• Title/Summary/Keyword: 고온 균열

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Effects of Curing Conditions on Compressive Strength and Tensile Behavior of Alkali-Active Slag-Based Fiber Reinforced Composites (양생 조건이 알칼리 활성 슬래그 기반 섬유보강 복합재료의 압축강도와 인장거동에 미치는 영향)

  • Park, Se-Eon;Choi, Jeong-Il;Lee, Bang Yeon
    • Journal of the Korean Recycled Construction Resources Institute
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    • v.9 no.3
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    • pp.260-267
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    • 2021
  • The purpose of this study was to experimentally investigate the effects of curing methods on the compressive strength and tensile behavior of alkali-activated slag-based fiber-reinforced composite with a water-to-binder ratio of 15%. Three kinds of mixtures according to the curing conditions were prepared and compressive strength and tension tests were performed. Test results showed that the compressive strength and the first cracking strength of composites decreased when high temperature curing and air curing were adopted, while tensile strain capacity of composites increased. It was also observed that crack spacing and crack width of composites decreased by applying high temperature and air curing.

Comparison of Crack Growth Test Results at Elevated Temperature and Design Code Material Properties for Grade 91 Steel (Grade 91 강의 고온 균열진전 실험 결과와 설계 물성치의 비교)

  • Lee, Hyeong-Yeon;Kim, Woo-Gon;Kim, Nak-Hyun
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.1
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    • pp.27-35
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    • 2015
  • The material properties of crack growth models at an elevated temperature were derived from the results of numerous crack growth tests for Mod.9Cr-1Mo (ASME Grade 91) steel specimens under fatigue loading and creep loading at an elevated temperature. These crack growth models were needed for defect assessment under creep-fatigue loading. The mathematical crack growth rate models for fatigue crack growth (FCG) and creep crack growth (CCG) were determined based on the test results, and the models were compared with those of the French design code RCC-MRx to investigate the conservatism of the code. The French design code RCC-MRx provides an FCG model and a CCG model for Grade 91 steel in Section III Tome 6. It was shown that the FCG model of RCC-MRx is conservative, while the CCG model is non-conservative compared with the present test data. Thus, it was shown that further validation of the property was required. Mechanical strength tests and creep tests were also conducted, and the test results were compared with those of RCC-MRx.

Reheat Cracking Susceptibility of CrMoV Steel (CrMoV강의 재열균열 민감도에 관한 연구)

  • 김광수
    • Proceedings of the KWS Conference
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    • 2004.05a
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    • pp.168-170
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    • 2004
  • 터빈로터는 발전설비 중에서 가장 핵심 부분이며 동시에 심한 고온 응력을 받는 부분이다. 터빈로터 재료로는 Ni-Cr-Mo-V강과 CrMoV 강등이 사용된다. CrMoV 강은 발전 설비로 장시간 사용 중 열적피로나 크립손상, 고온 부식 등의 문제가 단독 혹은 복합적으로 발생하여 재료에 손상을 입히게 되고 결국에는 설비의 수명을 단축 시키곤 한다. (중략)

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An Experimental Study of Creep Crack Initiation Behavior in 304 and 316 Stainless Steels (304스케인리스강과 316스테인리스강의 크립 균열 발생 거동에 관한 실험적 연구)

  • 최영환;엄윤용
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.13 no.6
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    • pp.1193-1202
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    • 1989
  • 본 논문에서는 발전소의 소재로 많이 쓰이고 있는 304 스테인리스강(앞으로는 304SS로 표기함)과 316스테인리스강(앞으로는 316SS로 표기함)의 크립 균열 발생 거동 을 각각 600.deg. C와 625.deg. C에서 조사한다. 이 온도는 발전소의 반응기(reactor)에 사용 되는 304SS와 316SS이 받는 온도이다. 즉 304SS와 316SS의 크립 균열 발생을 지배 하는 파괴 매개변수가 무엇인지가 크립 파괴 실험을 통하여 조사된다. 실험 결과는 이미 제안되어 있는 크립 균열 발생 모델에서 예측된 결과와 비교된다. 특히 304SS 와 316SS은 고온에서의 연성도가 변형률 속도에 따라 변하는 것으로 알려져 있다. 본 연구에서는 '변형률 속도에 따른 재료의 연성도의 변화에 근거한 균열 발생 모델' 을 제안하고, 그 모델에서 예측된 크립 발생 거동을 실험 결과와 비교한다.

A Study on Fatigue Crack Propagation Behavior of Pressure Vessel Steel SA516/70 at High Temperature. (압력용기용 SA516/70 강의 고온피로균열 진전거동에 대한 연구)

  • 박경동;김정호;윤한기;박원조
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2000.10a
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    • pp.147-153
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    • 2000
  • The fatigue crack propagation behavior of the SA516/70 steel which is used for pressure vessels was examined experimentally at room temperature, $150^{\circ}C$, $250^{\circ}C$ and $370^{\circ}C$ with stress ratio of R=0.1 and 0.3. The fatigue crack propagation rate da/dN related with the stress intensity factor range $\Omega\textrm{K}$ was influenced by the stress ratio within the stable growth of fatigue crack(Region II) with an increase in $\Omega\textrm{K}$. The resistance to the fatigue crack growth at high temperature is higher in comparison with that at room temperature, and the resistance attributed to the extent of plasticity-induced by compressive residual stress according to the cyclic loads. Fractographic examinations reveal that the differences of the fatigue crack growth characteristics between room and high temperatures are mainly explained by the crack closure and oxide-induced by high temperature.

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A Study on Fatigue Crack propagation Behavior of Pressure Vessel Steel SA516/70 at High Temperature (압력용기용 SA516/70 강의 고온피로균열 진전거동에 대한 연구)

  • 박경동;김정호;윤한기;박원조
    • Journal of Ocean Engineering and Technology
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    • v.15 no.2
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    • pp.105-110
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    • 2001
  • The fatigue crack propagation behavior of the SA516/70 steel which is used for pressure vessels was examined experimentally at room temperature, 150$^{\circ}C $, 250$^{\circ}C $ and 370$^{\circ}C $ with stress ratio of R=0.1 and 0.3. The fatigue crack propagation rate da/dN related with the stress intensity factor range $\Delta K$ was influenced by the stress ratio within the stable growth of fatigue crack(Region II) with an increase in $\Delta K$. The resistance to the fatigue crack growth at high temperature is higher in comparison with that at room temperature, and the resistance attributed to the extent of plasticity-induced by compressive residual stress according to the cyclic loads. Fractographic examinations reveal that the differences of the fatigue crack growth characteristics between room and high temperature are mainly explained by the crack closure and oxide-induced by high temperature.

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Fatigue Crack Growth Behavior of Powder Metallurgical Nickel-based Superalloy using DCPD Method at Elevated Temperature (DCPD법을 이용한 분말야금 니켈기 초내열합금의 고온 피로균열진전거동)

  • Na, Seonghyeon;Oh, Kwangkeun;Kim, Hongkyu;Kim, Donghoon;Kim, Jaehoon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.2
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    • pp.11-17
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    • 2016
  • Powder metallurgy nickel based superalloy has been used in a high temperature part of turbine engine for airplane. The fatigue crack growth behavior was investigated using CT specimens for the materials at room temperature(R.T.), $600^{\circ}C$ and $700^{\circ}C$. The direct current potential drop(DCPD) method suggested by ASTM E647 was used to measure the crack length during fatigue crack growth at various stress ratios. The fatigue crack growth rate at R=0.5 was faster than that at R=0.1 for all temperature conditions and increased with the increase of stress ratio and temperature. Fractography was conducted for analysis of fracture mechanism.

질소 이온빔을 이용한 인코넬690의 기계적 특성 변화 연구

  • 홍인석;황용석
    • Proceedings of the Korean Nuclear Society Conference
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    • 1997.05b
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    • pp.118-122
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    • 1997
  • 차세대 원자력발전소 증기발생기 전열관 재료로 채택된 니켈기저합금으로 기존 전열관 재료인 인코넬600에 비해 고온 고압 조건에서 응력부식균열에 강한 장점을 가진 합금인 인코넬690 시료에 최대 에너지 120 keV의 질소 이온빔을 조사하여 이 재료의 기계적 특성 변화를 관측하였다. 특성 시험으로는 표면 경화를 관찰하기 위한 미세 경도 시험을 수행하여 미세 경도 증가를 확인하였다 아울러 표면 경화가 피로 특성에 미치는 영향을 관찰하기 위해 피로 균열 전파 시험을 수행하여 이온 주입으로 인한 표면 경화가 피로 균열 전파를 촉진시킴을 관찰하였다.

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Method to Determine Elastic Follow-Up Factors to Predict C(t) for Elevated Temperature Structures (이차하중을 받는 고온 구조물의 C(t) 예측을 위한 탄성추종 계수 결정법)

  • Lee, Kuk-Hee;Kim, Yun-Jae
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.7
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    • pp.759-768
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    • 2012
  • This paper proposes a method to determine the elastic follow-up factors for the $C(t)$-integral under secondary stress. The rate of creep crack growth for transient creep is correlated with the $C(t)$-integral. Elastic follow-up behavior, which occurs in structures under secondary loading, prevents a relaxation of stress during transient creep. Thus, both the values of $C(t)$ and creep crack growth increase as increasing elastic follow-up. An estimation solution for $C(t)$ was proposed by Ainsworth and Dean based on the reference stress method. To predict the value of $C(t)$ using this solution, an independent method to determine the elastic follow-up factors for cracked bodies is needed. This paper proposed that the elastic follow-up factors for $C(t)$ can be determined by elastic-plastic analyses using the plastic-creep analogy. Finite element analyses were performed to verify this method.