Nuclear Engineering and Design 285 (2015) 23–30
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Nuclear Engineering and Design
jou rnal homepage: www.elsevier.com/locate/nucengdes
Pre-conceptual study of small modular PbBi-cooled nitride fuel reactor core characteristics
a,b a,∗ a
Xianbao Yuan , Liangzhi Cao , Hongchun Wu
a
School of Nuclear Science and Technology, Xi’an Jiaotong University, No. 28, Xianning West Road, Xi’an, Shanxi 710049, PR China
b
College of Mechanical & Power Engineering, China Three Gorges University, No. 8, Daxue Road, Yichang, Hubei 443002, PR China
h i g h l i g h t s
•
The nitride fuel, stainless steel cladding and Pb-Bi coolant have a perfect compatibility with each other, as well as with excellent neutronics characteristics.
•
High conversion ratios have been achieved by optimizing the designed parameters to ensure 20 EFPY without refueling and shuffling.
•
The burn-up swings slightly due to the perfect breeding capability.
•
All of the important reactivity coefficients are negative to assure SMoPN holding passive safety.
•
The control system can provide the enough shutdown margins in any operational conditions.
a r t i c l e i n f o a b s t r a c t
Article history: In this paper a pre-conceptual neutronics study on a small modular Pb-Bi cooled reactor with nitride fuel
Received 27 July 2014
(SMoPN) is presented. The SMoPN is designed to meet the requirements for nuclear energy expansion
Received in revised form
in the next decades, by using the plutonium and thorium nitride fuel to increase the efficiency and
27 November 2014
performance of fuel. Based on the existing experiences of nuclear reactor, the primary design parameters
Accepted 13 December 2014
were provided to match the design goals by the whole core three-dimensional calculation. The nitride fuel,
stainless steel cladding and Pb-Bi coolant have a perfect compatibility with each other, as well as with
excellent neutronics characteristics. High conversion ratios have been achieved to ensure 20 effective
full power years (EFPYs) without refueling and shuffling. During the core lifetime, the burn-up swings
slightly due to the perfect breeding capability. All of the important reactivity coefficients are negative to
assure the SMoPN holding passive safety. The control system can provide enough shutdown margins in
both normal and abnormal operational conditions. Therefore, the SMoPN concept satisfies completely
the advanced design idea and the requirements of advanced nuclear reactor system.
© 2014 Elsevier B.V. All rights reserved.
1. Introduction investment, a large number of redundant equipments and slow
repayment. Secondly, a single reactor with too large capacity may
Nuclear energy is considered to be the most effective solution do harm to the grid. The grid has the danger to break if the power
to the current worldwide energy crisis, environmental pollu- is too large for a single reactor. Thirdly, the reactor is too large to
tion and economic sustainable development issues (Kessides, control, consequently brings the safety issues. Thereafter the small
2012). Throughout the history of nuclear power development, modular reactor (SMR) (Smith, 2010; Vujic´ et al., 2012) comes
the direction of nuclear energy development has mainly been back to the sight of people and projects a ray of sunlight on the
focused on the traditional pressurized water reactors (PWRs) and development of nuclear power.
enlarging the power capacity of a single reactor for the economical The SMR characterized by lower nominal power less than
and technical reasons. However, it faces enormous challenges or equal to 300 MWe (IAEA-TECDOC-1451, 2005) and modular-
to enlarge the power capacity of a single reactor continuously. ized construction, is recognized world-widely as one of the most
Firstly, the improvement of economic benefits by increasing the important options for the future nuclear energy development.
power of single reactor exhibits limitation due to the vast upfront This is mainly because SMRs have some unique advantages. SMRs
can be used as energy source with multipurpose applications,
such as power generation, desalination, district heating, hydrogen
∗ production and industrial processes. They can be deployed in
Corresponding author.
E-mail address: [email protected] (L. Cao). remote areas, deserted coal plants; island and countries (or areas)
http://dx.doi.org/10.1016/j.nucengdes.2014.12.013
0029-5493/© 2014 Elsevier B.V. All rights reserved.
24 X. Yuan et al. / Nuclear Engineering and Design 285 (2015) 23–30
that do not have the mature electricity grid systems and cannot economic efficiency, increase the conversion ratio and avoid the
deploy large size nuclear reactors. These flexibilities allow for SMRs potential dangers.
to match energy requirements in light of the practical situation. This paper is organized as follows. In Section 2, the design crite-
At the same time, SMRs can be fabricated as an integrated modu- ria of fuel, coolant and cladding selection, the design parameters
lar in the factory, which can provide a unified standard to nuclear and the core detailed configuration are introduced. The neutronics
plant construction, shorten the approval process and construction performance including the effective multiplication factor, burn-up,
duration, and can be installed underground totally. Therefore, SMRs conversion ratio and the value of control system, was discussed by
have higher capability to decrease the risk of nuclear prolifera- assembly and core calculation with transport and diffusion calcu-
tion with more flexible ways to finance and more attraction to lation codes in Section 3, respectively. The conclusions are drawn
investors. out in Section 4.
In fact, the studies and utilizations of SMR can be traced back
to the 1950s, mainly focusing on the warship and submarine in
2. Core design
limited countries and regions, such as Russia, American and Japan.
It has comprehensively thrived from the end of last century for the
2.1. Design goals
requirements of fast improvement of nuclear energy. At present,
there are about 40 types of SMRs in the world, but most of them
According to the NEA reports, the available fuel resources of
are still in the pre-conceptual design stage and mainly focus on
235
U is about 300,000 tons distributed in unbalance in the world.
the PWR and fast neutron reactors with metallic coolant. The
It is just only enough for 50 years in light of the current annual
mPower (Halfinger et al., 2012), IRIS (Franceschini et al., 2008;
consumption. It is well known that a lot of depleted uranium is dis-
Shirvan et al., 2012), NuScale (Reyes and Lorenzini, 2010; Reyes
charged in the mining process, the discharged PWR spent fuel has
and Young, 2011) and SMART (Chang et al., 2000; Yoon et al.,
about 1% spent plutonium, and also there is plenty of thorium in
2012) are the representatives of integral PWR (IPWR), which are
nature. The fuel resource can be enlarged with several hundreds
well developed and have the chances with near-term deployment.
of times if the depleted uranium, spent fuel and thorium are uti-
However, in the Generation IV International Forum documents,
lized as fuel. Because the nitride fuel has high melting point, high
the liquid metal-cooled fast reactor is considered as the newest
density and excellent conductivity, the PuN (Kurosaki et al., 2000;
generation nuclear system that can be used for both electricity
Lyon et al., 1991; Kleykamp, 1999) and ThN (Adachi et al., 2005;
production and transuranium elements (TRU) incineration in the
Morss et al., 2007) are selected as the fuel in this design. The pluto-
closed nuclear fuel cycle. It was mainly classified into three kinds of
nium discharged from PWR after 33 GWd/t burn-up with 10 years
reactors according to the coolant: sodium, lead and lead-bismuth
of cooling (Ganda and Greenspan, 2009) and storage. The pluto-
fast reactor, such as Super-Safe, Small & Simple (4S) (Ishii et al.,
nium inventory for a single SMoPN unit is about 2845 kg, which is
2011), Encapsulated Nuclear Heat-Source (ENHS) (Brown et al.,
equivalent to the content of 300 tons spent fuel discharged from
2001; Greenspan, 2002; Greenspan et al., 2008) and SVBR-100
232
PWR, and the natural thorium (100% Th) are selected as fuel to
(Zrodnikov et al., 2008). The 4S is being developed by Toshiba and
increase the efficiency of fuel utilization and enlarge the available
the central research institute of electric power industry in Japan,
space of fuel.
with three decades lifetime, which is a 135 MWt cooled by liq-
As well known, the light water is the main coolant in the con-
uid sodium with U–Pu–Zr (11.5% Pu) metallic fuel. The ENHS is a
ventional nuclear reactor due to the plenty of practical experience.
liquid-lead-cooled reactor of 50 MWe being developed by the Uni-
However, it is also a perfect moderating media and the neutron
versity of California. It has 15–20 years life with U–Pu–Zr (11% Pu)
spectrum can be softened to decrease the breeding ability. The
metallic fuel or uranium–zirconium (13% uranium) and sits in 17 m
sodium has many merits as coolant, such as low melting point and
deep silo. The SVBR-100 was designed by AKME-engineering with
outstanding capacity of heat transmission. But the sodium fire is a
280 MWth cooled by lead–bismuth. It is an integral design, with
vital defect for sodium coolant. The Pb-Bi (Loewen et al., 2003) not
12 steam generators and two main circulation pumps sitting in the
◦ only has low melting point, high boiling temperature, outstanding
lead–bismuth pool at 340–490 C.
capacity of heat transmission and neutronic features, but also is
However, the uranium fuel is the main fuel adopted in those
chemical inert.
design schemes. A few design schemes selected the plutonium
The cladding is a critical factor to decide the safety of reactor,
as fuel, and very few designs considering the fertile thorium
which is always the main aspect of nuclear reactor research and
(Toshinsky et al., 2013). In most of these schemes the oxide fuel
design. The Zr-4 is the traditional cladding materials in thermal
(or metallic fuel) is used, and the advanced fuel type (nitride fuel)
reactors. It can only be permitted the highest temperature with
is only used in a few of design schemes (Smirnov, 2012). Several ◦
600 C to avoid the reaction between zirconium and water. How-
designs such as 4S use sodium as coolant, cannot avoid the potential
ever, the T91 ferritic-martensitic steel (FMS) (Weisenburger et al.,
dangers, for example: sodium-water reaction and coolant boiling
2008), an ASME codified structural materials, has been envisaged as
because the sodium has the active chemical characteristic and the
a candidate for structures exposed to higher coolant temperature.
low boiling point. In the light of those challenges of small modular
Therefore, the spent plutonium and thorium, lead-bismuth and
fast reactors, an innovative concept SMoPN is proposed, which is
stainless steel T91 are selected as the fuel, coolant and cladding to
designed to meet the requirements of nuclear power fast develop-
meet the following design goals in this study, respectively.
ment by enlarging the space of fuel utilization and increasing the
In this study, the following primary parameters for the SMoPN
efficiency of fuel utilization with plutonium extracted from PWR’s
are selected:
spent fuel and thorium. In addition, it has higher conversion ratio
232 233
from Th to U because the PuN and ThN are used as the fissile
233 •
fuel and fertile material, respectively. The U reprocessed from Core thermal power: 300 MW.
• ◦
the spent fuel discharged from SMoPN after 20 effective full power Core inlet/outlet temperature: 320/500 C.
•
years operation, has two utilization ways: first it can be used as the Number of fuel rods per assembly: 127.
•
fuel of SMoPN and form the U–Th closed fuel cycle in the further fuel Fuel rod active length less than: 2.0 m.
•
cycle; second, it can be used as the fissile fuel for PWR. The liquid FA maximum discharge burn-up: 250 GWd/t.
•
Pb-Bi is adopted as coolant and reflector material, and the whole Number of fuel assemblies: 240.
•
reactor core is sunk into the coolant. These improve the neutron Number of control assemblies: 13.
X. Yuan et al. / Nuclear Engineering and Design 285 (2015) 23–30 25
Fig. 1. Fuel rod and assembly design of the SMoPN.
For this study, the following design criteria are applied. is a closely packed array of tubes containing compacted born car-
bide pellets. It is grouped into two independent and diverse parts,
•
Negative coolant reactivity coefficient. viz. reactor control system (RCS) with seven control assemblies
•
Core shutdown margin greater than or equal to 2% dk/k. and reactor shutdown system (RSS) with six control assemblies,
•
Maximum linear heat generation rate (MLHGR) at rated power to avoid the accident of failure in part of control assemblies and
less than or equal to 10 kW/m. increase the control performance. The RCS with seven control
•
Maximum cladding surface temperature (MCST) at rated power assemblies serves as reactor startup, regulation of reactor power
◦
less than or equal to 650 C. and reactivity, and reactor shut-down. The RSS with six assemblies
•
Maximum temperature in the center of fuel rod less than or equal is only used to shutdown the reactor, and does not take part in the
◦
to 1000 C. power and reactivity regulation in normal operation. The assembly
•
The average conversion ration greater than or equal to 0.97. bundles of the RSS are fully placed above the active core and the cor-
responding ducts are filled with the liquid Pb-Bi eutectic when the
Based on these selections and primary parameters, the fuel reactor operates in the normal conditions. The number of absorber
design and load pattern, the core arrangement, and the control assemblies is confirmed to match the requirements of regulation of
assemblies design and position in the lifetime are optimized to sat- power and reactor shutdown. Their positions are shown in Fig. 3.
isfy all design criteria as well as to improve the economic benefits
and safety of the SMoPN. 2.4. Core arrangement
2.2. Fuel rod and assembly design In this design, the SMoPN contributes a 300 MWth nitride-fueled
core, composed by hexagonal fuel assemblies with pins arranged
The details of the fuel rod and assembly design are shown in on a hexagonal lattice. Fig. 3 shows a section of the core composed
Fig. 1. The fuel assembly of the SMoPN has a flat-to-flat diameter by 240 fuel assemblies surrounded by two rings of shielding assem-
of 11.2 cm and contains 127 fuel rods. The smear density of the blies, each of which consists of T91 stainless. The fuel assemblies
PuN and ThN fuel is 75%, and the fuel equivalent radius is 0.295 cm. of the core are arranged in four enrichments 14.04%, 15.18% 16.32%
The outer radius of the fuel rod is designed to be 0.415 cm, with and 17.45% from inside to outside with PuN for flattening the power
a 0.75 mm cladding thickness. The pitch-to-diameter ratio is 1.2 distribution and ensuring the core being at the critical during the
to get better breeding ratio. The assembly duct thickness is 0.30 cm
and the fuel assembly gap thickness is 0.1 cm. There is a Pb-Bi eutec-
tic plenum above the fuel region, and a Pb-Bi reflector is placed
below the fuel region. The radius is about 2.6 m with 1.957 m active
core in diameter and the height of the active core is 1.95 m. There is
one ring shield assembly with stainless steel in the outset core. And
the gap between the active core and the shield assembly is filled
with liquid Pb-Bi which has a perfect neutronic feature to serve
as the reflector. To get the negative void coefficient and improve
the conversion ratio, there is a 30 cm length blanket (ThN) in the
middle of the pins located at the three innermost rings assembly.
The blanket segment is only ThN in addition to the outside pin
claddings.
2.3. Control assembly design
The control assembly consists of an absorber bundle (seven
absorber pins, seven inner supplants and seven outer supplants)
contained within a wrapper (shown in Fig. 2). The absorber bundle Fig. 2. Control assembly design of the SMoPN.
26 X. Yuan et al. / Nuclear Engineering and Design 285 (2015) 23–30
Fig. 4. Calculation model for 1/6 core.
Fig. 3. Core arrangement of the SMoPN.
3, 3 and 39 meshes in X, Y and Z directions (see Fig. 4), respectively,
and the power is obtained for each mesh.
entire time of normal operation. Here, fuel enrichment is defined Using the result of neutronic analysis, a multi-channel thermal-
as the mass fraction of PuN in the mixed fuel PuN and ThN. A rela- hydraulic code (TH code) is used for the thermal-hydraulic
tively low PuN content (14.04 wt% PuN) has been used for the inner calculation. In the TH code, each channel is approximated as a
three rings with 36 fuel assemblies in order to limit the power fuel rod surrounded by coolant, because each fuel assembly in the
peaking factor at the beginning of the life and increase the inter- SMoPN is isolated by its wrapper, every fuel assembly can be sim-
nal conversion. Two rings of 42 fuel assemblies with slightly higher ulated as an independent channel, neglecting the inter wrapper
PuN fraction (15.18 wt% PuN) compose the second zone. 78 fuel flow and heat transfer. So, the scoping research of coolant flow in
assemblies with 16.32 wt% PuN are used in the third zone. 84 fuel each channel can be executed by the inlet temperature, the outlet
assemblies with 17.45 wt% PuN are put in the outer two rings of the temperature and the total thermal power of this channel. Typically,
active core. In this core arrangement, the SMoPN is assured to be the fuel assembly is composed of triangular rod bundles, and thus
in the criticality in 20 EFPYs and has 200 pcm reactivity margin at the Ushakov correlation (Ushakov et al., 1977) is used to analyze
the end of life. the heat convection between the heavy liquid metal coolant and
the cladding in the TH code. It is applied to the three-dimensional
3. Core neutronics analysis power distribution obtained by the core burn-up calculation. In
the TH code, the active core is divided into 10 axial meshes. In
3.1. Calculation method and tools each of the 10 axial planes, the fuel pellet, gas gap, cladding and
coolant are depicted by one dimensional model. In the calculation,
In this study, the neutronics analysis was performed using the the heat transfer and conduction in each the 10 axial planes are
in-house transport code PIJ and a diffusion code CITATION. The calculated from the bottom to the top of the active core. The heat
PIJ code based on collision probability techniques, which covers generation distribution in the fuel pellet is assumed to be uniform
16 lattice geometries, is used to perform the two-dimensional and the nitride fuel heat transfer coefficient from the fuel to gap
assembly transport calculation for lattice physics study, after one- is assumed to constant 34 which is the synthesis of ThN (Adachi
dimensional ultra-fine group pin cell calculation to obtain the et al., 2005; Morss et al., 2007) and PuN (Kurosaki et al., 2000;
effective self-shielding resonance cross-sections, and generate the Lyon et al., 1991; Kleykamp, 1999) by Bruggeman Model (Kim and
macroscopic cross sections and diffusion coefficients for subse- Hofman, 2003), due to the limited experiment and data about ThN
quent core calculations. The calculation for each assembly type was and PuN. SOBOLEV correlation (Sobolev, 2007) is used for evalu-
performed with 40 burn-up steps using nominal parameters, with ating the density, specific heat and thermal conductivity of Pb-Bi
the hexagonal geometry for fuel assembly and annular assembly coolant. The heat transfer and conduction calculation are repeated
geometry for control assemblies. The super cell model is used for until the inlet/outlet temperature, the surface temperature of clad,
preparation of macro cross-sections of control assembly. And the the centerline temperature of rod and coolant flow are converged.
calculations for different temperatures of fuel, cladding, coolant,
with/without coolant between fuel pins were performed when 3.2. Results and analysis
calculated the reactivity coefficients. All neutronics calculations
use 107-energy group structures in conjunction with JENDL-3.3 Fig. 5 shows the effective multiplication factor (KEFF) variation
nuclear data library. The 107-energy group cross-section struc- with the burn-up. The initial KEFF is about 1.0131 and then goes
tures are collapsed to 16 (eight thermal and eight fast) energy down to the 1.0022 because of the decrease of fissile materials plu-
groups at the end of the assembly calculations. Here, the ther- tonium and the thorium breeding is very slow at the beginning.
232 233
mal spectrum is separated with eight groups for more precise Although the conversion ratio from Th to U is above unity
calculation. In these calculations, the materials, such as different at the beginning of half year (as shown in Figs. 6 and 7), the fis-
233
enrichment fuels, the cladding materials and coolant are consid- sion neutron number of U fission is lower than that comes from
239
ered heterogeneously in a 1/6 symmetrical geometry. After the Pu fission at the fast neutron spectrum, it could be the contrib-
fuel assembly burn-up calculation, the 3-dimensional triangular utory cause of the KEFF decreasing. The KEFF arrives to 1.022 after
233
(XT–YT–Z) core burn-up calculations are carried out with macro- 4 EFPYs mainly due to the accumulation of the U. Subsequently,
scopic cross-sections obtained by the above calculations in a 1/6 the KEFF decreases gradually and less-than unity after 20 EFPYs.
symmetric core geometry. The fuel assemblies are separated into The fertile material content reduction is the reason of decreasing
X. Yuan et al. / Nuclear Engineering and Design 285 (2015) 23–30 27
Table 1
Reactivity coefficients for different variables.
Reactivity coefficients Results
Fuel temperature (pcm/K) −0.536
Coolant temperature (pcm/K) −0.21
−
Void (pcm) 4673.57
Axial expansion of rod (pcm/1%) −81.0
Radial expansion of rod (pcm/1%) −1.7
of fuel conversion ability. Within the whole lifetime, the KEFF is
slightly higher than 1, and the swing is near zero, which implies
that the reactor is easy to control.
Table 1 lists some of important reactivity coefficients viz. fuel
Doppler coefficient, void coefficient, Pb-Bi coolant temperature
coefficient, axial and radial expansion coefficients. The delayed
neutron fraction is about 0.00302 with a small changing in the
239
whole life-time, due to the depleting of Pu and the accumulat-
233
Fig. 5. KEFF variations with the burn-up in 20 EFPY.
ing of U. The fuel Doppler coefficient, one of the most important
parameters in dynamic analysis, was evaluated to be −0.536 pcm/K
for temperature changes in the fuel from 1200 K to 1600 K for a
flooded core state using diffusion calculation. The Pb-Bi coolant
temperature coefficient was obtained by the same diffusion the-
ory and way as the fuel Doppler coefficients, to be −0.21 pcm/K for
the coolant temperature changing from 600 K to 900 K, with the
corresponding density variation. The Pb-Bi coolant density is about
−
31.5 pcm for the 1% coolant density change. The Pb-Bi coolant
void coefficient was calculated in the state that the Pb-Bi coolant
was lost totally, which is −4673.57 pcm. The Pb-Bi was also used as
the reflector materials in the SMoPN, which is about two assembly
thickness. The reflective ability will fail when the Pb-Bi coolant in
the core leaks entirely. Naturally, the leakage of neutron should be
increased and the core fails to achieve criticality. It is a very impor-
tant feature for the SMoPN, which ensures the core safety with the
most severe leakage of coolant in the primary loop. The fuel pin will
prolong in the axial direction and the lattice will expand under the
irradiation and the temperature increased situation, especially, the
first several years at the beginning of reactor startup. These surely
induce the reactivity swing and finally affect the safety. Therefore,
in this section, the reactivity coefficients of axial prolongation and
radial expansion are also evaluated to be −81.0 pcm and −1.7 pcm
for the 1% pin prolonging in axial direction and the 1% broaden-
ing of the radial size of the fuel assemblies, respectively. From the
above analysis, all reactivity coefficients which are important fac-
Fig. 6. Conversion ratio for each assembly in one-sixth core. tors affecting the reactor safety are negative and assure that the
SMoPN possess passive safety.
1.06
Figs. 6 and 7 present the conversion ratio for each fuel assembly
in the one-sixth core at the beginning of life and the evolution of
1.04
average conversion ratio with the burn-up. The conversion ratios
for the assemblies with plutonium enrichments 14.04%, 15.18%
1.02
16.32% are larger than unity at the beginning of life and that of
the inner assemblies is the highest. Although the conversion ratio 1.00
tio
of the two outer rings of assemblies is less than 1, the averaged ra
conversion ratio for all fuel assemblies is larger than 1. The more 0.98
ion
s outer assembly, the lower value due to the fact that the neutron
er 232
v 0.96 flux and the fraction of fertile materials (mainly Th) in the inner
on
assemblies is higher than outer assemblies, as well as the blanket in
C
0.94 the innermost assemblies. The conversion decreases with burn-up,
and lower than unity after 5 EFPYs, which is resulted by the fer-
0.92 tile material consumed gradually as burn-up. The average internal
conversion ratio is about 0.97, which is higher than that of most cur-
0.90 rent small modular fast reactor design and satisfies self-sustainable.
0 5 10 15 20
The discharged burn-up is the capital factor to determine the
EFPY
cladding integrity in practice, which is about 150 GWd/tHM for fast
reactor due to the limitation of material (Dubberley et al., 2003).
Fig. 7. Evolution of conversion ratio with the burn-up for 20 EFPYs.
However, some special fast reactors with special cladding material
28 X. Yuan et al. / Nuclear Engineering and Design 285 (2015) 23–30
Fig. 8. Discharged burn-up for each assembly in one-sixth core (GWd/t).
Fig. 9. Relative power factor distributions for each assembly at the BOL.
the value can reach above 200 GWd/tHM (Douglas et al., 2007;
Kim et al., 2010) without any breach, Fig. 8 shows the discharged
burn-up for each assembly in one-sixth core. The value is higher
for inner assemblies than those of outers due to the higher neutron
flux in the inner region. The highest value is 229.62 GWd/t, which
is beyond the common value, but it can be endured due to that its
maximum linear power is only 8.2 kW/m in the whole lifetime and
more advanced cladding and structure materials can be used for
the future deployment. Moreover, as the average discharge burn-
up is only 186.33 GWd/t, the maximum discharge burn-up could
be further decreased by optimizing the fuel enrichment zoning.
Figs. 9–11 illustrate the power peak factor distribution for each
assembly at BOL (Beginning of Life), MOL (Middle of Life) and EOL
(End of Life) in one-sixth core. The largest power peak factor locates
at 15.18% enrichment assemblies at the BOL, and then moves grad-
ually to the center of the core. This is the synergy between the
fissile material enrichment and the neutron flux to induce the
phenomena. Although the two outmost rings assemblies have the
highest PuN enrichment, due to the severe neutron leakage, the
power peak factor is always the smallest, lower than unity.
Tables 2 and 3 present the detailed analysis on the ability of
control system by comparison of the requirements of reactivity
and the value of control systems for the two bundles of control
Table 2
Reactivity worth requirements.
Fig. 10. Relative power factor distributions for each assembly at the MOL.
Parameters Primary Secondary
Full power to hot standby ($) 2.52 2.52
Hot standby to refueling ($) 0.95 – assemblies. The requirements of reactivity cover the insertion of
Reactivity fault ($) 1.73 2.0
positive reactivity by temperature defect, reactivity fault and fuel
Fuel cycle excess reactivity ($) 4.5 –
cycle excess reactivity. The temperature defects are induced by the
Uncertainties ($) 0.93 –
reactor from full power to hot standby (the reactor power is zero
Maximum requirements ($) 10.27 4.5
but the coolant is at the inlet temperature for full power operation)
and from the hot standby to refueling. The reactivity fault implies
Table 3
the ejection accident of the assembly with the maximum value. The
Information of control assemblies.
total requirements of the reactivity are about 10.27$ and 4.5$ for
Parameters Primary Secondary primary (RCS) and secondary (RSS) bundles of control assemblies
with 10% uncertainty, separately. The available reactivity worth of
Number of control assemblies 7 6
Reactivity worth of control system ($) 14.10 7.0 RCS with seven control assemblies, which considers the worth of
Worth of 1 stuck assembly ($) 1.37 2.0
one stuck assembly with the maximum value, is 12.73$, the shut-
Reactivity worth available ($) 12.73 5.0
down margin is 2.46$. For RSS, there is about 0.5$ shutdown margin.
X. Yuan et al. / Nuclear Engineering and Design 285 (2015) 23–30 29
Table 4
Design parameters for reference core of the SMoPN.
Parameters Values Parameters Values/materials
Thermal power (MWt) 300 Cladding material Stainless T91
◦
Inlet temperature ( C) 320 Fuel material PuN + ThN
◦
Outlet temperature ( C) 500 Coolant material PbBi
Number of fuel assembly 240 Control absorber material B4C
Number of control assembly 13 Detailed size Ref. Figs. 1–3
Number of reflector assembly 60 Heavy metal inventory in core (ton) 19.41
Number of shielding assembly 138 Maximum linear power density (kW/m) 8.2
Flat to flat distance of FA (cm) 11.2 Average discharge burn-up (GWd/t) 186.33
Number of Pin in a FA 127 Average conversion ratio 0.975
◦
P/D 1.2 Maximum centerline temperature ( C) 676
◦
Fuel rod diameter (mm) 8.3 Maximum cladding surface temperature ( C) 650
Active fuel height (mm) 1950 Average flow velocity (m/s) 1.1
Active core diameter (mm) 1957
4. Conclusions
The innovative SMoPN is designed to satisfy the requirement for
the advanced nuclear reactor, which not only improves the safety,
but also enhances the utilization of nuclear fuel and decreases
the costs of fuel reprocessing. The innovative SMoPN concept that
has a 20-year core lifetime without refueling and shuffling was
proposed. The thermal output is 300 MWth in the normal opera-
tion.
The plutonium extracted from PWR and natural thorium are uti-
lized as fuel of the SMoPN for advanced nuclear fuel cycle, which
will increase the efficiency and space of fuel utilization. Espe-
cially, the nitride fuel used in the SMoPN can help to increase
the conversion ratio up to 0.97, which ensures the core has
a long lifetime, 20 full effective power years (EFPYs) without
refueling and shuffling. The burn-up reactivity loss of the inno-
vative the SMoPN rod is set up at the center of the reactor
core, hence burn-up swing is almost zero in the whole life-
time.
Using liquid Pb-Bi, which had several decades of operation expe-
rience as coolant, not only improves natural circulation, but also
enhances the safety and improves the economy of neutron at the
same time. To avoid the severest accident of LOCF (Loss of Coolant
Flow), the core was sunk in the coolant which was also used as
Fig. 11. Relative power factor distributions for each assembly at the EOL.
the reflector material. Assuming that the coolant was lost totally,
the leakage of neutron will be very high to induce the core going
subcritical.
Hence, the two control systems are reliable to control the reactor The integrated modular structure of the SMoPN provides an
in any operation considerations. opportunity to apply batch production of the standard reac-
tor modules and the production-line methods for the core and
construction. This will make it possible to reduce considerably
3.3. Summary of design the schedule period of the nuclear power plant construc-
tion.
Based on the above analysis, the core characteristics of the All of the important reactivity coefficients are negative to assure
SMoPN in the lifetime 20 EFPYs are summarized in the following. the SMoPN with passive safety. This innovative nuclear power tech-
nology based on the multi-purpose SMoPN with chemically inert
• Pb-Bi coolant, which may assure a high level of social acceptabil-
The core reactivity swing is near zero because the nitride thorium
ity of the nuclear plant. This will heighten the competitiveness of
is used as the fertile material with conversion ratio 0.975. All of
nuclear power plant at the investment market and promote nuclear
the reactivity coefficients are negative.
• power development.
The maximum discharge burn-up is about 230 GWd/t less than
the design criteria and the maximum linear power is 8.2 kW/m.
• Acknowledgements
The maximum peak power factor is about 1.35 in radial direction
and move gradually to center of core from outside with the burn-
This work was financially supported by the Program for
up.
• Changjiang Scholars and Innovative Research Team in Univer-
The control system can provide the enough reactivity to shut-
sity (IRT1280), China Postdoctoral Science and Technology Fund
down the reactor in any situation.
(2013M532051) and Shanxi Province Postdoctoral Science and
Technology Fund (20130018). Authors also appreciate helps from
All of the parameters and values of the SMoPN characteristics Yunlong Xiao, Baolin Liu, Chuanqi Zhao and Zhipeng Li of NECP
are listed in Table 4 and satisfy all design criteria and goals. laboratory of Xi’an Jiaotong University.
30 X. Yuan et al. / Nuclear Engineering and Design 285 (2015) 23–30
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