JPS6249946B2 - - Google Patents
Info
- Publication number
- JPS6249946B2 JPS6249946B2 JP55023621A JP2362180A JPS6249946B2 JP S6249946 B2 JPS6249946 B2 JP S6249946B2 JP 55023621 A JP55023621 A JP 55023621A JP 2362180 A JP2362180 A JP 2362180A JP S6249946 B2 JPS6249946 B2 JP S6249946B2
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- rods
- enrichment
- average
- layer
- 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
- 239000000446 fuel Substances 0.000 claims description 106
- 239000000463 material Substances 0.000 claims description 4
- 239000003758 nuclear fuel Substances 0.000 claims description 4
- CMIHHWBVHJVIGI-UHFFFAOYSA-N gadolinium(iii) oxide Chemical compound [O-2].[O-2].[O-2].[Gd+3].[Gd+3] CMIHHWBVHJVIGI-UHFFFAOYSA-N 0.000 description 22
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 11
- 230000000712 assembly Effects 0.000 description 9
- 238000000429 assembly Methods 0.000 description 9
- 238000010586 diagram Methods 0.000 description 8
- 230000009257 reactivity Effects 0.000 description 8
- 230000007423 decrease Effects 0.000 description 6
- 238000011068 loading method Methods 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000002574 poison Substances 0.000 description 2
- 231100000614 poison Toxicity 0.000 description 2
- 229910052770 Uranium Inorganic materials 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000004992 fission Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
Landscapes
- Monitoring And Testing Of Nuclear Reactors (AREA)
Description
本発明は原子炉燃料集合体に係り、特に沸騰水
形原子炉(以下BWRと略す。)に用いるのに好適
な原子炉燃料集合体に関するものである。
従来、原子炉の運転期間は約1年であり、1年
毎に全燃料集合体の約1/4を新しい燃料集合体と
取り換えて運転するようにしている。しかし、上
記のような運転方法では、定期検査や燃料交換の
ため原子炉を停止する期間が、全運転期間の約25
%を占めるようになるので、上記運転期間を延長
して、上記炉停止期間の全運転期間に占める割合
を小さくして、プラント利用率を高める努力がな
されている。
運転期間の長期化をはかるためには、燃焼初期
の核分裂性核種の量、すなわち、炉心平均濃縮度
を高くしなければならない。炉心平均濃縮度を高
める方法としては、濃縮度の高い燃料を装荷する
方法と、燃料交換体数を多くする方法とがある
が、後者は燃料交換に要する時間が長くなるの
で、一般には前者の方法が採用されている。
ところで、高濃縮燃料の使用は、炉停止余裕を
減少させるという欠点がある。炉停止余裕とは、
冷温(約20℃)状態において、反応度価値がもつ
とも大きい制御棒1本が引抜き状態にあり、他の
全制御棒が全挿入の状態にあるときの実効増倍率
の臨界値(1.0)からの差である。これは、上記
反応度価値のもつとも大きい制御棒を囲む4本の
燃料集合体の平均無限増倍率に依存する。
BWRでは、原子炉運転時(以下運転時と略
す。)にボイドの発生や減速材密度の減少にとも
なう中性子減速能力の低下や燃料中のウラン―
238のドツプラー効果による負の反応度が存在す
るため、燃料の無限増倍率が冷温時より小さい。
一般に上記冷温時の無限増倍率と運転時の無限増
倍率との差は、濃縮度が高くなるほど大きくな
る。さらに、余剰反応度を抑えるために用いられ
る可燃性毒物であるガドリニアの添加量を多くす
れば、この傾向は助長される。したがつて、運転
期間を延長するため濃縮度を高め、余剰反応度を
抑えるためガドリニアの添加量を多くした燃料で
は、運転時において、上記4燃料集合体の平均無
限増倍率が運転期間が短かい場合と同じであつて
も、冷温時には平均無限増倍率が高くなり、炉停
止余裕が減少する。
本発明は上記に鑑みてなされたもので、その目
的とするところは、運転期間の長期化をはかるこ
とができ、しかも、十分な炉停止余裕を確保する
ことができる原子炉燃料集合体を提供することに
ある。
本発明の特徴は、燃料集合体のチヤンネルボツ
クスに隣接する第1層燃料棒の核分裂物質平均濃
縮度に対して、上記第1層燃料棒の内側にあつて
これに隣接する第2層燃料棒の核分裂物質平均濃
縮度を1.5倍以上とした点にある。
まず、本発明の原理を詳細に説明する。第1図
はBWR燃料集合体の構造の一例を示すもので、
燃料棒A62体と水ロツドB2体とを8×8の正
方格子状にチヤンネルボツクスC内に束ねた構造
になつている。第2図は従来の燃料集合体の燃料
棒濃縮度分布の一例を示したもので、燃料集合体
中央に2体の水ロツドWを配置し、8体のガドリ
ニア(可燃性毒物)ロツドGを図のように装備し
てある。その他の番号1〜9で示した燃料棒およ
びガドリニアロツドGの濃縮度は、第1表に示し
てある。
The present invention relates to a nuclear reactor fuel assembly, and particularly to a nuclear reactor fuel assembly suitable for use in a boiling water nuclear reactor (hereinafter abbreviated as BWR). Conventionally, the operating period of a nuclear reactor is approximately one year, and approximately one quarter of all fuel assemblies are replaced with new fuel assemblies every year. However, with the above operating method, the period during which the reactor is shut down for periodic inspections and fuel changes is approximately 25% of the total operating period.
%, efforts are being made to increase the plant utilization rate by extending the operating period and reducing the ratio of the reactor shutdown period to the total operating period. In order to extend the operating period, it is necessary to increase the amount of fissile nuclides at the initial stage of combustion, that is, the average core enrichment. There are two ways to increase the average core enrichment: loading highly enriched fuel and increasing the number of fuel exchangers; however, the latter requires a longer time for fuel exchange, so the former is generally preferred. method has been adopted. However, the use of highly concentrated fuel has the disadvantage of reducing reactor shutdown margin. What is the reactor shutdown margin?
In a cold state (approximately 20℃), one control rod with the highest reactivity value is in the withdrawn state, and all other control rods are in the fully inserted state, from the critical value (1.0) of the effective multiplication factor. It's the difference. This depends on the average infinite multiplication factor of the four fuel assemblies surrounding the control rod, which has the highest reactivity value. In BWR, during reactor operation (hereinafter referred to as operation), voids occur and the neutron moderating ability decreases due to a decrease in moderator density, and uranium in the fuel
Since there is a negative reactivity due to the Doppler effect of 238, the infinite multiplication factor of the fuel is smaller than when it is cold.
Generally, the difference between the infinite multiplication factor at cold temperature and the infinite multiplication factor during operation increases as the degree of concentration increases. Furthermore, if the amount of gadolinia, which is a burnable poison used to suppress excess reactivity, is increased, this tendency will be exacerbated. Therefore, in a fuel that is enriched to extend the operating period and has a large amount of gadolinia added to suppress excess reactivity, the average infinite multiplication factor of the four fuel assemblies mentioned above during operation is Even if it is the same as in the case of cooling, the average infinite multiplication factor increases when the temperature is cold, and the margin for reactor shutdown decreases. The present invention has been made in view of the above, and its purpose is to provide a nuclear reactor fuel assembly that can extend the operating period and ensure sufficient margin for reactor shutdown. It's about doing. A feature of the present invention is that the average enrichment of fissile material in the first layer fuel rods adjacent to the channel box of the fuel assembly is compared with that of the second layer fuel rods located inside the first layer fuel rods and adjacent to the first layer fuel rods. The point is that the average enrichment of fissile material has been increased by more than 1.5 times. First, the principle of the present invention will be explained in detail. Figure 1 shows an example of the structure of a BWR fuel assembly.
It has a structure in which 62 fuel rods A and 2 water rods B are bundled in a channel box C in an 8×8 square grid. Figure 2 shows an example of the fuel rod enrichment distribution of a conventional fuel assembly, in which two water rods W are placed in the center of the fuel assembly, and eight gadolinia (burnable poison) rods G are placed in the center of the fuel assembly. It is equipped as shown in the figure. The enrichments of the other fuel rods numbered 1-9 and gadolinia rod G are shown in Table 1.
【表】
この例の場合の冷温時と高温時との出力分布の
差を各燃料棒についてパーセント単位で示すと第
3図aに示すようになる。いま、第3図bに示す
ように、最外周の燃料棒(チヤンネルボツクスC
に隣接する燃料棒)を第1層燃料棒、これの内側
にあつて隣接する燃料棒を第2層燃料棒、以下同
様に第3,第4層燃料棒と呼称すると、第1層燃
料棒では、高温時にくらべて冷温時の出力が相対
的に大きくなり、第2層燃料棒では逆に小さくな
つている。これは、冷温時には軽水中の中性子ス
ペクトルが高温時にくらべてソフト(低エネルギ
ーの中性子数の割合が大きくなる。)になり、核
分裂による中性子発生割合が増大するが、空間的
にみると、ギヤツプ水に隣接する第1層燃料棒で
は、燃料棒1体当りの周辺軽水領域の割合が大き
くなるためである。そのため、冷温時には第1層
燃料棒の出力が第2層燃料棒の出力にくらべて相
対的に大きくなる。第4層燃料棒は水ロツドにか
こまれているため、第1層燃料棒と同様の傾向を
示し、第3層燃料棒は水ロツドの影響が弱いた
め、変化が小さい。この出力分布の変動は、各燃
料棒位置での燃料棒の反応度価値の変動を近似的
に表わしている。したがつて、冷温時と高温時の
反応度変化を小さくするためには、第1層燃料棒
の濃縮度をできるだけ小さくし、第2層燃料棒の
濃縮度をできるだけ大きくすることがもつとも効
果的であるということがわかる。第4層燃料棒の
濃縮度を下げること、第3層燃料棒の水ロツドか
ら遠い燃料棒の濃縮度を上げることも効果的であ
るが、これは本数が2体で、寄与の程度が小さ
い。
以上が本発明における冷温―高温反応度変化低
減法の原理であるが、実際の燃料集合体設計にお
いては、燃料集合体内局所出力ピーキングを設計
基準値内に収めなければならないという制約があ
る。すなわち、燃料集合体平均出力に対する最大
出力燃料棒の出力比を、例えば、1.15以下に抑え
る必要がある。したがつて、本発明の原理を設計
に適用する場合、この基準内で濃縮度分布を最適
化する必要がある。いま、第2層燃料棒の平均濃
縮度と第1層燃料棒の平均濃縮度との比をαと
し、第2層燃料棒の平均出力と第1層燃料棒の平
均出力との比をβとして両者の関係を示せば、第
4図に示すようになる。第4図において、a曲線
は8体のガドリニアロツドを持つ燃料集合体の場
合、b曲線はガドリニアロツドを持たない燃料集
合体の場合の関係曲線である。第2図に示した燃
料集合体では、平均濃縮度3.03重量%で局所出力
ピーキング1.15となつており、第2層燃料棒平均
濃縮度は2.9重量%、第1層燃料棒平均濃縮度は
2.5重量%であるからα=1.16で、第1層燃料棒
の平均出力が第2層燃料棒の平均出力より大きく
なつている。冷温―高温の無限増倍率の差(Δk
cpld-hpt)は、燃焼度0Gwd/stで6%Δkであ
り、ガドリニアの燃焼とともに減少したのち回復
し、10Gwd/stで同程度の値を持ち、その後単調
に減少する。このように、第2図に示す燃焼集合
体では、第1層燃料棒の出力分担割合が大きくな
つているため、Δkcpld-hptが相対的に大きくなつ
ている。しかし、燃料集合体平均濃縮度が相対的
に低いため(2.9重量%程度)、従来は上記した燃
料集合体設計でも炉停止余裕の設計条件を満たす
ことは比較的容易であつた。
第5図は制御棒1本が引抜かれたときの冷温時
実効増倍率(kcpld)とαとの関係を2種の異な
る平均濃縮度の燃料集合体について示した線図で
ある。c直線は平均濃縮度2.8重量%の燃料集合
体、d曲線は平均濃縮度3.0重量%の燃料集合体
の場合を示す。kcpldの臨界値からの差が炉停止
余裕に相当し、通常の設計条件としては、1%Δ
kの炉停止余裕を考える。すなわち、kcpldが
0.99以下であることが炉心設計の必要条件であ
る。なお、kcpldは炉心の燃料装荷方式によつて
値が異なるが、第5図には通常の1/4炉心鏡面対
称装荷パターンのものについて示してある。第5
図から、燃料集合体の平均濃縮度が高くなるとと
もに炉停止余裕が小さくなつてゆくことがわか
る。第2図の燃料集合体は設計条件を満していな
いが、αの値を大きくした燃料集合体を設計すれ
ば、高濃縮度燃料集合体でも設計条件を満たすこ
とがわかり、平均濃縮度が3重量%を越える燃料
集合体では、α=1.5以上の燃料集合体を設計す
る必要があることを示している。
以下本発明を第2表、第3表に示した実施例を
用いて詳細に説明する。
第2表は本発明の燃料集合体の各燃料棒濃縮度
分布の一実施例を示したもので、水ロツドW、ガ
ドリニアロツドG、その他の燃料棒1〜9のチヤ
ンネルボツクスC(第1図参照)内での配置は第
2図と同一としてある。[Table] Figure 3a shows the difference in output distribution between cold and high temperatures for each fuel rod in percent units in this example. Now, as shown in Figure 3b, the outermost fuel rod (channel box C)
The fuel rods adjacent to the first layer) are referred to as the first layer fuel rods, and the adjacent fuel rods inside the second layer fuel rods are referred to as the third and fourth layer fuel rods. In this case, the output at cold temperatures is relatively larger than at high temperatures, and on the contrary, it is smaller in the second layer fuel rods. This is because at cold temperatures, the neutron spectrum in light water becomes softer than at high temperatures (the proportion of low-energy neutrons increases), and the proportion of neutrons generated by nuclear fission increases; This is because the ratio of the surrounding light water region per fuel rod becomes large in the first layer fuel rods adjacent to the fuel rods. Therefore, at cold temperatures, the output of the first layer fuel rods becomes relatively larger than the output of the second layer fuel rods. Since the fourth layer fuel rods are surrounded by water rods, they show the same tendency as the first layer fuel rods, and the third layer fuel rods are less affected by the water rods, so the changes are small. The variation in this power distribution approximately represents the variation in the reactivity value of the fuel rod at each fuel rod location. Therefore, in order to reduce the change in reactivity between cold and high temperatures, it is effective to minimize the enrichment of the first layer fuel rods and increase the enrichment of the second layer fuel rods as much as possible. It turns out that it is. It is also effective to lower the enrichment of the 4th layer fuel rods and increase the enrichment of the 3rd layer fuel rods that are far from the water rods, but this only has 2 rods and the degree of contribution is small. . The above is the principle of the cold-temperature-high-temperature reactivity change reduction method according to the present invention, but in actual fuel assembly design, there is a restriction that the local power peaking within the fuel assembly must be kept within the design reference value. That is, it is necessary to suppress the output ratio of the maximum output fuel rod to the average output of the fuel assembly to, for example, 1.15 or less. Therefore, when applying the principles of the present invention to a design, it is necessary to optimize the enrichment distribution within this criterion. Now, the ratio of the average enrichment of the second layer fuel rods to the average enrichment of the first layer fuel rods is α, and the ratio of the average output of the second layer fuel rods to the average output of the first layer fuel rods is β. The relationship between the two is shown in FIG. In FIG. 4, curve a is a relational curve for a fuel assembly having eight gadolinia rods, and curve b is a relational curve for a fuel assembly having no gadolinia rods. In the fuel assembly shown in Figure 2, the average enrichment is 3.03% by weight and the local power peak is 1.15, the average enrichment of the second layer fuel rods is 2.9% by weight, and the average enrichment of the first layer fuel rods is 2.9% by weight.
Since it is 2.5% by weight, α=1.16, and the average output of the first layer fuel rods is greater than the average output of the second layer fuel rods. Difference in infinite multiplication factor between cold and high temperatures (Δk
cpld-hpt ) is 6% Δk at a burnup of 0 Gwd/st, decreases with the combustion of gadolinia, then recovers, has a similar value at 10 Gwd/st, and then decreases monotonically. In this manner, in the combustion assembly shown in FIG. 2, the power sharing ratio of the first layer fuel rods is increased, so that Δk cpld-hpt is relatively large. However, because the fuel assembly average enrichment is relatively low (approximately 2.9% by weight), it has conventionally been relatively easy to satisfy the design conditions for reactor shutdown margin even with the above-mentioned fuel assembly design. FIG. 5 is a diagram showing the relationship between the cold effective multiplication factor (k cpld ) and α when one control rod is withdrawn for two types of fuel assemblies with different average enrichments. The c line represents a fuel assembly with an average enrichment of 2.8% by weight, and the d curve represents a fuel assembly with an average enrichment of 3.0% by weight. The difference from the critical value of k cpld corresponds to the reactor shutdown margin, and as a normal design condition, 1%Δ
Consider the reactor shutdown margin for k. That is, k cpld is
0.99 or less is a necessary condition for core design. Although the value of k cpld differs depending on the fuel loading method of the core, FIG. 5 shows a normal 1/4 core mirror symmetrical loading pattern. Fifth
The figure shows that as the average enrichment of the fuel assembly increases, the reactor shutdown margin decreases. Although the fuel assembly in Figure 2 does not meet the design conditions, it can be seen that if a fuel assembly with a large value of α is designed, even a high-enrichment fuel assembly can satisfy the design conditions, and the average enrichment can be reduced. This shows that for fuel assemblies containing more than 3% by weight, it is necessary to design fuel assemblies with α=1.5 or more. The present invention will be described in detail below using examples shown in Tables 2 and 3. Table 2 shows an example of the enrichment distribution of each fuel rod in the fuel assembly of the present invention, and shows channel boxes C of water rods W, gadolinia rods G, and other fuel rods 1 to 9 (see Fig. 1). ) is the same as in Figure 2.
【表】
第2表より、燃料集合体平均濃縮度3.03重量
%、第2層燃料棒平均濃縮度3.4重量%、第1層
燃料棒平均濃縮度2.1重量%、α=1.62となる。
すなわち、燃料集合体平均濃縮度は第1表の場合
と同一であり、同じ局所出力ピーキング1.15を満
している。しかも、第2層燃料棒の濃縮度を第1
層燃料棒の濃縮度より相対的に高くしてあるの
で、α=1.62となつており、第5図から、炉停止
余裕は約1.5%Δkとなり、設計条件を満してい
る。
なお、この実施例では、第2図からわかるよう
に、ガドリニアロツドGを8体としてあるが、こ
れは必要に応じて増減するようにしてもよい。ま
た、平均濃縮度を3.03重量%としてあるが、これ
は運転時間と燃料集合体の取替体数によつて増減
するようにしてもよく、従来の方式では、平均濃
縮度が3.03重量%以上のときは、設計基準を満足
できなかつたが、本発明の実施例によれば、それ
に応じてαを大きくすればよく、設計基準を満足
できる。
第3表は本発明の他の実施例を示したもので、
チヤンネルボツクスC内の各燃料棒、水ロツド等
の配置は上記と同様である。[Table] From Table 2, the average enrichment of the fuel assembly is 3.03% by weight, the average enrichment of the second layer fuel rods is 3.4% by weight, the average enrichment of the first layer fuel rods is 2.1% by weight, and α = 1.62.
That is, the fuel assembly average enrichment is the same as in Table 1 and satisfies the same local power peaking of 1.15. Moreover, the enrichment of the second layer fuel rods is
Since the enrichment is relatively higher than that of the bed fuel rods, α=1.62, and from Figure 5, the reactor shutdown margin is approximately 1.5% Δk, which satisfies the design conditions. In this embodiment, as can be seen from FIG. 2, there are eight gadolinia rods G, but this number may be increased or decreased as necessary. Also, although the average enrichment is set at 3.03% by weight, this may be increased or decreased depending on the operating time and the number of fuel assemblies replaced.In the conventional system, the average enrichment is 3.03% by weight or more. In this case, the design standard could not be satisfied, but according to the embodiment of the present invention, α can be increased accordingly, and the design standard can be satisfied. Table 3 shows other embodiments of the present invention,
The arrangement of each fuel rod, water rod, etc. in channel box C is the same as above.
【表】
第3表より、燃料集合体平均濃縮度3.03重量
%、第2層燃料棒平均濃縮度3.8重量%、第1層
燃料棒平均濃縮度2.0重量%、α=1.90となる。
第3表では第2表よりガドリニアロツドGの濃縮
度を高めてあるが、α=1.90で、炉停止余裕は第
5図から2.3%Δkとなり、第2表の場合と同
様、設計条件を十分満している。さらに、この濃
縮度分布では、燃料集合体平均濃縮度を約3.3重
量%まで高めることが可能である。
なお、これまでの議論は、1/4炉心鏡面対称燃
料装荷方式を前提として説明したが、燃料の異な
る燃料集合体を炉心全体に均一分散装荷する方式
では、一般に炉停止余裕がさらに1%Δk以上大
きくなるので、燃料集合体平均濃縮度の上限をさ
らに高くすることができる。
いま、第1表の従来の燃料集合体と第3表の本
発明の燃料集合体とを比較すると、kcpldの差は
約3%Δkとなり、1%Δkの炉停止余裕という
同一の設計条件に合せると、第3表の場合は、平
均濃縮度を約0.4重量%高くすることができる。
これは取出し平均燃焼度で約4000Mwd/tの差
に相当し、燃料取替体数を一定と設計すると、燃
料交換サイクル長さが約1000Mwd/st長くなつ
て、プラント利用率が約10%向上する。また、プ
ラント利用率を一定と設計すれば、燃料取替体数
が約10%減少し、燃料経済性が向上するととも
に、取替えに要する時間を低減できる。
以上説明したように、本発明によれば、運転期
間の長期化をはかつてプラント利用率を向上さ
せ、しかも、十分な炉停止余裕を確保することが
できるという効果がある。[Table] From Table 3, the average enrichment of the fuel assembly is 3.03% by weight, the average enrichment of the second layer fuel rods is 3.8% by weight, the average enrichment of the first layer fuel rods is 2.0% by weight, and α=1.90.
In Table 3, the concentration of gadolinia rod G is higher than in Table 2, but when α = 1.90, the reactor shutdown margin is 2.3% Δk from Figure 5, which fully satisfies the design conditions as in Table 2. are doing. Furthermore, with this enrichment distribution, it is possible to increase the fuel assembly average enrichment to about 3.3% by weight. Note that the discussion so far has been based on the 1/4 core mirror-symmetrical fuel loading method, but in a method in which fuel assemblies of different fuels are loaded uniformly throughout the core, the reactor shutdown margin is generally increased by an additional 1% Δk. Therefore, the upper limit of the fuel assembly average enrichment can be further increased. Now, when comparing the conventional fuel assembly shown in Table 1 and the fuel assembly of the present invention shown in Table 3, the difference in k cpld is approximately 3% Δk, which is the same design condition of a reactor shutdown margin of 1% Δk. In the case of Table 3, the average concentration can be increased by about 0.4% by weight.
This corresponds to a difference of about 4,000 Mwd/t in the average take-off burnup, and if the number of refueling bodies is designed to be constant, the refueling cycle length will increase by about 1,000 Mwd/st, improving the plant utilization rate by about 10%. do. Furthermore, if the plant is designed to have a constant utilization rate, the number of fuel replacement units will be reduced by approximately 10%, improving fuel economy and reducing the time required for replacement. As explained above, according to the present invention, there is an effect that the plant utilization rate can be improved by extending the operation period, and that a sufficient margin for reactor shutdown can be secured.
第1図はBWR用燃料集合体の構造説明図、第
2図は従来の燃料集合体の構造説明図、第3図は
高温時から冷温時に炉心状態が変化したときの燃
料集合体内燃料棒の局所出力の差をパーセント単
位で示した図、第4図はαとβとの関係を示す線
図、第5図はαと制御棒が1本引抜かれたときの
冷温時実効増倍率との関係を示す線図である。
A,1〜9…燃料棒、B,G…ガドリニアロツ
ド、C…チヤンネルボツクス、W…水ロツド。
Figure 1 is a structural diagram of a BWR fuel assembly, Figure 2 is a structural diagram of a conventional fuel assembly, and Figure 3 is a diagram of the fuel rods in the fuel assembly when the core condition changes from high temperature to cold temperature. Figure 4 is a diagram showing the difference in local output in percentage units, Figure 4 is a diagram showing the relationship between α and β, and Figure 5 is a diagram showing the relationship between α and the cold effective multiplication factor when one control rod is pulled out. It is a line diagram showing a relationship. A, 1 to 9... Fuel rod, B, G... Gadolinia rod, C... Channel box, W... Water rod.
Claims (1)
ツクスに隣接する第1層燃料棒の核分裂物質平均
濃縮度に対して前記第1層燃料棒の内側にあつて
これに隣接する第2層燃料棒の核分裂物質平均濃
縮度を1.5倍以上としてあることを特徴とする原
子炉燃料集合体。1. The average fissile material enrichment of the first layer fuel rods adjacent to the channel box of the fuel assembly loaded in the reactor is compared to the average enrichment of the second layer fuel rods adjacent to the first layer fuel rods. A nuclear reactor fuel assembly characterized by having an average enrichment of fissile material of 1.5 times or more.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2362180A JPS56119888A (en) | 1980-02-26 | 1980-02-26 | Nuclear fuel assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2362180A JPS56119888A (en) | 1980-02-26 | 1980-02-26 | Nuclear fuel assembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS56119888A JPS56119888A (en) | 1981-09-19 |
| JPS6249946B2 true JPS6249946B2 (en) | 1987-10-22 |
Family
ID=12115667
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2362180A Granted JPS56119888A (en) | 1980-02-26 | 1980-02-26 | Nuclear fuel assembly |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS56119888A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07111469B2 (en) * | 1985-07-18 | 1995-11-29 | 株式会社東芝 | Fuel assembly |
-
1980
- 1980-02-26 JP JP2362180A patent/JPS56119888A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS56119888A (en) | 1981-09-19 |
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