Patent GB-908180-A (GB)
Title: Improvements in or relating to nuclear reactor fuel elements
Inventor: DAVIS MICHAEL
IPC: G21C3/04
Filed: 1960-04-19
Abstract: 908,180. Nuclear fuel elements. UNITED KINGDOM ATOMIC ENERGY AUTHORITY. April 4, 1961 [April 19, 1960; April 26, 1960; Oct. 14, 1960], Nos. 13631/60, 14582/60 and 35395/60. Class 39 (4). Fuel elements stacked end to end upon one another in a fuel element channel of a nuclear reactor are restrained against vibration by means of members provided at or near one end and extending partway round the periphery of each element so as to be exposed to coolant flow, whereby a lateral component of the force exerted by the coolant moves each fuel element into a stable position. In one embodiment (Fig. 4, Provisional Specification No. 14582/60), each fuel element comprises a uranium rod 6 in a magnesium alloy sheath 7 carrying helical fins 2 and longitudinal splitter fins 3, which latter fins define four flow paths A, B, C and D. The fins 3 are held together at the lower ends of the fuel elements by braces 9 of small crosssection in flow paths B and D and by flow-gags 5 in flow paths A and C. Since the flow of coolant is upward, the difference in cross-section between the braces 9 and the flow-gags 5 gives rise to a difference in pressure drop between the flow paths B and D and the flow paths A and C which remains constant along the greater part of the lengths of the elements, resulting in a lateral force urging the fuel elements towards the wall of the channel in which they are located (towards the left in Fig. 4). At the upper ends of the fuel elements, flow-gags and braces are similarly provided but with their relative positions reversed to provide an overall pressure drop balance across the fuel elements. A second embodiment is shown in Fig. 1 (Provisional Specification 13631/60), each fuel element 1 having a sheath 2 with helical fins 3 and longitudinal splitter fins 4. Each sheath 2 has an upper end cap 5 provided with a spigot 6 screw-threaded into an end fitting 8 having a cup-shaped recess 9 for engagement by a correspondingly shaped cone on the lower end fitting (not shown) of the adjacent fuel element. A laterally projecting portion 12 on each end fitting 8 comprises an arcuate parallel-sided part 13 secured to the body of the fitting by parallel webs 14 to form a convergent passage 15 between the curved inclined inner surface 17 of the part 13 and the upright surface 16 on the body of the fitting. Flow of coolant through the passage 15 exerts a lateral force on the surface 17 and produces a region of lower pressure immediately above this passage, thus moving the upper end of the element laterally until the extremity of the part 13 and/or a splitter fin or fins 4 beneath the part 13 contact the wall of the channel 18. Alternatively, the lower end fitting (not shown) of the adjacent fuel element may be provided with a spider, one or more of the arms of which are moved into contact with the channel wall. To enable a degree of pivoting to take place at the cup- and-cone engagement, the cup-shaped recess 9 of each end fitting 8 is provided with a central aperture 19 which allows the point of the engaging cone to move a limited amount laterally as the upper end of the fuel element is moved by the coolant flow. In a further embodiment, as shown in Fig. 1, Provisional Specification 35395/60, the upper end of each Fuel element is provided with a member 3 of aerofoil section extending partly around the periphery of the fuel element and so disposed that the chord 4 of the aerofoil section is inclined to the axis of the channel 2. The member 3 is attached to an end fitting 7 by radially extending arms 8. When coolant flows through the channel 2, as indicated by the arrows 11, a lateral force or " lift " is exerted on the member 3 in the direction of the arrow 12 which presses the extremities of the arms 8 against the adjacent channel wall. In all three embodiments, the overall dimensions of the fuel elements are less than the internal dimensions of the fuel element channels to permit ease of refuelling.