular race for the armature, could be attached to the liner wall for supporting the armature ring. The apparatus of the present invention also includes means for supplying direct current to the bars 48 of the armature ring. As shown in FIG. 4, a first brush 56 is mounted on a first conductive standard 58 extending through a hole 60 in the liner wall inside an insulative bushing 62. The bushing 62 and standard 56 completely fill the hole 60 to prevent vacuum leaks. The brush 56 slidably engages the first annular end 44 of the armature ring 40. Similarly, a second brush 64 is mounted on a second conductive standard 66 extending through another hole 60 in the liner wall inside an insulative bushing 62. The second brush 64 slidably engages the second annular end 46 of the armature ring at a position generally aligned with the location of engagement of the first brush 56. The conductive standards 58 and 66 are connected to a source of direct current 68 as shown in FIG. 3. Due to the electrical resistance of the armature annular ends 44 and 46, more current flows through the bar 48A closest the areas of contact of the brushes with the corresponding annular ends, than through any other bar 48. The brushes 56 and 64 are angularly displaced relative to the helical conductor 42A so that flux lines resulting from current in conductor 42A intersect the bar 48A closest the brushes generally radially with respect to the center of the section 28. The interaction of the magnetic flux and the current through the bar 48A results in a force, the Lorenz force, which is in a direction perpendicular to both the current in bar 48A and the flux lines. Thus, as in a direct current motor, the armature ring rotates. Preferably another set of brushes is located diametrically across the section 28 to provide current to another bar located 180 degrees from bar 48A. The force resulting from the interaction of this current and magnetic flux provided by conductor 42C aids the first force and results in a more balanced application of forces to the armature ring. The presence of the brushes bearing on the sides of the armature ring limit it to poloidal rotation and prevent movement of the ring in the direction of the plasma path. While the magnet system 26 generates fields other than those shown in FIG. 3, the rings 40 are restrained from other than rotational movement in a plane extending transversely to the plasma path. The armature ring carries a protective coating in the form of a plurality of armor tiles 70 facing the plasma path. These tiles preferably abut one another and form a ring fully covering the armature ring with respect to the plasma path and extend laterally over the brushes and standards to form a first wall for contact by the plasma. These tiles are formed of a material having a higher melting temperature than the material from which the liner wall 22 is formed. The tiles are preferably formed of silicon carbide coated carbon, ceramic material or a nickel-chromium-iron alloy, with coated high density carbon being most preferable. The tiles 70, can be affixed to the ring by, for example, pins 71 having heads received in countersunk apertures in the tiles, with the shanks of the pins received in an interference fit in apertures 73 in the armature ring 40. In the case of the liner wall 22 in the shape of a torus, the number of rings 40 employed is preferably sufficient so that, on the inner side of the torus, the tiles of adjacent rings almost touch. Arcuate surface segments 72 of the torus are not covered by the tiles, as shown on FIG. 2. Although the tiles do not overlie the surface segments 72, under many operating conditions they substantially protect the segments from impingement by high energy charged particles, which leave the plasma and give up their energy to the first surface they strike. This is because these particles predominantly follow the direction of the composite magnetic field. Typically the radial component of the composite magnetic field is much smaller than the toroidal component. Thus the paths taken by most of the escaping charged particles intersect the liner wall at shallow angles. These angles are so shallow that most charged particles strike the tiles which are disposed above the level of the segments 72 and not the segments. Put another way, although the segments are visible in plan, they are in the shadow of the tiles in view of the direction of the plasma particles. Each armature ring 40 is sized to lie closely adjacent but spaced from the inside surface 36 of the respective section 28 when the section and the ring are at ambient temperature to enable the ring to rotate inside the section on the rollers 50. The armature ring, however, is made of a material having a coefficient of thermal expansion somewhat greater than that of the material forming the section 28. Accordingly, as heat from the plasma is transferred from the tiles 70 to the armature ring 40, the armature ring expands into full surface engagement with the liner wall causing the ring to stop rotating, and heat from the armature ring to transfer to the liner wall. With a pulsed plasma, this full surface engagement occurs shortly after the plasma is turned off, due to thermal inertia. This is analogous to the brake shoe expanding against the wheel drum in an automobile brake. The outside surface of the liner wall is actively cooled, for example, by running coolant pipes (not shown), around the liner wall. With the rings firmly against the liner wall, heat is efficiently transferred from the tiles to the coolant through the ring and the liner wall. As the armature ring cools, it shrinks and the springs 55 bias the rollers outwardly to center the ring inside its corresponding section 28. While the first and second annular ends 44, 46 of the ring have been described as being made entirely of conductive material, the portions of the ends disposed between the bars could be formed of an electrically insulating material 76 as shown in FIG. 4. The use of insulating components between bars 48 has the advantage of limiting current to the particular bar aligned with the brushes 56 and 64. However, heat transfer from the tiles may be reduced and the insulating material should have a thermal coefficient of expansion close to that of the conductive material of the annular ends 44 and 46. Operation of the apparatus of the present invention is as follows: Energization of the helical conductors 42 results in formation of a magnetic field extending inside the liner wall 22. When direct current is supplied to the bars 48 of the armature ring 40, the interaction of the current in the bars and the magnetic field results in a force which turns the ring 40 in the poloidal direction. The armored tiles carried by the armature ring act as plasma limiters (a first wall) and are heated. Heat transfer from the tiles to the armature ring causes expansion thereof resulting in a armature ring stopping rotation in full surface contact with the liner wall. This allows heat to be transferred from the tiles to a cooling means, disposed outside the liner wall, through the armature ring and the liner wall. It will be appreciated that the rings may be rotated over a broad range of frequencies and rotation of the rings tends to spread the plasma heat load over the entire surface of the liner wall to prevent damage to the liner wall resulting from a localized heat concentration. The plasma may be of pulsed operation with the plasma being turned off prior to expansion of the ring against the liner wall. In this case, the heat flow through the tiles, even with the plasma turned off, may be sufficient to result in expansion of the armature ring against the liner wall. After the heat has been transferred out through the coolant, the spring loaded rollers center the armature ring after it has contracted and place the ring in position for another plasma discharge. As a method, the present invention includes several steps: a. An armature ring 40 is rotatably mounted inside one of the sections 28 making up the liner wall 22. The ring 40 carries rollers 50 for engaging the inside surface of the section 28 and further includes armature conductors 48 extending at an angle to lines of force provided by a magnet system in the high energy plasma device 20. b. Armor tiles 70 are affixed to the ring 40 facing the plasma path 32 from the liner wall 22 for acting as plasma limiters. c. Direct current is caused to flow through the armature conductors 48 so that the interaction of the magnetic field and the current in the armature conductors results in rotation of the armature ring 40 to prevent damage to the section due to localized heat concentration. In view of the above, it will be seen that the several objects of the invention are achieved and other advantageous results attained. As various changes could be made in the above constructions without departing from the scope of the invention, it is intended that all matter contained in the above description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.