Patent Number: 042785014
Section: description

Referring now to the drawing, there is shown in FIG. 1 a perspective view as seen from the top onto the head 1 of a fuel assembly formed of a multiplicity of fuel rods 2. The head member 1 of this fuel assembly is connected to a non-illustrated base member by guide tubes 3 and, together with spacers 21, forms the rigid frame or skeleton of such a fuel assembly. The fuel rods 2 per se are held at a mutual spacing within this frame by the spacers 21 but can expand freely in axial direction. To control this nuclear reactor, control rods formed at least in part of neutron-absorbing materials are immersed in the guide tubes 3. In the interst of clarity, these control rods are not shown in detail, however, especially since illustration thereof is unnecessary for an understanding of the invention. The head 1 of the fuel assembly if formed in the conventional embodiment of FIGS. 1 and 2, by a laterally cut-out frame and has, at an end face thereof, four bores 5 for receiving adjusting or dowel pins which are fastened to a non-illustrated hold-down plate. A spring element 4 protrudes from the frame on both sides of each bore 5 for resiliently bracing or supporting the frame at the non-illustrated hold-down plate. The subject of the invention of the instant application is a spring element for holding down fuel assemblies which is an improvement over the conventional spring element illustrated in FIG. 1 which is mounted in the fuel assembly head. The conventional spring element of FIG. 1 is shown in enlarged and greater detail in FIG. 2. As is clearly shown in FIGS. 1 and 2, the conventional spring element 4 is formed of a pin which is slidably mounted in bores 11 and 12 provided in the fuel assembly head. A compression spring 41 is braced against the bottom of the fuel assembly head and forces the pin 4 upwardly in the illustrated manner. The upper end of this spring 41 rests, for this purpose, against stop 42 which is laterally inserted into a transverse slot formed in the pin 4. In FIG. 3, there is shown an embodiment of a new spring element 6 according to the invention, partly in longitudinal cross section, and in FIG. 4, the spring element 6 is shown, likewise in longitudinal section, but further in inserted position thereof in a fuel assembly head in a manner similar to the view of the conventional device of FIG. 2. In this regard, it is noted that FIGS. 2 and 4 represent longitudinal sections through the fuel assembly head of FIG. 1 taken along the line II--II in direction of the arrows. It can be seen, especially from FIG. 3, that the spring element 6 according to the invention is a part separate from the fuel assembly, and is inserted as a whole into the fuel assembly head 1 from the top, as shown in FIG. 4. The fuel element 6 can therefore also be withdrawn again as a whole; an operation which presents no difficulties even if performed by remote control. Also readily evident in FIG. 4 is the gain in "resilient length" of the spring element 6 for the same overall length that it has with respect to the coventional spring element 4 of FIG. 2. The spring element 6 is assembled telescopically of three parts, namely, an upper sleeve 6a, a screw bolt 6b and a lower sleeve 6c. The upper sleeve 6a is provided with a collar or shoulder 62, and the lower sleeve with a collar or shoulder 63 which serve as stops for the spring 61. The threaded bolt 6b is screwed into the lower sleeve 6c and thereby adjustable in length; the lower projecting end 64 of the threaded bolt 6b is provided for engagement in a bore 14 formed in the fuel assembly head 1. Movement of the projecting bolt end 64 in the fuel assembly head 1 is not possible, and interference thereof with fuel rods may possibly be located therebelow which is therefore precluded. The upper sleeve 6a is formed with an internal shoulder 66 by which it is braced against the head 67 of the threaded bolt 6b and can be forced downwardly on the latter telescopically against the force of the spring 61. To prevent rotation of the lower sleeve 6c on the threaded bolt 6b, which would result in a change in length of the entire spring element 6 and also to a change in the initial stress or pre-tensioning force thereof, a conventional screw securing device such as a pin 65 or a spot weld or any other rotation-preventing device known in the prior art is provided. This new spring element 6 according to the invention has not only the advantages of simplicity of construction, manufacture without problems, individual adjustibility with respect to length and initial spring stress, as well as ease of installation in the fuel-assembly head, but also the great advantage that it can be used instead of heretofore-known spring elements according to the state of the art, such as the elements 4 of FIGS. 1 and 2. For this purpose, it is necessary merely to enlarge the bore 11 (note FIG. 2) so that a bore 13 (FIG. 4) having a somewhat larger bore diameter is formed. This is an operation which can be performed without any problem on all fuel assembly heads employed heretofore, so that the new spring elements 6 according to the invention also can be exchanged for the heretofore employed ones, such as the spring elements 4 of FIG. 2, especially if there is a change in the operating condition. It is also possible, of course, to use these spring elements 6 according to the invention in fuel assembly heads of different construction than that shown in FIG. 4, since such heads need only to be provided with the bores 14 and 13 for receiving this spring element 6. In the illustrated embodiment of the instant application, eight such spring elements 6 have been provided for each fuel assembly head 1, but this number is in no way characteristic or limiting, since the required spring force for each fuel assembly is able to be adjusted or set by suitably selecting the strength of the individual springs 61 as well as the number of spring elements 6 themselves. In conclusion, yet another advantage of this new construction should be noted, namely that even in the event of a break in the spring 61, no loose parts can result, which would otherwise require retrieval at all costs at great expense for specialized apparatus for this purpose and in time consumption.