Patent Number: 06163588&
Section: description

DETAILED DESCRIPTION OF THE INVENTION FIG. 1 is a sectional view, with parts cut away, of a nuclear reactor pressure vessel (RPV) 10. RPV 10 has a generally cylindrical shape and is closed at one end by a bottom head 12 and at its other end by a removable top head (not shown). A bottom head petal 14 extends from the bottom head and supports the side wall (not shown) of RPV 10. A cylindrically shaped core shroud 16 surrounds the reactor core (not shown) and is supported by a shroud support 18. An annulus 20 is formed between shroud 16 and the sidewall of RPV 10. A baffle plate 22, which has a ring shape, extends between shroud 16 and bottom head petal 14. Baffle plate 22 includes a plurality of circular openings 24 that house reactor internal pump impellers 26. Reactor internal pump impellers 26 cause the water in RPV 10 to flow through annulus 20. Shroud 16 is formed by a lower shroud section 28 and an upper shroud section 30. A circular core plate ledge 32 is located between upper and lower shroud sections 28 and 30. RPV 10 also includes a core plate 34 coupled to core plate ledge 32. To measure the flow of water through the core, pressure measurements are made above and below core plate 34. The differential pressure can then be translated into a core flow. RPV 10 includes core flow differential pressure lines 36 (one shown). Differential pressure lines 36 enter RPV 10 through bottom head 12 and extend vertically along the inside of shroud 16. Differential pressure lines 36 are coupled to shroud 16 by a plurality of support brackets 38. Particularly, brackets 38 are welded to shroud 16 and differential pressure lines 36 are welded to support brackets 38. Additionally, reactor internal pump flow may be measured by measuring the differential pressure at a location above and below reactor internal pump impellers 26. RPV 10 also includes reactor internal pump flow differential pressure lines 40 (one shown). Differential pressure lines 40 enter RPV 10 through bottom head 12 and extend vertically along the inside of shroud 16. Differential pressure lines 40 also extend horizontally along the inside of shroud 16 to a point above or below reactor internal pump impeller 26. Like differential pressure lines 36, differential lines 40 are coupled to shroud 16 by support brackets 38. Differential pressure lines 36 and 40 are typically of welded construction using pipe and pipe fittings. FIGS. 2, 3, 4, and 5 are partial sectional views of an RPV 50 having a reactor core shroud 52 in accordance with an embodiment of the present invention. RPV 50 includes a bottom head petal 54 having a shroud support flange 56. RPV sidewall 58 extends from bottom head petal 54. Shroud 52 is supported by shroud support flange 56 of bottom head petal 54. Shroud 52 includes a first shroud section 60, typically referred to as the flange, a second shroud section 62, typically referred to as the lower shroud, and a third shroud section 64, typically referred to as the upper shroud. A core plate ledge 66 is located between second and third shroud sections 62 and 64. A core plate 68 is coupled to core plate ledge 66. To measure the core flow, RPV 50 includes modular differential pressure lines 70 (FIG. 2) and 72 (FIG. 3). Referring to FIG. 2, differential pressure line 70 includes first, second, third, and fourth pressure line sections 74, 76, 78, and 80. First pressure line section 74 is defined by a bore 82 extending from an outer surface 84 of bottom head petal 54 to an outer surface 86 of shroud support flange 56. Second pressure line section 76 is defined by a first bore 88 extending from a flange mating surface 90 of first shroud section 60 and a second bore 92 extending substantially perpendicularly from an end 94 of first bore 88 to an inside surface 96 of shroud 52. Second pressure line section 76 is configured to couple to first pressure line section 74. Third pressure line section 78 is defined by a pipe 98 extending toward core plate 68 along inner surface 96 of shroud 52. Pipe 98 is coupled to shroud 52 by support brackets 100. Third pressure line section 78 is configured to couple to second pressure line section 76 and fourth pressure line section 80. Fourth pressure line section 80 is defined by a first bore 102 extending into second shroud section 62, a second bore 104 extending substantially perpendicularly from an end 106 of first bore 102 through second shroud section 62, through core plate ledge 66, and into third shroud section 64, and a third bore 108 extending substantially perpendicularly from an end 110 of second bore 104 to an inside surface 112 of third shroud section 64. Referring to FIG. 3, differential pressure line 72 includes first, second, and third pressure line sections 114, 116, and 118. First pressure line section 114 is defined by a bore 120 extending from outer surface 84 of bottom head petal 54 to outer surface 86 of shroud support flange 56. Second pressure line section 116 is defined by a first bore 122 extending from flange mating surface 90 of first shroud section 60 and a second bore 124 extending substantially perpendicularly from an end 126 of first bore 122 to inside surface 96 of shroud 52. Second pressure line section 116 is configured to couple to first pressure line section 114. Third pressure line section 118 is defined by a pipe 126 extending toward core plate 68 along inner surface 96 of shroud 52 and terminating below core plate 68. Pipe 126 is coupled to shroud 52 by support brackets 100. To measure the reactor internal pump flow, RPV 50 includes modular differential pressure lines 128 (FIG. 4) and 130 (FIG. 5). Referring, to FIG. 4, differential pressure line 128 includes first and second pressure line sections 132 and 134. First pressure line section 132 is defined by a bore 136 extending from outer surface 84 of bottom head petal 54 to an inner surface 138 of bottom head petal 54. Second pressure line section 134 is defined by a pipe 140 coupled to bore 136 and terminating adjacent shroud support flange 56 opposite: to surface 86. Referring to FIG. 5, differential pressure line 130 includes first, second, third, and fourth pressure line sections 142, 144, 146, and 148. First pressure line section 142 is defined by a bore 150 extending from outer surface 84 of bottom head petal 54 to outer surface 186 of shroud support flange 56. Second pressure line section 144 is defined by a first bore 152 extending from a flange mating surface 90 of first shroud section 60 and a second bore 154 extending substantially perpendicularly from an end 153 of first bore 152 to inside surface 96 of shroud 52. Second pressure line section 144 is configured to couple to first pressure line section 142. Third pressure line section 146 is defined by a pipe 156 extending toward core plate 68 along inner surface 96 of shroud 52. Pipe 156 is coupled to shroud 52 by support brackets 100. Third pressure line section is configured to couple to second pressure line section 144 and fourth pressure line section 148. Fourth pressure line section 148 is defined by a bore 158 extending through second shroud section 62. In operation, modular differential pressure lines 70, 72, 128, and 130 measure the pressure at separate points within the reactor pressure vessel. The pressure differential is an indication of the flow between two points within the reactor. Typically, the core flow is measured by measuring the pressure above and below reactor core plate 68 by differential pressure lines 70 and 72. The flow in the annulus of the reactor may be measured by measuring the pressure above and below the reactor internal pump impellers by differential pressure lines 128 and 130. Because pressure lines 70, 72, 128, and 130 are modular, when a shroud section such as shroud section 60, 62, or 64 is removed for replacement, the modular pressure line sections or portions of those sections that are integral to the shroud section are removed with the shroud section. For example, if shroud section 64 was removed from reactor 50, the portions of integral pressure line section 80 that are associated with shroud section 64 would also be removed, i.e., second bore 104 and third bore 108. No cutting is required to disconnect a pressure line section from the corresponding pressure line section of an adjacent shroud section. The removed shroud section is then replaced with a shroud section that also includes integral pressure lines which re-couple to the pressure lines of an adjacent shroud section without welding. The above described modular differential pressure lines 70, 72, 128, and 130 permit the replacement of shroud sections 60, 62, and 64 without having to cut the differential pressure lines from the shroud. The modular differential pressure lines also permit the installation of a replacement shroud section without having to reinstall the pressure lines by welding the lines to core shroud 52. The modular differential pressure lines also simplify and speed up the process of replacing core shroud 52 in reactor pressure vessel 50. FIGS. 6, 7, 8, and 9 are sectional views of an RPV 200 having a reactor core shroud 202 in accordance with another embodiment of the present invention. RPV 200 includes a bottom head petal 204 having a shroud support flange 206. RPV sidewall 208 extends from bottom head petal 204. Shroud 202 is supported by shroud support flange 206 of bottom head petal 204. Shroud 202 includes a first shroud section 210, typically referred to as the shroud support, a second shroud section 212, typically referred to as the lower shroud, and a third shroud section 214, typically referred to as the upper shroud. A core plate ledge 216 is locate between second and third shroud sections 212 and 214. A core plate 218 is coupled to core plate ledge 216. To measure the core flow, RPV 200 includes modular differential pressure lines 220 (FIG. 6) and 222 (FIG. 7). Referring to FIG. 6, differential pressure line 220 includes first and second pressure line sections 224 and 226. First pressure line section 224 is defined by a bore 228 extending from an outer surface 230 of bottom head petal 204 to an outer surface 232 of shroud support flange 206. Second pressure line section 226 is defined by a first bore 234 extending from a flange mating surface 236 of first shroud section 210 through first shroud section 210, through second shroud section 212, through core plate ledge 216, and into third shroud section 214, and a second bore 238 extending substantially perpendicularly from an end 239 of first bore 234 to an inside surface 240 of shroud 202. Second pressure line section 226 is configured to couple to first pressure line section 224. Referring to FIG. 7, differential pressure line 222 includes first and second pressure line sections 242 and 244. First pressure line section 242 is defined by a bore 246 extending from outer surface 230 of bottom head petal 204 to an outer surface 232 of shroud support flange 206. Second pressure line section 244 is defined by a first bore 248 extending from a flange mating surface 236 of first shroud section 210 through first shroud section 210, through second shroud section 212, and into core plate ledge 216, and a second bore 250 extending substantially perpendicularly from an end 252 of first bore 248 to an inside surface 254 of core plate ledge 216. Second pressure line section 244 is configured to couple to first pressure line section 242. To measure the reactor internal pump flow, RPV 200 includes modular differential pressure lines 256 (FIG. 8) and 258 (FIG. 9). Referring to FIG. 8, differential pressure line 256 includes first and second pressure line sections 260 and 262. First pressure line section 260 is defined by a bore 264 extending from outer surface 230 of bottom head petal 204 to an inner surface 266 of bottom head petal 204. Second pressure line section 262 is defined by a pipe 268 coupled to bore 264 and terminating adjacent shroud support flange 206 and opposite to surface 232. Referring to FIG. 9, differential pressure line 258 includes first, second, third, and fourth pressure line sections 270, 272, 274 and 276. First pressure line section 270 is defined by a bore 278 extending from outer surface 230 of bottom head petal 204 to outer surface 232 of shroud support flange 206. Second pressure line section 272 is defined by a first bore 280 extending from flange mating surface 236 of first shroud section 210, through first shroud section 210 and into second shroud section 212, and a second bore 282 extending substantially perpendicularly from an end 284 of first bore 280 to inside surface 240 of shroud 202. Second pressure line section 272 is configured to couple to first pressure line section 270. Third pressure line section 274 is defined by a pipe 286 extending toward core plate 218 along inner surface 236 of shroud 202. Third pressure line section 274 is configured to couple to second pressure line section 272 and fourth pressure line section 276. Fourth pressure line section 276 is defined by a bore 288 extending through second shroud section 212. From the preceding description of various embodiments of the present invention, it is evident that the objects of the invention are attained. Although the invention has been described and illustrated in detail, it is to be clearly understood that the same is intended by way of illustration and example only and is not to be taken by way of limitation. Accordingly, the spirit and scope of the invention are to be limited only by the terms of the appended claims.