• 제목/요약/키워드: Initial Crack Location

검색결과 26건 처리시간 0.026초

항공용 복합재료에 대한 음향방출의 활용 (Acoustic Emission Application for Aerospace Composite Materials)

  • 이상호
    • 비파괴검사학회지
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    • 제21권3호
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    • pp.313-318
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    • 2001
  • 본 연구에서는 복합재료에 적용 가능한 음향방출 비파괴 시험 평가 기법의 정립을 목표로, 복합재 표준 시험용 평가 시편(STEB), 금속재 압력용기 내부의 복합재 내열튜브, 추진기관 토출관 등의 수압 보증 시험에서 음향방출 시험법을 적용하였다. 복합재 표준 시험용 평가 시편의 경우 음향방출 hit rate parameter를 이용하여 파열압력이 낮은 시편(2100psi이하)과, 파열압력이 높은 시편(2100psi이상)과의 구분이 가능하였으며, 파열압력이 낮은 시편은 파열압력의 50%범위내에서 과열위치의 탐지가 가능하였다. 금속재 압력용기 내부의 복합재료 내열튜브 및 추진기관 토출관의 시험 결과, 수압시험 중 크랙의 발생 압력, 초기 발생 위치, 및 진전과정의 탐지가 가능하였다.

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압입축에 발생하는 프레팅 마모가 피로균열 발생 위치에 미치는 영향 (The Effect of Fretting Wear on Fatigue Crack Initiation Site of Press-fitted Shaft)

  • 이동형;권석진;최재붕;김영진
    • 한국철도학회논문집
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    • 제10권5호
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    • pp.546-553
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    • 2007
  • 본 연구는 압입축에 프레팅이 발생할 경우 프레팅 마모에 의한 접촉형상의 변화가 접촉응력의 분포, 균열발생 위치에 미치는 영향을 분석하고자 하였다. 압입축의 프레팅 피로실험시 측정한 접촉면의 프로파일을 이용하여 유한요소 해석을 수행하고 피로 사이클별 마모형상 변화에 따른 접촉면의 응력 변화를 분석하였다. 접촉면의 응력 해석결과를 이용하여 프레팅 피로손상 파라미터와 다축 피로이론를 적용하여 마모에 따른 균열발생위치의 변화를 해석하고 실험과 비교, 분석하였다. 프레팅 마모에 의해 접촉 끝단의 응력집중은 초기에 급격하게 감소하며, 마모가 진행될수록 응력집중의 위치는 접촉끝단에서 안쪽으로 이동한다. 따라서 프레팅 마모에 의한 접촉응력의 변화가 균열발생 위치의 변차와 다중균열발생의 주요원인임을 명확히 하였다.

Fiber Optic Cable을 이용한 콘크리트 균열탐사 (Crack Detection of Concrete Using Fiber Optic Cables)

  • 조남소;김남식
    • 비파괴검사학회지
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    • 제27권2호
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    • pp.157-163
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    • 2007
  • 본 연구에서는 광섬유 케이블을 이용한 콘크리트 구조물의 균열 탐사 방법을 개발하였다. 광통신 분야에서 광섬유 케이블의 손상을 탐지하기 위해 널리 사용하고 있는 광신호 분석기인 OTDR과 일반 통신용 광섬유 케이블을 사용하여 콘크리트의 표면 및 내부에 발생한 균열의 탐사 실험을 수행하였다. 콘크리트가 균열 하중에 부과되어 초기 균열을 발생시킬 때 미리 부착된 광섬유가 균열의 위치에서 균열 거동을 함께 함으로써 손상을 입게 되어 균열의 발생 유무와 위치를 찾고자 하였다. 균열을 탐사하는데 있어 광섬유의 탈피 정도가 균열 탐사 여부를 결정짓는 가장 주요한 인자라고 파악하였으며, 예비 실험을 포함한 4차례의 실내 검증 실험을 통하여 균열을 탐사할 수 있었다. 이 연구 결과는 콘크리트 구조물의 균열 관리와 유지관리 차원으로의 활용도가 크다고 판단된다.

Diagonal Tension Failure Model for RC Slender Beams without Shear Reinforcement Based on Kinematical Conditions (I) - Development

  • 유영민
    • 한국해양공학회지
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    • 제21권6호
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    • pp.7-15
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    • 2007
  • A mechanical model was developed to predict the behavior of point-loaded RC slender beams (a/d > 2.5) without stirrups. It is commonly accepted by most researchers that a diagonal tension crack plays a predominant role in the failure mode of these beams, but the failure mechanism of these members is still debatable. In this paper, it was assumed that diagonal tension failure was triggered by the concrete cover splitting due to the dowel action at the initial location of diagonal tension cracks, which propagate from flexural cracks. When concrete cover splitting occurred, the shape of a diagonal tension crack was simultaneously developed, which can be determined from the principal tensile stress trajectory. This fictitious crack rotates onto the crack tip with load increase. During the rotation, all forces acting on the crack (i.e, dowel force of longitudinal bars, vertical component of concrete tensile force, shear force by aggregate interlock, shear force in compression zone) were calculated by considering the kinematical conditions such as crack width or sliding. These forces except for the shear force in the compression zone were uncoupled with respect to crack width and sliding by the proposed constitutive relations for friction along the crack. Uncoupling the shear forces along the crack was aimed at distinguishing each force from the total shear force and clarifying the failure mechanism of RC slender beams without stirrups. In addition, a proposed method deriving the dowel force of longitudinal bars made it possible to predict the secondary shear failure. The proposed model can be used to predict not only the entire behavior of point-loaded RC slender shear beams, but also the ultimate shear strength. The experiments used to validate the proposed model are reported in a companion paper.

독립형 LNG 화물창의 공학적 결함 평가 (Engineering Critical Assessement for an Independent Type-B LNG Cargo Tank)

  • 서재훈;박규식;차인환;정준모
    • 대한조선학회논문집
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    • 제60권4호
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    • pp.213-221
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    • 2023
  • The demand for Liquefied Natural Gas (LNG) carriers and LNG-fueled ships has significantly increased in recent years due to the sulfur-oxide emission regulations by the International Maritime Organization (IMO). The main goal of this paper is to introduce the process for the Engineering Critical Assessment (ECA) of IMO independent type-B cargo tanks made from 9% nickel alloy. A methodology proposed by the British Standard was used to conduct ECA for any structure with initial flaws. Based on this standard, a Matlab code was developed to perform ECA. Coarse mesh Finite Element Analysis (FEA) was performed on an independent type-B LNG cargo tank with a capacity of 15,000 m3. The location with the highest development of maximum principal stress was identified at the bottom of the cargo tank. Fine mesh FEA was performed to obtain the stress range required for ECA. The dynamic cargo tank loads used for FEA were determined using some ship rules presented by Det Norske Veritas. As a result of performing a 20-year long-term crack propagation analysis with a semi-elliptical surface crack, the fracture-to-yield ratio exceeded the Fracture Assessment Line (FAL) and some structural reinforcement was necessary. Performing a 15-day short-term crack propagation analysis, the fracture-to-yield ratio remained within the FAL, and no significant LNG leaks were expected. This paper is believed to provide a guide for performing ECA of LNG cargo tanks in the future by providing the basic theory and application sample necessary to perform ECA.

국부변형률방법을 이용한 용접시험편의 피로수명 해석 (Fatigue Life Analysis of Butt-welded specimen by Local Strain Approach)

  • 이동형;서정원;구병춘;석창성
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2003년도 추계학술대회 논문집(III)
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    • pp.73-78
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    • 2003
  • The residual stresses and. distortions of structures by welding exert negative effect on the safety of railroad structures. This investigation performs a thermal elasto-plastic analysis using finite element techniques to evaluate residual stresses in butted-welded joint. Considering this initial residual stresses, local stress and strain at the critical location (weld toe) during the loading were analyzed by elastic plastic finite element analysis. Fatigue crack initiation life and fatigue crack propagation life of butt-welded specimen were predicted by local strain approach and Neuber's role and Paris law. It is demonstrated that fatigue life estimates by local strain approach closely approximate the experimental results.

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매스콘크리트에서 타설블럭의 크기(L/H)와 구속체의 탄성계수가 온도응력에 미치는 영향에 관한 검토 (Evaluation on the Effect of the Size of Placing Block(L/H) and Elastic Modulus of Base Structure on the Thermal Stress in Mass Concrete)

  • 강석화;이용호;박칠림
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1996년도 봄 학술발표회 논문집
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    • pp.275-279
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    • 1996
  • In this study, the effect of external restraint on the thermal stresses and thermal cracking mode in mass concrete are analysed using the two major factors affecting external restraint such as the ratio of width go height of the placed structure (L/H) and the elastic modulus of base structure (E). For this parametric study, many cases with different values of L/H and Er are analysed by the FEM program and the co-relationship of the those major factors is examined. To evaluate the effect of external restraint on the thermal behavior of placing structure, internal restraint stress caused by temperature difference is subtracted from total thermal stress. In the case of small value of L/H or Er, it shows as internally restricted mode indicating maximum tensile stress in surface at early age, and the external restraint makes the possibility of thermal cracking higher. However, in the case of the large values of L/H and Er, the crack index at center is smaller than at surface due to the effect of external restraint. Thus, the initial location of the thermal crack is shifted from the surface to the center and the resulting crack is formed at later age.

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아연도금 강판의 점용접재의 피로균형에 관한 연구 (Fatigue Behavior of the Single Spot Welded Joint of Zinc Galvanized Steel Sheets)

  • 서창민;강성수;오상표
    • 한국해양공학회지
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    • 제6권2호
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    • pp.21-34
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    • 1992
  • The behavior of fatigue crack growth in the single spot welded joint of zinc galvanized steel sheets was studied experimentally and analytically based on fracture mechanics. Axial tension fatigue tests were carried out with the BSxGAB specimen that the bare plane(GAB) of monogalvanized steel sheet was spot welded to the double thickness bare steel sheet(BS), and with the GAxGAB specimen that the galvanized plane (GA) was spot welded to the equal thickness bare plane (GAB) 1. The relation between maximum stress intensity factor, K sub(max) and the number of cycles to failure, N sub(f) has shown a linear relation on log-log plot in the spot weld of the zinc galvanized steel sheet. 2. The fatigue strength of BSxGAB specimens is about 23% higher than that of GAxGAB specimens at the fatigue strength of $1\times10^6$ cycles. And the fatigue life of BSxGAB specimens at the same load range increases 6~9 times higher than that of GAxGAB specimens. 3. The general tendency at the angle of bending($\theta$) in an applied load has changed rapidly at the initial 20% of its life. After then, it has changed slowly. The change at the angle of bending has increased linearly as the load range increases. 4. It has shown a linear relation between the location ratio of initiation ${\gamma}$ and fatigue life $N_f$ on the semi-log graph paper. Here $\gamma$ means that the crack distance between main crack and sub-crack, 2L is divided by the nugget diameter, 2r. $\gamma=a{\cdot}log N_f+n$ (where a and n are material constant.)

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A7075-T6 알루미늄 합금의 프레팅 피로 손상 파라미터 비교 평가 (Comparison and Estimation of Fretting Fatigue Damage Parameters for Aluminum Alloy A7075-T6)

  • 황동현;조성산
    • 대한기계학회논문집A
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    • 제35권10호
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    • pp.1229-1235
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    • 2011
  • 신뢰성이 가장 우수한 프레팅 피로손상 파라미터를 찾아내기 위해 알루미늄 합금 A7075-T6 을 대상으로 피로시험을 수행하였다. 시편 표면에 홈을 가공하여 패드 접촉압력에 따라 패드-시편 접촉면에서 프레팅 피로균열이 발생하거나 또는 홈에서 일반 피로균열이 발생할 수 있게 하였다. 광학현미경을 이용하여 균열의 발생위치와 방향을 측정하고, 문헌에서 가장 많이 사용되는 프레팅 피로손상 파라미터들의 신뢰성을 평가하였다. 파라미터 값과 최대손상평면 방향을 산출하는데 필요한 응력과 변형률 자료는 유한요소해석으로 산출하였다. 전단모드 피로파손을 가정하는 Fatemi-Socie 파라 미터와 McDiarmid 파라미터가 가장 신뢰성이 높은 것으로 판명되었다.

Crude Oil Tanker 선저부 보강재 필렛 용접부 각장 설계에 관한 연구 (A Study on Design of Fillet Weld Size for Stiffener in the Hull Bottom of Crude Oil Tanker)

  • 강봉국;신상범;박동환
    • Journal of Welding and Joining
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    • 제32권1호
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    • pp.79-86
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    • 2014
  • The purpose of this study is to determine the proper fillet weld size for the stiffeners on hull bottom plate of crude oil tanker. To achieve it, the effective notch stress and hot spot stress of the fillet weld with leg length specified in the rule were evaluated by using comprehensive FE analyses. Based on the results, the fatigue damages at each location of weld were calculated. Meanwhile the transitional behavior of initial welding distortion in the hull bottom plate under the design conditions was investigated by using a non-linear FEA. Welding distortion and residual stress introduced during fabrication process were considered as initial imperfections. According to FE analysis results, if the fillet leg length satisfies the design criteria of the classification society, the concern on the root failure at the fillet welds in the bottom hull plate during the design life can be negligible. In addition, considering the transitional behavior of the distortion during the service life, the fillet leg length should be minimized.