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ABSTRACT (CONT.) However, the efficiency of fuel cycle can be improved by increasing the fuel residence time in the core up to six years. There are at least two ways how this goal could be achieved. The simplest way is to increase enrichment in fuel. There exists a limit, which is 5.0 w% of U 235. Taking into account some uncertainty, the calculation maximum is 4.95 w% of U 235. The second way is to change fuel assembly design. There are several possibilities, which seem to be suitable from the neutron – physical point of view. The first one is higher mass content of uranium in a fuel assembly. The next possibility is to enlarge pin pitch. The last possibility is to “omit” FA shroud. This is practically unrealistic; anyway, some other structural parts must be introduced.
42
17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš e-mail: [email protected] Jiří Švarný e-mail: [email protected] ŠKODA JS a.s. Orlík 266, 31600 Plzeň Czech Republic
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Page 1: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

17th Symposium of AERYalta, Ukraine, September 24-29, 2007

Extension of VVER-440 fuel cycles using improved FA design

 Pavel Mikoláš

e-mail: [email protected] Jiří Švarný

e-mail: [email protected] 

ŠKODA JS a.s.Orlík 266, 31600 Plzeň

Czech Republic

Page 2: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

ABSTRACT

Practically full five years cycle has been achieved at NPP Dukovany in the last years. There are two principal means how it could be achieved. First, it is necessary to use fuel assemblies with higher fuel enrichment and second, to use fuel loading with very low leakage. Both these conditions are fulfilled at NPP Dukovany at this time.

Page 3: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

ABSTRACT (CONT.)

However, the efficiency of fuel cycle can be improved by increasing the fuel residence time in the core up to six years. There are at least two ways how this goal could be achieved. The simplest way is to increase enrichment in fuel. There exists a limit, which is 5.0 w% of U235. Taking into account some uncertainty, the calculation maximum is 4.95 w% of U235. The second way is to change fuel assembly design. There are several possibilities, which seem to be suitable from the neutron – physical point of view. The first one is higher mass content of uranium in a fuel assembly. The next possibility is to enlarge pin pitch. The last possibility is to “omit” FA shroud. This is practically unrealistic; anyway, some other structural parts must be introduced.

Page 4: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

ABSTRACT (CONT.)

The basic characteristics of these cycles for up-rated power are presented showing that the possibilities of fuel assemblies with this improved design in enlargement of fuel cycles are very promising.

Page 5: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

1. INTRODUCTION

As stated in Abstract, the efficiency of fuel cycle can be improved if six years cycles would be applied. There are at least two ways how this goal could be achieved. The simplest way is to increase enrichment in fuel. There exists a limit, which is 5.0 w% of U235. Taking into account some uncertainty, calculation maximum is 4.95 w% of U235. The second possibility is to change fuel assembly design.

 In this paper, both possibilities are checked in different

range individually.

Page 6: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

2. FUEL ASSEMBLY WITH HIGHER ENRICHMENT

As it has been stated in introduction, we will suppose enrichment of 4.95 w% of U235 in some of fuel pins in a fuel assembly.

The other characteristics (it means excluding enrichment) are the same as for fuel assembly of Gd-2 or Gd-2M for up-rated power.

It seems to be clear that this maximal enrichment can not be applied in all fuel pins because in this case pin power non-uniformity would be very high (more than 1.15), which would be a problem from the point of view of pin power factor in the core.

 

Page 7: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Therefore, enrichment is lower in some pins and one from possible solutions is shown in Fig. VIIa, where the maximum (1,072) has been found in pin No. 17 according to Fig. II. at FA burn-up of 10000 [MWd/tU].

Kinf values of some similar designs are shown in Graph 1K (also with zoom for the beginning of burn-up process) and values of maximum of Fdh (Kr) in Graph 1P (three digits in name identify lower enrichment in FA).

2. FUL ASSEMBLY WITH HIGHER ENRICHMENT (CONT.)

Page 8: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

2. FUL ASSEMBLY WITH HIGHER ENRICHMENT (CONT.)

Fuel assemblies (according to Fig. VIIa) have been loaded into core in transient end equilibrium cycles of Dukovany NPP for up-rated power (cycles 27th to 34th of Unit III) and basic characteristics of these cycles are shown in Tables 1-4,

where in column 1 is cycle number, in column 2 are values for base calculation (WFA of enrichment 4.38 w% of U235 and

CFA of 4.25 w% of U235), in column 3 for the variant with WFAs according to Fig. VIIa and CAs acc. to Fig. III, in column 4 for the variant with WFAs according to Fig. VIIa and CAs according to Fig.

VI and in column 5 for the variant with WFAs according to Fig. VIIa (but with higher Gd2O3

content [5.0 w%]) and CAs according to Fig. III. It is seen that fuel cycles prolongation has been

achieved, but this prolongation may not be sufficient for six-year cycle.

Page 9: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

3. NEW FUEL ASSEMBLY DESIGN The other possibility how to extend the fuel cycle

(and how potentially achieve six year cycle) is the application of fuel assembly with an improved design.

There are several possibilities, which seem to be suitable from the neutron – physical point of view.

The first one is higher mass content of uranium in a fuel assembly. This can be achieved by two ways:

First, to remove central hole in fuel pellet and second, to enlarge fuel pellet diameter. In our checking, both conditions were applied

together. Other characteristics are the same as for FA for up-rated power (Gd-2M).

Page 10: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

The next possibility is to enlarge pin pitch. It has been applied too. The “last” possibility is to “omit” FA shroud. This is practically not realistic, in any way, some other

structural parts must be introduced in a FA; in our simplified model,

thickness of FA shroud was lowered in two steps, namely from 1.5 mm on 1.0 mm and then on 0.5 mm.

Kinf values for 5 different FAs are shown in Graph 7 (also with zoom for the beginning of burn-up process),

3. NEW FUEL ASSEMBLY DESIGN (CONT.)

Page 11: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

3. NEW FUEL ASSEMBLY DESIGN (CONT.)

where G - means FA according to Fig. VI, Gbezd - FA of the some type as in Fig. VI, but fuel pellet is

without central hole and with higher diameter, G124 - as previous, but fuel pin pitch is 12.4 mm (instead of 12.3 mm), G12410 - as previous, but FA shroud thickness is only 1.0 mm G12405 - as previous, but FA shroud thickness is only 0.5 mm.

The basic characteristics of these cycles for up-rated power are shown in Tables 5-7 showing that possibilities of fuel assemblies with this improved design in enlargement of fuel cycles are very promising.

All FAs features were calculated by WIMS8 code [1] and core calculations by MOBY-DICK code [2].

Page 12: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

4. FUEL CYCLES WITH 4.75W% ENRICHMENT FUEL (QO3)

Application of the higher fuel enrichment (WFA enriched on 4.75w%, see FA type QO3 with 3.35w% Gd2O3 and CFA enriched on 4.38w%) was realized for power up-rated design (1444 MWt) of NPP Dukovany. Optimization of low leakage fuel cycle sequences was provided by program OPAL_B [3] on the 3D level core burn up modeled by macrocode MOBY-DICK. Nearly 5.5 year cycle (see Fig. VIII) was reached by optimization, which is in Table 8 compared with original 5 years fuel cycle for up-rated power of NPP Dukovany (WFA enriched on 4.38w%, see FA type QS3 or Gd2M with 3.35w% Gd2O3 and CFA enriched on 4.25w%). From Table 8 is seen that average burn up of six years FA will be lower than 60 000 MWd/tU.

Page 13: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

4. FUEL CYCLES WITH 4.75W% ENRICHMENT FUEL (QO3) (CONT.)

During 5 years cycle we have loaded 12 fresh FAs in average in each cycle and during 6 years cycle we have loaded 10 fresh FA. From this it follows that each 6 years FA should (approximately) brought excess of reactivity by 20% higher compared to FA of 5 years cycle. That represents excess by 65 FPD in 326 FPD length of 5 years cycle. According Table 2 we have for QO5 FAs excess 27 FPD, which represents 8.3% increase in fuel cycle length. This agrees with decreasing number of FA by 9%.

  Additional excess cycle length (or reactivity) can be

achieved for example by loading of FA of new design QN1.

  Combination of improvement QO5 + QN1 potentially can

assure pure 6 years fuel cycle.

Page 14: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

4. DISCUSSION

The values shown in Tables 1 - 4 cannot be supposed to be quite real because pin power non-uniformity is too high. Different loadings have been found as it is shown in Table 8 and Fig.VIII. Pin power non-uniformity is still relatively big; it could be lowered by optimization, because we have still excess of reactivity (positive residual boric acid concentration).

Page 15: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

4. DISCUSSION (CONT.)

Loading with lower number of fresh FA has been found instead of simple enlargement of the fuel cycle. As stated above, although not yet proved, application of FAs with higher enrichment and improved design (see Tables 5-8) could lead to full six years cycle. So, it seems to be clear that FA have still potential in sense of the fuel cycle economy.

Page 16: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

5. CONCLUSION

Although only preliminary analyses described in the paper have been performed, it can be concluded that temporary design of VVER-440 FA is not optimal (as it is well known) and it exists a great potential how to increase FA reactivity, which is a necessary condition in achieving full six years loading strategy. (Potential in lowering core neutron leakage is practically exhausted as is also the possibility in reducing neutron absorption in construction parts of a FA.)

Page 17: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

6 CONCLUSIONS (CONT.)

Design change (it means FA of “KARKAS” type) seems to be more encouraging than an attempt still to increase fuel enrichment.

 Of course, both possibilities (or their combination) must be proved on very well designed loading strategies.

Page 18: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

REFERENCES

[1] Coll.: WIMS - A Modular Scheme for Neutronics Calculations, User Guide

for Version 8, ANSWERS/WIMS(99)9, Winfrith, 1999  [2] Krýsl, V.: MOBY-DICK Users Manual, Report of ŠKODA JS a.s. No.: Ae10068/Dok,

Rev. 3, Plzeň 2005, (In Czech)  [3] Švarný, J.: OPAL_B The In Core Fuel Cycle Management System Development,

Proceedings of the 13th Symposium of AER, Dresden, Germany, September 2003

Page 19: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Fig. I Calculation scheme of „asymptotic“ fuel assembly

Page 20: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

12

8

5

3

2

13

9

6

4

14

10

7

15

1116

1920

21

18

22

17

central tube

n.n % U235

Fig.II Numeration of fuel rods

Page 21: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

4.4 % U235

4.0 % U235

4.0 % U235 + 3.45 % Gd2O3

central tube

3.6 % U235

Gd

Gd

Gd

Gd

Gd

Gd

Gd

Fig.III Fuel enrichment [w%U235] in fuel rods of Russian design of FA „Gd-2“

(average enrichment 4.347619 w%U235)

Page 22: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

4.6 % U235

4.0 % U235

4.0 % U235

+ 3.35 % Gd2O3

central tube

3.6 % U235

Gd

Gd

Gd

Gd

Gd

Gd

Gd

Fig.VI Fuel enrichment [w%U235] in fuel rods of modified design of FA Gd-2 „Gd2M“ (average enrichment 4.380952 w%U235) for uprated power

Page 23: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

4.95 % U235

4.4 % U235

4.4 % U235

+ 3.35 % Gd2O3

central tube

4.2 % U235

Gd

Gd

Gd

Gd

Gd

Gd

Gd

Fig.VIIa Fuel enrichment [w%U235] in fuel rods of modified design of FA Gd-2 „Gd2Max“ (average enrichment „4.757143“ w%U235) for six-year cycle

Page 24: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Fig.VIII The odd and even equilibrium loadings of 5.5 years fuel cycle (Numbers represent residence time [years] of FA in core)

Page 25: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Fig.VIII The odd and even equilibrium loadings of 5.5 years fuel cycle (cont.)

(Numbers represent residence time [years] of FA in core)

Page 26: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 1 K-inf FAs with higher enrichment and different profilation [Gd2O3 content 3.35 w%]

0,8

0,86

0,92

0,98

1,04

1,1

1,16

1,22

0 10000 20000 30000 40000 50000 60000

burn-upí [MW d/tU]

k-in

f

Gd2M

G440415

G440420

G435420

G435415

Page 27: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 1K (zoom) K-inf FAs w ith higher enrichment and different profilation [Gd2O3 content 3.35 w%]

1,15

1,16

1,17

1,18

1,19

1,2

1,21

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

v yhoření [MWd/tU]

k-in

f

Gd2M

G440415

G440420

G435420

G435415

Page 28: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 1P Maximal relative power in FPs of FAs with higher enrichment and different profilation [Gd2O3 content 3.35 w%]

1,03

1,04

1,05

1,06

1,07

1,08

0 10000 20000 30000 40000 50000 60000

burn-up [MWd/tU]

Rela

tive

powe

r

G440410

G440420

G435420

G435415

Page 29: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 2K K-inf FAs with higher enrichment and different profilation [Gd2O3 content 5.0 w%]

0,82

0,92

1,02

1,12

1,22

0 10000 20000 30000 40000 50000 60000

burn-up [MWd/tU]

k-in

f

G440415

G440420

G435420

G435415

Page 30: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 2K (zoom) K-inf FAs w ith higher enrichment and different profilation [Gd2O3 content 5.0 w%]

1,15

1,16

1,17

1,18

1,19

1,2

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

burn-up [MWd/tU]

k-in

f

G440415

G440420

G435420

G435415

Page 31: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 2P Maximal relative power in FPs of FAs w ith higher enrichment and different profilation [Gd2O3 content 5.0 w%]

1,03

1,04

1,05

1,06

1,07

1,08

0 10000 20000 30000 40000 50000 60000

burn-up [MWd/tU]

Rel

ativ

e po

wer

G440415

G440420

G435420

G435415

Page 32: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 7 K-inf of FAs with improved design

0,8

0,9

1

1,1

1,2

0 10000 20000 30000 40000 50000 60000

burn-up [MWd/tU]

k-in

f

G

Gbezd

G124

G12410

G12405

Page 33: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Graph 7 (zoom) K-inf of FAs w ith improved design

1,145

1,15

1,155

1,16

1,165

1,17

1,175

1,18

1,185

1,19

1,195

1,2

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

burn-up [MWd/tU]

k-in

f

G

Gbezd

G124

G12410

G12405

Page 34: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Tables

Table 1 Cycles length with FAs with higher enrichmentTable 1 Cycles length with FAs with higher enrichment

Cycle\FA Base (QS3) QO3 (Gd-2+) QO3 (Gd-2M) QO5 (Gd-2+) 27 326 341 342 336 28 326 346 348 344 29 328 357 360 356 30 328 357 359 355 31 328 348 350 346 32 327 353 356 352 33 326 353 355 351 34 326 349 251 346

Page 35: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 2Table 2 Difference (profit) in cycles length [FPD] with FAs with Difference (profit) in cycles length [FPD] with FAs with higher fuelenrichment in relation with base variant (base [Gd2M])higher fuelenrichment in relation with base variant (base [Gd2M])

Cycle\FA Base (QS3) QO3 (Gd-2+) QO3 (Gd-2M) QO5 (Gd-2+) 27 0 15 16 10 28 0 20 22 18 29 0 29 32 28 30 0 29 31 27 31 0 20 22 18 32 0 26 29 25 33 0 27 29 25 34 0 23 25 20

Page 36: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 3Table 3 Residual boric acid concentration after power stretch- Residual boric acid concentration after power stretch-out at fuel out at fuel cycle cycle length found for FAs with higher fuel enrichment length found for FAs with higher fuel enrichment

Cycle\FA Base (QS3) QO3 (Gd-2+) QO3 (Gd-2M) QO5 (Gd-2+) 27 +0.026 +0.000 +0.010 +0.001 28 -0.013 +0.000 -0.001 +0.001 29 +0.061 -0.001 -0.007 -0.002 30 +0.082 +0.002 -0.004 +0.001 31 -0.041 -0.002 +0.002 +0.005 32 -0.027 +0.007 -0.008 -0.011 33 +0.008 +0.009 +0.006 -0.002 34 -0.062 -0.011 -0.012 +0.001

Page 37: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 4Table 4 Maximum Fdh (K Maximum Fdh (Krr) in cycles with FAs with higher fuel ) in cycles with FAs with higher fuel enrichment enrichment

(value in bracket gives burn-up [in FPD] where this maximum occurs)(value in bracket gives burn-up [in FPD] where this maximum occurs)

Cycle\FA Base (QS3) QO3 (Gd-2+) QO3 (Gd-2M) QO5 (Gd-2+) 27 1.519 (2*) 1.557 (200*) 1.556 (200) 1.541 (240*) 28 1.511 (0) 1.563 (180*) 1.561 (160*) 1.543 (240) 29 1.518 (2) 1.548 (160) 1.544 (140*) 1.543 (0) 30 1.497 (2) 1.539 (160*) 1.537 (160*) 1.517 (240) 31 1.514 (0) 1.542 (180) 1.539 (180*) 1.525 (8,260) 32 1.500 (2) 1.537 (180) 1.535 (180*) 1.523 (4) 33 1.511 (2*) 1.539 (180*) 1.537 (180*) 1.532 (4*) 34 1.510 (0) 1.542 (140*) 1.540 (160*) 1.528 (4*)

* means that value shown has been found in more consecutive time steps [ in FPD]; the first from these steps is marked

Page 38: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 5Table 5 Cycles length with different FAs types Cycles length with different FAs types

Cycle\FA Base „G“ (QS3)

„Gbezd“ (QND)

„G124“ (QN4)

„G12410“ (QN1)

„G12405“ (QN0)

27 326 329.91 329.91 331.16 341.46 28 326 333.82 333.82 336.36 345.50 29 328 339.81 339.81 243.68 351.70 30 328 243.74 243.74 348.96 355.77 31 328 347.68 347.68 354.29 359.85 32 327 346.62 346.62 353.21 358.75 33 326 345.56 345.56 352.13 357.65 34 326 245.56 245.56 352.13 357.65

Page 39: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 6Table 6 Difference (profit) in cycles length with different FAs Difference (profit) in cycles length with different FAs types types

in relation with base variant (base [Gd2M]) in relation with base variant (base [Gd2M])

Cycle\FA Base „G“ (QS3)

„Gbezd“ (QND)

„G124“ (QN4)

„G12410“ (QN1)

„G12405“ (QN0)

27 0 3.91 3.91 5.16 15.46 28 0 7.82 7.82 10.36 19.50 29 0 11.81 11.81 15.68 23.70 30 0 15.74 15.74 20.96 27.77 31 0 19.68 19.68 26.29 31.85 32 0 19.62 19.62 26.21 31.75 33 0 19.56 19.56 26.13 31.65 34 0 19.56 19.56 26.13 31.65

Page 40: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 7Table 7 Maximum Fdh (K Maximum Fdh (Krr) in cycles wit different FAs types ) in cycles wit different FAs types (value(value in bracket givein bracket givess burn-up[in FPD], where this maximum occurs) burn-up[in FPD], where this maximum occurs)

Cycle\FA Base „G“ (QS3)

„Gbezd“ (QND)

„G124“ (QN4)

„G12410“ (QN1)

„G12405“ (QN0)

27 1.519 (2*) 1.547 (4) 1.547 (2*) 1.545 (2*) 1.571 (2) 28 1.511 (0) 1.531 (200) 1.525 (200*) 1.530 (200) 1.564 (180) 29 1.518 (2) 1.537 (2) 1.547 (2) 1.536 (0) 1.562 (0) 30 1.497 (2) 1.489 (0) 1.504 (0) 1.489 (0) 1.545 (180) 31 1.514 (0) 1.511 (180) 1.525 (0*) 1.512 (0) 1.542 (180) 32 1.500 (2) 1.502 (2) 1.513 (0) 1.497 (0) 1.539 (180) 33 1.511 (2*) 1.517 (2*) 1.531 (2*) 1.507 (2*) 1.550 (180*) 34 1.510 (0) 1.508 (0) 1.516 (0*) 1.515 (0) 1.546 (140*)

* means that value shown has been found in more consecutive time steps [ in FPD]; the first from these steps is marked

Page 41: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 8 Comparison of design fuel cycle for Gd2M FA (QS3) loadings with upupgraded fuel cycle with 4.75w% FA (QO3) loadings

(both for uprated power 1444 MWt) QS3 fuel loadings

5 year cycle QO3 fuel loadings (5,5 year cycle)

Eq. cycles 32 33 39 40 WFA + CFA 11 + 1 10 + 2 9 +2 10 + 1 Teff [FPD] 327 326 326 330 CBBOC [gH3BO3/kg]

4.565 4.732 5.009 5.203

CBEOC [gH3BO3/kg] -0.027 0.008 0.028 0.084 Fdh 1.500 1.511 1.558 1549 Aver. burn-up [MWd/tU] Core

35161

35374

38589

38556

Aver.burn-up [MWd/tU] Reloaded FA

50794

51304

57391

56825

Aver.burn-up [MWd/tU] 1 year 2 year 3 year 4 year 5 year 6 year

13990 26764 38366 47908 51598

13618 27081 39170 47877 51601

14200 27694 37219 51014 56034 59073

14515 27542 40058 47209 57496 58832

Page 42: 17th Symposium of AER Yalta, Ukraine, September 24-29, 2007 Extension of VVER-440 fuel cycles using improved FA design Pavel Mikoláš

Table 8 (continuation) Comparison of design fuel cycle for Gd2M FA (QS3) loadings with upgraded fuel cycle with 4.75w% FA (QO3) loadings (both for up rated power 1444 MWt) – reactivity coefficients.

QS3 fuel loadings 5 year cycle

QO3 fuel loadings (5.5 year cycle)

BOC EOB

BOC EOB

BOC EOB

BOC EOB

/Nti [1/%N] Power coefficient with constant input temperature

-1.738E-4 -2.015E-4

-1.757E-4 -2.018E-4

-1.733E-4 -2.044E-4

-1.736E-4 -2.057E-4

/Nta [1/%N] Power coefficient with constant average temperature

-1.154E-4 -1.135E-4

-1.177E-4 -1.134E-4

-1.163E-4 -1.150E-4

-1.173E-4 -1.162E-4

/tM [1/C] Moderator temperature coefficient

-3.607E-4 -5.612E-4

-3.583E-4 -5.640E-4

-3.519E-4 -5.706E-4

-3.483E-4 -5.717E-4

/ [cm3/g] Moderator density coefficient

2.056E-1 3.137E-1

2.040E-1 3.149E-1

1.993E-1 3.153E-1

1.967E-1 3.161E-1

/CB [kg/g] Boron coefficient

-1.146E-2 -1.246E-2

-1.143E-2 -1.245E-2

-1.087E-2 -1.196E-2

-1.081E-2 -1.196E-2


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