CA1108316A - Integral nuclear fuel element assembly - Google Patents
Integral nuclear fuel element assemblyInfo
- Publication number
- CA1108316A CA1108316A CA300,417A CA300417A CA1108316A CA 1108316 A CA1108316 A CA 1108316A CA 300417 A CA300417 A CA 300417A CA 1108316 A CA1108316 A CA 1108316A
- Authority
- CA
- Canada
- Prior art keywords
- fuel
- pins
- pin
- moderator
- nuclear
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000003758 nuclear fuel Substances 0.000 title claims abstract description 8
- 239000000446 fuel Substances 0.000 claims abstract description 94
- XLYOFNOQVPJJNP-ZSJDYOACSA-N Heavy water Chemical group [2H]O[2H] XLYOFNOQVPJJNP-ZSJDYOACSA-N 0.000 claims description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 10
- 238000005253 cladding Methods 0.000 claims description 7
- 229910052778 Plutonium Inorganic materials 0.000 claims description 4
- OYEHPCDNVJXUIW-UHFFFAOYSA-N plutonium atom Chemical compound [Pu] OYEHPCDNVJXUIW-UHFFFAOYSA-N 0.000 claims description 4
- 238000009395 breeding Methods 0.000 abstract description 9
- 230000001488 breeding effect Effects 0.000 abstract description 9
- 238000006243 chemical reaction Methods 0.000 abstract description 5
- 230000002844 continuous effect Effects 0.000 abstract 1
- 239000002826 coolant Substances 0.000 description 19
- 125000006850 spacer group Chemical group 0.000 description 7
- 238000013461 design Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 5
- 238000005219 brazing Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 150000002500 ions Chemical class 0.000 description 3
- 229940076400 plutonium Drugs 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- AFCARXCZXQIEQB-UHFFFAOYSA-N N-[3-oxo-3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)propyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CCNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 AFCARXCZXQIEQB-UHFFFAOYSA-N 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000013459 approach Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004907 flux Effects 0.000 description 2
- 230000003071 parasitic effect Effects 0.000 description 2
- 230000009257 reactivity Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- HAAITRDZHUANGT-UHFFFAOYSA-N 1-[2-[(7-chloro-1-benzothiophen-3-yl)methoxy]-2-(2,4-dichlorophenyl)ethyl]imidazole;nitric acid Chemical compound O[N+]([O-])=O.ClC1=CC(Cl)=CC=C1C(OCC=1C2=CC=CC(Cl)=C2SC=1)CN1C=NC=C1 HAAITRDZHUANGT-UHFFFAOYSA-N 0.000 description 1
- OYEHPCDNVJXUIW-FTXFMUIASA-N 239Pu Chemical compound [239Pu] OYEHPCDNVJXUIW-FTXFMUIASA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 101100179590 Caenorhabditis elegans ins-21 gene Proteins 0.000 description 1
- 101150039033 Eci2 gene Proteins 0.000 description 1
- 101000852483 Homo sapiens Interleukin-1 receptor-associated kinase 1 Proteins 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 102100036342 Interleukin-1 receptor-associated kinase 1 Human genes 0.000 description 1
- 241000643898 Plutonium Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000004992 fission Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910001293 incoloy Inorganic materials 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000003595 spectral effect Effects 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21C—NUCLEAR REACTORS
- G21C3/00—Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
- G21C3/30—Assemblies of a number of fuel elements in the form of a rigid unit
- G21C3/32—Bundles of parallel pin-, rod-, or tube-shaped fuel elements
- G21C3/336—Spacer elements for fuel rods in the bundle
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21C—NUCLEAR REACTORS
- G21C3/00—Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
- G21C3/02—Fuel elements
- G21C3/28—Fuel elements with fissile or breeder material in solid form within a non-active casing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
Abstract
Case 4166 INTEGRAL NUCLEAR FUEL ELEMENT ASSEMBLY
A B S T R A C T
An integral nuclear fuel element assembly utilizes longitudinally finned fuel pins. The con-tinuous or interrupted pins of the fuel pins are brazed to fins of juxtaposed fuel pins or directly to the juxtaposed fuel pins or both. The integrally brazed fuel assembly is designed to satisfy the thermal and hydraulic requirements of a fuel assembly lattice having moderator to fuel atom ratios required to achieved high conversion and breeding ratios.
A B S T R A C T
An integral nuclear fuel element assembly utilizes longitudinally finned fuel pins. The con-tinuous or interrupted pins of the fuel pins are brazed to fins of juxtaposed fuel pins or directly to the juxtaposed fuel pins or both. The integrally brazed fuel assembly is designed to satisfy the thermal and hydraulic requirements of a fuel assembly lattice having moderator to fuel atom ratios required to achieved high conversion and breeding ratios.
Description
- - Case 4166 .
~ 3~
1. Field of the Invention This inyention relates to a fuel asse~bly design for use in a nuclear reactor and particularly to a fast breeder reactor utilizing plutonium as a fuel and pres-surlzed/hea~y water as a reactor coolant and moderator.
~ 3~
1. Field of the Invention This inyention relates to a fuel asse~bly design for use in a nuclear reactor and particularly to a fast breeder reactor utilizing plutonium as a fuel and pres-surlzed/hea~y water as a reactor coolant and moderator.
2, The ad~antages of utilizing nuclear ~reeder reactors which convert ~ertile material into fissile ma~erial and generate hea~, e~g. for power generation, ha~e been widely recognized in ~iew of the limited known fis3ionable material resources of the world. Develop-men~ o~ breeder reactors which convert the more abundant fertile uranium-238 into fissile plutonium-239 utilizing the latter as a fuel, possibly in conJunction wlth plu-tonium generated in other known reactors, and breed more ~issionable material~than is consumed, is highly desirable.
Since extens~ve tech~ological development and experience exists in the design and construction of pressurized light and heavy water reactor plants, use o~ the pressuri~ed ~ -water technology in a breeder application represents an attractive alterna~ive to development of other breeder options.
Heavy water, deuterium oxide (D2O), has essen-tially the same physical and chemical propertles as ligh~
water~ H2O. Its nuclear properties, howe~er, are dlf-ferent~ the neutron absorption cross-section and slowing - down power of D2O being mar~edly lower than that of H2O.
Hence~ the use of D2O as a coolant in a fast breeder - 2 ~
' Case 4166 ~f~3~$
application ls desirable due to its nuclear characteristics and the aprlicability of pressuri~ed water technology. In a pluton~um-uranium-deuterium oxide(Pu-U-D20~ reactor system, as the coolant to fuel atom ratio decreases~ it is known that the conversion or breeding ratios increase. The breed-ing ratio is the ratio of the number of fissile atoms produced to those consumed. High breeding ratics~ approach-ing a value o~ 1.40, may be realized in a Pu-U-D20 system i~ a fuel latt~ce geomekry is d~veloped wherein moderator to fuel volume ratios are ~d~us~ed to ~eld moderator ~o fuel atom rat~os approaching 1.0 or le~s. As the selection of a moderator to fuel atom ratio de~ines the volume of coolant per unit mass of fuel, it can be appreciated that difficulties arise in designing a ~uel lattice capable of passing adequa~e cooling flow rate at low moderator to fuel ratios. The high flow rates needed to assure adequate reactor core cooling necessitate high velocities in ~low :
channel3 tha~ are significantly restricted when achie~lng a low moderator to fuel ra~io. In the tightly packed fuel pin la~tices, the use of conventional spacer grids is dis-advantageous owing to inherent limits in fuel pin packing due to the interposed grids, a tendency to flow induced spacer grid ~ibration, the parasitic absorption of the grid plate ma~erial, and the increase in hydraulic pressure loss resulting from introduction of grids within ~he restricted flow passages.
The prior art teaches heavy water moderated and cooled reactor des~gns for particular fuel "rod" dia-meters and spacings wi~hin a moderator to fuel atom ratio range from 0.35 to 4.0 and suggests ~hat a moderator to fuel atom ratio of approxlmately 0.3 can be achieved
Since extens~ve tech~ological development and experience exists in the design and construction of pressurized light and heavy water reactor plants, use o~ the pressuri~ed ~ -water technology in a breeder application represents an attractive alterna~ive to development of other breeder options.
Heavy water, deuterium oxide (D2O), has essen-tially the same physical and chemical propertles as ligh~
water~ H2O. Its nuclear properties, howe~er, are dlf-ferent~ the neutron absorption cross-section and slowing - down power of D2O being mar~edly lower than that of H2O.
Hence~ the use of D2O as a coolant in a fast breeder - 2 ~
' Case 4166 ~f~3~$
application ls desirable due to its nuclear characteristics and the aprlicability of pressuri~ed water technology. In a pluton~um-uranium-deuterium oxide(Pu-U-D20~ reactor system, as the coolant to fuel atom ratio decreases~ it is known that the conversion or breeding ratios increase. The breed-ing ratio is the ratio of the number of fissile atoms produced to those consumed. High breeding ratics~ approach-ing a value o~ 1.40, may be realized in a Pu-U-D20 system i~ a fuel latt~ce geomekry is d~veloped wherein moderator to fuel volume ratios are ~d~us~ed to ~eld moderator ~o fuel atom rat~os approaching 1.0 or le~s. As the selection of a moderator to fuel atom ratio de~ines the volume of coolant per unit mass of fuel, it can be appreciated that difficulties arise in designing a ~uel lattice capable of passing adequa~e cooling flow rate at low moderator to fuel ratios. The high flow rates needed to assure adequate reactor core cooling necessitate high velocities in ~low :
channel3 tha~ are significantly restricted when achie~lng a low moderator to fuel ra~io. In the tightly packed fuel pin la~tices, the use of conventional spacer grids is dis-advantageous owing to inherent limits in fuel pin packing due to the interposed grids, a tendency to flow induced spacer grid ~ibration, the parasitic absorption of the grid plate ma~erial, and the increase in hydraulic pressure loss resulting from introduction of grids within ~he restricted flow passages.
The prior art teaches heavy water moderated and cooled reactor des~gns for particular fuel "rod" dia-meters and spacings wi~hin a moderator to fuel atom ratio range from 0.35 to 4.0 and suggests ~hat a moderator to fuel atom ratio of approxlmately 0.3 can be achieved
- 3 l~G`~3~ ~j case 4166 in a fuel lattice utilizing touchln~ ~uel rods arranged in a trian~ular pltch. Reduction of heat flux to the de~ree necess~ry to avoid potentially destructive hot spots at fuel pin contact polnks~ however, ~ould severely limit the capability of operating such a core at pres- - -surized water reactor conditio~s. ~urthermore, close spacing of the ~uel pins may lead to plugging by solid particles carried by the c~olant and prohibitiYely high reactor coolant pumping power requirements Other dif~
~iculties become readily apparent On the one hand, elim-in~tion o~ spacer grids ls desirable in order to permit the higher coolant flow velocities needed to approach the modera~or to fuel atom ratios yielding the high conversion ratio of the touching fuel rod configuration. On the other hand, elim~nation of spacer grids may result in impre~ise fuel pin spacing, flow induced vibration and unequal cool-ingi ~`~
SUMMARY OF THE INVENTION
- ~: , In accordance with the princlples of the inven-tion, the dlsad~antages of the prior art, discussed above, are effecti~ely surmou~ted by the practice of the in~
~ention. A fuel assem~ly, made in accordance with ~his inYention, utilizes longitudinally flnned fuel pin clad- i;
ding tubes arranged to form an integral fuel assembly by brazing together the continuous or interrupted ~ins of one fuel pin to the fins of other fuel pins. The in~
te~rally brazed fln ~uel pin assem~ly is designed to sat~sfy the thermal and hydraulic requirements of the very tight lattice required to achieve high breedlng ratios. ~:~
.
., :,........... .. - .. : . ~ .
~ Case 4166 In an alternate embod.iment the fins o~ some fuel pins may be connected directly to the tubular sect~on of other fuel ~ns 50 that the resulting assemblies have modera~or ~o fuel volume ratios which tend ko increase the breed~ng ratio in a Pu-U-D20 reac~or core.
In a further embodlment of the invent~on~ the core is fabricated from a solid mater~al ha~ng passages which are alternative~ suit,ed for coolant flo~ and ~uel retention.
Practice of the invention overcomes the dis~
advantages of the prior art by providing means ~or obtaining moderator to fuel ratios whlch are conducive to a high Pu-U-~20 reactor breeding ratio while assur-ing accurate spacing of the fuel pins without the para-sitic losses associated with the prior art~s use of spacer grlds. Furthermore~ the arrangemen~s of the ~ ~
inYention eliminate hydraulic pressure losses assoc- ;
;~
iated with conventional spacer grids~and reduce the - tendency o~ fuel pin~v~bration. ~he finned fuel pin arrangements, moreover, increase the strength of the pins, increase the available hea~ transfer surface and improve the overall heat transfer coeff~cient.
The various ~eatures of novelty which charac-terize the invention are pointed out with par~icularity ~-in the claims annexed to and forming a part of this specification. For a better understanding of the in-vention, its operatin~ ad~antages and ~peci~ic ob~ects ` attained by its u~e~ ~e~erence should be made to the .
accompanying drawings and descripti~e matter in which 3 there is illustrated and described a preferred embodi-~; ~ . ment of the lnvention .
; - 5 -Case 4166 BRIEF DESCRIPTION OF TH~ DRAWINGS
In the accompanying drawings, forming a part of this specification~ and in which reference numerals shown in the dra~ings designa~e like or corresponding parts throughout the same~
Figure 1 ~s a partial section in plan of a fuel ?
assembly;
Figure 2 is an ele~ation VieW of part of a number of finned fuel elements arranged ~n accordance 10with an alternate embodiment of the invention Figure 3 is an elevation vlew of part of a ~
number of fuel elements arranged in accordance with ~ -another alternate embodiment of the invention;
Figure 4 is a partial section plan of a ~uel assembly having ~uel elements arranged in accordance with still another embodiment of-the in~ention~ and Figure 5 is a part plan of a block core arrange-ment for a lo~ temperature reactor.
; ~
DESCRIPTION OF THE PREFERRED EMBODIMENTS :
Figure 1 shows part of a nuclear fuel asse~bly 10 of closely packed fuel plns 11 arranged in an array : with their longitudinal axes in parallel. ~ach fuel :--pin 1l consists of generally tubular cladding 12 which has a pluralIty of lcngltudinally extending fins 13 formed as part of the outer surface of the cladding and spaced circumferentially the~eabout. A nuclear fuel 14 consisting of a ~ixture of fisslle and fertile~material, is contained within the cladding 12. The fuel pins 11 :~ .
~ .
..
`. Case 4166 in Figure 1 are arranged so that .the extremity of each ~in 13A ~buts ~h the extremity of a fin 13B of a ~uxta-posed fuel pin; fins of peripheral fuel pins may abut the fuel assembly can structure 15, ~he extremities of the fins shown in Figure 1 are joined to each other and to the reactor can structure by means of brazing at 16 and 17, respectiyely~ to form the integral fuel assembly 10.
The rins 13, in one embodiment, extend without interrup~ion along the longitudinal surface of the ~uel pin forming channels 20 in the interspaces o~ the fuel pins which direct reactor coolant flow (not shown) there-of the ~n within generally in parallel with ~he longitudinal axis/
The fins 13, however, need not extend continuously:along the len~th of the fuel pins but can be interrupted ~ins 21, as shown in Figures 2 and 3,so as to allow transverse flow and intermixing of the coolant through the fuel pin i~ter-spaces. The axially interrupted fins 21 of juxtaposed , fuel p~ns may be brazed to each other at 22 (Figure 2) org as shown in Figure 3 directly to the tubular portion of the fuel pin at 23. An assembly utilizin~ a combina- ~.
tion of both arrangements shown in Figures 2 and 3, i.e., fin .to fin contact and fin to tube contact, is also possible.
A finned fuel pin 26 design utilizing ~road rins 24 brazed to each other a~ 25 is shown in Figure 4. Broad .P
fins may be utilized to further 1imit the moderator volume frac~ion at some sacrifice of specific core power.
Elimination Or conventional spacer grids and the formation of fins ~s part of the tube. cladding:permits : ~
3 reduction of the reactor core moderator volume fraction Case 4166 3~
to ~alues cons~stent with the achievement o~ thé desired moderator ~o fuel ato~ ratios, Illus~rat~e physlcal design parameters are set forth in Table 1.
TABLE I
Example 1 2 3 ~
Fuel Pin Diame~er~ inches.35 .40 .40 : :
Fuel Pin Pitch~ inches ,39 - .43 .43 Clad Thickness, in~hes ,015 .020 .020 Clad Material Incoloy Type 316 Type 316 800 Stainless Stainless . Steel Steel Pitch - Diameter, inches.040 .030 .030 Number o~ ~ins per Pin 6 3 3 .~:
Fin height~ inches .020 .030 .030 ~:
Fin w~dth, inches .Q20 .030 .030 -.
Fin interruption, percent of 0 30 Fuel Volume Fraction - .6105 .6357 .6357 Structural ~olume Fraction .1381 .1659 .~1541 2C Coolant Volu~e Fraction.2514 .1984 .2102 Fuel/Coolant Volume Fraction Ratio 2.43 3.20 3.02 ~.
~ Moderator/Fuel Atom Ratio .82 .624 .66 : The fuel pins in the examples o~ ~able I are - formed in the shapes of rods~ The fuel plns o~ examples 1 and 2 are pro~ided with continuous ~in~ along their length, Example 3 ill~strates an alternate embodiment of example 2 wherein the fins traYerse approximately thirty percent o~ the }ength of the rods. The values - for the moderator to fuel atom ratios shown ln Table I
3 approxima~e normal pressurized water reactor operating - 8 - ;
Case 4166 ti~3'~
conditions including primary coolant .temperature and pressure~ fuel ~ellet shape~ clearances between the fuel pellets and clad, and percent of theoretical U02 density achieyed in the pelle~, The fuel assemblies of Table I would be typlcally formed by furnace brazing in a hydrogen atmosphere at 1950 to 2000F ~th a braæing alloy tradenamed "N~crobraz ~available ~rom the Wall-Colmonoy Corp.~ Detroit, Michigan) usin~ ~igs, ~ix~ures and methods of braze alloy placement known ln the furnace brazing art.
In still another embodiment, Figure 5 illustrates a desi~n ~or low temperature reactors suitable for breed-ing plutonium and low heat generation purpose, e.g.
residential heating. In this e~bodimen~ a fuel assembly is fabricated from a block 32 of metal, e.g. aluminum alloy. Parallel channels are formed for ~low passage and for fuei 30. The surfaces of the flow ~hannels may be roughened where needed to increase critical heat flux.
Illustrative design parameters ~or a block type reactor :
are shown in Table II.
TABLE II
. .
Example 1 2 Fuel channel diameter, inches .40 .325 ~-Fuel channel pitch, inches .500 O40 Coolant channel diameter, lnches .156 .125 Coolant channel pitch, inches .500 .40 Fuel Yolume fra~tlon ~ 0503 .518 Structure Yolu~e fr~ction ~421 .405 Coolant Volume fractlon ~o76 .0766 3` Fuel/Coolant Volume Frac~ion Ratio 6~62 6.76 Modera~or/Fuel Atom Ratio .44 ~43 : Case 4166 ~ 3~$
The moderator to fuel atom ratio o~ Table II
correspo~ds to a primary coolant water temperacure of about 250F at low pressure. Other process parameters are similar to those assumed ~or Table I.
The geometry of the coolant and fuel channels in the block type fuel assembly will produce a degree o~ what might be termed "moderator escape probab~llty" which wlll ser~e to ~arden the neutron spectrum and improYe the core conversion or breeding ratio. This occurs because each fuel channel is not completely surrounded by moderator.
Hence, some neutrons produced in a fuel channel can pass to another fuel channel without traversing a volume con-- taining moderator, thereby lmproving the breeding or conversion ratio since the average neutron energy at which fission occurs is increased. This, combined w1th a mod-erator to fuel ratio less than that which can be aohieved with touching uel pins, should yield a uniquely high breeding ratio for either H~O or D20 coolin~
By vlrtue of the moderator to fuel atom ratios 23 made possible by these approaches to fuel assembly design, fast reactor physics can be applied to pressurized water reactor tehnology. This combination has important ad-vanta~es including:
a. A~oidance of gas or liquid metal coolants - otherwise used for fast reactors.
. Reduced clad operating temperature.
c. AYailability of additional methods of reactivity control, namely, chem~cal shim and spectral shift control~
.~ 3a Availabllity of additional methods of reactivity control ... .
reduces the nor~.al dependence of ~ast reactors on control rods. They allow a general reduction in required control .
. . , .
Case 4166 rod worth and provide a means for continuous a~jus~ment of e~cess react:lvity to a minimum value, thereby greatly enhancing the safety of fast reactor cores. This would lnclude operation with higher worth rods out of the core.
:
.
: ' . :
: j :
~ - : : :
, z ~:
:.
~iculties become readily apparent On the one hand, elim-in~tion o~ spacer grids ls desirable in order to permit the higher coolant flow velocities needed to approach the modera~or to fuel atom ratios yielding the high conversion ratio of the touching fuel rod configuration. On the other hand, elim~nation of spacer grids may result in impre~ise fuel pin spacing, flow induced vibration and unequal cool-ingi ~`~
SUMMARY OF THE INVENTION
- ~: , In accordance with the princlples of the inven-tion, the dlsad~antages of the prior art, discussed above, are effecti~ely surmou~ted by the practice of the in~
~ention. A fuel assem~ly, made in accordance with ~his inYention, utilizes longitudinally flnned fuel pin clad- i;
ding tubes arranged to form an integral fuel assembly by brazing together the continuous or interrupted ~ins of one fuel pin to the fins of other fuel pins. The in~
te~rally brazed fln ~uel pin assem~ly is designed to sat~sfy the thermal and hydraulic requirements of the very tight lattice required to achieve high breedlng ratios. ~:~
.
., :,........... .. - .. : . ~ .
~ Case 4166 In an alternate embod.iment the fins o~ some fuel pins may be connected directly to the tubular sect~on of other fuel ~ns 50 that the resulting assemblies have modera~or ~o fuel volume ratios which tend ko increase the breed~ng ratio in a Pu-U-D20 reac~or core.
In a further embodlment of the invent~on~ the core is fabricated from a solid mater~al ha~ng passages which are alternative~ suit,ed for coolant flo~ and ~uel retention.
Practice of the invention overcomes the dis~
advantages of the prior art by providing means ~or obtaining moderator to fuel ratios whlch are conducive to a high Pu-U-~20 reactor breeding ratio while assur-ing accurate spacing of the fuel pins without the para-sitic losses associated with the prior art~s use of spacer grlds. Furthermore~ the arrangemen~s of the ~ ~
inYention eliminate hydraulic pressure losses assoc- ;
;~
iated with conventional spacer grids~and reduce the - tendency o~ fuel pin~v~bration. ~he finned fuel pin arrangements, moreover, increase the strength of the pins, increase the available hea~ transfer surface and improve the overall heat transfer coeff~cient.
The various ~eatures of novelty which charac-terize the invention are pointed out with par~icularity ~-in the claims annexed to and forming a part of this specification. For a better understanding of the in-vention, its operatin~ ad~antages and ~peci~ic ob~ects ` attained by its u~e~ ~e~erence should be made to the .
accompanying drawings and descripti~e matter in which 3 there is illustrated and described a preferred embodi-~; ~ . ment of the lnvention .
; - 5 -Case 4166 BRIEF DESCRIPTION OF TH~ DRAWINGS
In the accompanying drawings, forming a part of this specification~ and in which reference numerals shown in the dra~ings designa~e like or corresponding parts throughout the same~
Figure 1 ~s a partial section in plan of a fuel ?
assembly;
Figure 2 is an ele~ation VieW of part of a number of finned fuel elements arranged ~n accordance 10with an alternate embodiment of the invention Figure 3 is an elevation vlew of part of a ~
number of fuel elements arranged in accordance with ~ -another alternate embodiment of the invention;
Figure 4 is a partial section plan of a ~uel assembly having ~uel elements arranged in accordance with still another embodiment of-the in~ention~ and Figure 5 is a part plan of a block core arrange-ment for a lo~ temperature reactor.
; ~
DESCRIPTION OF THE PREFERRED EMBODIMENTS :
Figure 1 shows part of a nuclear fuel asse~bly 10 of closely packed fuel plns 11 arranged in an array : with their longitudinal axes in parallel. ~ach fuel :--pin 1l consists of generally tubular cladding 12 which has a pluralIty of lcngltudinally extending fins 13 formed as part of the outer surface of the cladding and spaced circumferentially the~eabout. A nuclear fuel 14 consisting of a ~ixture of fisslle and fertile~material, is contained within the cladding 12. The fuel pins 11 :~ .
~ .
..
`. Case 4166 in Figure 1 are arranged so that .the extremity of each ~in 13A ~buts ~h the extremity of a fin 13B of a ~uxta-posed fuel pin; fins of peripheral fuel pins may abut the fuel assembly can structure 15, ~he extremities of the fins shown in Figure 1 are joined to each other and to the reactor can structure by means of brazing at 16 and 17, respectiyely~ to form the integral fuel assembly 10.
The rins 13, in one embodiment, extend without interrup~ion along the longitudinal surface of the ~uel pin forming channels 20 in the interspaces o~ the fuel pins which direct reactor coolant flow (not shown) there-of the ~n within generally in parallel with ~he longitudinal axis/
The fins 13, however, need not extend continuously:along the len~th of the fuel pins but can be interrupted ~ins 21, as shown in Figures 2 and 3,so as to allow transverse flow and intermixing of the coolant through the fuel pin i~ter-spaces. The axially interrupted fins 21 of juxtaposed , fuel p~ns may be brazed to each other at 22 (Figure 2) org as shown in Figure 3 directly to the tubular portion of the fuel pin at 23. An assembly utilizin~ a combina- ~.
tion of both arrangements shown in Figures 2 and 3, i.e., fin .to fin contact and fin to tube contact, is also possible.
A finned fuel pin 26 design utilizing ~road rins 24 brazed to each other a~ 25 is shown in Figure 4. Broad .P
fins may be utilized to further 1imit the moderator volume frac~ion at some sacrifice of specific core power.
Elimination Or conventional spacer grids and the formation of fins ~s part of the tube. cladding:permits : ~
3 reduction of the reactor core moderator volume fraction Case 4166 3~
to ~alues cons~stent with the achievement o~ thé desired moderator ~o fuel ato~ ratios, Illus~rat~e physlcal design parameters are set forth in Table 1.
TABLE I
Example 1 2 3 ~
Fuel Pin Diame~er~ inches.35 .40 .40 : :
Fuel Pin Pitch~ inches ,39 - .43 .43 Clad Thickness, in~hes ,015 .020 .020 Clad Material Incoloy Type 316 Type 316 800 Stainless Stainless . Steel Steel Pitch - Diameter, inches.040 .030 .030 Number o~ ~ins per Pin 6 3 3 .~:
Fin height~ inches .020 .030 .030 ~:
Fin w~dth, inches .Q20 .030 .030 -.
Fin interruption, percent of 0 30 Fuel Volume Fraction - .6105 .6357 .6357 Structural ~olume Fraction .1381 .1659 .~1541 2C Coolant Volu~e Fraction.2514 .1984 .2102 Fuel/Coolant Volume Fraction Ratio 2.43 3.20 3.02 ~.
~ Moderator/Fuel Atom Ratio .82 .624 .66 : The fuel pins in the examples o~ ~able I are - formed in the shapes of rods~ The fuel plns o~ examples 1 and 2 are pro~ided with continuous ~in~ along their length, Example 3 ill~strates an alternate embodiment of example 2 wherein the fins traYerse approximately thirty percent o~ the }ength of the rods. The values - for the moderator to fuel atom ratios shown ln Table I
3 approxima~e normal pressurized water reactor operating - 8 - ;
Case 4166 ti~3'~
conditions including primary coolant .temperature and pressure~ fuel ~ellet shape~ clearances between the fuel pellets and clad, and percent of theoretical U02 density achieyed in the pelle~, The fuel assemblies of Table I would be typlcally formed by furnace brazing in a hydrogen atmosphere at 1950 to 2000F ~th a braæing alloy tradenamed "N~crobraz ~available ~rom the Wall-Colmonoy Corp.~ Detroit, Michigan) usin~ ~igs, ~ix~ures and methods of braze alloy placement known ln the furnace brazing art.
In still another embodiment, Figure 5 illustrates a desi~n ~or low temperature reactors suitable for breed-ing plutonium and low heat generation purpose, e.g.
residential heating. In this e~bodimen~ a fuel assembly is fabricated from a block 32 of metal, e.g. aluminum alloy. Parallel channels are formed for ~low passage and for fuei 30. The surfaces of the flow ~hannels may be roughened where needed to increase critical heat flux.
Illustrative design parameters ~or a block type reactor :
are shown in Table II.
TABLE II
. .
Example 1 2 Fuel channel diameter, inches .40 .325 ~-Fuel channel pitch, inches .500 O40 Coolant channel diameter, lnches .156 .125 Coolant channel pitch, inches .500 .40 Fuel Yolume fra~tlon ~ 0503 .518 Structure Yolu~e fr~ction ~421 .405 Coolant Volume fractlon ~o76 .0766 3` Fuel/Coolant Volume Frac~ion Ratio 6~62 6.76 Modera~or/Fuel Atom Ratio .44 ~43 : Case 4166 ~ 3~$
The moderator to fuel atom ratio o~ Table II
correspo~ds to a primary coolant water temperacure of about 250F at low pressure. Other process parameters are similar to those assumed ~or Table I.
The geometry of the coolant and fuel channels in the block type fuel assembly will produce a degree o~ what might be termed "moderator escape probab~llty" which wlll ser~e to ~arden the neutron spectrum and improYe the core conversion or breeding ratio. This occurs because each fuel channel is not completely surrounded by moderator.
Hence, some neutrons produced in a fuel channel can pass to another fuel channel without traversing a volume con-- taining moderator, thereby lmproving the breeding or conversion ratio since the average neutron energy at which fission occurs is increased. This, combined w1th a mod-erator to fuel ratio less than that which can be aohieved with touching uel pins, should yield a uniquely high breeding ratio for either H~O or D20 coolin~
By vlrtue of the moderator to fuel atom ratios 23 made possible by these approaches to fuel assembly design, fast reactor physics can be applied to pressurized water reactor tehnology. This combination has important ad-vanta~es including:
a. A~oidance of gas or liquid metal coolants - otherwise used for fast reactors.
. Reduced clad operating temperature.
c. AYailability of additional methods of reactivity control, namely, chem~cal shim and spectral shift control~
.~ 3a Availabllity of additional methods of reactivity control ... .
reduces the nor~.al dependence of ~ast reactors on control rods. They allow a general reduction in required control .
. . , .
Case 4166 rod worth and provide a means for continuous a~jus~ment of e~cess react:lvity to a minimum value, thereby greatly enhancing the safety of fast reactor cores. This would lnclude operation with higher worth rods out of the core.
:
.
: ' . :
: j :
~ - : : :
, z ~:
:.
Claims (3)
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A fuel assembly for use in a pressurized water moderated and cooled nuclear fast breeder reactor comprising a nuclear fuel, a plurality of fuel pins disposed with parallel longitudinal axes in closely packed array, each fuel pin consisting essentially of a generally tubular cladding bearing said nuclear fuel and at least one longitudinally extending fin formed as part of the surface of the cladding of each of said fuel pins, and a brazed connection fixedly joining the extremity of said fin to the tubular cladding of a juxtaposed fuel pin to form an integral fuel assembly having a moderator to fuel atom ratio in the range from 0.624 to 0.82.
2. A fuel assembly according to claim 1 wherein at least one of the fuel pins includes a plurality of said fins extending continuously without interruption along the longitudinal surface of said fuel pin generally in parallel with the longitudinal axis of the pin.
3. A fuel assembly according to claim 1 wherein the nuclear fuel is plutonium and the pressurized water is heavy water.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US81640177A | 1977-07-18 | 1977-07-18 | |
US816,401 | 1977-07-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1108316A true CA1108316A (en) | 1981-09-01 |
Family
ID=25220487
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA300,417A Expired CA1108316A (en) | 1977-07-18 | 1978-04-04 | Integral nuclear fuel element assembly |
Country Status (14)
Country | Link |
---|---|
JP (1) | JPS5422090A (en) |
AT (1) | AT364041B (en) |
BE (1) | BE866444A (en) |
CA (1) | CA1108316A (en) |
CH (1) | CH639792A5 (en) |
DE (1) | DE2825142A1 (en) |
ES (1) | ES469174A1 (en) |
FR (1) | FR2398368A1 (en) |
GB (1) | GB1604075A (en) |
IL (1) | IL54460A (en) |
IT (1) | IT1103093B (en) |
LU (1) | LU79480A1 (en) |
NL (1) | NL7804259A (en) |
SE (2) | SE436809B (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2168192B (en) * | 1984-12-07 | 1989-08-31 | Atomic Energy Authority Uk | Gas cooled nuclear reactors |
JPS61257843A (en) * | 1985-05-09 | 1986-11-15 | Nippon Seimitsu Kogyo Kk | Paper feed device |
JPS61257844A (en) * | 1985-05-09 | 1986-11-15 | Nippon Seimitsu Kogyo Kk | Copy paper feed device |
US7694950B2 (en) | 2005-03-30 | 2010-04-13 | Brother Kogyo Kabushiki Kaisha | Sheet feed device and image recording apparatus having such sheet feed device |
CN112424875A (en) * | 2018-06-21 | 2021-02-26 | 博沃艾特核能公司 | Universal inverted reactor and method for design and manufacture of universal inverted reactor |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1062351B (en) * | 1958-01-15 | 1959-07-30 | ||
FR1287558A (en) * | 1960-03-15 | 1962-03-16 | Sulzer Ag | nuclear reactor fuel element |
NL289409A (en) * | 1962-03-07 | |||
FR1347499A (en) * | 1962-03-07 | 1963-12-27 | Euratom | Improvements to nuclear fuel elements |
DE1203888B (en) * | 1963-08-17 | 1965-10-28 | Kernforschung Gmbh Ges Fuer | Nuclear reactor fuel bundle |
FR1408920A (en) * | 1964-07-10 | 1965-08-20 | Commissariat Energie Atomique | nuclear reactor fuel element |
GB1056905A (en) * | 1964-08-28 | 1967-02-01 | Ca Atomic Energy Ltd | Fuel rod structure |
SE316246B (en) * | 1964-08-28 | 1969-10-20 | Ca Atomic Energy Ltd | |
DE1464962A1 (en) * | 1964-09-05 | 1969-04-17 | Kernforschung Gmbh Ges Fuer | Fuel element for nuclear reactors |
DE1464986A1 (en) * | 1964-12-30 | 1969-06-04 | Kernforschung Gmbh Ges Fuer | Fuel element for nuclear reactors |
US4060454A (en) * | 1975-04-07 | 1977-11-29 | General Atomic Company | Nuclear fuel element and method for making same |
-
1978
- 1978-04-04 CA CA300,417A patent/CA1108316A/en not_active Expired
- 1978-04-06 JP JP3982078A patent/JPS5422090A/en active Granted
- 1978-04-06 IL IL54460A patent/IL54460A/en unknown
- 1978-04-20 LU LU79480A patent/LU79480A1/en unknown
- 1978-04-21 NL NL7804259A patent/NL7804259A/en not_active Application Discontinuation
- 1978-04-26 ES ES469174A patent/ES469174A1/en not_active Expired
- 1978-04-27 BE BE187162A patent/BE866444A/en not_active IP Right Cessation
- 1978-04-28 CH CH464078A patent/CH639792A5/en not_active IP Right Cessation
- 1978-05-05 AT AT0324578A patent/AT364041B/en not_active IP Right Cessation
- 1978-05-12 IT IT09456/78A patent/IT1103093B/en active
- 1978-05-19 GB GB20769/78A patent/GB1604075A/en not_active Expired
- 1978-06-08 DE DE19782825142 patent/DE2825142A1/en not_active Withdrawn
- 1978-06-16 SE SE7806955A patent/SE436809B/en not_active IP Right Cessation
- 1978-07-12 FR FR7820789A patent/FR2398368A1/en active Granted
-
1984
- 1984-12-28 SE SE8406663A patent/SE456377B/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
SE436809B (en) | 1985-01-21 |
FR2398368A1 (en) | 1979-02-16 |
JPS5718599B2 (en) | 1982-04-17 |
IT7809456A0 (en) | 1978-05-12 |
IT1103093B (en) | 1985-10-14 |
SE456377B (en) | 1988-09-26 |
FR2398368B1 (en) | 1984-10-19 |
LU79480A1 (en) | 1978-09-29 |
JPS5422090A (en) | 1979-02-19 |
ES469174A1 (en) | 1979-04-16 |
SE7806955L (en) | 1979-01-19 |
SE8406663D0 (en) | 1984-12-28 |
NL7804259A (en) | 1979-01-22 |
SE8406663L (en) | 1984-12-28 |
IL54460A (en) | 1983-07-31 |
BE866444A (en) | 1978-08-14 |
ATA324578A (en) | 1981-02-15 |
DE2825142A1 (en) | 1979-01-25 |
CH639792A5 (en) | 1983-11-30 |
AT364041B (en) | 1981-09-25 |
GB1604075A (en) | 1981-12-02 |
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