Patent Number: 047524332
Section: description

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is an elevational view, partly in cross-section, of a pressurized water reactor 10 comprising a vessel 12 of generally conventional configuration including an upper dome, or head, 12a, cylindrical sidewalls 12b, and a bottom closure 12c comprising the base of the reactor 10. Within the bottom closure 12c, as schematically indicated, is so-called bottom-mounted intrumentation 14. The lower barrel assembly 16 comprises a generally cylindrical sidewall 17 affixed at its lower and upper ends to respective lower and upper core plates 18 and 19. Fuel rod assemblies 20 are positioned in generally vertically oriented, parallel axial relationship within the lower barrel assembly 16. A neutron reflector and shield 21 is mounted interiorly of the cylindrical sidewalls 17, in conventional fashion. The inner barrel assembly 24 includes a cylindrical sidewall 26 within which is positioned a plurality of rod guides in closely spaced, parallel axial relationship; for simplicity of illustration, only two such rod guides are shown in FIG. 1, namely rod guide 28 housing a cluster of radiation control rods 30 (RCC) and a rod guide 32 housing a cluster of water displacement rods 34 (WDRC). Mounting means 36 and 37 are provided at the respective upper and lower ends of the rod guide 28 and, correspondingly, mounting means 38 and 39 are provided at the respective upper and lower ends of the rod guide 32, the lower end mounting means 37 and 39 mounting the respective rod guides 28 and 32 to the upper core plate 19, and the upper mounting means 36 and 38 mounting the respective rod guides 28 and 32 to a calandria assembly 50. The calandria assembly 50 includes a lower calandria plate 52, an upper calandria plate 54, and a plurality of parallel axial calandria tubes 56 which are positioned in alignment with corresponding apertures in the lower and upper calandria plates 52 and 54 and to which the calandria tubes 56 are mounted at their respective, opposite ends. Calandria extensions 58 project downwardly from the calandria tubes 56 and connect to corresponding mounting means 36 for the upper ends, or tops, of the RCC rod guides 28. The upper end mounting means 38, associated with the WDRC rod guides 32, may be interconnected by flexible linkages to the mounting means 36 of the RCC rod guides 28, in accordance with the invention of the pending application, entitled: "FLEXIBLE ROD GUIDE SUPPORT STRUCTURE FOR INNER BARREL ASSEMBLY OF PRESSURIZED WATER REACTOR"--Gillett et al., assigned to the common assignee herewith. Alternatively, the WDRC rod guides 32 may be connected independently to the lower calandria plate 52 by the top end support structure of the invention disclosed in the copending application, entitled: "TOP END SUPPORT FOR WATER DISPLACEMENT ROD GUIDES OF PRESSURIZED WATER REACTOR"--Gillett et al., assigned to the common assignee hereof. Extending upwardly beyond the upper calandria plate 54 and, more particularly, within the dome 12a of the vessel 12, there is provided a plurality of flow shrouds 60 respectively aligned with the calandria tubes 56. A corresponding plurality of head extensions 62 is aligned with the plurality of flow shrouds 60, with respective adjacent ends thereof in generally overlapping relationship. The head extensions 62 pass through the head or upper wall of the dome 12a and are sealed thereto. Control rod cluster (RCC) displacement mechanisms 64 and water displacement rod cluster (WDRC) displacement mechanisms 66 are associated with the respective head extensions 62, flow shrouds 60 and calandria tubes 56 which, in turn, are associated with respective clusters of radiation control rods 30 and water displacement rods 34. The RCC displacement mechanisms (CRDM's) 64 may be of well known type, as are and have been employed with conventional reactor vessels. It will be understood that the drive rods which are connected to the respective RCC clusters 30 extend from the top thereof through the corresponding mechanisms 64, projecting upwardly above same as the clusters are raised and progessing in telescoping fashion downwardly through the mechanisms 64 as the clusters 30 are lowered into association with the fuel assemblies 20. The displacer mechanisms (DRDM's) 66 for the water displacer rod clusters (WDRC's) 34, as employed with the vent system of the present invention, may be in accordance with the disclosure of U.S. Pat. No. 4,439,054--Veronesi, as before noted. The RCC and WDRC displacement mechanisms 64 and 66 connect through corresponding control shafts, or drive rods (not shown in FIG. 1), to the respective clusters of radiation control rods and water displacements rods 30 and 34, to control the respective vertical positions thereof and, particularly, selectively to lower and/or raise same through corresponding openings (not shown) provided therefore in the upper core plate 19, telescopingly into or out of surrounding relationship with the respectively associated fuel rod assemblies 20. In this regard, the clusters 30 and 34 have an extent of travel corresponding to the height of the fuel rod assemblies 20, as seen in FIG. 1. While the particular control function is not relevant to the present invention, insofar as the specific control over the reaction within the core is effected by the selective positioning of the respective rod clusters 30 and 34, it is believed that those skilled in the art will appreciate that moderation or control of the reaction is accomplished in accordance with the extent to which the control rod clusters 30 are inserted into or withdrawn from the core and with the effective water displacement adjustment which is achieved by selective positioning of the water displacement rod clusters 34. It is significant, however, that the RCC's 30 are adjusted in position relatively frequently, compared to the WDRC's 34, to achieve the desired power output level from the reactor. Conversely, the WDRC's 34, initially, are lowered, or inserted, fully into the lower barrel assembly 16 which contains the core of fuel rod assemblies 20, following each refueling and thus at the initiation of each fuel cycle. The WDRC's 32, through their respective drive rods (not shown in FIG. 1) and DRDM's 66, then are selectively removed as the excess reactivity is depleted, over the fuel cycle. Typically, this is performed by simultaneously removing a group of four such WDRC's 34 from their fully inserted positions in association with the fuel assemblies 20, to a fully raised position within the corresponding WDRC guide 32 and thus within the inner barrel assembly 24, in a continuous and controlled withdrawal operation. Each group of four WDRC's 34 is selected so as to maintain a symmetrical power balance within the reactor core. Typically, all of the WDRC's 34 remain fully inserted in the fuel assemblies 20 for approximately 60% to 70% of the approximately 18 month fuel cycle. Groups thereof then are selectively and successively withdrawn to the fully withdrawn position as the excess reactivity is depleted, so as to maintain a nominal, required level of reactivity which can sustain the desired output power level, under control of the variably adjustable RCC's 30. The vent system of the present invention thus serves to provide hydraulic energizing fluid to the DRDM's 66 in accordance with selectively controlling the WDRC raising and lowering functions, as above described. The water flow through the vessel 10 proceeds generally from a plurality of inlet nozzles 11, one of which is seen in FIG. 1, downwardly through the annular chamber between an outer generally cylindrical surface defined by the cylindrical sidewall 12b of the vessel 12 and an inner generally cylindrical surface defined by the cylindrical sidewall 26 of the inner barrel assembly 24 and the cylindrical sidewall 17 of the lower barrel assembly 16. The flow then reverses direction and thereafter passes axially upwardly through flow holes 18a in the lower core plate 18 and into the lower barrel assembly 16, from which it exits through a plurality of flow holes 19a in the upper core plate 19 to pass into the inner barrel assembly 24, continuing in parallel axial flow therethrough and finally exiting upwardly through flow holes (not shown in FIG. 1) in the lower calandria plate 52. Thus, parallel axial flow conditions are maintained through both the lower and inner barrel assemblies 16 and 24. Within the calandria 50, the flow in general turns through 90.degree. to exit radially from a plurality of outlet nozzles 13 (one of which is shown in FIG. 1). The pressure of the flowing water, or reactor coolant, within the vessel 10 typically is in the range of about 2,250 psi. The reactant coolant pressure furthermore is communicated from the DRDM's 66 through respectively associated conduits 80, flow restricting devices 81, and conduits 82 to a group manifold 84; as shown in part, four DRDM's 66 are connected through respective conduits 82 to each associated group manifold 84. Additionally, a head vent 86 communicates through the dome 12a with this same source of reactant coolant pressure, as a part of the vent sytem of the present invention. FIG. 2 is a cross-sectional, schematic bottom planar view of the lower calandria plate 52 at a position, in FIG. 1, intermediate the mounting means 36 and 38 for the RCC and WDRC rod guides 28 and 32, respectively, and the plate 52; further, FIG. 2 is on an enlarged scale and represents only a quadrant of the internal structure of the calandria 50, for illustrating diagramatically the dense packing of the arrays of plural control and water displacer rod clusters 30 and 34 within the inner barrel assembly 24. Each of the circles labelled "D" represents an aperture, or hole, in the calandria plate 52 through which is received a corresponding DRDM drive rod, associated with a corresponding WDRC cluster; similarly, each of the circles marked "C" corresponds to an aperture in the calandria plate 52 through which is received a corresponding CRDM drive rod, associated with a corresponding RCC cluster 30. These apertures C and D provide fluid communication with the corresponding RCC and WDRC calandria tubes 56 and, particularly, through the shrouds and head extensions 62 for communicating the reactant coolant pressure to the DRDM's 66. Further, the remaining unlabelled circles in the lower calandria plate 52 in FIG. 2 provide for communicating the reactor coolant flow from the inner barrel assembly 24 to the calandria 50. Elements 74 comprise leaf springs which are mounted in oppositely oriented pairs generally in alignment with the diameters of the RCC associated apertures "C," in an alternating, orthogonally related pattern. The free ends of the springs 74 bear downwardly upon the upper surfaces of the RCC mounting means 36 of a next-adjacent aperture "C," so as to provide a frictional force opposing lateral displacement thereof and accordingly of the associated rod guide 28, while affording a degree of flexibility to the axial position of the rod guide. While the use of springs 74 is one preferred structural mounting means for the RCC guides, in accordance with the disclosure of the above noted, copending application, entitled: "FLEXIBLE ROD GUIDE SUPPORT STRUCTURE FOR INNER BARREL ASSEMBLY OF PRESSURIZED WATER REACTOR," alternative mounting means may be employed for this purpose and thus the foregoing described structure is not to be deemed limiting in any sense, but merely illustrative. FIG. 2 also illustrates the relative locations of the plural inlet and outlet nozzles 11 and 13 as seen in FIG. 1, it being understood that the quadrant of the vessel shown in the plan view of FIG. 12 is reflected as a mirror image about the 90.degree. axis illustrated thereon and the combined configuration then is reflected about the 0.degree./180.degree. axis to establish the full (360.degree.) configuration of the vessel 12. Thus, there are provided a total of four inlet nozzles 11, two being equiangularly displaced about each of the 90.degree. and 270.degree. positions, and a total of four outlet nozzles 13, two being equiangularly displaced about each of the 0.degree. and 180.degree. positions. As will be apparent by comparison of FIGS. 1 and 2 and as will become more apparent with reference to the subsequent FIGS. 3 through 8 hereof, the RCC clusters and WDRC clusters are disposed in densely packed, interleaved arrays, substantially across the entire cross-sectional area of the inner barrel assembly 24. The RCC and WDRC rod clusters 30 and 34 are supported by corresponding spiders 100 and 120, as illustratively shown in FIGS. 3 to 6, in turn connected through corresponding drive rods to the CRDM's 64 and DRDM's 66, an example of the DRDM 66 being shown in FIGS. 7 and 8, as hereafter described. FIGS. 3 and 4 are plan and elevational views of an RCC spider 100, FIG. 3 being schematic in form and FIG. 4 being a partly broken-away, cross-sectional view taken along the line 4--4 in FIG. 3. The RCC spider 100 comprises a central hub 102 of generally cylindrical configuration having an upper, interiorally threaded end 103 for connection to a drive rod (not shown) which extends, as before described, upwardly to an RCC adjustment mechanism 64 by which the spider 100 and its associated control rods 30 (FIG. 1) may be vertically adjusted in position within and relative to the RCC rod guide 28 and correspondingly relative to the fuel rod assemblies 20, of FIG. 1. Vane assemblies 106 are secured at the respective inner edges thereof to the hub 102 and extend radially therefrom in quadrature, relative relationship. Each vane assembly 106 includes a pair of cylindrically-shaped rod support mounts 108, each thereof having an interior bore 109 including an interiorally threaded portion 110 into which the upper, correspondingly threaded end of a control rod (not shown) is threadingly engaged so as to be supported by the vane assembly 106 and corresponding hub 102. FIGS. 5 and 6 illustrate a WDRC spider 120, FIG. 5 being a planar, generally schematic view, and FIG. 6 being an elevational view, partially in cross-section and taken along the line 6--6 in FIG. 5. Similarly to the RCC spider 100, the WDRC spider 120 includes a central hub 122 of generally cylindrical configuration, the upper end 123 being interiorally threaded to receive a drive rod which, as discussed in connection with FIG. 1, connects to a corresponding WDRC control mechanism 66. First and second types of vane assemblies 126, 127 are connected to the hub 122 in alternating, equiangularly displaced relationship so as to extend radially therefrom. The vane assemblies 126 are substantially similar to the RCC vane assemblies 106, as seen in FIGS. 3 and 4, and thus include a pair of radially displaced WDRC rod support mounts 128. As best seen in FIG. 5, the vane assemblies 126 are disposed to extend radially from the hub 122 in quadrature relationship, each intermediate an adjacent quadrature-related pair of vane assemblies 106 in the alternating sequence as above described. The vane assemblies 127 include integral, transverse vanes 125 extending from the integral radial vane segments 123' and 124' as first and second aligned and oppositely oriented pairs 125A and 125B, each thereof carrying a WDRC rod support mount 128 at its extremity. Each of the WDRC rod support mounts 128 includes a threaded bore 129 at its lower extremity for receiving, in threaded engagement therein, the top end of a corresponding WDRC rod. The vane assemblies 106 and 126 include corresponding first and second planar vane elements 112, 114 and 123, 124, respectively, each thereof having longitudinal flanges for connecting the associated vane assemblies 106 and 126 to the respective, RCC spider hub 102 and WDRC spider hub 122. This structure is illustrated for the RCC spider 100 in FIG. 4 by the receiving slot 111 in the hub 102 and the flange 115 received therein, and is illustrated for the WDRC spider 120 in FIG. 6 by the receiving slot 121 in the hub 122 and the flange 131 associated with the first planar vane element 123, received therein. The second type of vane assembly 127 of the WDRC spider 120, as seen in FIG. 6, corresponds substantially to the first vane assembly 126 in that it includes first and second planar vane element portions 123' and 124' which are integrally formed and extend radially from the hub 122, the first portion 123' having a longitudinal flange 131' received in a corresponding receiving slot 121' in the hub 122. The assembly 127 furthermore includes first and second pairs 125a and 125b of third planar vane elements 125 integrally formed with and extending transversely from the first and second integral vane element portions 123' and 124', the first pair 125a being formed intermediate the portions 123' and 124' and the second pair 125b being formed on the outer longitudinal edge of the second vane element portion 124'. Each of the elements 125 carries a rod support mount 128 on its outer longitudinal edge. It will be understood that the third, or transverse, planar vane elements 125 may include similar flange structures on their outer longitudinal edges for mounting the corresponding rod support mounts 128. In assembling the respective RCC and WDRC spiders 102 and 120, the innermost planar vane elements 112, and 123, 123' preferably are positioned with the respective flanges 115 and 131, 131' inserted into the corresponding receiving slots 111 and 121, 121' of the associated hubs 102 and 120, and then spot welded in place at the upper and lower extremities thereof, as indicated by weld beads. Thereafter, the joints are brazed along the entirety of the lengths thereof. Referring now to FIG. 7, the displacer rod drive mechanism (DRDM) 66 receives a drive rod 132 which is connected to a WDRC spider 120. The DRDM 66 is shown more fully in the noted U.S. Pat. No. 4,439,054. Briefly, the DRDM 66 comprises a substantially cylindrical metal housing 136 which is welded to a head extension 62, which extends through the dome, or head 12a. Housing 136 has a cap 138 attached to the top thereof which has a channel 140 therethrough that is connected to conduit 80, as shown in FIG. 1. Since the interior of housing 136 is exposed to the interior of reactor vessel 12, the reactor coolant fills the void spaces within housing 136 and flows therefrom through channel 140 and conduit 80 under controlled conditions, to be explained. A bearing housing 146 is removably disposed within housing 136 and has a plurality of first piston rings 148 attached to the outside thereof near its lower end which extend into contact with the inside of housing 136 for aligning bearing housing 146 within housing 136 but allowing for the removal of bearing housing 146. Drive rod 132 is slidably disposed within bearing housing 146 in a manner so as to be able to be moved axially with respect to bearing housing 146 and housing 136 under the influence of the reactor coolant pressure. A plurality of second piston rings 150, which may be Inconel, are removably disposed within bearing housing 146 so as to be able to contact drive rod 132. Second piston rings 150 provide a mechanism for allowing drive rod 132 to slide within bearing housing 146 while limiting the flow of reactor coolant through bearing housing 146 and housing 136 when the vent system permits fluid flow through conduit 80, the movement of drive rod 132 thus being controlled by the vent system of the invention. Second piston rings 150 are arranged so that they may be replaced when bearing housing 146 is removed from housing 136. Referring now to FIGS. 7 and 8, a plurality of roller bearings 152 are disposed on a like number of axles 154 in a manner so as to allow the outer surface of roller bearings 152 to contact the outer surface of drive rod 132 whle allowing the rotation of roller bearings 152. As shown in FIG. 8, four roller bearings 152 may be used so as to align drive rod 132 within bearing housing 146 while aiding in the movement of drive rod 132. A plurality of screws 156 corresponding to the number of roller bearings 152 are used to attach holding member 158 to bearing housing 146 so as to hold roller bearings 152 within bearing housing 146 yet allow replacement thereof by removal of screws 156 and holding member 158. In a like manner, a second set of roller bearings 160 are disposed at the other end of bearing housing 146 to provide alignment of drive rod 132. Referring again to FIG. 7, drive rod 132 has a flexible rod 162 attached to the top end thereof which may be an Inconel rod. Flexible rod 162 has a spear-shaped member 164 attached to its top end. A hollow cylindrical divider 166 is attached to the lower end of cap 138, in colinear alignment with channel 140. Divider 166 defines chambers 168, 169 and 170 in the bottom end of cap 138, each of a size to accommodate the spear member 164. The spear-shaped member 164 cooperates with a pivoted latch mechanism 172 in a manner more fully described in U.S. Pat. No. 4,439,054. The latch 172 is normally spring biased to the slanted, or angularly offset position indicated in FIG. 7, and is mounted for pivotal movement in a clockwise direction in which the right-hand side thereof engages the interior of the wall of housing 136. Generally, during upward movement of the rod 132, the spear-shaped member moves upwardly along the slanted surface of the latch mechanism 172 as indicated in phantom lines, ultimately passing beyond the upper edge thereof and being received in the first chamber 168, the latch 172 being deflected by that movement to pivot in a clockwise direction and provide clearance for the motion of the spear shaped member 164 and then returning to its initial position by the spring biasing. The bottom end of cap 138 functions as a stop to prevent further upward movement of the member 164 and thus the drive rod 132. When pressure is equalized within the DRDM 66 so as to remove the differential pressure driving the rod 132 upwardly, in a manner to be described, the weight of the rod 132 and attached WDRC cluster causes the same to fall by gravity, the member 164 being received in the first bore 178 of the latch 172 and supported on ledge 182 to stop the downward movement, this action furthermore pivoting latch 172 to a vertically aligned position this locking, or parking, the rod 132 in its up position. To release the drive rod 132 from the locked, up position, the vent system is operated to cause a pressure differential again to be created, acting on the rod 132 so as to drive it upwardly through the bore 178 and into the central chamber 170, upward movement again being halted by the lower surface of cap 168 which acts as a stop on the element 164. The pressure differential then is removed by suitable controls of the vent system and the rod 132 and its associated WDRC 34 then falling by weight of gravity, pulling the member 164 through the second bore 180 and in turn pivoting the latching mechanism 172 in a clockwise direction; since bore 180 extends axially throughout the latch mechanism 172, member 164 is free to pass therethrough and thus permit rod 132 and its associated WDRC 34 to fall gradually throughout the entire extent of its travel, fully inserting the WDRC 34 into association with the fuel assemblies 20 in the lower barrel 16. As described more fully in the referenced U.S. Pat. No. 4,439,054, latch mechanism 172 includes suitable slots in the generally vertically oriented sidewalls thereof through which the flexible rod 162 may pass, to permit movement thereof transversely through the sidewalls defining the bores 178 and 180 of the latch mechanism 172, the slots of course being smaller than the element 164, which travels through the bores 178 and 180, as above described. An alternative configuration of the DRDM 66, relative to that shown in FIGS. 7 and 8, as well as a more detailed illustration of the vessel 12, are disclosed in the concurrently filed application entitled "PRESSURIZED WATER REACTOR HAVING DISCONNECTABLE TWO-PIECE DRIVE ROD ASSEMBLIES, AND RELATED METHODS OF ASSEMBLY AND MAINTENANCE OPERATIONS," having coinventors common to those of the present invention and assigned to the common assignee hereof, and incorporated herein by reference. FIG. 9 is a schematic of the vent system of the invention, in which like elements are identified by like numerals as in FIG. 1. As before noted, four WDRC's 34 are joined in a group for common actuation, and thus FIG. 9 illustrates four DRDM's 66 in each of groups A and B, having respective flow restricting devices 81 connected through corresponding conduits 82 (individually designated 82-1, 82-2, 82-3 and 82-4, for group A), a group manifold 84a, through a corresponding group valve V.sub.1a to a system manifold 90. Group B is correspondingly connected through a group manifold 84b and valve V.sub.1b to the system manifold 90. System manifold 90 schematically indicates connections to plural such groups; as above noted, 22 groups, of four DRDM's 66 each, comprises an exemplary implementation of the system. The system manifold 90 further is connected through conduit 91, system valve V.sub.2, and orifice 92 to a conventional reactor coolant drain tank (RCDT) 93, maintained at and thus functioning as a reservoir of normal atmospheric pressure (i.e., 15 psi). Additionally, the system manifold is connected through a bypass line 94 and system valve V.sub.3 directly to the RCDT 93, thus bypassing the orifice 94. Finally, a conduit 95 connects the head vent 86 (FIG. 1) through system valve V4 to the manifold 90. The flow designations I, II, and III and the associated flow direction arrows correspond to the three selected modes of operation and flow conditions, selectively established by the control functions of the vent system of the invention. Flow condition I corresponds to a normal withdrawal operation. For example, to withdraw group A, system valve V2 is opened first, to vent the system manifold 90 through orifice 92 to the RCDT 93. Group valve V.sub.1a then is opened to vent the DRDM's 66 of group A through the corresponding flow restrictors 81 to the manifold 90. The reactor coolant pressure applied to the interior of the DRDM's 66, as before noted, is about 2,250 psi, whereas a pressure of about 15-30 psi is established at the common orifice 92. By proper selection of the characteristics of the flow restricting devices 81 and the orifice 92, and the predetermined leakage past the piston rings 150 of the DRDM 66, controlled, reasonably slow movement of the drive rods associated with the respective DRDM's 66 results, gradually withdrawing the corresponding WDRC's 34 from within the lower barrel assembly 16 and into the fully withdrawn position within the inner barrel assembly 24. Group valve V.sub.1a then is closed, following which the pressure differential within the DRDM 66 is dissipated through leakage of the reactor coolant past the piston rings 150. Once equilibrium is reached, the associated WDRC's 34 begin to drop, under the force of gravity, causing the respective engaging latches 72 of the DRDM's 66 to pivot and lock the associated WDRC's 34 in their parked, raised position. Flow condition (II) corresponds to an insertion operation for releasing WDRC's 34 which are in the fully withdrawn and locked position, and then inserting same into the lower barrel assembly 16. As before noted, release from the latched position requires that the drive rod 132 first be raised; thus, the flow condition (I) is initiated for a sufficient time to raise the drive rods 132, by briefly opening group valve V.sub.1a and system valve V.sub.2. System valve V.sub.2 then is closed and system valve V.sub.4 opened, conveying the system coolant pressure from head vent 86 through conduit 95 to system manifold 90 and through the still opened group valve V.sub.1a, group manifold 84a, and conduits 82 and flow restrictors 81 to the respective channels 140 of the DRDM's 66, thereby equalizing the pressure on the drive rods 132 and permitting the respective WDRC's 34 to fall by force of gravity and be inserted fully into the lower barrel assembly 16. The positive pressure equalization step achieved by opening system valve V4 is dictated by the fact that tolerances, temperature differences, and the like can result in inadvertent sealing of, and thus the absence of the intended leakage past, the piston rings 150. Flow condition (III) is afforded to accommodate certain unexpected circumstances, such as that of a WDRC 34 which is inadvertently stuck in position, preventing movement thereof in respect to the normal flow condition (I). As later described, sensors detect such a condition, in which one or more of the WDRC's 34 of a given group, e.g., group A, has or have failed to achieve the withdrawn state. In that circumstance, the system valve V.sub.3 in the bypass conduit 94 is opened (system valve V.sub.2 and group valve V.sub.1 remaining in the opened condition), bypassing the common orifice 92. This produces a substantial incease, typically by several hundred psi, in the pressure differential across the piston rings 150, thereby seating the malfunctioning piston rings 150 and reestablishing a sufficient pressure differential to withdraw the affected WDRC's 34 to the intended, fully raised position. At this juncture, with all of the four WDRC's 34 in the fully withdrawn position, group valve V.sub.1 and system valves V.sub.2 and V.sub.3 are closed, permitting the WDRC's 34 to settle into the parked position, engaging the respective latch mechanisms 72 of the associated DRDM's 66. FIG. 10 is a schematic representation of the movement of a drive rod 132' and associated WDRC 34' from position 1 representing a fully inserted condition, through intermediate positions 2 (indicated by a single such position) during movement, which may be either withdrawal or insertion in this respect, position 3 which is the above-latched position to which the rod and element 164' must be moved for interacting with the latch mechanism 172 of FIG. 7, and position 4 which is the parked position in which the element 164' rests on the ledge 182', the primed numerals corresponding to the structural elements of FIG. 7 in each instance. FIG. 10 also illustrates a stop 138', corresponding to the lower surface of cap 138 in FIG. 7 and the abutment of element 164 therewith for limiting upward movement. Sensors S.sub.IN, S.sub.MOV, and S.sub.OUT detect the presence of the assemblage of the rod guide 132' and WDRC 34', generally illustrated in this instance as detecting the WDRC 34'. Other sensor locations of course may be adopted, where more convenient. Thus, S.sub.IN detects the fully inserted position of WDRC 34'; any interim position of WDRC 34' is detected by sensor S.sub.MOV, and sensor S.sub.OUT detects the WDRC 134' when raised to the over-latch position 3 and also when parked at position 4. An independent sensor may be employed to detect position 3, and thus to delineate between positions 3 and 4, if desired, as will be apparent. FIG. 11 is a schematic illustration of a display 200 associated with the sensors 190 corresponding to a typical group of four WDRC's 34 of a group. Thus, each of the,position sensors S.sub.OUT, S.sub.MOV and S.sub.IN includes four sensors S.sub.1 through S.sub.4, respectively corresponding to the four WDRC's 34 of the associated group. Display 200 correspondingly includes plural indicators 202, which may be conventional lights, including a first row of lights 202 representing the S.sub.IN position of each of a group of four WDRC's 34, the vertical columns of indicators 202 thus being designated 34-1 through 34-4, and the rows of indicators 202 correspondingly being designated S.sub.IN, S.sub.MOV and S.sub.OUT. As will be apparent, indicators 202 correspondingly are energized in response to the sensor signals to indicate the positions of the respective WDRC's 34-1 through 34-4. Normally, the indictors will sequence in substantially coordinated fashion from S.sub.IN through S.sub.MOV to S.sub.OUT and remain at the latter during a normal withdrawal and park operation, or will sequence in reverse during a normal insertion operation. Should any missequencing occur, the indicator lights 202 for each WDRC 34 which is out of sequence with the others will correspondingly produce an indication which is inconsistent with the remainder. For example, WDRC 34-1 may produce an S.sub.MOV indication whereas WDRC's 34-2 through 34-4 may produce S.sub.OUT indications, the display thus alerting the operator to the circumstance that WDRC 34-1 failed to achieve a fully withdrawn and latched state whereas the remainder performed the function as intended. As before noted, condition III in which valve V.sub.4 is opened produces an additional pressure differential for driving WDRC 34-1 upwardly to the latch position. A successful operation will then result in the proper indication for WDRC 34-1, consistent with the remainder of the group. A special circumstance also may occur which again will produce a missequenced display indication on the display panel 200. For example, if the V.sub.1 or V.sub.2 valves of FIG. 9 are closed prematurely, in that some but not all of the WDRC's 34 of a given group have reached position 3 of FIG. 10, those which have done so will progress to the parked position 4, but the remainder will continue to be in position 2. Reestablishing flow condition I to complete withdrawal of the nonlocked WDRC 34 will cause those in the locked position 4 to progress through the unlatching and insertion sequence, while the WDRC 34 which failed to achieve that state may proceed to the fully withdrawn and parked condition 4--continuing the missequencing problem. To remedy this circumstance, the following procedure is implemented. If such missequencing occurs, the vent system is operated in the following procedure. Flow condition II is initiated, by opening valve V.sub.4 and then, assuming group A to be missequenced, valve V.sub.1a is opened; this circumstance is maintained until the partially withdrawn WDRC 34 (i.e., in position 2) reaches a fully inserted position, i.e., position 1 of FIG. 10 as indicated by extinction of the S.sub.in indicator 202 of FIG. 11 for the affected WDRC 34. Valve V.sub.4 then is closed, terminating condition II. Valve V.sub.2 thereupon is opened for a period of approximately 30 seconds, and then closed; since valve V.sub.3 is assumed to be closed in this step, and valve V.sub.1a is open, the operation of valve V.sub.3 reestablishes flow condition I for a sufficient time to unlatch the WDRC's 34 of the group which theretofore had properly been advanced to the latched and parked, fully withdrawn position. The previously malfunctioning WDRC 34 will be driven in the upward, or withdrawal direction as well (e.g., advancing from position 1 to an intermediate position 2 as illustrated in FIG. 10); however, the time interval for that WDRC 34 to rise to the fully withdrawn position (e.g., position 3 of FIG. 10) is significantly longer (e.g., 1.5 to 2 minutes) than the interval (of approximately 30 seconds) during which valve V.sub.2 is opened, such that the malfunctioning WDRC 34 will not rise to a fully withdrawn position. The subsequent opening of valve V.sub.4 to establish flow condition II thus serves to permit the malfunctioning WDRC 34 to fall by gravity to the fully inserted position 1 (of FIG. 10), and to permit the WDRC's 34 which had been in the intended, proper sequence to proceed from the fully withdrawn, but now unlatched position, and descend under the force of gravity to join the theretofore missequenced WDRC 34 in the fully inserted position 1. Flow condition I then is reestablished to withdraw all WDRC's 34 of the group in proper coordinated and sequenced relationship to the fully withdrawn and, then, latched positions 3 and 4 (FIG. 10). The foregoing operations of valves V.sub.1 through V.sub.4 may readily performed by an operator through the control panel 192 of FIG. 9, in response to the display indications of display panel 200 of FIG. 11. Particularly, the control panel 192 may provide for transmitting respective solenoid actuating signals s.sub.1a, s.sub.1b, . . . s.sub.2, s.sub.3, s.sub.4 to the respectively corresponding valves V.sub.1a, V.sub.1b, . . . V.sub.2, V.sub.3, and V.sub.4 achieve the foregoing flow conditions, consistent with establishing the desired positions of the WDRC's 34, at all times throughout the fuel cycle. The flow restrictors 81 may be of a commercially available type sold under the trade name "LEE AXIAL VISCO JET," having a typical Lohms rating of 680 or 910 depending upon the speed of withdrawal required. Each of the valves V may comprise direct lift solenoid valves sold by Valcor Engineering Corporation of Springfield, N.J. under the designation 2-WAY "N" Series 526D. The orifice 92 may be formed by drilling a hole through a plate or disk which is then positioned in the vent line either by welding or bolting it between flanges. The size of the hole is selected to attain the proper flow impedance which, in conjunction with the flow restrictor 81, controls the speed of withdrawal. As an example, a 0.075 inch diameter hole would give a Lohm rating of approximately 150. In accordance with the foregoing, the vent system of the present invention provides for efficient and effective control of the displacer rod drive mechanisms (DRDM's) 66 and the respectively associated groups of plural symmetrically disposed WDRC's 34, including the capability of correcting for possible malfunctions in the travel of any given WDRC 34 and/or missequenced conditions which may inadvertently occur. The vent system moreover is economical and efficient both in its assemblage and operation, utilizing the available pressure within the vessel 12 as the power source, while permitting use of commercially available components to implement the system. The vent system moreover affords significant safety factors in its disclosed implementation, while achieving an economic and efficient design. The provision of a common manifold 90 enables use of a single orifice 92 and associated valve V.sub.2 as well as a single valve V.sub.3 affording the bypass function before noted, and a single valve V.sub.4 providing connection of the head vent 86 to the common manifold 90. These common, or system, elements thus are time shared by the plural groups of DRDM's 66, achieving cost economies. Further, this design takes into account safety factors in the operation of a reactor system. Specifically, if two or plural groups of WDRC's 34 were withdrawn simultaneously, power overshoots might occur, presenting a potential danger. The present system, however, eliminates that possible concern, through the use of the single, common orifice 92 which limits the total system flow rate to a Lohm value consistent with the desired rate of withdrawal of only a single group of WDRC's 34. Thus, if inadvertent connection of two or more groups of WDRC's 34 to the common manifold 90 occur, the resulting flow rate established by the common orifice 92 would be shared in parallel by the DRDM's 66 of the subject groups, greatly reducing the rate of simultaneous withdrawal of the plural groups. Indeed, if several groups were simultaneously connected to the common manifold 90, the shared flow rate for any individual DRDM, or group thereof, would be so limited that withdrawal of any thereof effectively would be precluded. Thus, the system minimizes components, and thus the cost, while affording a significant safety feature as well. In a related, safety aspect, the provision of individual flow restrictors 81, while not necessary to restrict the flow in view of the provision of the common orifice 92 which theoretically could suffice, alone, for that purpose, affords a safety feature in the event that the common orifice 92 were bypassed, such as by a break in the conduit 91. Numerous modifications and adaptations of the present invention will be apparent to those of skill in the art and thus it is intended by the appended claims to cover all such modifications and adaptations which fall within the true spirit and scope of the present invention.