...
首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Advanced High Temperature Gas-Cooled Reactor Systems
【24h】

Advanced High Temperature Gas-Cooled Reactor Systems

机译:先进的高温气冷堆系统

获取原文
获取原文并翻译 | 示例

摘要

Three systems have been proposed for advanced high-temperature gas-cooled reactors: a supercritical carbon dioxide (S-CO_2) gas turbine power conversion system, a new micro-channel heat exchanger (MCHE), and a once-through-then-out (OTTO) refueling scheme with burnable poison (BP) loading. A S-CO_2 gas turbine cycle attains higher cycle efficiency than a He gas turbine cycle because of reduced compression work around the critical point of CO_2. Considering temperature reduction at the turbine inlet by 30℃ through intermediate heat exchange, the S-CO_2 indirect cycle achieves an efficiency of 53.8% at a turbine inlet temperature of 820℃ and a turbine inlet pressure of 20 MPa. This cycle efficiency value is higher by 4.5% than that (49.3%) of a He direct cycle at a turbine inlet temperature of 850℃ and 7 MPa. A new MCHE has been proposed as an intermediate heat exchanger between the primary cooling He loop and the secondary S-CO_2 gas turbine power conversion system and as recuperators of the S-CO_2 gas turbine power conversion system. This MCHE has discontinuous "S-shaped" fins providing flow channels resembling sine curves. Its pressure drop is one-sixth that of a conventional MCHE with a zigzag flow channel configuration, but it has the same high heat transfer performance. The pressure drop reduction is ascribed to suppression of recirculation flows and eddies that appear around bend corners of the zigzag flow channels in the conventional MCHE. An optimal BP loading in an OTTO refueling scheme eliminates the shortcoming of its excessively high axial power peaking factor, reducing the power peaking factor from 4.44 to about 1.7, and inheriting advantages over the multipass scheme because it obviates reloading in addition to fuel handling and integrity checking systems. Because of the power peaking factor reduction, the maximum fuel temperatures are lower than the maximum permissible values of 1250℃ for normal operation and 1600℃ during a depressurization accident.
机译:对于先进的高温气冷堆,已经提出了三种系统:超临界二氧化碳(S-CO_2)燃气轮机功率转换系统,新的微通道换热器(MCHE)和一次通过后输出(OTTO)加注可燃毒物(BP)的加油方案。 S-CO_2燃气轮机循环比He燃气轮机循环获得更高的循环效率,因为在CO_2临界点附近的压缩功降低了。考虑到通过中间换热使涡轮机入口温度降低30℃,在820℃的涡轮机入口温度和20MPa的涡轮机入口压力下,S-CO_2间接循环的效率达到53.8%。在850℃和7 MPa的涡轮入口温度下,该循环效率值比He直接循环的效率(49.3%)高4.5%。已经提出了一种新的MCHE,作为在主冷却He回路和次级S-CO_2燃气轮机功率转换系统之间的中间热交换器,以及作为S-CO_2燃气轮机功率转换系统的换热器。该MCHE具有不连续的“ S形”散热片,提供类似于正弦曲线的流道。它的压降是采用曲折流道配置的传统MCHE的六分之一,但具有相同的高传热性能。压降的降低归因于常规MCHE中在曲折流道的弯曲拐角附近出现的再循环流和涡流的抑制。 OTTO加油方案中的最佳BP负载消除了其轴向功率峰值因数过高的缺点,将功率峰值因数从4.44降低到约1.7,并继承了多程方案的优势,因为它除了可处理燃料和保持完整性之外还避免了重新负荷检查系统。由于降低了功率峰值因数,因此最高燃料温度低于正常运行时的最高允许温度1250℃和降压事故时的最高允许温度1600℃。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号