CA1129565A - Control rod guide tube assembly - Google Patents
Control rod guide tube assemblyInfo
- Publication number
- CA1129565A CA1129565A CA380,043A CA380043A CA1129565A CA 1129565 A CA1129565 A CA 1129565A CA 380043 A CA380043 A CA 380043A CA 1129565 A CA1129565 A CA 1129565A
- Authority
- CA
- Canada
- Prior art keywords
- control rod
- guide tube
- sleeve
- rod guide
- lock
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
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- Monitoring And Testing Of Nuclear Reactors (AREA)
Abstract
ABSTRACT
A typical embodiment of the invention provides a nuclear fuel assembly lock structure for control rod guide tubes. Illustratively, a sleeve telescopes over an end portion of a control rod guide tube which bears against an internal shoulder of the tube. The upper end of the sleeve protrudes beyond the control rod guide tube spider and is locked in place by means of a resilient cellular lattice or lock that is seated in a mating groove in the outer surface of the sleeve. A special tool is provided for disengaging the entire lock structure, washer, spider, spring and grill from the end of the fuel assembly in order to enable these components to be removed in an assembled state and subse-quently replaced on the fuel assembly after inspection and repair.
A typical embodiment of the invention provides a nuclear fuel assembly lock structure for control rod guide tubes. Illustratively, a sleeve telescopes over an end portion of a control rod guide tube which bears against an internal shoulder of the tube. The upper end of the sleeve protrudes beyond the control rod guide tube spider and is locked in place by means of a resilient cellular lattice or lock that is seated in a mating groove in the outer surface of the sleeve. A special tool is provided for disengaging the entire lock structure, washer, spider, spring and grill from the end of the fuel assembly in order to enable these components to be removed in an assembled state and subse-quently replaced on the fuel assembly after inspection and repair.
Description
.~ ; 6 5 BACXGROUND OF THE INVENTION
FIELD OF THE INVENTION
This invention relates to fuel assemblies for use in nuclear reactors and, more particularly, to locking techniques for the end fittings and control rod guide tubes in a nuclear fuel assembly, and the like.
DESCRIPTION OF THE PRIOR ART
. _ - To produce useful power from a nuclear reactor it - is necessary to assemble fissionable material in a concen- -- 10 tration that is sufficient to sustain a continuous sequence of neutron-induced fissions. Frequently, this concentration is attained by sealing uranium dioxide pellets in long, slender hollow rods. These rods, when filled with a charge of nuclear fuel and sealed at the ends, are called "fuel rods".
The fuel rods are arranged in a generally cylind-rical array, or reactor core, to form the required concen-tration of ~issionable material. In order to extract the heat generated in these fuel rods through the fission -process, the fuel rods usually are sPaced laterally from each other and water is pumped under pressure through the reactor core. ~he water absorbs the fission process heat and transfers this heat to secondary cooling water. The secondary cooling water rises into steam that is used to drive power generating turbine machinery.
In the reactor core, the radiation,pressures, tem~er-atures and cooling water flow velocities create an en~iron-ment that is quite hostile to the structural integrity of the reactor core. To cope with this environment, it has been customary to arrange the fuel rods that com~rise , .
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9 5 ~ r- ``
the reactor core into a number of groups each of about two hundred fuel rods. These groups are f~equently called fuel assemblies.
To enhance the structtlral integrity of each of the fuel assemblies and to stabilize the fuel rods in the assembly, it is common ~o moun~ the fuel rods between "end fittings" and to engage the mid-portions of each of the rods in the fuel assembly by means of c~llular grid structures that are positioned at predetermined intervals along the lengths of the rods.
The structure of the fuel assembly, moreover, is not rest-ricted to fuel rods, end fittings and grids. As a general rule one or more control rod guide tubes also are accommodated in the usual fuel assembly. Typically, to control the power generated in a nuclear reactor it is customary to add neutron absorbing materials to the reactor - core. These materials have the effect of decreasing the ~ission activity within the core and thereby decreasing . the power output from the reactor. As might be expected, there are a number of ways in which these neutron absorbing materials are introduced into the reactor core. Quite frequently, for example, the neutron absorbing materials are loaded into control rods. These control rods are re-ceived in hol30w metal control rod guide tubes that extend through the length of the respective fuel element. In these circumstances, ~he depth of the penetration of the control rods into the associated fuel element determines, to some extent, the level of neutron fission activity and associated power output from the reactor core.
So~,e fuel assembly designs have a further use for , , .
ll,?~C;o5 the cont-rol Tod guide tubes beyond aligning the individual control rod5 within the respective fuel assembly. Typically in this Tegard, the control rod guide tubes are often used to spacP the two end fittings from each other and, essentially, to clamp the fuel rods in Proper relative position between these end fittings through enabling ~ the end fittings to engage the extreme ends of the fuel rods.
Thrs foregoing fuel assembly construction pro-duces a rugged, sturdy stTucture that is able to cope with -the forces that characterize a reactor core environment.
Ther~ is, howeverJ a somewhat countervailing need to pro-viae a ~uel assembly structure that can be assembled and dismantled with ease in order ~o reduce manufacturing costs, - improve qualitr assurance and facilitate.inspec~ion and replacement. If it is realized t~a~fuel assemblies, once ha~ing been made radioactive, must subsequently be manipu-lated behind shielaing with remote handling e~uiD~ent, the importance of the need for simple disassembly techniques becomes immediately apparent.
In this respect, the ty~ical fuel element is dis-mounted by unthr~ading nuts that connect the control rod guide tubes to the end fittings, releasing one or more springs and,~ in general, taking the entire fuel assembly apart piece-by-piece. Not only is this a very laboriousand expen6ive :practice but it also introduces the possibility that one or more of ~he smaller fittings might go astray, ieaaing to further lost time and expense, or damage if not discove,red.
Thus, there is a clear ~eed for an improYed fuel assembly that will,t~ alarge exten~, overcome many of these ~ ~ ~9565 inadequacies that have char~cterized the prior art.
SUMMARY OF THE INVENTION
An improved fuel assembly in accordance with the principles of the invention is characterized by a sleeve that engages one end of a control rod guide tube, essentially fixing the guide tube to one of the fuel assembly end structures.
An end of the sleeve protrudes above the surface of the end fitting. The outer surface of the sleeve has a peripheral groove that engages the resilient sides of a cellular grid or lattice shaped lock. This lock fixes the sleeve in position - between the various elements that comprise the end fitting, thereby eliminating a profusion of costly and potentially troublesome nuts, threaded studs and the like that frequently are employed in the fuel assemblies that are typical of the prior art.
To dismount the end fitting from the fuel assembly a special grapple has jaws that engage a portion of the end fitting. The jaws first clamp the upper grill that supports the ends of the control rod guide tubes and their respective sleeves. The-spider which engages the control rod guide tube sleeves then is pressed against the springs that circumscribe these sleeves in order to establish some degree of longitudinal clearance between the spider and the lock mechanism. After this clearance is established individual tools are pressed into the respective open, protruding ends of each of the sleeves to engage exposed portions of the grid~shaped lock.
The tools press these sides out of the groove, so engage the lock that the lock will be withdrawn from the sleeve when the grapple is withdrawn from the end of the fuel assembly. This permits the upper end fitting to be removed as a unit that captures the components which are associated with the end fitting as an assembled unit, while leaving the control rod ~.12~65 guide tubes and the associated sleeves w:ith the balance of the fuel assembly. In this way, end fitting components that are captured by the grapple in this manner subsequently can be replaced intact on the fuel asse~ly structure without indulging in the cumbersome and expensive remote manipulator detailed disassembly and assembly of scores of small parts that has characterized the prior art.
In accordance with the present invention there is provided a control rod guide tube assembly comprising a hollow control rod guide tube having at least one open end, a hollow cylindrical sleeve telescoped over a portion of said guide tube, said sleeve having a flange formed on the inner surface thereof to engage said control rod guide tube, an annular groove formed in the outer surface of said sleeve, said sleeve having an end portion having at least one longitudinally arrayed slot that extends througb said annular groove, a collar circumscribing a portion of said telescoped guide tube and sleeve, said collar and circumscribed guide tube and sleeve portions being joined together to form an integral control rod guide tube assembly.
Thus, the invention provides techniques for reducing the number of parts re~uired for fuel assembly construction, reduces manufacturing costs and simplifies quality assurance and inspection problems.
The various features of novelty which characterize the invention are pointed out with particularity in the claim annexed to and forming a part of this specification. For a better understanding of the invention, its operating advantages and specific objects attained by its use, reference should be had to the accompanying drawing and descriptive matter in which there is illustrated and described a preferred embodiment of the inventionO
BRIEF DESCRIPTION OF THE DRAWING
Fig. 1 is a front elevation in part section of a l129~5 typical fuel assembly that embodies principles of the invention.
Fig. 2 is a front elevation in ull section of a control rod guide tube structure for use in connection with the structure that is shown in Fig. l.
Fig. 3 is a plan view in partial section of the control rod guide tube structure that is shown in Fig. 2 taken along the line 3 - 3 of Fig. 2;
Fig. 4 is a front elevation of a grapple and tool engaging a portion of the fuel assembly that is shown in Fig. l;
Fig. 5 is a plan view in broken section of the grapple that is shown in Fig. 4;
Fig. 6 is a schematic drawing of a portion of the grapple in an initial operational position;
Fig. 7 is a schematic drawing of a portion of the grapple in another operational position;
Fig. 8 is a schematic drawing of a portion of the grapple in still another operational position; and Fig. 9 is a schematic drawing of a portion of the grapple after the lock has been disengaged.
DETAILED DESCRIPTION OF THE PREFERRED_EMBODIMENTS
As shown in Fig. l, an illustrative fuel assembly 10 comprises an array of more than two hundred fuel rods ll. It will be recalled in this respect, that the fuel rods ll are made from long, slender, thin-walled tubes that enclose pellets of uranium dioxide or other suitable nuclear fuel, ancl that these fuel rods are gr~uped together within the fuel assembly 10 with the longitudinal axes of the fuel rods in general parallel alignment.
Control rod guide tubes 12 are nested within the fuel assembly ll amongst and in parallel with the fuel rods.
The control rod guide tubes 12 each are hollow, thin-, .
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1129~6~
walled tubes that extend through the entire fuel assembly10 parallel to the longitudinal axis of the ~uel assembly.
A lower end support fitting 13 that is transversely disposed relative to the longitudinal axes of the ~uel rods 11 engages the abutting ends of the fuel rods. As described subsequently in more complete detail, the control rod guide tubes 12 pass through the end fitting 13 in order to secure the end fitting to the fuel assembly structure.
Ends of the control rod guide tubes 12 protrude above the plane established by the sealed ends of the fuel rods 11. These protruding ends of the control rod guide tubes 12 terminate, as shown in Fig. 2, within the confines of a transversely disposed grill 14. The grill 14 is assembled from a parallel array of generally flat, -`
slotted plates that are meshed with mating slots in a perpendicular array of essentially flat plates in order to form a cellular grill structure. The parallel grouping of the fuel rods 11 and the control rod guide tubes 12 is established and stabilized by means of transversely disposed grid structures 15, similar in ~ `
~` construction to the grill 14 described above, and through which the fuel rods and guide tubes extend.
; Toward the ends of the fuel rods 11 that are close to the protruding portions of the control rod guide tubes, howevex, a transversely disposed upper grid 16 is posi-tioned. The upper grid 16 has a somewhat greater depth in the direction of the longitudinal axes of the fuel rods 11 than the grid structures 15 in order to enhance the structural integrity of this portion of the fuel assembly.
- . , ' . . : ,. :-9 5 6 ~
In accordance with a feature of the invention a parallel array of hollow cylindrical sleeves 17 tele-`~' s-cope over the res,ective protrud:ing ends o~ the control rod guide tubes 12 in order to extend from within the confines of the upper grid 16 through the yrill 14, through a transversely disposed spider 20 and an immediately superjacent control rod guide tube assembly lock 21. Spring means, such as individual coil springs 22, each associated with a respective one of the sleeves 17 are interposed in a biasing relationship between the grill 14 and the spider 20 in order to provide some : means for compensating and absorbing movement of the fuel element 10 in th,e direction of the longitudinal axes of the fuel rods 11. Note that in the illustrative embodiment of the invention shown in Fig. 2 that the sleeve 17 is in general axial alignment with the guide tube 12, and that the sleeve serves as a guide for the coil spring 22. The coil spring 22, moreover, also has a longitudinal axis that generally coincides with the longitudinal axis of the guide tube 12.
Attention is invited to Fig. 2 for a more detailed appreciation of the novel features of this ~' invention that characterize the invention. More parti-cularly, the control rod guide tube 12 is secured to a ~ "
lower grid 23 by means of a bolt structure 24. The bolt structure 24 has a head 25 that is received within the ad-jacent open end of the control rod guide tube 12. A bolt shank 26 extends through the lower grid 23 in order to protrude from the end support fitting 13. The protruding portion of the shank 26 is thr,eaded in order to receive a fastening nut 27. A nut retainer 30 is interposed between .
the end fitting and the nut 27 in order to prevent the nut from working loose and becoming disengaged from the fuel assembly.
As shown in Fig. 2, the control rod guide tube 12 extends through the main portion of the fuel assembly and - through an upper grid 16. r~ithin the upper grid 16 the guide tube 12 is telescoped within the sleeve 17, open end portion 31 of the control rod guide tube :L2 abutting and bearing against a flange or shoulder 32 that is formed within the inner surface of the sleeve 17. The shoulder 32 in the sleeve 17 transfers compression loads directly to the guide tube in the manner described subsequently in more complete detail.
Through the lengths of the control rod guide tube 12 and the sleeve 17 that are coextensive protrusions or "dimples" 33 are swaged or otherwise suitably formed in the control rod guide tube 12 and the sleeve 17 in order to hold `
the sleeve and the guide tube together and form a tight joint.
Immediately below the grill 14, circumscribing a portion of the sleeve 17 and bearing against a transverse surface of the grill 14 is a ring shaped collar 34. As shown, the collar 34 and the encircled portions of the sleeve 17 and the control rod guide tube 12 also are provided with protrusions or dimples 35, 36 that Kave been swaged or otherwise formed in the materials in order to position the collar 34 properly relative to the balance of the fuel assembly structure and to permit the collar to sustain loads imposed in the direction of control rod guide tube longitudinal axis 37 and to transfer these loads between the grill 14 and the combination sleeve 17 and control rod guide tube 12.
A washer 40 rests upon the transverse surface of the grill 14 that is opposite from the transverse grill surface that engages the collar 34. The coil spring 22 as illustrated 9 r f~ c U ~J
in Fig. 2, is mounted on the washer 40 and encloses a portion of the sleeve 17 that protrudes above the grill 140 The longitudinal axis of the coil spring 22 ~enerally coincides with the longitudinal axis 37 in order to press against a further washer 41. Thus, the coil spring 22 interposed between the grill 14 and the spider assembly 20, respectively biases the grill and spider assembly against the collar 34 and the lock 21.
Illustratively, the washer 41 is in engagement with the cellular spider assembly 20. As shown, the sleeve 17 is received within a cellular recess 42 in the spider 20 with sufficient clearance between the sleeve and the walls of the spider recess 4~ to permit the spider and the sleeve to move - relative to each other in the direction of the longitudinal axis 37.
A terminal portion 43 of the sleeve 17 pxotrudes above the spider 20 ln order to engage the lock 21. To engage r the lock 21, the outer surface of the portion 43 is provided with a circumferential groove 44 that forms a protruding shoulder 45 which serves to engage edges of the lock 21.
; Perhaps, as best shown in Fig. 3, the lock 21 is assembled from an arr`ay of resilient parallel plates 46, 47 that are meshed and interlock with similarly resilient plates 50, 51 that are generally perpendicular to the plates 46, 47 at the respective lines of intersection to form a cellular grid structure. As shown, the separation between the parallel plates 46, 47 is less than the maximum outside diameter of the groove 44 that is formed in the portion 43.
The plate 50 has a generally arcuate shape that conforms to and bears against a segment of the grooved surface of the terminal sleeve portion 43. The companion plate 51, however, has a plane profile that permits part of an edge of 1, ~9~,~5 this plate to engage the shoulder 45 (Fig. 2). In this manner, all of the control rod guide tubes 12 that are shown in Fig. 1 are locked together as a single unit.
sest shown in Figs. 2 and 3, the terminal sleeve portion 43 is provided with four longitudinal slots 52, 53, 54 and 55 that are parallel with the longitudinal axis 37.
The slots 52, 53, 54 and 55 each are spaced ~rom the next adjacent slots by about 90 and penetrate the portion 43 to a depth that is at least equal to the combined longi-tudinal depth of the shoulder 45 and the width of theplates 50, 51.
In accordance with an additional feature of the invention a grapple 56 is shown in Fig. 4. The grapple 56 releases the lock 21 from the control rod guide tube sleeves 17 and also provides a means for installing or removing as one entire unit the complete assembly that comprises the lock 21, the washers 40, 41, the spider 20, the coil springs 22 and the grill 14. To accomplish these results, the grapple 56 is provided with a member 57 that is movable in the direction of longitudinal axis 60. A transversely disposed linkage 61 is secured through a cross piece 62 (Fig. 5) to the vertically movable member 57. The end portions of the linkage 61 (Fig. 4) has slots 63, 64 which receive respective pins 6~, 66. The pins 65, 66 are transversely mova~le within the respective slots in order to ena~le two jaws 67, 7~ that are pivotally connected to a transversely disposed tool frame 71 to move in a scissors-like manner.
As shown in Fig. 4 the jaw 70 is provided at its exteme end with a clamp 73 that engages a longitudinal edge of the grill 14. In a similar manner, the extreme end of the jaw 67 also is provided with a clamp 74 that is 9~65 .
- oppositely disposed from the clamp 73 on the jaw 70.
Perhaps best shown in Fig. 5, a comPanion linkage 75 with pinned and ~ivoted jaws 76, 77 also are joined by means o~ the cross piece 62 to the longitudinally movable member 57. This companion structure matches and bala~ces the structural arrangement described above with res~ect to the jaws 67, 70.
:. -The transversely disposed tool frame ~1 also is pro~ided with an array of longitudinally aligned apertures 'h, 10 80 that each accommodate one of a grou~ of tools 81. As illustrated in Fig. 4, the t'ools 81iare formed from .. . .
generally cylindrical rods that are longitudinally aligned with the axis ~0. Each of the tools 81 has a generally conical end portion 82. The mid-section of the tool 81 has four fins 83, of which only three OftheSe fins are sholm in the plane of the drawing. As illustrated~ each of the fins 83 are spaced about 9Q from the next adjacent fins.
Each of the fins 83 has a tapered slope 84 in w~ich the narrow edge of`the slope is oriented toward ~he e~d portion B2. The tapered slope 84 ends in a generallr flat surface 85. The width of each of the fins 83 is slightly less than the transverse width of the indivdual slots 52, 53, 54, 55 (Figs. 2 and 3). The transverse depth of each of these fins, however, between the flat surFace 85 (Fig. 4) ana t~e adjacent surface of the tool 51 is greater than :
the correspondL~g wall thickenes5 of the terminal slee~e . ---portion 43 as s'~own in Figs. 2 and 3.
An annular collar 86 is secured to the tool 81and spaced longitud;nally from the flat suTfaces 85 on 3() the fLns 83 a sufficient distance to enable the fins when aligned ~ith the respective slots in the terminal sleeve 11~)3~b5 portîon 43 to bear against the terminal portion and prevent ~ the flat surfaces 85 of the fins 83 from penetrating the ; sleeve 17 to a depth greater than the longitudinal protru-sion of the slots ln the terminal sleeve portion 43 (Fig. 2~ above the spider 20.
As illustrated in ~ig. 4, the tool 81 has been '~hreaded-87 at the end.opposite from the end poItion 82 ; ' to enable nuts 90, 91 to secure the tool 81 to a trans- .
versely disposeL plate 92 that is movable in longitudinal directions as indicated by means of arrows 93, 94.under - :-the control of spring biased pneumatic cylinders 95, 96. ' ' Thus,''depending on the relative activation of the pneumatic cylinders 95j 96, the tools 81, when aligned with respect-ive terminal sleeYe portions 43 are driven into the sleeves . 17 to a sufficient depth to permit the flat surfaces 85' on the fins ~3 to bear'against the plates 46, 47 50, 51 (Figs. 2 and 3). The flat surfaces 83~press these plates in a radially outward direction relative to the longitudinal axis 37 through a distance that is sufficient to perm~t all .i.
of the plates to clear the shoulder 45 that is formed in 1' the terminal sleeve portion 43. In this manner the entire cellular lock 21 is ~eleased from its engagement with the sleeYes 17 and fixes itself temporarily to the tools 81 in'the array of tools.
In operation, and, as perhaps best understood ~:
through an examination of Fig. 6 the grapple 56 ~s aligned with the end fitting to permit the clamps 73 on t~e jaw 70 ~as well as the cl.amps 74 on the jaws 67, and the clamps o~ the jaws 76, 77 on the grapple that are not shown in Fig. 6) to be spaced outwaTdly of the grill 14, but within the same transverse plane as the grill.
~ 1-'9~5 During ~his phase of the operation of the grapple 56, the sprlngs associated wlth the springs loaded pins 97 aTe compressed through activation of the air cylindeI 95 whicfi moves the plate 92 in the direction of the arrow 93.
As illustrat~d-in Fig. 7, the clamps 73, 74 on ; . the jaNS 70, 67, respecti~ely, tas well as the changes on the cOmpaTiSOn pair of jaws 76, 77) swing inwardly in the directions indica~ed by arrows 101, 102 in oTder to grzsp firmly peripheral portionsof the grill 14. This inwardly swinging movement of the clamps 73, 74 is achieved through longitudinal movement of the member 57 in the direction of arrow 103. This movement of the member 57,causes the ~
pins 65, 66 to ride within the respective slots 63, 64 toward the longitudinal axis 60. The motion of these pins within the 510ts compels the jaws 67, 70 to pivot cente~-clockwise and clockwise, respectively, about the pivot 72 ~for the ~aw 70~ and a similar pivot tnot shown in ~ig. 7) foT the jaw 67.
20. . - The next.illustTative step in the technique for dismounting the end fitting from the balance of the fuel ; assembly is shown in Fig. 8. Thus, air cylinders 96 are activated to drive pis;on rods lD4 in the longitudinal directions indicated by means of arrow 105. The exposed ends of the piston rods 104 bear against the adjacent transverse surface of the ~pider 20. The force applied by the piston rods 104 to the spider 20 overcomes the oppositely directed forces e~tablished by means of the coil springs that are received on the sleeves, o~ wfiich the coil spring 22 and the sleeve 17 in Fig. 8 are illus-trati~e. In response to this new ~alance of ~orces the .. . .
11~35~5 spider 20 also moves in the longitudinal direction of the arTOW 105 in order to provide a longitudinal clear-ance 106 between the spider 20 and the lock 21 to relieve the force that the spider 20 applies to the lock 21.
In a typ;cal embod;ment of the invention, the next step~ in the technique involves movemen~ of the grapple 56 that is be~t illustrated in Fig. 9. Recall :for a moment . that the cellular structure of the lock 21 . is so designed that the groove 44 ~Fig. 2~ and the _shoulder 45 that is formed in the terminal sleeve portion - 43 engage the plàte.s 46, 47, 50, 51 tFig. 3) that comprise the -structure.of the cells in the lock 21.
. Turning now once more to Fig. 9, the air cylinders 95 are deactivated to ena~le the coiled springs on the spring loaded pins 97 to release and press the plate 92 in a longitudinal direction as indicated by an.
arrow 107. Because the recess and shoulders on the sleeves restrain the lock 21 from engaging in any longitudinal movement in the direction of the arrow 107, the tools that are fastened to the plate 92, of which the tools 81 is typical> are pressed thTough the individual cells in the - locks 21 into the TespeCtiVe sleeves 17. The fins 83 that pTotsude radially from the tools 81 also are driver. into matinp siots 52, 53, 5i, 55 ~ig. 2 and 3j. This ;~
longitudinal movèment of the tools 81 permits the tapered slope 84 of the pins 83 CFig 9) to press the plates 46, 47, 50, 51 on t~! lock 21 in a radially outward diTection n oTder to disengage these plates from the nested engagement withiII the annular groove 44 (Figs. 2 and 3) that is formed ill the terminal sleeve portion 43.
In those circumstances, further longitudinal ~ r ~,-1 lLJ~ ~V
movement of the tools 81~(Fig. 9) in the direction of the aTrow 107 under the force of the released springs on the pins 97 is limitea o~ly~~by the braking action of the collars - 86 on eac~ of the tools. The collar 86 is so spaced relative ~o the lock 71 that the plates which foTm each of the cells in the lock 21 are forced onto the corresponding flat surface 85 of the fins 83. I'he effect of this engagement ~etween the plates that form t~e cells on the lock'21 and the 1a~ surfaces 85 of the fins 83 is to 10 , press the plates out of e,ngagement with the respective annular-grooves 44 (Figs. 2 an,d 3) and'shoulders 45.
' In the'next illustrative disassembly step , the - . - - . .
- enti~e grapple 56 is moved,longitudinally,in the direction - - . . . ~ ~ ......................... .. . .
of arrow 108. 'The grapple, withdrawn from'the balance of the fuel assembly in the foregoing manner, takes with it most of the e~d fitting components in'their'pToper relative position. Typically, the lock 21, the spider 20, and the gTill 14 ~emain with the grapple 56. The coil springs 22 with their associated washers 40, 41 (Fig. 2) also are drawn away with the grapple 56 (Fig. 9). In this instance, the tools 81 serve as temporary spring guides or keepers for the coil springs 22 and the washers. The springs--22, moreover, serYe to keep an approximately proper longitudinal s'eparation between the grill 14 and the spider 20. Note in th~^s Tespect that the sleeves 17 remain ~ith the ~alance of the fuel ass'em~ly.
To reassemble the end fitting components on t~e main portion of the fuel assembly, t~e end portion 82 of the tools 81 on the grapple 56 are longitudina~y aligned ~ith thei.r respective sleeves. ~he grapple 56 then is moved longitudlnally m the direction of the : ~
~ 5 arrow 107 untll each of the tools 81 are fully seated in the respective sleeves 17. One or more clamps ~not shown n the'drawing) hold the lock 21 in suitableposition relative to the. grooves 44, CFigs. 2 and 3~ and shoulders 45 on the terminal sleeve portion 43. In this condition the-air cylinders 95 ~Fig. 9) are activated to compress the spTings on the spring loaded pins 97, thereby extracting the pins 83 from engagement with the plates that form the cells in the lock 21. The disengagement ,,,, . I
-10 ' of the tools 81'and the lock 21 permits the plates that . form each'of.the lock's cells to snap back into the annu-- - - - . . . I
lar recesses 44 ~Figs. 2 and 3) and shoulders 45 in the.
terminal sleeve portion 43. - '. -. . -~
.
The spider 20 ~Fig. 9) under the action vf the ' .
coil springs 22 bears against the adjacent surfa e of the -lock 21. The member 57, moreover, is moved longitudinally .
.in the direction of the àrrow 107 to permit the jaws 67, ', , 70 to pivot in clockwise and counter-clockwise directions, respectively. ~his pivoting movement of the jaws 67, 70 releasés the grip that the clamps 73, 74 had on the grill 1' 14. The further clamps (not shown in the drawlng) that ' . engage the lock 21 also are removed.
The entire end fitting now is reassembled on the balance of the fuel asse~bly in a manner that clearly avoids the prior art requirement for tedious, detailed, p;ece-~y-piece disassembly and reassem~ly. Th~s techni-que that characterizes the inYention also avoids the hazards that might attend the loss of one of these small end fitting components, and the like.
FIELD OF THE INVENTION
This invention relates to fuel assemblies for use in nuclear reactors and, more particularly, to locking techniques for the end fittings and control rod guide tubes in a nuclear fuel assembly, and the like.
DESCRIPTION OF THE PRIOR ART
. _ - To produce useful power from a nuclear reactor it - is necessary to assemble fissionable material in a concen- -- 10 tration that is sufficient to sustain a continuous sequence of neutron-induced fissions. Frequently, this concentration is attained by sealing uranium dioxide pellets in long, slender hollow rods. These rods, when filled with a charge of nuclear fuel and sealed at the ends, are called "fuel rods".
The fuel rods are arranged in a generally cylind-rical array, or reactor core, to form the required concen-tration of ~issionable material. In order to extract the heat generated in these fuel rods through the fission -process, the fuel rods usually are sPaced laterally from each other and water is pumped under pressure through the reactor core. ~he water absorbs the fission process heat and transfers this heat to secondary cooling water. The secondary cooling water rises into steam that is used to drive power generating turbine machinery.
In the reactor core, the radiation,pressures, tem~er-atures and cooling water flow velocities create an en~iron-ment that is quite hostile to the structural integrity of the reactor core. To cope with this environment, it has been customary to arrange the fuel rods that com~rise , .
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9 5 ~ r- ``
the reactor core into a number of groups each of about two hundred fuel rods. These groups are f~equently called fuel assemblies.
To enhance the structtlral integrity of each of the fuel assemblies and to stabilize the fuel rods in the assembly, it is common ~o moun~ the fuel rods between "end fittings" and to engage the mid-portions of each of the rods in the fuel assembly by means of c~llular grid structures that are positioned at predetermined intervals along the lengths of the rods.
The structure of the fuel assembly, moreover, is not rest-ricted to fuel rods, end fittings and grids. As a general rule one or more control rod guide tubes also are accommodated in the usual fuel assembly. Typically, to control the power generated in a nuclear reactor it is customary to add neutron absorbing materials to the reactor - core. These materials have the effect of decreasing the ~ission activity within the core and thereby decreasing . the power output from the reactor. As might be expected, there are a number of ways in which these neutron absorbing materials are introduced into the reactor core. Quite frequently, for example, the neutron absorbing materials are loaded into control rods. These control rods are re-ceived in hol30w metal control rod guide tubes that extend through the length of the respective fuel element. In these circumstances, ~he depth of the penetration of the control rods into the associated fuel element determines, to some extent, the level of neutron fission activity and associated power output from the reactor core.
So~,e fuel assembly designs have a further use for , , .
ll,?~C;o5 the cont-rol Tod guide tubes beyond aligning the individual control rod5 within the respective fuel assembly. Typically in this Tegard, the control rod guide tubes are often used to spacP the two end fittings from each other and, essentially, to clamp the fuel rods in Proper relative position between these end fittings through enabling ~ the end fittings to engage the extreme ends of the fuel rods.
Thrs foregoing fuel assembly construction pro-duces a rugged, sturdy stTucture that is able to cope with -the forces that characterize a reactor core environment.
Ther~ is, howeverJ a somewhat countervailing need to pro-viae a ~uel assembly structure that can be assembled and dismantled with ease in order ~o reduce manufacturing costs, - improve qualitr assurance and facilitate.inspec~ion and replacement. If it is realized t~a~fuel assemblies, once ha~ing been made radioactive, must subsequently be manipu-lated behind shielaing with remote handling e~uiD~ent, the importance of the need for simple disassembly techniques becomes immediately apparent.
In this respect, the ty~ical fuel element is dis-mounted by unthr~ading nuts that connect the control rod guide tubes to the end fittings, releasing one or more springs and,~ in general, taking the entire fuel assembly apart piece-by-piece. Not only is this a very laboriousand expen6ive :practice but it also introduces the possibility that one or more of ~he smaller fittings might go astray, ieaaing to further lost time and expense, or damage if not discove,red.
Thus, there is a clear ~eed for an improYed fuel assembly that will,t~ alarge exten~, overcome many of these ~ ~ ~9565 inadequacies that have char~cterized the prior art.
SUMMARY OF THE INVENTION
An improved fuel assembly in accordance with the principles of the invention is characterized by a sleeve that engages one end of a control rod guide tube, essentially fixing the guide tube to one of the fuel assembly end structures.
An end of the sleeve protrudes above the surface of the end fitting. The outer surface of the sleeve has a peripheral groove that engages the resilient sides of a cellular grid or lattice shaped lock. This lock fixes the sleeve in position - between the various elements that comprise the end fitting, thereby eliminating a profusion of costly and potentially troublesome nuts, threaded studs and the like that frequently are employed in the fuel assemblies that are typical of the prior art.
To dismount the end fitting from the fuel assembly a special grapple has jaws that engage a portion of the end fitting. The jaws first clamp the upper grill that supports the ends of the control rod guide tubes and their respective sleeves. The-spider which engages the control rod guide tube sleeves then is pressed against the springs that circumscribe these sleeves in order to establish some degree of longitudinal clearance between the spider and the lock mechanism. After this clearance is established individual tools are pressed into the respective open, protruding ends of each of the sleeves to engage exposed portions of the grid~shaped lock.
The tools press these sides out of the groove, so engage the lock that the lock will be withdrawn from the sleeve when the grapple is withdrawn from the end of the fuel assembly. This permits the upper end fitting to be removed as a unit that captures the components which are associated with the end fitting as an assembled unit, while leaving the control rod ~.12~65 guide tubes and the associated sleeves w:ith the balance of the fuel assembly. In this way, end fitting components that are captured by the grapple in this manner subsequently can be replaced intact on the fuel asse~ly structure without indulging in the cumbersome and expensive remote manipulator detailed disassembly and assembly of scores of small parts that has characterized the prior art.
In accordance with the present invention there is provided a control rod guide tube assembly comprising a hollow control rod guide tube having at least one open end, a hollow cylindrical sleeve telescoped over a portion of said guide tube, said sleeve having a flange formed on the inner surface thereof to engage said control rod guide tube, an annular groove formed in the outer surface of said sleeve, said sleeve having an end portion having at least one longitudinally arrayed slot that extends througb said annular groove, a collar circumscribing a portion of said telescoped guide tube and sleeve, said collar and circumscribed guide tube and sleeve portions being joined together to form an integral control rod guide tube assembly.
Thus, the invention provides techniques for reducing the number of parts re~uired for fuel assembly construction, reduces manufacturing costs and simplifies quality assurance and inspection problems.
The various features of novelty which characterize the invention are pointed out with particularity in the claim annexed to and forming a part of this specification. For a better understanding of the invention, its operating advantages and specific objects attained by its use, reference should be had to the accompanying drawing and descriptive matter in which there is illustrated and described a preferred embodiment of the inventionO
BRIEF DESCRIPTION OF THE DRAWING
Fig. 1 is a front elevation in part section of a l129~5 typical fuel assembly that embodies principles of the invention.
Fig. 2 is a front elevation in ull section of a control rod guide tube structure for use in connection with the structure that is shown in Fig. l.
Fig. 3 is a plan view in partial section of the control rod guide tube structure that is shown in Fig. 2 taken along the line 3 - 3 of Fig. 2;
Fig. 4 is a front elevation of a grapple and tool engaging a portion of the fuel assembly that is shown in Fig. l;
Fig. 5 is a plan view in broken section of the grapple that is shown in Fig. 4;
Fig. 6 is a schematic drawing of a portion of the grapple in an initial operational position;
Fig. 7 is a schematic drawing of a portion of the grapple in another operational position;
Fig. 8 is a schematic drawing of a portion of the grapple in still another operational position; and Fig. 9 is a schematic drawing of a portion of the grapple after the lock has been disengaged.
DETAILED DESCRIPTION OF THE PREFERRED_EMBODIMENTS
As shown in Fig. l, an illustrative fuel assembly 10 comprises an array of more than two hundred fuel rods ll. It will be recalled in this respect, that the fuel rods ll are made from long, slender, thin-walled tubes that enclose pellets of uranium dioxide or other suitable nuclear fuel, ancl that these fuel rods are gr~uped together within the fuel assembly 10 with the longitudinal axes of the fuel rods in general parallel alignment.
Control rod guide tubes 12 are nested within the fuel assembly ll amongst and in parallel with the fuel rods.
The control rod guide tubes 12 each are hollow, thin-, .
.
1129~6~
walled tubes that extend through the entire fuel assembly10 parallel to the longitudinal axis of the ~uel assembly.
A lower end support fitting 13 that is transversely disposed relative to the longitudinal axes of the ~uel rods 11 engages the abutting ends of the fuel rods. As described subsequently in more complete detail, the control rod guide tubes 12 pass through the end fitting 13 in order to secure the end fitting to the fuel assembly structure.
Ends of the control rod guide tubes 12 protrude above the plane established by the sealed ends of the fuel rods 11. These protruding ends of the control rod guide tubes 12 terminate, as shown in Fig. 2, within the confines of a transversely disposed grill 14. The grill 14 is assembled from a parallel array of generally flat, -`
slotted plates that are meshed with mating slots in a perpendicular array of essentially flat plates in order to form a cellular grill structure. The parallel grouping of the fuel rods 11 and the control rod guide tubes 12 is established and stabilized by means of transversely disposed grid structures 15, similar in ~ `
~` construction to the grill 14 described above, and through which the fuel rods and guide tubes extend.
; Toward the ends of the fuel rods 11 that are close to the protruding portions of the control rod guide tubes, howevex, a transversely disposed upper grid 16 is posi-tioned. The upper grid 16 has a somewhat greater depth in the direction of the longitudinal axes of the fuel rods 11 than the grid structures 15 in order to enhance the structural integrity of this portion of the fuel assembly.
- . , ' . . : ,. :-9 5 6 ~
In accordance with a feature of the invention a parallel array of hollow cylindrical sleeves 17 tele-`~' s-cope over the res,ective protrud:ing ends o~ the control rod guide tubes 12 in order to extend from within the confines of the upper grid 16 through the yrill 14, through a transversely disposed spider 20 and an immediately superjacent control rod guide tube assembly lock 21. Spring means, such as individual coil springs 22, each associated with a respective one of the sleeves 17 are interposed in a biasing relationship between the grill 14 and the spider 20 in order to provide some : means for compensating and absorbing movement of the fuel element 10 in th,e direction of the longitudinal axes of the fuel rods 11. Note that in the illustrative embodiment of the invention shown in Fig. 2 that the sleeve 17 is in general axial alignment with the guide tube 12, and that the sleeve serves as a guide for the coil spring 22. The coil spring 22, moreover, also has a longitudinal axis that generally coincides with the longitudinal axis of the guide tube 12.
Attention is invited to Fig. 2 for a more detailed appreciation of the novel features of this ~' invention that characterize the invention. More parti-cularly, the control rod guide tube 12 is secured to a ~ "
lower grid 23 by means of a bolt structure 24. The bolt structure 24 has a head 25 that is received within the ad-jacent open end of the control rod guide tube 12. A bolt shank 26 extends through the lower grid 23 in order to protrude from the end support fitting 13. The protruding portion of the shank 26 is thr,eaded in order to receive a fastening nut 27. A nut retainer 30 is interposed between .
the end fitting and the nut 27 in order to prevent the nut from working loose and becoming disengaged from the fuel assembly.
As shown in Fig. 2, the control rod guide tube 12 extends through the main portion of the fuel assembly and - through an upper grid 16. r~ithin the upper grid 16 the guide tube 12 is telescoped within the sleeve 17, open end portion 31 of the control rod guide tube :L2 abutting and bearing against a flange or shoulder 32 that is formed within the inner surface of the sleeve 17. The shoulder 32 in the sleeve 17 transfers compression loads directly to the guide tube in the manner described subsequently in more complete detail.
Through the lengths of the control rod guide tube 12 and the sleeve 17 that are coextensive protrusions or "dimples" 33 are swaged or otherwise suitably formed in the control rod guide tube 12 and the sleeve 17 in order to hold `
the sleeve and the guide tube together and form a tight joint.
Immediately below the grill 14, circumscribing a portion of the sleeve 17 and bearing against a transverse surface of the grill 14 is a ring shaped collar 34. As shown, the collar 34 and the encircled portions of the sleeve 17 and the control rod guide tube 12 also are provided with protrusions or dimples 35, 36 that Kave been swaged or otherwise formed in the materials in order to position the collar 34 properly relative to the balance of the fuel assembly structure and to permit the collar to sustain loads imposed in the direction of control rod guide tube longitudinal axis 37 and to transfer these loads between the grill 14 and the combination sleeve 17 and control rod guide tube 12.
A washer 40 rests upon the transverse surface of the grill 14 that is opposite from the transverse grill surface that engages the collar 34. The coil spring 22 as illustrated 9 r f~ c U ~J
in Fig. 2, is mounted on the washer 40 and encloses a portion of the sleeve 17 that protrudes above the grill 140 The longitudinal axis of the coil spring 22 ~enerally coincides with the longitudinal axis 37 in order to press against a further washer 41. Thus, the coil spring 22 interposed between the grill 14 and the spider assembly 20, respectively biases the grill and spider assembly against the collar 34 and the lock 21.
Illustratively, the washer 41 is in engagement with the cellular spider assembly 20. As shown, the sleeve 17 is received within a cellular recess 42 in the spider 20 with sufficient clearance between the sleeve and the walls of the spider recess 4~ to permit the spider and the sleeve to move - relative to each other in the direction of the longitudinal axis 37.
A terminal portion 43 of the sleeve 17 pxotrudes above the spider 20 ln order to engage the lock 21. To engage r the lock 21, the outer surface of the portion 43 is provided with a circumferential groove 44 that forms a protruding shoulder 45 which serves to engage edges of the lock 21.
; Perhaps, as best shown in Fig. 3, the lock 21 is assembled from an arr`ay of resilient parallel plates 46, 47 that are meshed and interlock with similarly resilient plates 50, 51 that are generally perpendicular to the plates 46, 47 at the respective lines of intersection to form a cellular grid structure. As shown, the separation between the parallel plates 46, 47 is less than the maximum outside diameter of the groove 44 that is formed in the portion 43.
The plate 50 has a generally arcuate shape that conforms to and bears against a segment of the grooved surface of the terminal sleeve portion 43. The companion plate 51, however, has a plane profile that permits part of an edge of 1, ~9~,~5 this plate to engage the shoulder 45 (Fig. 2). In this manner, all of the control rod guide tubes 12 that are shown in Fig. 1 are locked together as a single unit.
sest shown in Figs. 2 and 3, the terminal sleeve portion 43 is provided with four longitudinal slots 52, 53, 54 and 55 that are parallel with the longitudinal axis 37.
The slots 52, 53, 54 and 55 each are spaced ~rom the next adjacent slots by about 90 and penetrate the portion 43 to a depth that is at least equal to the combined longi-tudinal depth of the shoulder 45 and the width of theplates 50, 51.
In accordance with an additional feature of the invention a grapple 56 is shown in Fig. 4. The grapple 56 releases the lock 21 from the control rod guide tube sleeves 17 and also provides a means for installing or removing as one entire unit the complete assembly that comprises the lock 21, the washers 40, 41, the spider 20, the coil springs 22 and the grill 14. To accomplish these results, the grapple 56 is provided with a member 57 that is movable in the direction of longitudinal axis 60. A transversely disposed linkage 61 is secured through a cross piece 62 (Fig. 5) to the vertically movable member 57. The end portions of the linkage 61 (Fig. 4) has slots 63, 64 which receive respective pins 6~, 66. The pins 65, 66 are transversely mova~le within the respective slots in order to ena~le two jaws 67, 7~ that are pivotally connected to a transversely disposed tool frame 71 to move in a scissors-like manner.
As shown in Fig. 4 the jaw 70 is provided at its exteme end with a clamp 73 that engages a longitudinal edge of the grill 14. In a similar manner, the extreme end of the jaw 67 also is provided with a clamp 74 that is 9~65 .
- oppositely disposed from the clamp 73 on the jaw 70.
Perhaps best shown in Fig. 5, a comPanion linkage 75 with pinned and ~ivoted jaws 76, 77 also are joined by means o~ the cross piece 62 to the longitudinally movable member 57. This companion structure matches and bala~ces the structural arrangement described above with res~ect to the jaws 67, 70.
:. -The transversely disposed tool frame ~1 also is pro~ided with an array of longitudinally aligned apertures 'h, 10 80 that each accommodate one of a grou~ of tools 81. As illustrated in Fig. 4, the t'ools 81iare formed from .. . .
generally cylindrical rods that are longitudinally aligned with the axis ~0. Each of the tools 81 has a generally conical end portion 82. The mid-section of the tool 81 has four fins 83, of which only three OftheSe fins are sholm in the plane of the drawing. As illustrated~ each of the fins 83 are spaced about 9Q from the next adjacent fins.
Each of the fins 83 has a tapered slope 84 in w~ich the narrow edge of`the slope is oriented toward ~he e~d portion B2. The tapered slope 84 ends in a generallr flat surface 85. The width of each of the fins 83 is slightly less than the transverse width of the indivdual slots 52, 53, 54, 55 (Figs. 2 and 3). The transverse depth of each of these fins, however, between the flat surFace 85 (Fig. 4) ana t~e adjacent surface of the tool 51 is greater than :
the correspondL~g wall thickenes5 of the terminal slee~e . ---portion 43 as s'~own in Figs. 2 and 3.
An annular collar 86 is secured to the tool 81and spaced longitud;nally from the flat suTfaces 85 on 3() the fLns 83 a sufficient distance to enable the fins when aligned ~ith the respective slots in the terminal sleeve 11~)3~b5 portîon 43 to bear against the terminal portion and prevent ~ the flat surfaces 85 of the fins 83 from penetrating the ; sleeve 17 to a depth greater than the longitudinal protru-sion of the slots ln the terminal sleeve portion 43 (Fig. 2~ above the spider 20.
As illustrated in ~ig. 4, the tool 81 has been '~hreaded-87 at the end.opposite from the end poItion 82 ; ' to enable nuts 90, 91 to secure the tool 81 to a trans- .
versely disposeL plate 92 that is movable in longitudinal directions as indicated by means of arrows 93, 94.under - :-the control of spring biased pneumatic cylinders 95, 96. ' ' Thus,''depending on the relative activation of the pneumatic cylinders 95j 96, the tools 81, when aligned with respect-ive terminal sleeYe portions 43 are driven into the sleeves . 17 to a sufficient depth to permit the flat surfaces 85' on the fins ~3 to bear'against the plates 46, 47 50, 51 (Figs. 2 and 3). The flat surfaces 83~press these plates in a radially outward direction relative to the longitudinal axis 37 through a distance that is sufficient to perm~t all .i.
of the plates to clear the shoulder 45 that is formed in 1' the terminal sleeve portion 43. In this manner the entire cellular lock 21 is ~eleased from its engagement with the sleeYes 17 and fixes itself temporarily to the tools 81 in'the array of tools.
In operation, and, as perhaps best understood ~:
through an examination of Fig. 6 the grapple 56 ~s aligned with the end fitting to permit the clamps 73 on t~e jaw 70 ~as well as the cl.amps 74 on the jaws 67, and the clamps o~ the jaws 76, 77 on the grapple that are not shown in Fig. 6) to be spaced outwaTdly of the grill 14, but within the same transverse plane as the grill.
~ 1-'9~5 During ~his phase of the operation of the grapple 56, the sprlngs associated wlth the springs loaded pins 97 aTe compressed through activation of the air cylindeI 95 whicfi moves the plate 92 in the direction of the arrow 93.
As illustrat~d-in Fig. 7, the clamps 73, 74 on ; . the jaNS 70, 67, respecti~ely, tas well as the changes on the cOmpaTiSOn pair of jaws 76, 77) swing inwardly in the directions indica~ed by arrows 101, 102 in oTder to grzsp firmly peripheral portionsof the grill 14. This inwardly swinging movement of the clamps 73, 74 is achieved through longitudinal movement of the member 57 in the direction of arrow 103. This movement of the member 57,causes the ~
pins 65, 66 to ride within the respective slots 63, 64 toward the longitudinal axis 60. The motion of these pins within the 510ts compels the jaws 67, 70 to pivot cente~-clockwise and clockwise, respectively, about the pivot 72 ~for the ~aw 70~ and a similar pivot tnot shown in ~ig. 7) foT the jaw 67.
20. . - The next.illustTative step in the technique for dismounting the end fitting from the balance of the fuel ; assembly is shown in Fig. 8. Thus, air cylinders 96 are activated to drive pis;on rods lD4 in the longitudinal directions indicated by means of arrow 105. The exposed ends of the piston rods 104 bear against the adjacent transverse surface of the ~pider 20. The force applied by the piston rods 104 to the spider 20 overcomes the oppositely directed forces e~tablished by means of the coil springs that are received on the sleeves, o~ wfiich the coil spring 22 and the sleeve 17 in Fig. 8 are illus-trati~e. In response to this new ~alance of ~orces the .. . .
11~35~5 spider 20 also moves in the longitudinal direction of the arTOW 105 in order to provide a longitudinal clear-ance 106 between the spider 20 and the lock 21 to relieve the force that the spider 20 applies to the lock 21.
In a typ;cal embod;ment of the invention, the next step~ in the technique involves movemen~ of the grapple 56 that is be~t illustrated in Fig. 9. Recall :for a moment . that the cellular structure of the lock 21 . is so designed that the groove 44 ~Fig. 2~ and the _shoulder 45 that is formed in the terminal sleeve portion - 43 engage the plàte.s 46, 47, 50, 51 tFig. 3) that comprise the -structure.of the cells in the lock 21.
. Turning now once more to Fig. 9, the air cylinders 95 are deactivated to ena~le the coiled springs on the spring loaded pins 97 to release and press the plate 92 in a longitudinal direction as indicated by an.
arrow 107. Because the recess and shoulders on the sleeves restrain the lock 21 from engaging in any longitudinal movement in the direction of the arrow 107, the tools that are fastened to the plate 92, of which the tools 81 is typical> are pressed thTough the individual cells in the - locks 21 into the TespeCtiVe sleeves 17. The fins 83 that pTotsude radially from the tools 81 also are driver. into matinp siots 52, 53, 5i, 55 ~ig. 2 and 3j. This ;~
longitudinal movèment of the tools 81 permits the tapered slope 84 of the pins 83 CFig 9) to press the plates 46, 47, 50, 51 on t~! lock 21 in a radially outward diTection n oTder to disengage these plates from the nested engagement withiII the annular groove 44 (Figs. 2 and 3) that is formed ill the terminal sleeve portion 43.
In those circumstances, further longitudinal ~ r ~,-1 lLJ~ ~V
movement of the tools 81~(Fig. 9) in the direction of the aTrow 107 under the force of the released springs on the pins 97 is limitea o~ly~~by the braking action of the collars - 86 on eac~ of the tools. The collar 86 is so spaced relative ~o the lock 71 that the plates which foTm each of the cells in the lock 21 are forced onto the corresponding flat surface 85 of the fins 83. I'he effect of this engagement ~etween the plates that form t~e cells on the lock'21 and the 1a~ surfaces 85 of the fins 83 is to 10 , press the plates out of e,ngagement with the respective annular-grooves 44 (Figs. 2 an,d 3) and'shoulders 45.
' In the'next illustrative disassembly step , the - . - - . .
- enti~e grapple 56 is moved,longitudinally,in the direction - - . . . ~ ~ ......................... .. . .
of arrow 108. 'The grapple, withdrawn from'the balance of the fuel assembly in the foregoing manner, takes with it most of the e~d fitting components in'their'pToper relative position. Typically, the lock 21, the spider 20, and the gTill 14 ~emain with the grapple 56. The coil springs 22 with their associated washers 40, 41 (Fig. 2) also are drawn away with the grapple 56 (Fig. 9). In this instance, the tools 81 serve as temporary spring guides or keepers for the coil springs 22 and the washers. The springs--22, moreover, serYe to keep an approximately proper longitudinal s'eparation between the grill 14 and the spider 20. Note in th~^s Tespect that the sleeves 17 remain ~ith the ~alance of the fuel ass'em~ly.
To reassemble the end fitting components on t~e main portion of the fuel assembly, t~e end portion 82 of the tools 81 on the grapple 56 are longitudina~y aligned ~ith thei.r respective sleeves. ~he grapple 56 then is moved longitudlnally m the direction of the : ~
~ 5 arrow 107 untll each of the tools 81 are fully seated in the respective sleeves 17. One or more clamps ~not shown n the'drawing) hold the lock 21 in suitableposition relative to the. grooves 44, CFigs. 2 and 3~ and shoulders 45 on the terminal sleeve portion 43. In this condition the-air cylinders 95 ~Fig. 9) are activated to compress the spTings on the spring loaded pins 97, thereby extracting the pins 83 from engagement with the plates that form the cells in the lock 21. The disengagement ,,,, . I
-10 ' of the tools 81'and the lock 21 permits the plates that . form each'of.the lock's cells to snap back into the annu-- - - - . . . I
lar recesses 44 ~Figs. 2 and 3) and shoulders 45 in the.
terminal sleeve portion 43. - '. -. . -~
.
The spider 20 ~Fig. 9) under the action vf the ' .
coil springs 22 bears against the adjacent surfa e of the -lock 21. The member 57, moreover, is moved longitudinally .
.in the direction of the àrrow 107 to permit the jaws 67, ', , 70 to pivot in clockwise and counter-clockwise directions, respectively. ~his pivoting movement of the jaws 67, 70 releasés the grip that the clamps 73, 74 had on the grill 1' 14. The further clamps (not shown in the drawlng) that ' . engage the lock 21 also are removed.
The entire end fitting now is reassembled on the balance of the fuel asse~bly in a manner that clearly avoids the prior art requirement for tedious, detailed, p;ece-~y-piece disassembly and reassem~ly. Th~s techni-que that characterizes the inYention also avoids the hazards that might attend the loss of one of these small end fitting components, and the like.
Claims
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A control rod guide tube assembly comprising a hollow control rod guide tube having at least one open end, a hollow -cylindrical sleeve telescoped over a portion of said guide tube, said sleeve having a flange formed on the inner surface thereof to engage said control rod guide tube, an annular groove formed in the outer surface of said sleeve, said sleeve having an end portion having at least one longitudinally arrayed slot that extends through said annular groove, a collar circumscribing a portion of said telescoped guide tube and sleeve, said collar and circumscribed guide tube and sleeve portions being joined together to form an integral control rod guide tube assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA380,043A CA1129565A (en) | 1977-10-26 | 1981-06-17 | Control rod guide tube assembly |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US845,767 | 1977-10-26 | ||
| US05/845,767 US4208248A (en) | 1977-10-26 | 1977-10-26 | Fuel assembly with a removable end fitting |
| CA308,864A CA1110783A (en) | 1977-10-26 | 1978-08-08 | Fuel assembly with a removable end fitting |
| CA380,043A CA1129565A (en) | 1977-10-26 | 1981-06-17 | Control rod guide tube assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1129565A true CA1129565A (en) | 1982-08-10 |
Family
ID=27165792
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA380,043A Expired CA1129565A (en) | 1977-10-26 | 1981-06-17 | Control rod guide tube assembly |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA1129565A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112837832A (en) * | 2020-12-30 | 2021-05-25 | 中国原子能科学研究院 | Rotary type material changing special structure for replacing outer sleeve of control rod assembly |
-
1981
- 1981-06-17 CA CA380,043A patent/CA1129565A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112837832A (en) * | 2020-12-30 | 2021-05-25 | 中国原子能科学研究院 | Rotary type material changing special structure for replacing outer sleeve of control rod assembly |
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