• 제목/요약/키워드: Thermal creep

검색결과 258건 처리시간 0.024초

TMA 열분석을 이용한 ACM 고무의 압축크립거동 연구 (A Study on Compressive Creep Behavior of ACM Rubber using TMA Thermal Analysis)

  • 안원술;이형석
    • Elastomers and Composites
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    • 제48권2호
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    • pp.156-160
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    • 2013
  • 자동차 엔진 개스킷용으로 사용되는 아크릴 고무(ACM)의 압축크립 거동을 TMA 열분석기를 이용하여 연구하였다. 160, 180, 200, 및 $220^{\circ}C$의 서로 다른 온도에서 1N의 일정한 힘을 가하고 등온시험을 행한 결과, 시간에 따른 압축크립거동을 얻었고, 이로부터 시간-온도 중첩원리를 이용하여 기준온도 $160^{\circ}C$에서의 이동인자 $a_T$를 실험적으로 결정하고, 고온 데이터의 기준온도로의 평행 이동에 의하여 마스터 곡선을 얻을 수 있었다. 또한 WLF(Williams-Landel-Ferry) plot을 통하여 계산된 $C_1$$C_2$는 각각 -1.107 및 11.571로 계산되었으며, WLF식을 이용하는 $120^{\circ}C$에서의 ACM 고무재료의 수명은 약 24,000시간으로 예측되었다.

Modelling of effective irradiation swelling for inert matrix fuels

  • Zhang, Jing;Wang, Haoyu;Wei, Hongyang;Zhang, Jingyu;Tang, Changbing;Lu, Chuan;Huang, Chunlan;Ding, Shurong;Li, Yuanming
    • Nuclear Engineering and Technology
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    • 제53권8호
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    • pp.2616-2628
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    • 2021
  • The results of effective irradiation swelling in a wide range of burnup levels are numerically obtained for an inert matrix fuel, which are verified with DART model. The fission gas swelling of fuel particles is calculated with a mechanistic model, which depends on the external hydrostatic pressure. Additionally, irradiation and thermal creep effects are included in the inert matrix. The effects of matrix creep strains, external hydrostatic pressure and temperature on the effective irradiation swelling are investigated. The research results indicate that (1) the above effects are coupled with each other; (2) the matrix creep effects at high temperatures should be involved; and (3) ranged from 0 to 300 MPa, a remarkable dependence of external hydrostatic pressure can be found. Furthermore, an explicit multi-variable mathematic model is established for the effective irradiation swelling, as a function of particle volume fraction, temperature, external hydrostatic pressure and fuel particle fission density, which can well reproduce the finite element results. The mathematic model for the current volume fraction of fuel particles can help establish other effective performance models.

크맆피드연삭에서 공작물로 유입되는 에너지 비율 (Energy Partition to Workpiece in Creep feed Grinding)

  • 홍순익
    • 한국생산제조학회지
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    • 제7권6호
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    • pp.42-48
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    • 1998
  • This paper is concerned with the heat flux distribution and energy partition for creep-feed grinding. From measurements of transient grinding temperatures in the workpiece sub-surface using an embedded thermocouple, the overall energy partition to the workpiece was estimated from moving heat source theory for a triangular heat flux distribution as 3.0% for down grinding and 4.5% for up grinding. The higher energy partition for up grinding can be attribute to the need to satisfy thermal compatibility at the grinding zone. The influence of cooling outside the grinding zone can be analytically taken into account by specifying convective heat transfer coefficients on the workpiece surface ha ahead of the heat source (grinding zone) and hb behind the heat source. The smaller energy partition together with slightly lower grinding power favors down grinding over up grinding.

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보일러관의 수명에 부식이 미치는 영향에 대한 수치해석 (Numerical Analysis of Corrosion Effects on the Life of Boiler Tube)

  • 홍성호;김종성
    • 대한기계학회논문집A
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    • 제24권11호
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    • pp.2812-2822
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    • 2000
  • Several methods have been developed to predict the rupture time of the boiler tubes in thermal power plant. However, existing life prediction methods give very conservative value at operating stress of power plant and rupture strain cannot be well estimated. Therefore, in this study, rupture time and strain prediction method accounting for creep, corrosion and heat transfer is newly proposed and compared with the current research results. The creep damage evolves by continuous cavity nucleation and constrained cavity growth. The corrosion damage evolves by steam side and fire side corrosion. The results showed good correlation between the theoretically predicted rupture time and the current research results. And rupture strain may be well estimated by using the proposed method.

크리피드연삭에서 공작물로 유입되는 에너지 비율 (Energy Partition to Workpiece in Creep feed Grinding)

  • 김남경;박호성;홍순익;송지복
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1997년도 춘계학술대회 논문집
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    • pp.799-804
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    • 1997
  • This paper is concerned with the heat flux distribution and energy partition for creep-feed grinding. Form measurements of transient grinding temperatures in the workpiece sub-surface using an embeded thermocouple, the overall energy partition to the workpiece was estimated form moving heat source theory for a triangular heat flux distribution as 3.0% for down grinding and 4.5% for up grinding. The higher energy partition for up grinding can be attributed to the need to satisfy thermal compatibility at the grinding zone. The influence of cooling outside the grinding zone can be analytically taken into account by specifying convective heat transfer coefficients on the workpiecs surface h /sab a/ heat source (grinding zone) and h /sab b/ behind the heat source. The smaller energy patition together with slightly lower grinding power favors down grinding over up grinding.

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범용 연삭 숫돌의 고능률 단속 연삭특성 (Grinding characteristics of High Efficient Intermittant Grinding Wheel with Conventional Grinding Wheel)

  • 이상철;홍순익;구양;송지복
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1996년도 추계학술대회 논문집
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    • pp.61-65
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    • 1996
  • This paper experimentally describes the grinding characteristic of discontinuous grinding wheels in creep-feed grinding. In creep-feed grinding, grinding temperature increases rapidly and thermal damage such as a burn occurs on a workpiece. Discontinus grinding wheel with Conventional grinding wheel shows an exellent cooling effect has been developed. The wheels have 6, 12, 24 pieces of slotted which compare with characteristics of each wheels

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고온 내열재료를 사용한 스마트 무인기 덕트의 열 구조 해석 (Thermal Structural Analysis of a Duct with Heat Resistant Metal Materials for Smart UAV)

  • 임종빈;윤동영;이근명;박정선
    • 한국항공운항학회지
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    • 제12권2호
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    • pp.17-28
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    • 2004
  • In unmanned aerial vehicle (UAV), the high temperature results from friction with the air, combustion of fuel and combustion gas of a nozzle etc. It causes serious problems in the UAV structure. The characteristic analysis of heat resistant metal and ceramic materials and creep analysis for the functionally graded material (FGM) is presented in this paper. FGM is composed of two constituent materials that are mixed up according to the specific volume fraction distribution in order to withstand high heat condition. In addition, the creep behavior of FGM applied in duct structure of an engine is analyzed.

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Mechanical analysis of surface-coated zircaloy cladding

  • Lee, Youho;Lee, Jeong Ik;NO, Hee Cheon
    • Nuclear Engineering and Technology
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    • 제49권5호
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    • pp.1031-1043
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    • 2017
  • A structural model for stress distributions of coated Zircaloy subjected to realistic incore pressure difference, thermal expansion, irradiation-induced axial growth, and creep has been developed in this study. In normal operation, the structural integrity of coating layers is anticipated to be significantly challenged with increasing burnup. Strain mismatch between the zircaloy and the coated layer, due to their different irradiation-induced axial growth, and creep deformation are found to be the most dominant causes of stress. This study suggests that the compatibility of the high temperature irradiation-induced strains (axial growth and creep) between zircaloy and the coating layer and the capability to undergo plastic strain should be taken as key metrics, along with the traditional focus on chemical protectiveness.

경사기능재료를 사용한 스마트 무인기 덕트의 열해석과 크리프 해석 (Thermal and Creep Analysis of an Exhaust Duct of Smart UAV with FGM)

  • 임종빈;박정선;윤동영;이정진
    • 한국항공우주학회지
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    • 제34권1호
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    • pp.65-73
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    • 2006
  • 무인항공기는 엔진에서 연료의 연소, 배기관에서 고온의 연소 배기 가스등으로 인하여 많은 부분에 고온이 발생한다. 이는 전체 구조물의 안정성에 심각한 영향을 미칠 수 있는 사항이다. 경사기능재료는 고온의 환경에서 열에 저항하기 위해 한쪽 재료는 세라믹으로, 다른 쪽 재료는 가볍고 구조적 강성을 지닌 금속재료로 점차적으로 변화된 재료를 사용한 일종의 복합재료이다. 경사기능재료는 뛰어난 내열성을 가지는 특성으로 고온 상태에서 많이 사용된다. 이에 따라 본 논문에서는 경사기능재료를 무인항공기의 엔진 배기 덕트에 적용하여 열적 거동을 고찰하였고, 경사기능 층이 20개, 40개, 60개, 80개, 100개인 경사기능재료를 덕트 구조물에 적용하여 각각의 열 및 열응력 해석을 수행하여 비교 분석하였다. 또한, 경사기능재료를 사용한 고온 내열 배기 덕트의 크리프 해석을 수행하여 그 특성에 대해 고찰하였다.

Structural assessment of reactor pressure vessel under multi-layered corium formation conditions

  • Kim, Tae Hyun;Kim, Seung Hyun;Chang, Yoon-Suk
    • Nuclear Engineering and Technology
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    • 제47권3호
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    • pp.351-361
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    • 2015
  • External reactor vessel cooling (ERVC) for in-vessel retention (IVR) has been considered one of the most useful strategies to mitigate severe accidents. However, reliability of this common idea is weakened because many studies were focused on critical heat flux whereas there were diverse uncertainties in structural behaviors as well as thermal-hydraulic phenomena. In the present study, several key factors related to molten corium behaviors and thermal characteristics were examined under multi-layered corium formation conditions. Thereafter, systematic finite element analyses and subsequent damage evaluation with varying parameters were performed on a representative reactor pressure vessel (RPV) to figure out the possibility of high temperature induced failures. From the sensitivity analyses, it was proven that the reactor cavity should be flooded up to the top of the metal layer at least for successful accomplishment of the IVR-ERVC strategy. The thermal flux due to corium formation and the relocation time were also identified as crucial parameters. Moreover, three-layered corium formation conditions led to higher maximum von Mises stress values and consequently shorter creep rupture times as well as higher damage factors of the RPV than those obtained from two-layered conditions.