WO1996019811A1

WO1996019811A1 - Fuel assembly and spacer for a nuclear reactor

Info

Publication number: WO1996019811A1
Application number: PCT/SE1995/001472
Authority: WO
Inventors: Dietmar Wolfram
Original assignee: Abb Atom Ab
Priority date: 1994-12-21
Filing date: 1995-12-07
Publication date: 1996-06-27
Also published as: SE9404433D0; SE503776C2; EP0871959A1; US5862196A; JPH10510925A; SE9404433L

Abstract

The present invention relates to a spacer (7) comprising a plurality of cells (9) to retain and mutually fix, at a plurality of spacer levels, parallel, elongated elements (3, 8), extending through the cells, into a bundle in a fuel assembly for a nuclear reactor. A coolant is adapted to flow from below and upwards through the fuel assembly. Between the cells (9) of the spacer (7), secondary channels (10) are formed. The invention is characterized in that at least the majority of the spacer levels in the secondary channels (10) comprise at least two deflection members (14) which are axially spaced-apart in the direction of flow for guiding at least part of the coolant flow towards the fuel rods which are aranged close to the secondary channels (10).

Description

Fuel assembly and spacer for a nuclear reactor

TECHNICAL FIELD

The present invention relates to a fuel assembly and a spacer for a light-water nuclear reactor, more particularly a boiling water reactor or a pressurized-water reactor. The fuel assembly comprises a bundle of elongated fuel rods retained and fixed by a number of spacers arranged in spaced relation- ship to each other along the bundle. The spacers comprise a number of cells for mutually fixing the fuel rods. A coolant, for example water, is adapted to flow from below and up through the normally vertically arranged fuel assembly and, during a nuclear reaction, to cool the fuel rods arranged in the assembly.

BACKGROUND ART, PROBLEMS

A fuel assembly in a boiling water nuclear reactor consists of an elongated tubular container, often with a rectangular or square cross section, which is open at both ends forming a continuous flow passage, through which the coolant of the reactor is able to flow. The fuel assembly comprises a large number of equally elongated tubular fuel rods, arranged in parallel in a certain definite, normally symmetrical pattern. At the top, the fuel rods are retained by a top tie plate and at the bottom by a bottom tie plate. To allow coolant in the desired manner to flow past the fuel rods, it is important to keep them at a distance from each other and prevent them from bending or vibrating when the reactor is in operation. For this purpose, a plurality of spacers are used, distributed along the fuel assembly in the longitudinal direction.

A fuel assembly for a pressurized-water nuclear reactor has, in principle, the same design as a fuel assembly for a boiling water nuclear reactor, apart from the fact that the fuel rods are not enclosed by any tubular container and the fact that their number is higher.

Between the fuel rods secondary channels are formed, through which the coolant flows through the fuel assembly.

An important factor when designing a spacer for a light-water reactor is to ensure that the spacer brings about a good cooling of the fuel rods by a suitable mixing of the coolant. In those cases where the cooling is not sufficient, so-called dryout may occur in a boiling water reactor and so-called DNB (Departure from Nucleate Boiling) may occur in a pressurized- water reactor. In serious cases, dryout and DNB, respectively, give rise to penetration of the fuel rods.

The spacers thus influence the flow of the coolant and hence the cooling of the fuel. It is known that, in a region imme¬ diately below the spacer where the coolant has still not passed through the spacer, a deterioration of the coolant film on the fuel rods occurs, whereas in a region above the spacer, where the coolant has just passed through the spacer, a rein¬ forcement of the water film instead occurs. The reinforcement of the coolant film is due to the turbulence which arises in the coolant when it passes through a spacer. The greatest risk of dryout exists in the upper part of the fuel immediately below the spacers.

One way of increasing the cooling of fuel rods by means of the arrangement of guide vanes at the downstream edge of the spacer in the fuel assembly is described in WO 91/13442. Two or four guide vanes are arranged extending from the mentioned edge and curved in such a way that a swirl is formed in the upwardly flowing coolant. Further, the guide vanes are exposed and may become damaged in connection with the mounting of the fuel rods. Another method is described in SE 9303583-0. The spacer described in this document comprises an orthogonal latticework formed from sleeves, in which guide vanes are formed as tabs in the sleeve material. The disadvantage of this solution is that the larger the tab chosen, the larger part of the suppor¬ ting length of the fuel rod is lost.

Known spacers are often designed completely or partially of Inconel which is a material with a good strength and good properties as far as manufacture of spacers is concerned.

However, it is desirable to manufacture spacers of a material with less ability to absorb neutrons, that is, a low-absorbing material, for example a zirconium alloy. Spacers of zirconium alloy are an advantage from the point of view of reactivity economy. In addition, spacers of a low-absorbing material are less radioactive after irradiation, which is an advantage when handling these after reactor operation.

The object of the invention is to provide a spacer which gives good cooling, small flow resistance, and which is simple to manufacture and, in addition, is possible to construct of zirconium alloy.

SUMMARY OF THE INVENTION, ADVANTAGES

The present invention relates to a fuel assembly and a spacer completely or partially made of zirconium alloy for a nuclear reactor wherein the spacer comprises an orthogonal lattice¬ work, composed of spacer cells, wherein each cell positions an elongated element, extending through the cell, at a plurality of spacer levels, for example a fuel rod or a control rod guide tube. Between the fuel assemblies, so-called secondary channels are formed for the passage of coolant flow through the fuel assembly. In at least the majority of these secondary channels, at least in the majority of spacer levels, so-called guide vane trees with a trunk and branches are arranged. The trunk consists, for example, of a rectangular plate with its longitudinal edge arranged parallel to the flow, or of a pipe or of sheet-metal strip, shaped like a helical spring, arranged with its respective conceived centre line parallel to the coolant flow. The branches project from the trunk at at least two axially separated levels along the trunk and conduct the coolant flow towards the fuel rods arranged around the guide vane tree.

The coolant flowing in the fuel assembly, that is, through the primary channel, from below and upwards, first reaches the trunk of the tree which preferably has a minimum extension across the direction of flow. The trunk conducts the coolant to the branches, or guide vanes, of the tree. By the axial distribution of the guide vanes along the length of the trunk, the coolant flow is diverted in several steps, whereby the control of the coolant flow towards the fuel rods is ensured.

The guide vane tree is intended to be arranged in a secondary channel and between the spacer cells which surround the secondary channel, or at the downstream edge of the spacer cells.

The size and length of the guide vane tree may be varied depending on where in the fuel assembly it is intended to be arranged. The shape of the guide vanes may vary for optimi¬ zation of the control of the coolant flow. The guide vanes may, for example, be smooth or arched. The need to stir and direct the coolant towards the fuel rods is greatest down- stream of the fuel assembly where the steam content, and hence the risk of so-called dryout, is greatest. Each guide vane contributes to the pressure drop across the fuel assembly. Upstream of the fuel assembly, guide vanes may be completely omitted in order to reduce the total pressure drop. In a particularly advantageous embodiment, the guide vane tree has the same extent in the flow direction as the spacer cells and are arranged therebetween so that the guide vane tree does not project from the spacer. The advantage of this design is that the cells in the spacer reflect the coolant towards the guide vane tree such that a greater part thereof may be diverted thereby.

Each spacer which is provided with a plurality of guide vane trees according to the invention may, in addition, be provided with conventional structural parts such as a four-sided frame or skirt comprising the whole bundle.

The advantage of the invention is that a spacer, which in the majority of the secondary channels is provided with guide vane trees, provides good cooling of the fuel rods arranged around the guide vane tree, whereby the output power from the fuel assembly may be increased. Further, the guide vane tree con¬ stitutes a small flow resistance which is important, not least from the point of view of two-phase pressure drop, that is, the pressure drop which usually arises in the upper part of the fuel assembly where the steam mixture contains the two phases water and steam.

Another advantage of the invention is that the design of the guide vane tree permits a simple manufacturing process.

Still another advantage is that the guide vane tree is possible to construct in zirconium alloy. Using zirconium alloy instead of Inconel in the spacers entails, inter alia, a reduction of the radiation to which reactor personnel are exposed, the so-called personnel dose. The reason for the influence on the personnel dose is that, upon irradiation of nickel which is part of Inconel, radioactive cobalt isotopes are formed in the process water. Smaller amounts of nickel thus lead to a lower cobalt content, which causes the personnel dose to be reduced. The design of the guide vane tree permits considerable options for guiding the flow in an optimum manner and achieving good cooling. Some of these embodiments will be described below under the description of the preferred embodiments.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention will be most readily understood with reference to the accompanying drawings.

Figure 1 shows a fuel assembly for a boiling water reactor.

Figure 2 shows a fuel assembly for a pressurized-water reactor.

Figures 3a-d show different types of spacer structures.

Figures 4a-c show, in a view from the side and in a view from above, an embodiment of a guide vane tree according to the invention with two axially spaced-apart guide vanes.

Figures 5a-c show, in a view from the side and in a view from above, an embodiment of a guide vane tree according to the invention with three axially spaced-apart guide vanes.

Figures 6a-d show, in a view from the side and in a view from above, an embodiment of a guide vane tree according to the invention with four axially spaced-apart guide vanes.

Figures 7a-c show, in a view from the side and in a view from above, an embodiment of a guide vane tree according to the invention with four guide vanes, of which three are spaced apart in the axial direction. Figures 8a-d show, in principle, in a view from the side and in a view from above, different ways of attaching a guide vane tree according to the invention to a spacer structure.

Figures 9a-b show an embodiment, in a view from the side and in a view from above, respectively, of a guide vane tree according to the invention with four axially spaced-apart guide vanes arranged externally on the surface of a helical spring-shaped trunk.

Figures lOa-b show an embodiment, in a view from the side and in a view from above, respectively, of a guide vane tree according to the invention with four axially spaced-apart guide vanes arranged internally on the surface of a helical spring-shaped trunk.

Figures lla-b show an embodiment, in a view from the side and in a view from above, respectively, of a guide vane tree according to the invention with four axially spaced-apart guide vanes arranged on the surface of a pin-shaped trunk.

Figures 12a-b show an embodiment, in a view from the side and in a view from above, respectively, of a guide vane tree according to the invention with four axially spaced-apart guide vanes arranged externally on the surface of a tubular trunk.

Figures 13a-b show an embodiment, in a view from the side and in a view from above, respectively, of a guide vane tree according to the invention with four axially spaced-apart guide vanes arranged internally on the surface of a tubular trunk.

Figures 14a-b show an embodiment, in a view from the side and in a view from above, respectively, of a guide vane tree according to Figures 6a-d, wherein the guide vanes exhibit an arched surface.

Figure 15 shows an explanatory sketch of how the guide vane trees direct the coolant flow towards the surrounding fuel rods in part of a fuel assembly according to Figure 1 or 2. All the guide vane trees are adapted to direct the flow in the counterclockwise direction.

Figure 16 shows the same as in Figure 15, but the guide vane trees are adapted to alternately direct the flow in a counter¬ clockwise and a clockwise direction, respectively.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

Figure 1 shows a boiling water reactor fuel assembly 1 which comprises an elongated tubular container, of rectangular cross section, referred to as fuel channel 2. The fuel channel 2 is open at both ends so as to form a continuous flow passage through which the coolant of the reactor flows. The fuel assembly 1 comprises a large number of equally elongated tubular fuel rods 3, arranged in parallel in a bundle, in which pellets 4 of a nuclear fuel are arranged. The fuel rods 3 are retained at the top by a top tie plate 5 and at the bottom by a bottom tie plate 6. The fuel rods 3 are kept spaced from each other by means of spacers 7 and are prevented from bending or vibrating when the reactor is in operation.

Figure 2 shows a pressurized-water reactor fuel assembly 1 which comprises a number of elongated tubular fuel rods 3 and control rod guide tubes 8 arranged in parallel. The fuel rods 3 contain pellets 4 of a nuclear fuel. The control rod guide tubes 8 are retained at the top by a top nozzle 5 and at the bottom by a bottom nozzle 6. The fuel rods 3 are kept spaced from each other by means of spacers 7. Figure 3a-b show, in perspective views, a spacer 7 with an orthogonal latticework. Figure 3 shows a spacer 7 composed of sleeves 9 wherein each sleeve 9 is intended to position an elongated element, extending therethrough, for example a fuel rod 3 or a control rod guide tube 8. Figure 3b shows a spacer 7 composed of cells 9. Between the fuel rods 3 arranged in the cells 9 and the sleeves 9, respectively, channels 10, referred to as secondary channels, are arranged. Figures 3c-d show, in a view from above and a view from the side, respectively, a latticework of sheet-metal strips 9a, 9b, arranged crosswise and standing on edge, which are surrounded by a frame 9c.

Figure 4-13 illustrate several alternative embodiments of guide vane trees according to the invention. Figures 4-8 show an example with two, three or four branches arranged at a trunk in the form of a substantially rectangular plate arranged parallel to the substantial coolant flow. Figures 9- 13 show alternative embodiments of the guide vane tree.

Figure 4a shows a blank for a guide vane tree 11 with a first and a second folding line 12a, b and a centre line 13 where the angle of the folding lines 12a, b to the centre line 13 is designated μ° and shown to be 45°. A first tab 14a to the left of and above the first folding line 12a is intended to be folded 90° around the first folding line 12a in a direction towards the viewer whereas a second tab 14b to the right of and above the second folding line 12b is intended to be folded 90° around the second folding line 12b and in a direction away from the viewer. When the first and second tabs 14a, b are folded down, an appearance of the guide vane tree 11 from the side as shown in Figure 4b is obtained. Figure 4c shows the guide vane tree 11 in a view from above arranged between four fuel rods 3. The tree 11 is attached to a structure which is comprised by the spacer 7 and which consists of sheet-metal strips, arranged crosswise and standing on edge, which form cells through which the fuel rods 3 are running. Figure 5a shows a blank for a guide vane tree 11 with a first, a second and a third folding line 12a, b, c and a centre line 13. The blank is provided with a slit 15a arranged between the second 12b and third 12c folding lines and the centre line 13. A first tab 14a to the left of and above the first folding line 12a is intended to be folded 90° around the first folding line 12a, in a direction towards the viewer. A second tab 14b to the right of and above the second folding line 12b is intended to be folded 90° around the second folding line 12b, in a direction away from the viewer and 90° around the centre line 13, in a direction towards the viewer. A third tab 14c arranged to the right of and above the third folding line 12c is intended to be folded 90° around the third folding line 12c and in a direction away from the viewer. When the first, second and third tabs 14a, b, c are folded to their final positions, an appearance of the guide vane tree 11 from the side as shown in Figure 5b is obtained. Figure 5b also shows a fourth and fifth folding line 16a, b on each side of the centre line 13. On each outer side of the fourth 16a and fifth 16b folding lines, respectively, a first 17a and a second 17b attachment tab are folded around the fourth 16a and fifth 16b folding lines, respectively, in a direction towards the viewer. The angle for the folding is adapted to the available space. Further, the blank is folded around the centre line 13 in a direction away from the viewer so as to form an angle d° of 120° in the figure, between the fourth 16a and fifth 16b folding lines. Figure 5c shows the guide vane tree 11 in a view from above arranged between four fuel rods 3. The tree 11 is attached to a structure which is comprised by the spacer 7 and which consists of sheet-metal strips, arranged crosswise and standing on edge, forming cells through which the fuel rods 3 are running.

Figure 6 shows a guide vane tree of a particularly advan- tageous design. Figure 6a shows a blank for a guide vane tree 11 with a first, a second, a third, and a fourth folding line 12a-d as well as a centre line 13. The blank is provided with a first slit 15a arranged between the second 12b and third 12c folding lines and the centre line 13 and a second slit 15b arranged between the third 12c and fourth 12d folding lines and the centre line 13. A first tab 14a to the left of and above the first folding line 12a is intended to be folded 90° around the first folding line 12a, in a direction towards the viewer. A second tab 14b to the right of and above the second folding line 12b is intended to be folded 90° around the second folding line 12b, in a direction away from the viewer and 90° around the centre line 13, in a direction away from the viewer. A third tab 14c is arranged to the right of and above the third folding line 12c and intended to be folded 90° around the third folding line 12c and in a direction away from the viewer and 90° around the centre line 13, in a direction towards the viewer. A fourth tab 14d arranged to the right of and above the fourth folding line 12d is intended to be folded 90° around the fourth folding line 12d, in a direction away from the viewer. When the first, second, third, and fourth tabs 14a-d are folded to their final positions, an appearance of the guide vane tree 11 from the side as shown in Figure 6b is obtained. Figure 6c shows the guide vane tree 11 in a view from above arranged between four fuel rods 3 in a structure of sleeve spacers 9 of the type shown in Figure 3a. Figure 6b also shows a fifth 16a and a sixth 16b folding line on each side of the centre line 13. Figure 6d shows that, on the outer side of the fifth folding line 16a, a first attachment tab 17a is folded around the fifth folding line 16a in a direction away from the viewer. On the outer side of the sixth folding line 16b, a second attachment tab 17b is folded around the sixth folding line 16b in a direction towards the viewer. Figure 6d shows the guide vane tree 11 in a view from above arranged between four fuel rods 3. The guide vane tree 11 is attached in a structure which is comprised by the spacer 7 and which consists of sheet-metal strips, arranged crosswise and standing on edge, forming cells through which the fuel rods 3 are running. The somewhat twisted attachment of the guide vane tree 11 at an angle β°, in the figure shown to be 20°, gives an optimum cooling of the surrounding fuel rods 3. The loca¬ tion of the guide vane tree 11, rotated through an angle of β°, may also be used for spacers 7 of the type indicated in

Figure 3a.

Figure 7 shows a guide vane tree 11 with four guide vanes 14a- d, as shown in Figure 6, but where two of the guide vanes 14a, b are placed at the same level. Figure 7a shows a blank for a guide vane tree 11 with a first, a second, a third, and a fourth folding line 12a-d as well as a centre line 13. The blank is provided with a first slit 15a arranged between the second 12b and third 12c folding lines and the centre line 13 and a second slit 15b arranged between the third 12c and fourth 12d folding lines and the centre line 13. The first tab 14a to the left of and above the first folding line 12a is intended to be folded 90° around the first folding line 12a, in a direction towards the viewer. The second tab 14b to the right of and above the second folding line 12b is intended to be folded 90° around the second folding line 12b, in a direction away from the viewer and 90° around the centre line 13, in a direction away from the viewer. The third tab 14c is arranged to the right of and above the third folding line 12c and intended to be folded 90° around the third folding line

12c and in a direction away from the viewer and 90° around the centre line 13, in a direction towards the viewer. The fourth tab 14d arranged to the right of and above the fourth folding line 12d is intended to be folded 90° around the fourth fold- ing line 12d, in a direction away from the viewer. When the first, second, third, and fourth tabs 14a-d are folded to their final positions, an appearance of the guide vane tree 11 from the side as shown in Figure 7b is obtained. Figure 7c shows the guide vane tree 11 in a view from above arranged between four fuel rods 3 in a structure of sleeves 9, also shown in Figure 3a. Figure 8 shows in a view from the side the attachment of a guide vane tree 11 of the same type as that shown in Figure 6b. Figure 8a shows an attachment where the guide vane -tree 11 is intended to project outside the upper edge of the spacer 7, this upper edge being arranged at the reference numeral 18. Figure 8b shows an attachment where the guide vane tree 11 is intended to be arranged fully immersed into the spacer 7. This is a particularly advantageous embodiment when the guide vane tree is fully integrated into the structure. The immersed location gives the tree good protection against external influence during, for example, mounting of fuel rods. Figure 8c shows in a view from the side how the guide vane tree 11 may be attached on one side to the spacer 7. This one-sided attachment is also clear from Figure 8d, showing a view from above. The guide vane tree 11 may, of course, also be attached on three or four sides, although this is not explicitly shown in any figure.

Figure 9a shows in a view from the side a guide vane tree 11, the trunk of which consists of a sheet-metal strip twisted into a helical spring 19. Four guide vanes 14 are attached to the outwardly facing surfaces of the helical spring 19, at different levels and with an angular pitch of 90°. The guide vanes 14 consist of square plates folded 90° around their respective diagonals and attached to the helical spring 19 by one plate edge 14e. Figure 9b shows the guide vane tree 11 according to Figure 9a in a view from above.

Figure 10a shows in a view from the side a guide vane tree 11, the trunk of which consists of a sheet-metal strip twisted into a helical spring 19, as in Figure 9. In the surfaces of the helical spring 19, along three out of four sides, four square tabs are punched out at different levels and with a 90° angular pitch. The non-punched side 20 is parallel to a con- ceived centre line 13 through the helical spring 19. The square tabs are then folded 90° around a line through the non- punched side 20 and 90° around a diagonal through the square tab. Figure 10b shows the guide vane tree 11 according to Figure 10a in a view from above.

Figure 11a shows a guide vane tree 11, the trunk of which consists of a solid pin 21 to which are attached guide vanes 14 in the same way as in Figure 9. Figure lib shows the guide vane tree 11 according to Figure 11a in a view from above.

Figure 12a shows a guide vane tree 11, the trunk of which consists of a tube 22 to which are attached guide vanes 14 in the same way as in Figures 9 and 11. Figure 12b shows the guide vane tree 11 according to Figure 12a in a view from above.

Figure 13a shows a guide vane tree 11, the trunk of which consists of a tube 22 to which are attached guide vanes 14 in the same way as in Figure 10. Figure 13b shows the guide vane tree 11 according to Figure 13a in a view from above.

Figures 14a b show a guide vane tree 11 corresponding to that shown in Figure 6 but where the guide vanes 14a-d exhibit an arched shape. Figure 14a shows the guide vane tree 11 with arched guide vanes 14a-d in a side view and Figure 14b shows, in a view from above, the guide vane tree 11 arranged between four fuel rods 3, each surrounded by a spacer cell 9.

Figure 15 is a sketch showing the principle of how the guide vane trees 11 direct the coolant flow towards the fuel rods 3, arranged around them, in part of a fuel assembly according to Figure 1 or 2. All the guide vane trees 11 are adapted to direct the flow in a counterclockwise direction.

Figure 16 is a sketch showing the principle of how the guide vane trees 11 direct the coolant flow towards the fuel rods 3, arranged around them, in part of a fuel assembly. The guide vane trees 11 are alternately adapted to direct the flow in a counterclockwise and a clockwise direction, respectively.

Common to the exemplified guide vane trees is that the coolant, flowing from below and upwards, is diverted in several stages. When the coolant reaches the lowermost tab, the coolant changes direction and is deflected away from the tree. The tab arranged immediately above is reached by coolant which has already, at least partially, been diverted with the aid of the change of the direction of the coolant caused by the tabs located below. By series connection of tabs which are arranged axially displaced, the coolant is deflected upon passage of the guide vane tree. By this series connection of axially displaced tabs, an increased cooling capacity and a reduced pressure drop are obtained in comparison with tabs positioned in one and the same plane.

In those cases where the guide vane tree is arranged immersed in the spacer structure and the spacer structure consists of a sleeve structure corresponding to that shown in Figure 3a, part of the upwardly flowing coolant is guided by the sleeve walls and towards the guide vanes. By arranging the guide vane tree inside the spacer, the effect of the spacer is thus increased.

The shape of the guide vane tree may be varied in many ways with respect to the size, the shape, the number, the deflec¬ tion in relation to the trunk, and the location of the vanes along the trunk.

In all the figures, the deflection member 14 are folded 90° around the folding lines 12. For optimum function, however, an arbitrary magnitude of this angle may be chosen. The same applies to the angle μ of the folding lines 12 to the centre line 13, which in all the figures is shown as 45° but may be chosen arbitrarily to achieve an optimum function. In the embodiments according to Figures 9-13, it may be of interest in certain cases to arrange more than four axially spaced- apart deflection members 14 along the guide vane (19, 21. 22).

It is possible to construct the guide vane trees of Inconel or of a zirconium alloy.

Claims

1. A spacer (7) comprising a plurality of cells (9) to retain and mutually fix, at a plurality of spacer levels, parallel, elongated elements (3, 8), extending through the cells, into a bundle in a fuel assembly for a nuclear reactor where a coolant is adapted to flow from below and upwards and where, between the cells (9), secondary channels (10) are formed, characterized in that at least the majority of the spacer levels in the secondary channels (10) comprise at least two deflection members (14) which are axially spaced-apart in the direction of flow for guiding at least part of the coolant flow towards the fuel rods which are arranged close to the secondary channels (10) .

2. A spacer (7) according to claim 1, characterized in that the deflection members (14) are arranged at a guide vane (13a, 19, 21, 22) for guiding the coolant flow to the deflection members (14) .

3. A spacer (7) according to claim 2, characterized in that the guide vane (13a) is designed as a substantially rectangu¬ lar plate and that the deflection members (14) are arranged in the form of tabs at the longitudinal edge of the guide vane (13a) .

4. A spacer (7) according to claim 2, characterized in that the guide vane (19) is designed as a spiral and that the deflection members (14) are arranged at the inner or outer surface of the spiral.

5. A spacer (7) according to claim 2, characterized in that the guide vane (22) is designed as a tube and that the deflec¬ tion members (14) are arranged at the inner or outer surface of the tube.

6. A spacer (7) according to claim 2, characterized in that the guide vane (21) is designed as a pin and that the deflec¬ tion members (14) are arranged at the envelope surface of the pin.

7. A spacer (7) according to claim 1, characterized in that the deflection members (14) are adapted to direct the coolant in at least two directions in a plane separated from the main flow direction.

8. A spacer (7) according to claim 1, characterized in that the axial extent in the flow direction of the deflection members (14) is smaller than or equal to the axial extent of the spacer (7) in the flow direction and that the deflection members are completely surrounded by the spacer cells (9) comprised by the spacer (7) .

9. A spacer (7) according to claim 1, characterized in that the deflection members (14) are four in number.

10. A spacer (7) according to claim 1, characterized in that the deflection members (14) are arranged relative to each other with a pitch angle.

11. A spacer (7) according to claim 1, characterized in that the deflection members (14) and the guide vanes (13a, 19, 21, 22) are made of a zirconium alloy.

12. A spacer (7) according to claim 1, characterized in that the deflection members (14) are arched.

13. A fuel assembly (1) for a nuclear reactor with a bundle of elongated elements (3, 8) retained by a plurality of spacers (7), arranged at different spacer levels along the bundle, each one of these spacers (7) comprising a plurality of spacer cells (9) between which are formed secondary flow channels (10) , characterized in that it comprises spacers (7) according to claim 1.