Patent Number: 040594831
Section: description

DESCRIPTION OF THE PREFERRED EMBODIMENT With reference to FIG. 1, a fuel assembly incorporating improved spacer grids and seismic grid is illustrated generally at 10. Fuel assembly 10 includes, extending longitudinally therethrough, five guide tubes 12. Control rods, in the form of neutron absorber elements, move within guide tubes 12 and extensions thereof which are not shown in the drawing; such control rods serving as a means for regulating the thermal output power of the reactor. The fuel assembly also includes a plurality of fuel rods 14. In a typical 16 .times. 16 array, there will be 236 fuel rods in each fuel assembly and the reactor core may receive as many as 18 of the fuel assemblies 10. Each fuel rod 14 comprises a hermetically sealed elongated tube, known in the art as the cladding, which contains a fissionable fuel material such as uranium in the form of pellets. As may best be seen from FIG. 2, the individual fuel rods 14 are supported in the fuel assembly, by means of a plurality of spacer grids 16, such that an upwardly flowing liquid coolant may pass over the fuel rods thus preventing overheating and possible melting through of the cladding. In the manner well known in the art, the coolant, after passing through the reactor core and being heated through contact with the fuel rods, will be delivered to a heat exchanger and the heat extracted from the circulating coolant will be employed to generate steam for driving a turbine. As noted, and as may be seen from joint consideration of FIGS. 1 and 2, the positioning and retention of the fuel rods in fuel assembly 10 is accomplished through use of a plurality of spacer grids 16. All or several of spacer grids 16 may be of the improved design depicted in FIGS. 2-4. If the operating environment so warrants, fuel assembly 10 may also be provided with one or more seismic grids 18. If a single seismic grid 18 is employed it will be located as shown intermediate the ends of the fuel assembly. It may, in some circumstances, be desirable to employ a pair of additional seismic grids 18 positioned equidistant between the seismic grid of FIG. 1 and the opposite ends of the fuel assembly. The seismic grids, when employed, will preferably be comprised of stainless steel and will be of the type depicted in FIGS. 5 and 6. As briefly noted above, and as will be understood by those skilled in the art, the reactor core will comprise a plurality of fuel assemblies 10 supported in a core shroud mounted within a core support barrel; the core shroud typically be comprised of stainless steel. There will be gaps between the adjacent fuel assemblies 10, as positioned within the core shroud, and also between the outermost fuel assemblies and the wall of the shroud. These gaps, which allow a limited degree of relative movement between adjacent fuel assemblies, are necessary to permit the withdrawal and insertion of fuel assemblies, as incident to a refueling operation, and to permit the irradiation induced growth of the zircaloy components of the fuel assemblies. Thus, by way of example, in the assembly of a reactor core a cold spacing of 0.074 inches, corresponding to a hot spacing of 0.1 inches, will be left between adjacent fuel assemblies to permit relative vertical movement therebetween during refueling. It is to be noted that, due to differential expansions which will not be described herein, when the reactor is running hot the spacing between the fuel assemblies will be larger than under cold conditions. The aforementioned spacing includes the clearance required to accommodate thermal and irradiation induced growth. Under a seismic load the fuel assemblies could, with this spacing, move about and impact against each other and against the walls of the core shroud. Such impacts could, if sufficiently strong, cause the permanent distortion of the fuel assembly spacer grids of the prior art and could also cause bending of the guide tubes and could result in damage to the cladding of individual fuel assemblies through varying the coolant flow characteristics of the fuel assembly or otherwise. Additionally, high seismic loading could also cause the exceeding of the elastic limit of the integral internal grid assembly springs of the prior art fuel assemblies; this particularly being true for those springs in the outer rows of the fuel assemblies. With reference now jointly to FIGS. 2-4, a zircaloy spacer grid of increased strength is indicated generally at 16. In the manner known in the art, the spacer grid 16 supports and aligns the fuel rods 14 through the establishment of six points of contact therewith. Thus, in conventional practice as depicted in FIG. 2, each of fuel rods 14 is contacted by a pair of generally transversely oriented springs which respectively urge the fuel rod against oppositely disposed stop members in each sector of the grid. The stop members will customarily be provided in pairs with the individual stops of each pair being respectively vertically above and below a plane through the point of contact of the springs with the fuel rod cladding. Thus, considering fuel rod 14', this element is urged by means of springs 26 and 28, respectively integral with spacer grid internal spring members 20 and 22, against pairs of arches formed respectively on spring members 20' and 22'. The spacer grid 16 is assembled by interleaving of the internal spring members 20 and 22 and the ends of members 20 and 22 may be engaged in slots 30 provided in the spacer grid perimeter strip 32. Welds are formed at all points of intersection within the spacer grid and the ends of the spring members 20 and 22 are either welded into the slots 30 in perimeter strip 32 or are butt welded to the perimeter strip. When compared to the prior art, the spacer grid of the present invention has a longer spring member to perimeter strip weld line and thus greater resistance to deformation. Referring to FIG. 3, perimeter strip 32 is provided with cut-outs or "windows" 34 in regions corresponding to alternate sectors of the outer row of the spacer grid. These "windows," which are of smaller dimensions when compared to the windows of prior art perimeter strips such as shown in referenced U.S. Pat. No. 3,607,640, enhance coolant flow while simultaneously minimizing the neutron capture of the spacer grid. The perimeter strip 32 is also stamped so as to form, in sectors which alternate with the sectors provided with "windows" 34, inwardly extending integral springs 36. As may be seen from FIG. 2, each of springs 36 cooperates with an internal spring on a grid defining spring members to support and align a fuel rod of the outer row of the fuel assembly. The perimeter strip 32 is also provided, above and below each of windows 34, with inwardly extending dimples 38. Dimples 38, in the manner known in the art, enhance the rigidity of perimeter strip 32. Restated, the presence of dimples 38 increases the resistance of strip 32 to bending in response to a force component directed along the length of the perimeter strip. Additionally, as may be seen in the case of fuel rod 14", dimples 38 function as stops or arches against which the fuel rod will be urged by the internal spring integral with the spring member 22. The dimples 38 must be provided above and below each of perimeter strip "windows" 34. Additional pairs of dimples 39 may also be provided in the perimeter strip sectors which have the integral springs 36 formed therein. In the interest of facilitating understanding of the drawing, the dimples 39 have not been shown in FIG. 2. When employed, dimples 39 will not extend into the fuel assembly sector as far as the fuel rod contacting springs 36 and the dimples 39 will thus function as back-up arches to prevent the elastic limit of springs 36 from being exceeded should the fuel assembly be subjected to vibration in excess of that encountered during normal operation as a result of coolant flow. The pairs of dimples 39, if provided, will also enhance the rigidity of perimeter strip 32. The perimeter strips 32 of the improved spacer grid of FIGS. 2-4 are also provided, as may best be seen from a joint consideration of FIGS. 3 and 4, with inwardly extending upper and lower edge portions; the inwardly extending edge portions flaring inwardly from bend lines 40. The presence of the bent over edge portions of perimeter strip 32, which for the purposes to be described below are serrated, increases the section modulus of the perimeter strip and results in the perimeter strip functioning as a beam characterized by increased resistance to bending in response to a longitudinal force component when compared to a flat perimeter strip or a strip provided with a plurality of irregularities. The serrations; i.e., the valleys between the teeth 42; start outwardly with respect to bend lines 40. The valleys of the serrated upper and lower edges of perimeter strip 32 function as lead-in and lead-out cuts or slots which facilitate insertion of the fuel rods 14; the bases of the slots or cuts being aligned with the center of the windows 34 and springs 36 in the perimeter strip 32. The teeth 42 of the serrated upper and lower perimeter strip edges function as anti-hang-up tabs; these tabs or teeth 42 preventing the hanging or interference between adjacent fuel assemblies during refueling. Although not absolutely essential for operation, it may be desirable to include, in spacer grid 16, back-up arches 44 formed in the spring members 20 and 22. The back-up arches 44, which will be provided in pairs, are shown in FIG. 2 as being provided only in the outer rows of fuel rod receiving grid sectors. Thus, in FIG. 2, the back-up arches are formed in spring members 20' and 22. It will be understood that pairs of back-up arches can be provided for aech internal spacer grid spring. The back-up arches extend into the spacer grid sectors above and below the springs 26 in the same direction as but for a shorter distance than springs 26. As described above in the discussion of dimples 38 and 39 in the perimeter strip 32, the back-up arches 44 prevent compression of the internal springs to a point where the elastic limit thereof would be exceeded. To summarize the significant features of the spacer grid of FIGS. 2-4, the perimeter strip 32 is, when compared to the prior art, wider and contains stiffening dimples. The perimeter strip 32 of the spacer grid is also characterized by inwardly angled upper and lower edge portions which also add to the stiffness of the strip. The connection between the perimeter strip and the internal spring members is defined by a weld seam of increased length when compared to prior art spacer grids and the serrated upper and lower edges of the perimeter strip define anti-hang-up tabs and lead-in and lead-out cuts. Also, pairs of back-up arches may be associated with some or all of the internal springs of the spacer grid to prevent the elastic limit of the internal springs from being exceeded. Tests have shown that the spacer grid of FIGS. 2-4 exhibits an improvement in impact strength by a factor in excess of 2 and this increase in impact strength has been achieved with essentially no perturbation in enrichment or added resistance to coolant flow; i.e., no increase in pressure drop across the fuel assembly; and with little change in the cost of fabrication of the grid. Referring now to FIGS. 5 and 6, the seismic grid 18 is preferably comprised of stainless steel and is designed for optimum strength with minimum material. Stainless steel is a high parasitic material which has a strong influence on fuel enrichment and, accordingly, the amount of steel present in seismic grid 18 is limited to an amount commensurate with the requisite grid strength. Seismic grid 18 will be employed in fuel assembly 10 only in cases where extreme seismic loading would be a possibility. It is also to be noted that, while FIG. 1 depicts a single seismic grid 18 located at the mid point of the length of the fuel assembly, it may in some cases be necessary to employ two additional seismic grids positioned intermediate centrally located grid 18 and the opposite ends of the fuel assembly. The seismic grid 18 reduces lateral deflection of fuel assembly 10 by means of reducing the clearance or gap between adjacent fuel assemblies. Seismic grid 18 thus extends outwardly from the sides of the fuel assembly a slight distance further than the most outwardly disposed portions of the spacer grids 16. This outward extension of seismic grid 18 is shown greatly exaggerated in FIG. 1. Reducing the gap between adjacent fuel assemblies lowers the impact and bending forces which may be generated as a result of seismic loading since the movements of the fuel assembly will be limited by contact between adjacent seismic grids. Through the use of stainless steel, or another metal having equivalent characteristics, the gap between fuel assemblies may be made significantly less than that which must be left between the zircaloy spacer grids, at the beginning of reactor life, because only minimal allowance must be made for irradiation induced growth of the stainless steel. Also, the size of the gap between the seismic grids on adjacent fuel assemblies will not increase at temperature because of differential expansion between the seismic grids and the upper and lower end plates of the fuel assembly; these upper and lower plates typically being comprised of Inconel. Conversely, the gap between the zircaloy spacer grids will increase with temperature. Thus, to summarize, the possibility of severe impact of the fuel assemblies upon each other and upon the wall of the core shroud is eliminated by reducing the spacing between fuel assemblies and between the outer fuel assemblies and the shroud. This reduction in clearance between fuel assemblies, which limits the lateral displacement of the fuel assemblies when subjected to severe vibratory loading such as would accompany a seismic event is permitted by the use of one or more stainless steel seismic grids. The seismic grid or grids, as may be clearly seen from FIG. 5, do not replace a standard zircaloy spacer grid and do not support the fuel rods. Thus, seismic grid 18 will serve only as an amplitude limiting device in reducing the possible lateral deflection of the fuel assemblies to thereby reduce spacer grid impact and the possible bending of the fuel assembly guide tubes. Referring jointly to FIGS. 5 and 6, the seismic grid 18 of the present invention includes a perimeter strip 50. Perimeter strip 50 need not be continuous around the entire periphery of the seismic grid. Thus, in the interest of reducing the amount of stainless steel employed, perimeter strip 50 may only extend along portions of each side of the seismic grid; such portions extending from the mid point of each side toward the corners of the grid. Also in the interest of reducing the amount of steel, and additionally in the interest of enhancing coolant flow and imposing minimum resistance to such flow, the perimeter strip 50 is provided with "windows" which are preferably in registration with each of the fuel rods 14 in the outer rows of the fuel assembly. The resistance of the perimeter strips to distortion when subjected to a longitudinal force component is enhanced by the formation of dimples 54 above and below each of the windows 52 in perimeter strip 50. Dimples 54, which permit the reduction of the width of strip 50, also serve to limit the motion of the individual fuel rods 14 and thus are equivalent to the dimples 40 of the spacer grid of FIG. 3. As noted above, dimples 54 are normally not in contact with the fuel rods 14. Perimeter strip 50 may also be further reduced in size, or further rigidized, by bending over the upper and lower edges thereof in the same manner as described above with respect to the spacer grid perimeter strip 32. The seismic grid perimeter strip 50 is also provided with serrated upper and lower edges with the teeth of the serrations being bent inwardly to define anti-hang-up tabs. Preferably, as shown in FIG. 6, with the exception of the corner regions of the grid, the serration in the edges of the seismic grid perimeter strip 50 provides anti-hang-up tabs only in the regions where a seismic grid internal member is joined to the perimeter strip. Since the seismic grid, as clearly seen from FIG. 5, employs fewer internal members than the spacer grid of FIGS. 2-4, the valleys between the serrations in the edges of perimeter strip 50 may be of larger dimension thus further reducing the amount of steel employed. It is to be noted that, should the perimeter strip 50 extend around the corners of the fuel assembly as shown in FIGS. 5 and 6, the frequency of anti-hang-up tabs will be increased in the perimeter strip in the corner segments of the seismic grid. As noted above, the internal members of seismic grid 18 define a grid structure having larger sectors when compared to the spacer grid wherein a sector is provided for each fuel rod. As shown in FIG. 5, four fuel rods pass through each sector of seismic grid 18. The internal grid defining members, such as members 58 and 60, are welded to each other at their points of intersection and are also joined to perimeter strip 50 by means of a butt or a seam weld. Internal grid members 58 and 60 are, like the perimeter strip 50, provided with pairs of dimples, the dimples of each pair being vertically displaced, which limit the motion of fuel rods 14 but which normally do not contact the fuel rods. The seismic grid 18 is mounted on the fuel assembly by a means of being attached to the guide tubes 12. The mounting of the seismic grid is accomplished by providing, in the grid, tube segments 62 which may be comprised of either zircaloy or stainless steel. When comprised of zircaloy, the tube segments 62 will be inserted in the grid and thereafter expanded to mechanically lock the elements comprised of dissimilar metals together. When comprised of steel, the tube segments 62 will be welded to the grid internal members. The tube segments 62 will slide over the guide tubes and will be joined to the exterior thereof by any appropriate method. Since the guide tubes will customarily be comprised of zircaloy, if tube segments 62 are steel the guide tubes will be expanded, for example to form outwardly extending dimples, so as to be mechanically locked to the tube segments 62. While a preferred embodiment has been shown and described, various modifications and substitutions may be made thereto without departing from the spirit and scope of the invention. Accordingly, it is to be understood that the present invention has been described by way of illustration and not limitation.