منوی کاربری
  • پشتیبانی: ۴۲۲۷۳۷۸۱ - ۰۴۱
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دانلود رایگان مقاله آنالیز حرارتی-هیدرولیک پوسته شدن ماژول هدف در ADS

عنوان فارسی
آنالیز حرارتی-هیدرولیک پوسته شدن یکپارچه ماژول هدف در ADS
عنوان انگلیسی
Thermal-hydraulic analysis of an integrated spallation target module in ADS
صفحات مقاله فارسی
0
صفحات مقاله انگلیسی
7
سال انتشار
2016
نشریه
الزویر - Elsevier
فرمت مقاله انگلیسی
PDF
کد محصول
E1082
رشته های مرتبط با این مقاله
مهندسی انرژی و فیزیک
گرایش های مرتبط با این مقاله
نانو فیزیک، فیزیک هسته ای و فناوری های انرژی
مجله
تاریخچه انرژی هسته ای - Annals of Nuclear Energy
دانشگاه
آزمایشگاه های نوترونیک، موسسه فناوری ایمنی انرژی هسته ای، علوم آکادمی چین
کلمات کلیدی
ADS، هدف پوسته شدن یکپارچه، تجزیه و تحلیل حرارتی و هیدرولیک، اصلاح هندسه
۰.۰ (بدون امتیاز)
امتیاز دهید
چکیده

Abstract


As a key component in Accelerator Driven System (ADS), the spallation target is exposed to high irradiation intensity radiation, and a larger amount of heat is deposited on it. Therefore, the cooling of the target is a challenging task in the target design. Integrated target module with a solid beam window, and cooled by reactor primary coolant is a good contender for ADS system. The numerical analysis of two target modules was performed by using finite element code to assess the target cooling capacity. It was found that with uniform inlet velocity, the geometry modification of the inlet could improve the heat transfer effectively. But with non-uniform inlet velocity, the geometry modification of the inlet had little effect on cooling capacity.

نتیجه گیری

6. Conclusion


Due to the intense heat deposition and the limited space in the reactor core, the target geometrical configuration and the inlet flow distribution had been carefully designed to ensure adequate coolant velocity for cooling the target material. CFD analyses were performed to define the velocity and the temperature distribution in the window and the coolant bulk. The results achieved are summarized as follows: In the uniform inlet condition, the maximum temperature on the window of the typical design is 1255.5 C. With same mass flow rate, the maximum temperature on the window of the proposed design is reduced to 846 C. While an increase in the inlet velocity to about 3 times, the temperature difference has reduced by 40%. The inlet flow velocity is an important design parameter affecting the window temperature. The divided inlet schemes can effectively reduce the maximum temperature on the window. The maximum temperature change on the window in the nonuniform inlet velocity is complicated. The proposed target can get same temperature with small mass flow rate. The velocity near the window is the main influence of the window temperature. And the maximum temperature on the window reduces with a rise in the velocity near the window surface. Further, the methods to increase the velocity on the window are being investigated by numerical simulation.


بدون دیدگاه