Patent Number: 043326404
Section: description

DETAILED DESCRIPTION OF THE INVENTION The invention involves a refueling method and apparatus for the removal of spent fuel assemblies from a reactor core by applying axial force and vibration to the spent fuel assemblies to overcome weight and frictional loads without exceeding the allowable axial force limit that can be safely applied to a fuel assembly without damage thereto or to adjacent assemblies. Vibration reduces the effective coefficient of friction created between adjacent fuel assemblies as they undergo irradiation within a reactor core which results in swelling and creep behavior. By the addition of vibrational action to the axial force applied to a spent fuel assembly undergoing removal, the withdrawal capability is greatly increased without exceeding the allowable axial force limit. Vibration is produced by incorporating into the fuel grapple mechanism a pneumatic vibrator involving a steel ball pneumatically driven around a track by a gas, such as argon used as the reactor cover gas, such that the centrifugal force created by the ball is transmitted through the grapple to the fuel assembly handling socket which in turn applies a vibration to the fuel assembly being removed. The gas utilized to drive the ball may be argon reactor cover gas. Referring now to the drawings, the fuel grapple assembly generally indicated at 10 is shown extending through a hold down tube 11 into a fuel assembly 12. Fuel grapple 10 includes a casing or housing 13 composed of interconnecting sections 13a, 13b and 13c which is provided at its outer end (section 13c) with a grapple latch mechanism generally indicated at 14 and provided with a plurality of latches 15 (only one shown) adapted to engage with an annular notch 16 in a fuel handling socket or tube 17 of fuel assembly 12. As shown in FIG. 2, hold down tube 11 rests against adjacent fuel assemblies surrounding the one to which the grapple is engaged. Latch mechanism 14 is controlled by a push-pull latch actuator 18 such that movement of actuator 18 as indicated by the arrows moves collars 19 and 20 secured thereto to force latch 15 into engagement with notch 16, as shown for removal of the fuel assembly from a reactor core, not shown, or to disengage the latch 15, as conventionally known in the art. Fuel grapple 10 is also provided with a pneumatic vibrator mechanism generally indicated at 21 and located within casing 13 adjacent latch mechanism 14, with latch actuator 18 extending therethrough. As seen in FIGS. 1 and 2, pneumatic vibrator mechanism 21 includes a collar-shaped housing 22, secured intermediate casing sections 13b and 13c, having an annular groove 23 extending around its periphery and defining an annular, tapered raceway or track 24 on the interior surface thereof. The track 24 includes a centrally located annular groove 25 with a plurality of tangentially directed gas passageways 26 (two shown) extending between grooves 23 and 25 (see FIG. 2). A plurality of gas passageways 28 extend between groove 23 and an exterior surface 29 of housing 22 which are in communication with an annular chamber or groove 30 in casing section 13b which in turn is connected to a gas passage 31-32 having a fitting 33 secured thereto to which is connected a gas (such as argon or other cover gas, for example) inlet tube or line 34. A rotating ball 35 (constructed of steel for example) is rotatably positioned within track or raceway 24 and a seal assembly 36 is mounted in casing section 13c about latch actuator 18 to prevent leakage of the gas from the pneumatic vibrator mechanism 21 into the latch mechanism area of the grapple and the associated coolant (liquid sodium) about fuel assembly 12. Coolant vent passageways 37 and cooperating vent holes, 38 are located in grapple casing section 3c and hold down tube 11 to prevent entrapment of liquid sodium, for example, therein. In operation, with the fuel grapple assembly inserted such that the latch mechanism 14 is engaged with fuel handling tube 17 of the fuel assembly 12 to be removed, and with the hold down tube 11 positioned against the outer surface of the adjacent fuel assemblies, as known in the art, the pneumatic vibrator mechanism 21 is activated by directing gas under pressure, such as argon, from a source, not shown, into tube 34, as indicated by the legend and arrow. The gas flows from tube 34 and fitting 33 through passages 32-31, chamber 30, passages 28, groove 23, tangential passages 26 and is directed against rotating ball 35 which drives the ball around track 24 as indicated by the arrows in FIG. 2. The gas is exhausted, as indicated by legend and arrow, through a chamber 40 defined within casing sections 13b and 13a and passes through a plurality of openings 41 in casing section 13a into the reactor cover gas, as indicated by legend and arrow. Centrifugal force created by rotating ball 35 being driven around track 24 produces a vibrating which is transmitted through the grapple assembly to the fuel assembly handling socket or tube 17. The vibration, as pointed out above, reduces the effective coefficient of friction between the fuel assemblies thereby reducing the friction load, thus enabling additional withdrawal capability without exceeding the allowable axial force limit applied to the fuel assembly being removed. It has thus been shown that the present invention provides a refueling method an improved refueling fuel grapple mechanism for use in removing fuel assemblies from a reactor core which have swelled due to exposure to radiation, and thus difficult to remove due to friction loading, without exceeding the allowable safe axial force limit. This is accomplished by the incorporation of a pneumatic vibrator mechanism into the grapple wherein a rotating ball is driven around a track by means of a gas, the centrifugal force created thereby producing vibration in the grapple mechanism which is transmitted to the fuel assembly attached to the grapple. While a particular embodiment of the invention has been illustrated and described, modifications will become apparent to those skilled in the art, and it is intended to cover in the appended claims all such modifications as come within the spirit and scope of the invention.