• Title/Summary/Keyword: 열 변형률

Search Result 157, Processing Time 0.021 seconds

Creep Analysis for the Pressurized Water Reactor Spent Nuclear Fuel Disposal Canister (가압경수로 고준위페기물 처분용기에 대한 크립해석)

  • Ha Joon-Yong;Choi Jong-Won;Kwon Young-Joo
    • Journal of the Computational Structural Engineering Institute of Korea
    • /
    • v.17 no.4
    • /
    • pp.413-421
    • /
    • 2004
  • In this paper, a structural analysis for the pressurized water reactor(PWR) spent nuclear fuel disposal canister which is deposited under the 500m deep underground is carried out to predict the creep deformation of the canister while the underground water and swelling bentonite pressure are applied on the canister. Usually the creep deformation may be caused due to the Pressure and the high heat applied to the canister even though additional external loads are not applied to the canister. These creep deformations depend on the time. In this paper, oかy the underground water and bentonite swelling Pressure are considered for the creep deformation analysis of the canister, because the heat distribution inside canister due the spent fuel is not simple and depends on time. A proper creep function is adopted for the creep analysis. The creep analysis is carried out during $10^8$ seconds. The creep analysis results show that the creep strains are very small and these strains occur usually in the lid and bottom of the canister not in the cast iron insert. A much smaller strain is found in the cast iron insert. Hence, the creep deformation doesn't affect the structural safety of the canister, and also the creep stress which shows the stress relaxation phenomenon doesn't affect the structural safety of the canister.

Recovery Behaviors of Natural Rubber Composites Thermally Aged in Altering Medium Systems of Air and Water (공기와 물의 교매질 시스템에서 열노화된 천연고무 복합체의 회복 거동)

  • Choi, Sung-Seen;Kim, Ok-Bae
    • Elastomers and Composites
    • /
    • v.48 no.3
    • /
    • pp.181-189
    • /
    • 2013
  • Unfilled, carbon black-filled, and silica-filled natural rubber (NR) composites were aged with a circular deformation at $60-90^{\circ}C$ and the recovery behaviors were investigated. The samples were aged under the altering aging medium systems of air and distilled water every day for 10 days. The order of the recoveries according to the filler systems was unfilled > silica > carbon black. The recoveries of the samples aged in the air to water altering system were greater than those of the samples aged in the water to air altering system. The initial aging medium dominantly influenced the deformation level.

Modeling of Differential Shrinkage Equivalent Temperature Difference for Concrete Pavement Slabs (콘크리트 포장 슬래브 부등 건조수축 등가 온도차이의 모형화)

  • Lim, Jin-Sun;Choi, Ki-Hyo;Lee, Chang-Joon;Jeong, Jin-Hoon
    • International Journal of Highway Engineering
    • /
    • v.11 no.4
    • /
    • pp.59-68
    • /
    • 2009
  • Torsional behavior of concrete pavement slabs due to temperature and moisture effects is constrained by self weight and friction etc, and causes stress as the result. The stress due to humidity variation in the slab is difficult to calculate while that due to temperature variation can easily be calculated by a commercial structural analysis program. Thus, the slab behavior can be predicted more accurately if the humidity effect is converted to equivalent temperature and is used as an input of structural analysis. In this study, a concrete pavement slab was constructed and strains of the slab due to environmental loadings were measured for long-term period. Thermal strains were subtracted from the measured strains by using thermal expansion coefficient of the concrete measured in a laboratory. Shrinkage strains, the remained strains, was supposed as additional thermal strains to calculate imaginary temperature with equivalent effect of the shrinkage by dividing the shrinkage with the thermal expansion coefficient. An existing shrinkage model was modified by considering the self weight and friction to be used in another model which can convert differential shrinkage between top and bottom of the slab to equivalent temperature difference. Addition research efforts on tensile stress reduction according to steady increase in the compressive strains are warranted for more accurate stress calculation.

  • PDF

The effect of factors for thermal problems in diesel engine (디이젤 엔진의 열문제에 대한 인자들의 영향)

  • 오성환
    • Journal of the korean Society of Automotive Engineers
    • /
    • v.6 no.4
    • /
    • pp.18-28
    • /
    • 1984
  • 디이젤 엔진은 피스톤이 실린더 내를 왕복 운동하면서 압축행정에서 연료의 연소에 의해 발생된 고열을 받아 고온에서 작동되기 때문에 피스톤 헤드에서 받은 열은 속히 아래부분으로 전달시 키고 동시에 실린더 벽으로 전달되게 하여야 한다. 여기서 열이 문제가 되는 요소를 생각해 보면, (1) 고압 : 연소 최고폭발압력이 높기 때문에 압력상승률도 커져 격렬한 연소상태가 된다. (2) 고온 : 격심한 가스 유동과 실린더 직경이 크기 때문에 피스톤 헤드부의 온도가 높아진다. (3) 연소생성물 중에 엔진 및 윤활유에 악 영향을 주는 성분이 많다. (4) 경량, 저가격 구조 때문에 열적 및 역학적 변형이 일어나기 쉽다. (5) 사용조건이 가혹해 연료가 이상 현상을 가져온다. 위의 요소들을 가지고 온도의 분포, 열의 전달과정, 피스톤 냉각 등에 대해서 알아본다.

  • PDF

Cure Shrinkage Behavior of Polymer Matrix Composite according to Degree of Cure (경화도에 따른 고분자 기지 복합재의 경화 수축률 거동)

  • Kwon, Hyuk;Hwang, Seong-Soon;Choi, Won-Jong;Lee, Jae-Hwan;Kim, Jae-Hak
    • Composites Research
    • /
    • v.27 no.3
    • /
    • pp.90-95
    • /
    • 2014
  • Cure shrinkage during cure process of polymer matrix composites develope residual stress that cause some structural deformation, such as spring-in, spring-out and warpage. The carbon/epoxy prepreg used in this study is Hexply M21EV/34%/UD268NFS/IMA-12K supplied by Hexcel corp. Cure shrinkage and degree of cure measured by TMA(thermomechanical analyzer) and DSC(differential scanning calorimetry). Cure shrinkages are measured by TMA within a temperature range of $140{\sim}240^{\circ}C$ in a nitrogen atmosphere, and degree of cure determined by the heat of reaction using dynamic and isothermal DSC runs in argon atmosphere. As a result, the cure shrinkage is increased dramatically in a degree of cure range between 27~80%. the higher the cure temperature, the lower the degree of cure occurring to begin cure shrinkage.

Non-linear Temperature Dependent Deformation Anaysis of CBGA Package Assembly Using Moir′e Interferometry (모아레 간섭계를 이용한 CBGA 패키지의 비선형 열변형 해석)

  • 주진원;한봉태
    • Journal of the Microelectronics and Packaging Society
    • /
    • v.10 no.4
    • /
    • pp.1-8
    • /
    • 2003
  • Thermo-mechanical behavior of a ceramic ball grid array (CBGA) package assembly are characterized by high sensitive moire interferometry. Moir fringe patterns are recorded and analyzed at various temperatures in a temperature cycle. Thermal-history dependent analyses of global and local deformations are presented, and bending deformation (warpage) of the package and shear strain in the rightmost solder ball are discussed. A significant non-linear global behavior is documented due to stress relaxation at high temperature. Analysis of the solder interconnections reveals that inelastic deformation accumulates on only eutectic solder fillet region at high temperatures.

  • PDF

Modeling of Tension Stiffening Effect Based on Nonlinear Bond Characteristics in Structural Concrete Members (비선형 부착 특성에 기반한 철근콘크리트 부재의 인장증강효과 모델)

  • Lee, Gi-Yeol;Ha, Tae-Gwan;Kim, Woo
    • Journal of the Korea Concrete Institute
    • /
    • v.19 no.6
    • /
    • pp.745-754
    • /
    • 2007
  • This paper presents a unified modeling technique for tension stiffening effect in structural concrete members. The model is mathematically derived from the bond stress-slip relationships which account for splitting crack. The relationships in CEB-FIP Model Code 1990 and Eurocode 2 are employed together with the assumptions of a linear slip distribution along the interface and the uniform condition of concrete tensile contribution for the mid section of cracked member at the stabilized cracking stage. With these assumptions, a model of tension stiffening effect is proposed by accounting for the force equilibrium and strain compatibility condition associated to the steel strain and concrete contribution by bond stress. The model is applied to the test results available in literatures, and the predicted values are shown to be in good agreement with the experimentally measured behavior.

Collapse Analysis of Ultimate Strength Considering the Heat Affected Zone of an Aluminum Stiffened Plate in a Catamaran (카타마란 알루미늄 보강판의 열영향부 효과를 고려한 최종강도 붕괴 해석)

  • Kim, Sung-Jun;Seo, Kwang-Cheol;Park, Joo-Shin
    • Journal of the Korean Society of Marine Environment & Safety
    • /
    • v.26 no.5
    • /
    • pp.542-550
    • /
    • 2020
  • The use of high-strength aluminum alloys for ships and of shore structures has many benefits compared to carbon steels. Recently, high-strength aluminum alloys have been widely used in onshore and of shore industries, and they are widely used for the side shell structures of special-purpose ships. Their use in box girders of bridge structures and in the topside of fixed platforms is also becoming more widespread. Use of aluminum material can reduce fuel consumption by reducing the weight of the composite material through a weight composition ratio of 1/3 compared to carbon steel. The characteristics of the stress strain relationship of an aluminum structure are quite different from those of a steel structure, because of the influence of the welding[process heat affected zone (HAZ). The HAZ of aluminum is much wider than that of steel owing to its higher heat conductivity. In this study, by considering the HAZ generated by metal insert gas (MIG) welding, the buckling and final strength characteristics of an aluminum reinforcing plate against longitudinal compression loads were analyzed. MIG welding reduces both the buckling and ultimate strength, and the energy dissipation rate after initial yielding is high in the range of the HAZ being 15 mm, and then the difference is small when HAZ being 25 mm or more. Therefore, it is important to review and analyze the influence of the HAZ to estimate the structural behavior of the stiffened plate to which the aluminum alloy material is applied.

Thermal Fatigue Life Prediction of Engine Exhaust Manifold (엔진 배기매니폴드의 열피로 수명 예측)

  • Choi, Bok-Lok
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.15 no.1
    • /
    • pp.139-145
    • /
    • 2007
  • This paper presents the low cycle thermal fatigue of the engine exhaust manifold subject to thermomechanical cyclic loadings. The analysis includes the FE model of the exhaust system, temperature dependent material properties, and thermal loadings. The result shows that at an elevated temperature, large compressive plastic deformations are generated, and at a cold condition, tensile stresses are remained in several critical zones of the exhaust manifold. From the repetitions of thermal shock cycles, plastic strain ranges could be estimated by the stabilized stress-strain hysteresis loops. The method was applied to assess the low cycle thermal fatigue for the engine exhaust manifold. It shows a good agreement between numerical and experimental results.

Collapse Analysis of Ultimate Strength for the Aluminium Stiffened Plate subjected to Compressive Load (알루미늄 보강판의 압축 최종강도 붕괴 해석)

  • Park, Joo-Shin;Ko, Jae-Yong;Kim, Yun-Young
    • Journal of Navigation and Port Research
    • /
    • v.31 no.10
    • /
    • pp.825-831
    • /
    • 2007
  • The use of high-strength aluminum alloys for ship and offshore structure generally has many benefits compared to the structural steels. These materials are used widely in a variety of fields, especially in the hull and deck of high speed craft, box-girder of bridges, deck and side plates of offshore structure. The structural weight can be reduced using these aluminum structure, which can enable high speed The characteristics of stress-strain relationship of aluminum structure are fairly different from the steel one, because of the influence of Heat Affected Zone(HAZ) by the welding processing. The HAZ of aluminum is much wider than that of steel with its high heat conductivity. In this paper, the ultimate strength characteristics of aluminum stiffened panel subjected to axial loading, such as the relationship between extent of HAZ and the behavior of buckling/ultimate strength, are investigated through the Finite Element Analysis with varying its range.