Patent Number: 049903047
Section: claims

1. In a fuel assembly having a instrumentation tube with a hollow interior and a flux thimble tube inserted in said hollow interior of said instrumentation tube for taking flux measurements, said flux thimble tube radially spaced inwardly at its exterior surface from an interior surface of said instrumentation tube so as to define a coolant flow annulus therebetween, means for reducing coolant flow-inducing vibration of said thimble tube, comprising: a plurality of mechanical elements defined on said interior surface of said instrumentation tube in said hollow interior of said instrumentation tube at a plurality of axially spaced points therealong for engaging said exterior surface of said flux thimble tube within said instrumentation tube and inducing a controlled elastic sinuous deflection of said thimble tube to reduce vibration thereof induced by coolant flow in said annulus between said instrumentation and thimble tubes.  a plurality of mechanical elements defined on said interior surface of said instrumentation tube in said hollow interior of said instrumentation tube at a plurality of axially spaced points therealong for engaging said exterior surface of said flux thimble tube within said instrumentation tube and inducing a controlled elastic sinuous deflection of said thimble tube to reduce vibration thereof induced by coolant flow in said annulus between said instrumentation and thimble tubes, said elements being disposed at the elevations of said grids along said instrumentation tube. 2. The fuel assembly as recited in claim 1, wherein said mechanical elements are int he form of dimples formed in sad interior surface of said instrumentation tube and projecting radially inwardly therefrom. 3. The fuel assembly as recited in claim 2, wherein said dimples are bulged from a wall of said instrumentation tube. 4. The fuel assembly as recited in claim 1, wherein said mechanical elements are in the form of cantilevered spring fingers formed in said interior surface of said instrumentation tube and projecting radially inwardly therefrom. 5. The fuel assembly as recited in claim 4, wherein said spring fingers are cut out from a wall of said instrumentation tube. 6. The fuel assembly as recited in claim 1, wherein said mechanical elements are formed at a plurality of points on said instrumentation tube interior surface staggered on a single diametral plane through said tube. 7. The fuel assembly as recited in claim 6, wherein said points are at spaced axially and 180 degrees from one to the next. 8. The fuel assembly as recited in claim 1, wherein said mechanical elements are defined by an undulating longitudinal configuration of said instrumentation tube. 9. The fuel assembly as recited in claim 1, wherein said mechanical elements are defined by a spiral configuration of said instrumentation tube. 10. The fuel assembly as recited in claim 1, wherein said mechanical elements are defined by a zig-zag configuration of said instrumentation tube. 11. In a fuel assembly having a skeleton including a plurality of fuel rod-supporting grids being spaced apart from one another along an axis of said skeleton, a instrumentation tube extending through said grids and having a hollow interior, and a flux thimble tue inserted in said hollow interior of said instrumentation tube for taking flux measurements, said flux thimble tube radially spaced inwardly at its exterior surface from an interior surface of said instrumentation tube so as to define a coolant flow annulus therebetween, means for reducing coolant flow-inducing vibration of said thimble tube, comprising: 12. The fuel assembly as recited in claim 11, wherein said mechanical elements are in the form of spring fingers formed in said interior surface of said instrumentation tube by being cut out lengthwise and projecting radially inwardly therefrom. 13. The fuel assembly as recited in claim 12, wherein said spring fingers by being cut out from said instrumentation tube leave holes in said tube which are substantially covered by said grids. 14. The fuel assembly as recited in claim 11, wherein said mechanical elements are formed at a plurality of points on said instrumentation tube interior surface staggered on a single diametral plane through said tube. 15. The fuel assembly as recited in claim 14, wherein said points are at spaced axially and 180 degrees from one to the next.