Patent Number: 
Section: claims

1. A method of surface finishing a cladding tube for a fuel element of a nuclear reactor core in which the cladding tube contains a plurality of fuel, comprising the steps of:heating the tube to thermal creep temperatures for the sapphire; andslowly drawing and/or pushing the heated tube through a plug and die set to reduce heights of ridges on respective inner and outer surfaces of the tube while limiting changes in the crystalline structure, especially the crystal orientation, of the bulk of the tube. 2. A method according to claim 1, wherein the plug and die set are dimensioned to provide substantially uniform wall thickness of the tube while reducing ridge height and limiting changes in the crystalline structure, especially the crystal orientation, of the bulk of the tube. 3. A method according to claim 1, wherein the forming displaces irregularities by producing shear along an “a” plane parallel to a principal “c” axis of the tube material. 4. A method according to claim 1, wherein the tube is drawn or pushed in a similar manner through a plurality of plug and die sets, each succeeding plug and die set having a slightly larger inner diameter and slightly smaller outer diameter, respectively, than its predecessor so as to reduce ridge height in successive steps, a final plug and die set having respective inner and outer diameters corresponding to finished outer and inner diameters of the tube. 5. A method according to claim 4, wherein the tube is allowed to thermally soak between die passes at a temperature slightly above the drawing temperature to alleviate any work hardening and make the ridges workable during subsequent drawing. 6. A method of surface finishing a sapphire tube by thermal creep differential expansion moulding using a mould that is made of a material that has a different coefficient of expansion than sapphire and is non-wettable by sapphire, the mould being sized and shaped to give desired diameters and surface uniformity of at least one of inner and outer surfaces of the tube, the method comprising:placing the rough sapphire tube in the mould and slowly heating the tube-mould assembly to the range of the creep temperature of the sapphire and causing pressure at an interface between the sapphire and the mould;maintaining the assembly at the upper end of the creep temperature range for a creep and soak period to allow creep to progress and relieve the stresses from the pressure upon the sapphire tube from the mould; andslowly cooling the assembly, allowing the sapphire tube to part from the mould so that it can be withdrawn. 7. A method according to claim 6, wherein the mould is configured and dimensioned to apply pressure to form the inner surface of the sapphire tube. 8. A method according to claim 6, wherein the mould is configured and dimensioned to apply pressure to form the outer surface of the sapphire tube. 9. A method according to claim 6, wherein the mould is configured and dimensioned to apply pressure to form both inner and outer surfaces of the sapphire tube at the same time. 10. The method according to claim 1 wherein the step of heating comprises heating to the tube to a temperature in the range of 1700-2000 degrees Celsius. 11. The method according to claim 6 wherein the step of heating comprises heating the tube-mold assembly to a temperature in the range of 1700-2000 degrees Celsius.