Patent Number: 040509869
Section: description

The reactor shown in the drawings includes a generally cylindrical pressure vessel 21 (FIGS. 1A and B) closed at the bottom by a bell 23 which bounds an inlet plenum 25. The vessel 21 has a plurality of inlet nozzles 27 above the bell 23 through which a heat-transfer or cooling fluid such as liquid sodium is supplied to the plenum 25 under pressure. The vessel 21 has an outlet plenum 29 from which the hot fluid is derived through a plurality of outlet nozzles 31. The vessel is provided with a thermal liner 33 encircling the outlet plenum 29 and the regions above and below the outlet plenum. The permissible upper level and the minumum safe lower level of the fluid are indicated in FIGS. 1A and 1B by wavy lines 35 and 37 respectively. Above the surface (37) of the fluid there is an inert gas such as argon at low positive differential gauge pressure above atmospheric pressure (about 2 or 3 inches of water). At the top the vessel 21 is closed by a head 41. The head 41 has a stationary outer ring 43 which is bolted to a flange 45 of the vessel 21. The joint of the ring 43 and flange 45 is sealed internally (of the bolts not shown) by an omega seal 47. The vessel 21 is supported on a support ledge 49 of a concrete containment. The ring 43 is bolted to the ledge 49. The head 41 has a plurality of rotating plugs 51, 53, 55 which are sealed to prevent leakage of the reactor cover gas to the containment building atmosphere. Plug 51, of largest diameter, is coaxial with the vessel. The stationary ring 43 supports the plug 51 through an annular riser 57 and a bearing 59 (FIG. 1). Plug 53, of intermediate diameter, and plug 55, of smallest diameter, are eccentric to the axis of the vessel 21. Plug 51 supports plug 53 through an annular riser 61 and a bearing 63 and plug 53 supports plug 55 through an annular riser 65 and a bearing 67. The risers 57, 61 and 65 are cylindrical extensions above the periphery of the stationary 43, the plug 51 and the plug 53. The risers 57, 61, 65 serve to mount the bearings 59, 63, 67, pressure seals (not shown) for the plugs and part of the gearing (not shown) for driving the plugs. The rotating plugs 51, 53, 55 position the fuel and control handling equipment over all core assembly locations. The plug 55 supports an in-vessel transfer machine port 71 eccentrically. The plug 51 supports the ex-vessel transfer machine port 73 eccentrally. The plug 53 supports columns 75 which support the upper internals 77, the primary control-rod assembly drive mechanisms 81, the auxiliary control-rod drive mechanism 83, and one or more sealed serveillance ports 85. By rotating the plugs 51, 53, 55, the in-vessel transfer machine port 71 can be positioned over the various components within the vessel as shown by the arrows 87 (FIG. 2) and over the ex-vessel transfer machine port 73 as shown by the arrows 89. During the rotation of plug 53, the column 75, the control-assembly drives 81 and 83 and the port 85 are rotated as shown by the arrows 91. When the plugs 51, 53, 55 are to be rotated, the upper internals 77 are raised and the drives 81 and 83 are disconnected from the driven parts. Jacks (not shown) are provided for raising the upper internals. Typically, the in-vessel transfer machine port 81 is positioned over the fuel transfer ports after the plugs 51, 53, 55 are each rotated through 180.degree.. Within the vessel 21 there are, in addition to the upper internals 77, the core 93 and the lower internals 95. The core includes an inner zone 101 of fuel assemblies 103 (typically 108 in number) of lower enrichment (typically 18.7%, labeled 1C) and an outer zone 105 of fuel assemblies 107 (typically 90) of higher enrichment (typically 27.1%, labeled 0C). Around the zone 105 there is a radial blanket 109 of radial blanket assemblies 111 (typically 150, labeled RB). Around the zone 109 there is a zone 113 of removable radial shielding assemblies 115 labeled RS. About the removable shield 115 there is a fixed shield 116. The fixed shield is enclosed by a core barrel 118. Core restraint former rings 120 (FIGS. 20, 21) are provided spaced along the core 93 for restraining deformation of the core. The former rings 120 are formed in sections of arcs and are secured together by pins 452 between rings 454 and 456. The keyways 280 are secured to spacers 458 (FIG. 19) welded to the upper rings 454. The keyways 280 are in the form of slots into which the keys 278 slide. Since there are three keys and keyway pairs the upper internals 77 can only be moved vertically. A thermal shield 460 is provided over the upper end of the core barrel. This shield 460 holds in place shear rings 462 in slots on the core barrel. The shear rings 462 prevent the assembly 456, 120, 454 from moving vertically. The rings 454 have keys 464 which engage slots (not shown(in the core barrel. The inner zone 101 includes, in addition to the fuel assemblies, primary control-rod assemblies 117 (typically 15 in number, labeled PC) and secondary control-rod assemblies 119 (typically 4 in number, labeled SC). The control-rod assembly drives 81 and 83 can be set so that the control-rod assemblies 117 are either completely removed or positioned at any axial position within the core 93. The lower and higher enrichments in the zones 101 and 105 promote uniform power generation across the core 93. Typically each fuel-rod assembly contains 217 fuel rods. The fuel rod bundle or assembly 130 (FIGS. 4 and 5) is contained within a thin-walled hexagonal duct 121 which serves to guide the heat-transfer fluid through the assembly and to protect the bundle during handling. The fuel pins have a plenum 122 above the fuel and axial fertile blanket sections for containing gaseous fission products. There is a core restraint load pad 124 intermediate the ends of the duct 121. The fuel rods 132 in bundle or assembly 130 are wrapped in wires 134 and are thus spaced by the wires. A rod attachment facility (not shown) is provided in the lower part of the duct 121 to provide for uniform flow distribution and axial restraint of the rods. The attachment sub-assembly rails mate with a keyhold slot in the bottom end-cap 123 of the duct in a discriminatory manner to prevent mixing of different enrichments. The duct 121 has an inlet nozzle 125 and an outlet nozzle 127. The inlet nozzle has lateral openings 129 through which fluid is admitted to the duct 121. Below this opening there is a circumferential slot 131 for a piston ring which seals the region below the opening 129 against fluid flow when the assembly is inserted in a socket. The duct may contain orifice plates (not shown) for controlling the flow of the fluid. At the end of inlet nozzle 125, there is a discrimination port 133 which assures that the fuel assembly 103 or 107 cannot be inserted in a control-assembly position. Each outlet nozzle 127 directs fluid flow through an aligned openin 136 (FIGS. 5A, 5B) in a holddown grid 138 of an associated outlet module 140 and thence through a chimney 142 to the outlet plenum 29. The grid 138, outlet module 140 and chimney constitute part of the upper internals 77. The primary function of the radial-blanket assemblies 111 is to convert fertile material (typically depleted U-238) into fissile material (typically Pu) by neutron capture. A secondary function of assemblies 111 is to absorb and reflect neutrons from the fuel assemblies 103 and 107, thus to shield the structures outside of the blanket. The radial blanket assemblies 111 also generate energy. An operational feature of the radial blanket 109 is the facility for shuffling of the assemblies 111 from positions adjacent zone 105 to peripheral positions. Fresh fertile assemblies in the inner rows of the radial blanket 109 generate little energy because of the absence of fissionable material. As the fissionable material increases the generated energy increases. By moving the assemblies 111 to outer rows of blanket 109, the raising of the cladding to excessive temperatures beyond design limits is avoided. Shuffling of radial assemblies equalizes the energy generated in the radial blanket 109 and reduces radial temperature gradients. Typically shuffling of the assemblies 111 is performed annually during reflueling. The control-rod assemblies 117 and 119, the blanket assemblies 111 and radial-shielding assemblies 115 have ducts 137, 139, 141 of the same countour as the ducts 21 with core restraint load pads 336, 338, 340 and inlet nozzles 143, 145 and 147 as described above. The core 93 includes a surveillance specimen 149 of adjacent the blanket 109 and another specimen 151 adjacent the barrel 118. The surveillance specimen 151 is encircled by flow guides 153 and 155. There are also fuel-transfer and storage containers 157 adjacent the barrel 118 and also encircled by flow guide 155. The upper internals 77 function to: 1. Provide a backup mechanical hold-down for the core 93 in the event of a malfunction of the core hydraulic hold-down system. PA1 2. Position, protect, guide and support the core instrumentation. PA1 3. Assure alignment of the control-assembly system under steady state and seismic conditions and protect the control-assembly drive line 179 from flow induced vibration. PA1 4. Control flow in the vessel outlet plenum 29 to minimize flow stratification during a scram transient. PA1 1. Low thermal inertia. The upper internals is relatively insensitive to differences in bulk temperature of the members 75, 136, 138, 140, 142 which make it up. PA1 2. The mechanical attachment of the top end of the chimney 142, which is composed of highly refractory nickel-chromium alloy, to the adjacent structure which is predominately composed of stainless steel. PA1 3. The peripheral seal. This is a low-pressure hydraulic seal which forces or directs the bulk of the coolant up the chimneys 142 to the outlet plenum 29 and in addition acts as a back-up core bundling device. The unique features of the upper internals 77 apparatus according to this invention are: The main body of the load-bearing structure of the upper internals 77 is a weldment (FIGS. 6, 7, 8) of stainless steel (316). This weldment includes the columns 75 and a plurality of pairs 161 and 163 of plates, which may be described as sandwich plates, and which include the plates 165, 167, 169, 171. Stub tubes 175 are welded to the plates 165 and 167 and 169 and 171 of each pair 161 and 163 by circumferential welds 210 and circumferential butt welds 212 (FIG. 12). The stub tubes 175 serve as shear webs for the pairs of plates 161 and 163. The columns 75 are also welded to the plates 165 to 171. In addition there are ribs 450 between each column 75 and its adjacent stub tubes 175a and 175b. The ribs 450 are welded to the columns 75, the sandwich plates 165 and 167 and 169 and 171 and to the stub tubes. Above the upper plate 165 each column 75 is provided with a liner or sleeve 176 which is welded to an inner shell 178. The inner shell 178 is in abutting sections 178a, 178b, 178c welded around their abutting peripheries. Sections 178a and 178c are forgings while sections 178 and 178b are pipes. The upper section 178a and the lowermost section 178c are welded to the upper plate 165 of pair 161 and to plate 169 of pair 163 by peripheral lateral welds 180 and 182. The plate 167 of the pair 161 is welded to the intermediate section 178b and to the upper section 178a by butt welds 184 and the lower plate 171 is welded to the lower section 178c by a butt weld 186. The plate 169 includes a penetration 190 (FIGS. 7 and 8) for the in-vessel transfer mechanism 71. The column 75, including the sleeves 176 and the shell 178, the plates 165, 167, 169 and 171 and the studs 175 are composed of stainless steel (typically 316). The upper internals 77 includes a plurality of outlet modules 140 (FIGS. 5A, 5B, 10-18). These modules 140 are composed throughout of highly refractory nickel-chromium-iron alloy and are joined mechanically to the weldment 75-161-163-175. Each module 140 includes the grid 138, the flow collector 192, and the chimney 142. Each module 140 serves to direct the coolant streams from a plurality of core-component assemblies 103, 107, 117 and 119 into its associated chimney 142. Each grid 138 has the general appearance of an egg crate. FIG. 9 shows the disposition of the grids 138. Typically there are twenty-one grids 138, each receiving the coolant from nine core-component assemblies, ten grids each receiving the coolant from sixteen assemblies, and four grids each receiving the coolant from twelve assemblies; thirty-five grids in all. The outlet modules 140 and their chimneys are of different dimensions (FIG. 6). The chimneys 142a for modules including control assemblies have the greatest diamter, (about 10 inches inside diameter). The chimneys 142b for modules including 12 and 16 assemblies have intermediate diameters (about 71/2 inches inside diameter) and the chimneys 142c for the remaining modules have the smallest diameter 16 5/8 inches. The effluent from the radial shielding zone 113 is not channeled. It is emphasized that each grid 138 channels streams of widely different temperature into its associated chimney 142. Typically the central grid 138a channels relatively cool effluent from control rod 117a and the relatively hot effluent from fuel rods 103a. Another grid 138b channels relatively cool effluent from control rod 117b, hot fluid from the lowerenriched fuel rod 103b and still hotter fluid from the more highly enriched control rod 107b. Peripheral grid 138c channels fluid from fuel rods 107c and cooler fluid from fertile rods 111c. The effluent through the shielding rods 115 is cool and requires no channeling. The outlet modules 140 including the associated chimneys 142 are composed of highly refractory nickel-chromium-iron alloy (typical INCONEL-718). Each module 140 (FIGS. 10-18) includes in addition to the grid 138 a transition member 200 to effect the transition between the diamond configuration of the grid and the circularly-cylindrical configuration of the chimney 142. The grid 138 and the transition member 200 are enclosed in a shell 208 (of INCONEL-718) which is secured to these members by welding. At the top the transition member 200 has a shoulder 202 which extends along the lower plate 171. Rotation of the transition member 200 relative to the weldment 75-161-163-175 is prevented by a pin 204 which extends from plate 171 and engages member 200. The grid 138 and the transition member 200 also have projections 240 and 242 which engage the shell 208. At the top the transition member 200 also has a lip 206 to which the chimney 142 is welded. The chimney 142 is encircled by, or housed in, the stub tubes 175 with which it is coaxial and which are composed of stainless steel. Since this alloy is not weld compatible with the refractory alloy, it is necessary that the chimney 142 by mechanically secured to the weldment 75-161-163-175. To accomplish this urpose a circularly-cylindrical extension 214 (FIG. 12) of nickel-chromium-iron alloy (typically INCONEL-600) is welded to the end of the upper stub 175. This alloy is weld compatible with the stainless steel of the stub 175 and has about the same thermal coefficient of expansion as the refractory nickel-chromium-iron alloy of the chimney 142. The extension 214 is a close tolerance fit to the chimney and because the thermal coefficients of expansion are nearly the same, this fit is maintained in the face of fluctuations in temperature and flow-induced vibrations are suppressed. The extension 214 is welded to another extension 216 of stainless steel which is itself welded to the plate 165. The purpose of this extension 216 is to space the extension 214 sufficiently from plate 165 to reduce local bending moments at operating temperatures to acceptable levels. The extension 214 has a ledge 218 at the top. The ledge 218 engages the chimney 142 in a shoulder 220. Above the extension 214 there is a key 222, which is in the form of a split ring, and which tightly engages the chimney near its top in a groove. The key 222 has a ledge 224 penetrating into the groove. The key 222 is composed of the same alloy (INCONEL718) and is held by a locking band 226 of the same alloy. A thermal liner 228 also of INCONEL 718 is held in place by the locking band 226. The mechanical joint 214-222-142 not only carries lateral loads but it also carries vertical loads both up and down. Up loads are carried by the ledge 218 of extension 216 and down loads by the ledge 224 of the key 222. A lateral load pad is also provided between the lower stub 175 and the chimney 142. In this case an extension 230 of stainless steel is welded to the plate 169 and an extension 232 of the nickel-chromium-iron alloy which is weld compatible with the stainless steel and of the same thermal cofficient of expansion as the refactory alloy, is welded to the extension 230. The extension 232 is a close tolerance fit to the chimney 142. Each opening 136 in the grid 138 has a socket for receiving the outlet nozzle (127 of duct 121 for the fuel rod assemblies) of the duct whose effluent is channeled through the opening (FIG. 10). FIG. 12 shows an opening 136 which receives the outlet nozzle 244 of the outer duct 260 of a control assembly. The control assembly also has an inner duct (not shown) which is movable through the outer duct. In this case the socket 246 is double ended. The socket 246 is a shell of the refractory nickel-chromium-iron alloy wleded to the adjacent walls 248 of the grid 138. The shell 246 has a lower opening 250 to receive the nozzle 244. The shell also has an upper tapered opening 252 to receive the end 254 of a shell to which a flow tube 177 is attached. The end 256 of the flow tube 177 of seated in the rim of the shell 246. The shroud 179 (FIG. 1A) is attached to the flow tube 177. The shell 254 and the flow tube 177 are composed of the highly refractory alloy. The inner duct (not shown) of the control assembly is connected to a control assembly drive line 117 (FIG. 5A) and is movable along flow tube 177 and shroud 179. The flow tube is aligned or centered in the chimney 142 by coaxial rings 262 and 264 and spider 266 all composed of the refractor nickel-chromium-iron alloy. The modules 140 are enclosed in a shroud 135 (FIGS. 7, 8) composed of stainless steel (316). The shroud 135 is formed of a top plate coextensive with the plate 171 of the pair 163, a bottom annular plate 270 and inner and outer annular plates 272 and 274. The plate 171 whose extension serves as top plate is connected to the upper plate 169 of sandwich 163 by an annular plate 276 of the refractory alloy which is welded to plates 169 and 171. The keys 278 of stainless steel (316) are secured at positions spaced about 120.degree. around the periphery of the shroud 135 between the top plate 171 and the bottom plate 270. Each key 278 engages a keyway 280 secured to the assembly 456, 120, 454 which is keyed to the core barrel 118 (FIGS. 18, 19, 20, 21 and the core). The upper internals 77 is thus firmly supported through the columns 75 between and by the head plate 41 and the core barrel 118. In FIG. 1 a fragmentary section of the shroud 135 is shown in broken lines. The core-component assemblies extend into the shroud. A peripheral seal 282 extends around the periphery of the core 93 between the core outlet and the shroud 135. The seal 282 includes a plurality of abutting blocks 284 which extend over the second and third rows, radially outwardly, of the removable shielding assemblies 115 (seeFIG. 18). The seal blocks 284 are secured to the bottom plate 270 of the shroud 135. The lower internals 95 (FIG. 1B) is described in detail in the Pennell and Rylatt applications. The internals 95 include a plate 191 in the form of an inverted truncated cone which is welded integrally with the vessel 21. The core barrel 118 is welded to the periphery of the horizontal plate 193 of this support. A liner 203 (FIGS. 1B) is slidably mounted in openings in the plate 193. The liner is of generally hollow cylindrical form. From the bottom of the liner 203 a flow-distribution and blockage-prevention disc 205 is suspended into the inlet plenum 25. The liner 203 is suspended from the top of plate 193 by a collar 207 which is screwed into and welded to the liner 203 and engages the plate 193 along a recess about the corresponding opening in plate 193. An inlet modular unit 221 is removably mounted in each of the liners 203. The modular unit 221 may be of different types and the type which is mounted in a liner 203 in any position of plate 193 depends on the purpose which it is to serve. Some units 221 receive fuel assemblies 103 or 107 or control-rod assemblies 117 or 119 which require high fluidcooling flow; other units receive blanket assemblies 111 or removable shielding assemblies 115. Assemblies 103, 107, 117 or 119 are plugged into the inlet modules 21. Each assembly, as the case may be, has a greater specific gravity than the coolant fluid. Because the pressure above and below the assembly is balanced, the assembly remains in its receptacle under its own weight. The inlet modules 221 are mounted in the liners 203 in seals so that the pressure above and below the modules 221 is balanced. Leakage through the seals is carried to the outer region of the vessel 21 through the vent pipes 275. While a preferred embodiment has been disclosed herein, many modifications thereof are feasible. This invention is not to be restricted except insofar as is necessitated by the spirit of the prior art.