• 제목/요약/키워드: fuel behavior

검색결과 1,169건 처리시간 0.019초

핵연료피복관용 Zr 합금의 제조공정에 따른 미세조직 및 부식거동 (Microstructure and Corrosion Behavior of Zr Alloys with Manufacturing Process)

  • 김현길;최병권;김규태;김선두;박찬현;정용환
    • 열처리공학회지
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    • 제18권5호
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    • pp.288-296
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    • 2005
  • The corrosion behaviors of Zr-based alloys were very sensitive to their microstructures which were determined by manufacturing process. The specimens of Zr-based alloy named as HANA-4 for nuclear fuel cladding were investigated in order to get the optimized manufacturing process such as the intermediate annealing temperature and cold working steps after the ${\beta}$ quenching. From the microstructural analysis, cold worked microstructure of the samples was changed to the recrystallized microstructure by performed process. The corrosion behaviors of HANA-4 alloy were affected by the different manufacturing process. The ${\beta}$-Zr phase was formed in the matrix and the Nb concentration in the ${\beta}$-Zr phase was increased as progressing the manufacturing process. So, it was found that the corrosion rate of HANA-4 alloy was affected by the Nb concentration in the matrix.

A Thermal Conductivity Model for LWR MOX Fuel and Its Verification Using In-pile Data

  • Byung-Ho Lee;Yang-Hyun Koo;Jin-Silk Cheon;Je-Yong Oh;Hyung-Koo Joo;Dong-Seong Sohn
    • Nuclear Engineering and Technology
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    • 제34권5호
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    • pp.482-493
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    • 2002
  • The MOX fuel for LWR is fabricated either by direct mechanical blending of UO$_2$ and PuO$_2$ or by two stage mixing. Hence Pu-rich particles, whose Pu concentrations are higher than pellet average one and whose size distribution depends on a specific fabrication method, are inevitably dispersed in MOX pellet. Due to the inhomogeneous microstructure of MOX fuel, the thermal conductivity of LWR MOX fuel scatters from 80 to 100 % of UO$_2$ fuel. This paper describes a mechanistic thermal conductivity model for MOX fuel by considering this inhomogeneous microstructure and presents an explanation for the wide scattering of measured MOX fuel's thermal conductivity. The developed model has been incorporated into a KAERI's fuel performance code, COSMOS, and then evaluated using the measured in-pile data for MOX fuel. The database used for verification consists of homogeneous MOX fuel at beginning-of-life and inhomogeneous MOX fuel at high turnup. The COSMOS code predicts the thermal behavior of MOX fuel well except for the irradiation test accompanying substantial fission gas release. The over-prediction with substantial fission gas release seems to suggest the need for the introduction of a recovery factor to a term that considers the burnup effect on thermal conductivity.

ANS과도조건 I 및 II에서 17x17 KOFA 핵연료봉의 기계적 건전성이 유지되는 과도상태 허용 출력준위에 관한 연구 (Investigation on the Allowable Transient Power Levels to Maintain the Mechanical Integrity of the 17$\times$17 KOFA Fuel Rod During the ANS Conditions I and II)

  • Lee, Chan-Bock;Kim, Ki-Hang;Kim, Kyu-Tae
    • Nuclear Engineering and Technology
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    • 제26권1호
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    • pp.119-125
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    • 1994
  • 핵연료봉의 과도상태 출력준위는 핵연료봉의 과도상태 거동에서 가장 중요한 변수중의 하나이다. 핵연료 성능 데이타베이스의 분석과 핵연료의 과도상태 거동에 영향을 줄 수 있는 핵연료봉 출력이력, 속중성자속, 농축도 및 주기길이 등의 인자들의 민감도 분석을 통해서, ANS 과도조건 I 및 II에서 핵연료봉의 기계적 건전성이 유지되는 허용가능 과도상태 출력을 구하기 위해 일반적으로 적용이 가능한 방법론이 유도되었으며, 이를 통해 17$\times$17 KOFA 핵연료봉의 허용가능 과도상태 출력이 연소도의 함수로써 결정되었다. 이 방법론을 도입함으로써, 현재와 같이 매 주기마다 핵연료봉 과도상태 설계분석을 수행할 필요가 없이 단지 해당주기에서의 과도상태 최대 출력준위 평가로써 핵연료봉의 과도상태 설계를 대체할 수 있으며, 17$\times$17 KOFA 핵연료에 대하 낮은 연소도영역에서 기존의 최대 허용 과도상태 출력 준위인 591 w/cm보다 큰 최대 689.5 w/cm까지 허용함으로써 원자로 운전에 유연성을 줄 수 있다.

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외부 연료탱크 수평 핀 동적거동이 피로수명에 미치는 영향 (The effect on fatigue life for dynamic behavior of external fuel tank horizontal fin)

  • 김근원;신기수
    • 한국항공우주학회지
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    • 제40권3호
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    • pp.209-214
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    • 2012
  • 최근 F-5 항공기 외부 연료탱크 수평 핀의 균열결함이 크게 증가함에 따라 원인 규명이 필요하다. 본 연구에서는 수평 핀의 동적거동을 유한요소법을 이용하여 피로해석 측면에서 정량적으로 평가하였다. 이를 위해 스피드 브레이크(speed brake)에 의한 동하중 이력을 적용하여 시간영역과 주파수영역의 피로해석을 수행하였다. 연구결과 수평 핀은 동적거동 영향으로 피로수명이 감소되었음을 입증하였다.

Study on relocation behavior of debris bed by improved bottom gas-injection experimental method

  • Teng, Chunming;Zhang, Bin;Shan, Jianqiang
    • Nuclear Engineering and Technology
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    • 제53권1호
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    • pp.111-120
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    • 2021
  • During the core disruptive accident (CDA) of sodium-cooled fast reactor (SFR), the molten fuel and steel are solidified into debris particles, which form debris bed in the lower plenum. When the boiling occurs inside debris bed, the flow of coolant and vapor makes the debris particles relocated and the bed flattened, which called debris bed relocation. Because the thickness of debris bed has great influence on the cooling ability of fuel debris in low plenum, it's very necessary to evaluate the transient changes of the shape and thickness in relocation behavior for CDA simulation analysis. To simulate relocation behavior, a large number of debris bed relocation experiments were carried out by improved bottom gas-injection experimental method in this paper. The effects of different experimental factors on the relocation process were studied from the experiments. The experimental data were also used to further evaluate a semi-empirical onset model for predicting relocation.

Development and testing of the hydrogen behavior tool for Falcon - HYPE

  • Piotr Konarski;Cedric Cozzo;Grigori Khvostov;Hakim Ferroukhi
    • Nuclear Engineering and Technology
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    • 제56권2호
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    • pp.728-744
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    • 2024
  • The presence of hydrogen absorbed by zirconium-based cladding materials during reactor operation can trigger degradation mechanisms and endanger the rod integrity. Ensuring the durability of the rods in extended time-frames like dry storage requires anticipating hydrogen behavior using numerical modeling. In this context, the present paper describes a hydrogen post-processing tool for Falcon - HYPE, a PSI's in-house tool able to calculate hydrogen uptake, transport, thermochemistry, reorientation of hydrides and hydrogen-related failure criteria. The tool extracts all necessary data from a Falcon output file; therefore, it can be considered loosely coupled to Falcon. HYPE has been successfully validated against experimental data and applied to reactor operation and interim storage scenarios to present its capabilities.

기계식 연료펌프를 사용하는 혼소엔진에서 노즐특성에 따른 경유 분사특성 측정 (Measurements of Spray Characteristics According to Nozzle Property in Dual Fuel Engine with a Mechanical Fuel Pump)

  • 조승환;유승헌;이범호;김동현;이대엽
    • 한국분무공학회지
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    • 제17권2호
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    • pp.94-99
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    • 2012
  • The characteristics of spray behavior and injected amount were studied with two types of nozzles for using in a compression ignition engine with dual fuel technology for construction machines. A penetration length of spray tends to shorten due to a decrease of injected amount of a diesel fuel with dual fuel engine application. In order to ignite the gaseous fuel premixed with air during intake process, a diesel fuel, which was compression ignited, needs to penetrate somehow similar depth compared with the case of a diesel fuel-only-injection. In this work, a nozzle with reduced hole diameter and increased number of holes was tested and demonstrated that, compared to diesel 100% case, its penetration lengths are comparable to 74% and 79%, respectively, of those of 100% and 50% supply of a diesel fuel with the baseline nozzle that has four holes and 30.4% increased diameter. This will presumably enhancement the combustion in a dual fuel engine. A design suggestion was also made in this work to achieve similar penetration length of spray with diesel 100% case to prevent combustion from being deteriorated in a dual fuel engine.

Atomistic simulations of nanocrystalline U0.5Th0.5O2 solid solution under uniaxial tension

  • Xiao, Hongxing;Wang, Xiaomin;Long, Chongsheng;Tian, Xiaofeng;Wang, Hui
    • Nuclear Engineering and Technology
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    • 제49권8호
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    • pp.1733-1739
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    • 2017
  • Molecular dynamics simulations were performed to investigate the uniaxial tensile properties of nanocrystalline $U_{0.5}Th_{0.5}O_2$ solid solution with the Born-Mayer-Huggins potential. The results indicated that the elastic modulus increased linearly with the density relative to a single crystal, but decreased with increasing temperature. The simulated nanocrystalline $U_{0.5}Th_{0.5}O_2$ exhibited a breakdown in the Halle-Petch relation with mean grain size varying from 3.0 nm to 18.0 nm. Moreover, the elastic modulus of $U_{1-y}Th_yO_2$ solid solutions with different content of thorium at 300 K was also studied and the results accorded well with the experimental data available in the literature. In addition, the fracture mode of nanocrystalline $U_{0.5}Th_{0.5}O_2$ was inclined to be ductile because the fracture behavior was preceded by some moderate amount of plastic deformation, which is different from what has been seen earlier in simulations of pure $UO_2$.

KMRR 핵연료 알루미늄 피복재의 부식 거동 평가 (Evaluation of the Corrosion Behavior of the Aluminum Cladding in the KMRR Fuel)

  • Lee, Chan-Bock;Sohn, Dong-Seong
    • Nuclear Engineering and Technology
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    • 제26권4호
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    • pp.526-535
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    • 1994
  • KMRR(다목적 연구용원자로) 핵연료의 알루미늄 피복재의 부식거동을 평가하기 위해, 부식 예측치와 노내 부식 실측치의 비교를 통해 유도된 열속인자를 도입한 수정된 Griess 경험식을 유도하였다. KMRR 핵연료의 건전성이 유지되는 부식의 설계기준으로써는 산화층의 박리 방지가 보수적으로 설정되었으며, 산화층의 박리는 산화층에서의 온도차이가 114$^{\circ}C$ 이상에서 일어난다고 보수적으로 가정하였다. KMRR 핵연료의 출력이력을 첫 주기부터 평형주기까지 분석하여, 한계출력이력을 결정하였다. 한계출력이력을 가진 KMRR 핵연료의 부식량 예측계산 결과, 최대 산화층의 두께는 50$\mu\textrm{m}$ 이하였으며, 산화층 박리의 설계기준은 2배의 여유도를 가지고 만족하였다. 따라서, KMRR 핵연료는 피복재의 부식으로 인해 손상되지 않을 것으로 판단된다. 그러나, 수정된 Griess 부식경험식의 KMRR에의 적용 타당성은 KMRR 핵연료의 부식 감시를 통해 추가로 검증될 필요성이 있다.

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음향 가진 된 프로판 확산 화염의 부상 거동에 관한 실험적 연구 (Experimental Study on the Lift-off Behavior of Tone-excited Propane Jet Diffusion flames)

  • 김승곤;박정;김태권;이기만
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 제26회 KOSCO SYMPOSIUM 논문집
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    • pp.65-73
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    • 2003
  • An experimental study on flame lift-off characteristics of propane jet flame highly diluted with nitrogen has been conducted introducing acoustic forcing with a tube resonant frequency. A flame stability curve is attained according to forcing strength and nozzle exit velocity for $N_2$ diluted flames. Flame lift-off behavior with forcing strength and nozzle exit velocity is globally categorized into three; a well premixed behavior caused by a collapsible mixing for large forcing strength, a coexistent behavior of well-premixed and edge flames interacting with well-organized inner fuel vortices for moderate forcing strengths, and edge flame behavior for small forcing strengths. Special focus is concentrated on the coexistent behavior of the flame base in lifted flame since this may give a hint to a possibility which the flame base behaves like a well-mixed premixed flame in highly turbulent lifted flames. It is also shown that the acoustic forcing to self-pulsating laminar lifted flame affects flame lift-off behavior considerably which is closely related to downstream flow velocity, mixture strength, effective fuel Lewis number, and flame stretch.

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