fuel element
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2021 ◽  
Author(s):  
Anton Vladimirovich Eremin ◽  
Sofya Alekseevna Zinina ◽  
Dmitry Mikhailovich Bragin ◽  
Svyatoslav Sergeevich Leonov ◽  
Kristina Vladimirovna Gubareva

2021 ◽  
Vol 2096 (1) ◽  
pp. 012090
Author(s):  
A V Eremin ◽  
K V Gubareva ◽  
A I Popov

Abstract This article presents the results of the development of a numerical - analytical method for solving the problem of thermal conductivity in a plate fuel element. An unsteady temperature field inside a fuel element is investigated for a given spatial distribution of heat sources. The heat release rate is given by the quadratic function of the coordinate. Modeling the temperature state of bodies with internal heat sources allows you to study the operation of equipment in transient modes, control heating/cooling modes of elements, determine temperature stresses, etc. It is shown in the work that regardless of the power of internal sources of heat, the temperature state is stabilized at a temperature level that depends on the Pomerantsev number.


2021 ◽  
Vol 9 ◽  
Author(s):  
Guan Wang ◽  
Long Gu ◽  
Di Yun

The China initiative Accelerator Driven System (CiADS) and the corresponding lead-bismuth eutectic (LBE) cooled subcritical reactor, as the research subject of one of the major national science and technology infrastructure projects, are undertaken by the Institute of Modern Physics-Chinese Academy of Sciences (IMP-CAS). And in the first phase, UO2 fuels will be loaded in the subcritical core to test the coupling technology and achieve a long-term steady operation. A brief description of CiADS subcritical reactor, fuel assembly and fuel element are presented here, and a multi-physics performance analysis and design evaluation of CiADS UO2 fuel are carried out by means of the FUTURE code. FUTURE is a fuel performance analysis code to evaluate the synergy of phenomena occurring in the fuel element and their impact on the fuel design improvement for the liquid metal fast reactor, which was developed jointly by IMP-CAS and Xi’an Jiaotong University (XJTU). In this paper, the FUTURE code was modified and updated focusing on characteristics of CiADS fuels. Relocation and densification models were added. Results of the hottest fuel element, mainly concerning the thermo-mechanical behaviors, are discussed concerning both fuel and cladding performance on the basis of indicative design limits. According to the preliminary design, the CiADS UO2 fuel exhibits good performance, and the main safety parameters are far below the indicative limits. The Fuel Cladding Mechanical Interaction (FCMI) is not very serious, and the permanent cladding strains and Cumulative Damage Fraction (CDF) are small and even negligible thanks to the low level of fuel temperature and corresponding stress. However, some critical issues may still exist, especially on LBE corrosion near the coolant inlet, where protective oxide layers are very thin from BoL to EoL. The modeling is useful for providing feedback to the conceptual design of the CiADS LBE-cooled subcritical reactor and the update of FUTURE code.


2021 ◽  
Vol 2048 (1) ◽  
pp. 012014
Author(s):  
H Yang ◽  
H Zhao ◽  
X Liu ◽  
K Zhang ◽  
T Wang ◽  
...  

Abstract A Ti3SiC2-TiC-Si composite coating was prepared by molten salt technique on the surface of SiC coated matrix graphite (MG) spheres of HTR fuel element with different Ti content. The coating is composed of a transition layer, a SiC layer and an outer Ti- rich layer. When the content of Ti is 0.6g, the coating consists of Ti3SiC2, SiC, and TiC; when Ti content are 1.2g and 2.4g, the coating is composed of Ti3SiC2, SiC, TiC, and Si. Oxidation tests show that the kinetics of oxidation is parabolic at the beginning of oxidation; then it becomes linear after oxidation for 5h. The coating prepared with 0.6g Ti shows the best oxidation resistance, and the weight reduction of the coated MG spheres is only 0.33% after oxidation in static air at 1773K for 50h. These results show that Ti-based composites coating a kind of anti-oxidation coating system worth studying.


2021 ◽  
Author(s):  
Cezary Bojanowski ◽  
Guanyi Wang ◽  
Ron Kmak ◽  
Andrew Hebden ◽  
Aaron Weiss ◽  
...  

2021 ◽  
Vol 160 ◽  
pp. 108400
Author(s):  
Ruibo Lu ◽  
Zhifang Qiu ◽  
Yuhao He ◽  
Wen Yang ◽  
Zhongchun Li ◽  
...  

2021 ◽  
Author(s):  
Cezary Bojanowski ◽  
Guanyi Wang ◽  
Ron Kmak ◽  
Andrew Hebden ◽  
Aaron Weiss ◽  
...  

2021 ◽  
Author(s):  
Zhaoyu Liang ◽  
Yu Ji ◽  
Jun Sun ◽  
Chenrui Mao ◽  
Lei Shi

Abstract The nuclear thermal propulsion (NTP) system can shorten the travel time in deep space exploration and reduce the initial mass of the launch vehicle due to its superior characteristics including high specific impulse and large thrust. Particle bed reactor (PBR) is one of the most appropriate reactor concepts to equip the NTP systems. To make the best use of PBR, the thermal-hydraulic design of the fuel element should be carefully considered and a flow-power matching technology should be developed. In this paper, a novel design employing a divergent hot gas channel is proposed to achieve a uniform flow distribution with lower maximum temperature and pressure drop. Through the analysis of the 1D modified momentum equation in the inlet plenum and hot gas channel, the model of pressure drop is established. Then, the differential equation of the ideal cross-section of the hot gas channel is derived. At last, the flow and heat transfer process in the fuel element with divergent hot gas channel is simulated by using computational fluid dynamics (CFD) code, and the reduction of pressure drop and temperature verifies the theoretical model. This study shows that the proposed design of the divergent hot gas channel can provide a new idea for thermal-hydraulic optimization of the PBR fuel element.


2021 ◽  
Author(s):  
Guanyi Wang ◽  
Cezary Bojanowski ◽  
Andrew Hebden ◽  
Dhongik Yoon ◽  
Erik Wilson ◽  
...  

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