Patent GB-1087493-A (GB)
Title: Nuclear reactor control mechanisms
Inventor: CHALLENDER RONALD SCOTT
IPC: G21C7/14
Filed: 1965-03-17
Abstract: 1,087,493. Controlling reactors. UNITED KINGDOM ATOMIC ENERGY AUTHOR- 1TY. Dec. 13, 1965 [March 17, 1965], No. 11313/85. Heading G6C. A nuclear reactor control mechanism, for normal control movement of a control rod relative to a reactor core and releasable to allow for rapid movement of the rod in a direction to reduce reactivity of the core, comprises a drive member engaging a driven member, first means for restraining the driven member against rotation during normal control movement, a releasable mechanical coupling between the driven member and a control rod carrier, and second means for effecting limited rotation of the driven member to release the coupling so as to allow for rapid movement of the carrier in the direction to reduce reactivity of the core, one of the means utilizing spring loading and the other utilizing fluid pressure opposing the spring loading. In the embodiment described, the driven member is a nut 36 housed in a main control mechanism body 60 outside and above the reactor pressure vessel (the reactor being a pressurized water reactor) and an extension tube 37 extends downwardly from the nut 36 to pass through a port in the vessel lid to a releasable mechanical coupling formed by a hammerhead consisting of rollers mounted on the ends of a shaft. The hammerhead is adapted to be inserted through a diametral slot in the enlarged end of a tubular member connected to the control rod carrier and rotated through 90 degrees to engage the underside of flanges defining the diametral slot. The enlarged end of the tubular member serves as a damping piston, being movable axially in a coaxial damping tube. The nut 36 engages a screw member 62 mounted for rotation within the body 60 and at its upper end is secured to a drive-shaft of a glandless reluctance motor (not shown). The extension tube 37 is keyed to the lower end of an elongate restraint tube 64, preferably by way of balls 65 engaging in longitudinally extending grooves 66 in the outer surface of the extension tube 37 and longitudinally extending tubes 67 in the inner surface of the restraint tube 64. Adjacent its upper end (Fig. 1E) the restraint tube 64 has a stepped portion 70 having a radially outward projecting step 71 extending into a circumferential groove 72 in the inner surface of the body 60. The body 60 has a stop 73 extending radially inward into the groove 72, and an auxiliary coil spring 74 extending round the restraint tube 64 serves to normally hold the stops 71, 73 in abutment. Below the level of the stops 71, 73 (Fig. IF), the stepped portion 70 has a radially outward projecting blade 75 extending into one end of a 90 degrees groove 76 in the inner surface of the body 60 which has two valved ducts 77, 78, one at each end. During assembly, the ducts 77, 78 are momentarily opened to sources of high and low pressure fluid, respectively, so as to rotate the blade 75 through 90 degrees. In this way, the restraint tube 64 and hence the extension tube 37 are also rotated through 90 degrees, the stop 71 moving away from the stop 73 against the loading of the spring 74. After the hammerhead has entered the diametral slot, the ducts 77, 78 are closed and the spring 74 rotates the restraint tube 64 and extension tube 37 back through 90 degrees so that the hammerhead is similarly rotated to engage the coupling as described above. The groove 76 is exposed to reactor coolant at high pressure through the duct 77 and for emergency control the duct 78 is opened to a low-pressure sump causing the blade 75 to rotate rapidly through 90 degrees, thus releasing the coupling. The control rod carrier is then free for rapid downward movement under the action of gravity and a normally compressed main spring.