Patent Number: 046559957
Section: description

DETAILED DESCRIPTION OF THE INVENTION Reference will now be made in detail to the presently preferred embodiment of the invention, an example of which is illustrated in the accompanying drawings. Turning first to FIG. 1 there is illustrated a fuel assembly 100. The fuel assembly comprises a plurality of elongated fuel rods 102 which are further described below and which are spaced in a lateral array. The fuel rods 102 are disposed between substantially identical top and bottom tie plates 104 and 106 respectively and are retained in lateral array by one or more spacer grids 108. The precise number and configuration of the spacer grids 108 is selected in accordance with the particular thermal, hydraulic, nuclear, and mechanical properties of the fuel assembly 100. The fuel assembly 100 includes an elongated, flow impervious, outer fow channel 110 that is preferably formed from an alloy of zirconium commonly known as Zircaloy, that extends substantially along the entire length of the fuel assembly 100 and that is structurally connected to a lower nozzle assembly or base 112. Preferably, the base 112 is formed from reactor grade stainless steel. Preferably, channel 110 is connected to the base 112 by what may be referred to as tongue and groove connection formed by the receipt of a lower end 114 of the flow channel against an axially or vertically extending elongated portion 116 with reduced lateral dimensions that extend about the periphery of the base 112. The lower end 114 of the flow channel 110 also is designed to rest against a laterally or radially outwardly extending shoulder 118 that is formed about the periphery of the base 112. Once in position on the shoulder 118 and against the connecting portion 116, the lower end 114 of the flow channel 110 may be secured to the base 112 by the receipt of the plurality of threaded retaining screws 120 through a plurality of apertures 122 formed in the lower end 114 of the flow channel 110 for threaded engagement with correspondingly elongated threaded apertures 124 formed through the connecting portion 116 of the base 112. Preferably, the screws 120 are counter sunk into the lower end 114 of the flow channel 110 to present a smooth surface thereon. In this manner, each of the four sides of the lower end 114 of the flow channel 110 may be structurally interconnected with the base 112. As will be understood by the artisan, the base 112 is adapted to be inserted into a core plate hole (not illustrated) in the reactor core. Guide bars 125 may be provided for guiding the fuel assemblies into the core plate holes. In a preferred embodiment of the invention, each fuel assembly 100 comprises a fuel bundle which includes a plurality of sixty four fuel rods arranged in an 8.times.8 array. Each of the fuel rods 102 include an end plug 126 at each end thereof. In accordance with an important feature of the present invention, the top and bottom tie plates 104 and 106 are substantially identical and may be fabricated as a connected series of thin metal bars or strips 128 which are formed by an convenient means such as casting or machining. At each of the fuel rod lattice positions, a small cylinder having cylindrical aperture 130 is formed to receive with a slip fit an elongated vertical extension 132 of the end plug 126 of the fuel rod 102. The slip between the top and bottom tie plates 104 and 106 and the fuel rods 102 provides lateral restraint for the fuel rods but permits relative axial movement therebetween. A plurality of elongated compression springs 134 are disposed over the vertical extensions 132 of upper end plugs 100 and bear against the lower surface of the top tie plate 104 to maintain the fuel rods 102 seated in the lower tie plate 106 and to support the upper tie plate 104. Preferably, at least one fuel rod in each fuel bundle is a tie rod 136 that is used to interconnect as a unit the upper tie plate 104, the lower tie plate 106, and the plurality of fuel rods 102. Tie rod 136 may include a threaded elongated vertical extension 138 as a portion of its upper and lower end plugs 126. The extension 138 will preferably pass through an aperture 140 in the tie plates 104 and 106 for receipt of a threaded locking or retaining nut 142. As best seen in FIG. 2, the tie plates 104 and 106 comprise an egg-crate grid type structure which allows fuel assembly coolant flow to pass therethrough. In accordance with a further feature of the present invention the flow channel 110 is provided with an integrally formed lifting slot 144 that facilitates handling of the fuel assembly 100. Turning again to FIG. 1, the fuel assembly 100 is further provided with bumpers 146 for contacting, when necessary, similarly configured bumpers on adjacent fuel assemblies to insure a minimum spacing and fluid gap between adjacent fuel assemblies. In addition, a pillar 148 may be provided for supporting a channel spring assembly 150 and an elongated, threaded, spring assembly retaining bolt 152. The spring assembly 150 may comprise a bi-directional leaf spring which is designed to contact corresponding leaf springs on adjacent fuel assemblies to maintain spacing between adjacent fuel assemblies and to transmit loads from one fuel assembly to another. Reference may be had to U.S. Pat. No. Re 27,173 for details with regard to an exemplary channel spring assembly. In order to accommodate the radially outwardly projecting portions of the bumpers 146 and of the spring assembly 150, the upper end of the flow channel 110 is advantageously provided with a plurality of appropriately configured cutouts 154. The base 112 includes an inlet nozzle 156 having an inlet opening or aperture 158 for the receipt of coolant core moderator flow. The nozzle 156 may be eccentrically formed during the casting of the base 112 or subsequent thereto by machining the material of the base 112 that forms the nozzle 156 to vary the thickness of the nozzle 156 about its periphery. Thus, the fuel assemblies 100 having larger outer lateral dimensions may be used to replace spent fuel assemblies having small outer lateral dimensions during the refueling of a nuclear reactor core. Disposed above the nozzle 156 is an opening or plenum region 160 for the receipt of the fow of coolant or moderator and for the distribution thereof to an orifice plate 162 which evenly distributes the incoming moderator or coolant for the fuel assembly and also functions to adjust the fuel assembly pressure drop to render it approximately equal to the pressure drop of other fuel assemblies in the core into which the new fuel is being inserted. Where the tie plates 104 and 106 are designed to provide a large enough pressure drop, the orifice plate 162 may be omitted. As alluded to above, each of fuel rods 102 comprises a cladding tube 164 and a plurality of fuel pellets 166 stacked in a column. At one end of the fuel rod 102 a fission gas plenum 168 is formed. A retaining spring 170 is provided to maintain the fuel pellets 166 in a closely stacked column and to maintain the gas plenum 168. A zirconium oxide pellet 172 or the like is used to space the retaining spring 170 from the fuel pellets 166. A crimp 171 may be formed in the cladding 164 to prevent fuel pellets from shifting downward into the fission gas plenums 168 in the event of failure of the retaining spring 170. As will be further explained below, the gas plenums 168 of alternate fuel rods 102 are preferably disposed at the bottom of the fuel bundle while the gas plenums of the intervening alternate fuel rods are disposed at the top of the fuel bundle. Such a configuration enhances the power distribution in the fuel assembly and reduces the fuel cycle costs. The orifice plate 162 is supported in the fuel assembly by cantilever springs 174 which seat against a shoulder 176 formed in the inside circumference of the base 112. The cantilever springs 174 are preferably fastened to the orifice plate by fastening means such as rivets or bolts 178 to hold the orifice plate from moving as a result of fluid pressure against its bottom surface. The orifice plate 162 is futher provided with upstanding sidewalls 180 which generally conform to an upper portion 182 of the base 112. The sidewalls 180 terminate at a lip or flange 184 which cooperates with a shoulder 186 on the inside circumference of the upper portion 182 of the base 112. During normal operation, a space 188 is maintained between the lip 184 and the shoulder 186. The tie plates are provided with tie plate legs 190 which are preferably formed with integral fuel bundle lifting slots 192. The bottom tie plate 106 of the fuel bundle engages the upper portion of 182 of the base 112 at a shoulder 194 which is preferably inclined to mate with a complimentary inclined surface 196 on the upper portion 182 of the base 112. The tie plate leg 190 is also preferably provided with a shoulder 198 which engages the lip 184 of the sidewalls 180. As alluded to above, the upper and lower tie plates are identical and both have similar tie plate legs 190 for engaging the base 112 in orifice plate 162. Preferably, the flat protruding surfaces 200 of the tie plate legs 190 are dimensioned to fit snugly within the flow channel 110. As should now be apparent, the peripheral and support components of the fuel assembly, such as the flow channel 110, the base 112, and the orifice plate 162 form a relatively permanent external envelope or "can" for the fuel bundle 202 which mainly comprises the fuel rods 102, the top and bottom tie plates 104 and 106 respectively, and the spacer grids 108. The fuel bundles 202 are designed to be inserted into the "can" by means of the complimentary geometry between the base 122, orifice plate 162, and the tie plate legs 190. Since the top and bottom tie plates 104 and 106 are identical, the fuel bundle can be raised and lowered independently of the "can" by means of the fuel bundle lifting slots 192. In this manner, after the fuel assembly has been inserted into a reactor core and has been operating for a period of time, it can be raised by the lifting slots 192, inverted, and then reinserted into "can" for an additional period of time in order to achieve more complete fuel burn up. Whenever the entire fuel assembly needs to be handled, resort can be had to the fuel assembly lifting slots 144. Thus, the present invention takes advantage of the reactivity increase achievable in a BWR core when a partially burned fuel assembly is inverted. As explained above, this increase is produced because the top of the assembly is less burned than the bottom as a result of the void distribution in a BWR which skews the power and burn up to the bottom of the core. Thus, inverting the assembly places less burned fuel at the bottom of the core where the water density is higher. This acts to increase the reactivity and consequently lower the fuel cycle costs. Two significant design features of the present invention facilitate inverting the assembly. The first feature is that the fuel bundle is disposed in a can or external envelope and that the fuel bundle is provided with mirror symmetrical bottom and top tie plates which permit inversion of the bundle without having to move or change the bottom nozzle 112, the flow channel 110 or other related structures. The essentially identical top and bottom tie plates produce a fuel bundle 202 within the fuel assembly 100 which is the same from a mechanical and hydraulic standpoint whether it is inverted or not. The second feature is that of placing every other fission gas plenum 168 at the bottom of the core in order to produce a fuel bundle which is axially symmetrical from the nuclear point of view. The active fuel length and position in the core of the bundle is the same whether the fuel bundle is inverted or not. In addition, placing every other fission gas plenum at the bottom increases the H/U ratio at the ends of the core. This functions to increase the reactivity because a BWR operates under an undermoderated condition especially at the top of the core. Conversely, at cold conditions the ends of the core are overmoderated. This will reduce reactivity and in some cores may permit use of fuel assemblies according the present invention without any control rod length change. Of course, for optimization reasons, fuel rod arrangements other than the alternating fission gas plenum arrangement described above may be employed. Inversion of the fuel bundle is estimated to provide about a two or three percent fuel cycle cost benefit in BWRs. The economic benefit of disposing approximately half of the fission gas plenums at the bottom of the core is also estimated to provide a two to three percent fuel cycle cost benefit for a BWR reactor. The present invention is therefore estimated to provide a total benefit of about five percent decrease in fuel cycle cost over conventional fuel assemblies. The present invention provides an additional advantage in that it is designed to be compatible with many other BWR fuel assemblies and can be easily integrated into a BWR core containing other fuel assembly designs during refueling operations. The foregoing description of a preferred embodiment of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above teachings. The embodiment was chosen and described in order to best explain the principles of the invention and its practical application to thereby enable others skilled in the art to best utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims appended herreto.