• 제목/요약/키워드: 굽힘 하중

검색결과 344건 처리시간 0.026초

대형 선박의 파이프 루프 설계식 개발 (I) (The Development of Design Formulas for Pipe Loops Used in Large Vessels (I))

  • 박치모;양박달치;이종훈
    • 한국해양공학회지
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    • 제22권5호
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    • pp.132-137
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    • 2008
  • Ship structures are subject to severe environmental loads causing appreciable hull girder bending which in turn affects the piping system attached to the main hull in the form of a displacement load. While this load may cause failure in the pipes, loops have been widely adopted as a means of preventing this failure, with the idea that they may lower the stress level in a pipe by absorbing some portion of the displacement load. But since such loops also have some negative effects, such as causing extra manufacturing cost, deteriorating the function of the pipe, and occupying extra space, the number and dimensions of the loops adopted need to be minimized. This research developed design formulas for pipe loops, modeling them as frames composed of beam elements, where not only bending but also shear deflection is taken into account. The accuracy of the proposed design formulas was verified by comparing two results respectively obtained by the proposed formulas and MSC/NASTRAN. The paper concludes with a sample example showing the efficiency of the proposed formulas.

여러 형상의 감육부를 가진 엘보우의 소성붕괴 굽힘 하중의 평가 (Evaluation of Plastic Collapse Bending Load of Elbows with Thinning Area of Various Shapes)

  • 신규인;이성호;윤기봉
    • 한국안전학회지
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    • 제23권3호
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    • pp.17-24
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    • 2008
  • Elbows with various shapes of local wall thinning were numerically analyzed by finite element method to get load-displacement curves and the maximum loads. Results were compared with the experimental data obtained by another study. Elastic-plastic analysis were carried out under the combined loading conditions of internal pressure and in-plane bending loads. Two types of bending loads were considered such as elbow opening mode and elbow closing mode. Also, two different wall thinning geometries were modeled. Wall thinning area located extrados or intrados of elbow inner surface was considered. Longitudinal and circumferential lengths of the thinning area and the thinned thickness were varied for analysis. The results showed that the maximum load of the wall-thinned elbow decreased with increasing of the circumferential thinning length and the thinned thickness in both of extrados and intrados thinning locations in both loading types. The maximum load obtained by the analysis were in good agreement with the experimentally measured maximum load with the same wall thinning type and dimensions. This supports accuracy of the analysis results obtained in this study.

슬래밍 충격하중을 고려한 선체 휘핑 해석 (Whipping analysis of hull girders considering slamming impact loads)

  • 박성환;이근배;임채환
    • 대한조선학회논문집
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    • 제37권3호
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    • pp.99-109
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    • 2000
  • 본 연구에서는 대파고 파랑 중을 항해하는 선박의 슬래밍 충격에 대한 선체 전체의 동적 탄성응답 해석법을 개발하였다. 선체구조는 전단효과를 고려하는 박판보 유한요소이론을 활용하였으며, 선체 각 단면에 작용하는 유체력은 통상의 선형 운동체 이론에 덧붙여 물체 경계의 비선형성을 고려하여 추정하였다. 즉 매 순간 선체와 파 입자간의 접수 형상을 고려하는 비선형 유체력 추정법을 모멘텀 슬래밍 이론에 근거하여 정식화하였다. 개발된 해석법의 검증을 위해 V형 단면 선형과 S-175 선형 모델을 대상으로 수치해석을 수행하였다. 시간 영역에 있어 각 단면에서의 파면에 대한 상대 변위 성분과 속도 성분들을 계산하였으며, 선체 중앙 단면에서의 굽힘 모멘트 값의 시간이력을 검토하였다.

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유기 및 무기 섬유로 보강한 포트랜드 시멘트의 물성 연구 (Physical Properties of Organic- and Inorganic-Fiber Reinforced Portlandcement)

  • 장복기;김윤주
    • 한국세라믹학회지
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    • 제41권9호
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    • pp.690-695
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    • 2004
  • 본 연구에서는 무기(강, 아스베스트와 카본) 및 유기(폴리아크릴과 폴리아마이드) 섬유가 포트랜드 시멘트의 물성 보강에 미치는 영향을 조사하였다. 각 시편의 하중-변형 관계도로부터 굽힘강도, 탄성계수, 파괴에너지 및 파괴인성 값을 구하여 서로 비교하였다. 그리고 따로 충격에너지 실험도 수행하였으며 파괴에너지와 비교하였다. 휨강도 개선에는 무기(아스베스트) 섬유보강이 가장 효과적이었으며, 충격에너지의 보강섬유로는 유기(폴리아크릴) 섬유가 가장 좋았다. 한편 강 섬유는 휨 강도와 충격에너지 양자를 동시에 보강하는 데에 가장 적합했다. 또한 강 섬유는 모든 섬유 중에서 가장 높은 파괴에너지와 파괴인성 값을 나타내었다.

충격하중을 받은 CFRP 적층판의 손상거동과 잔류굽힘피로강도 (Damage Behavior and Residual Bending Fatigue Strength of CFRP Composite Laminates Subjected to Impact Loading)

  • 임광희;양인영
    • 대한기계학회논문집A
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    • 제20권6호
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    • pp.1836-1842
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    • 1996
  • In this paper, static and fatigue bending strengths of CFRP(carbon fiber reinforced plastic laminates having impact damage(FOD) are evaluated. Composite laminates used for this experiment are CF/EPOXY and CF/PEEK orthotropy laminated plates, which have two-interfaces[${0^0}_4{90^0}_4}$]$_sym$. A steel ball launched by the air gun colides against CFRP laminates to generate impact damages. The damage growth during bending fatigue test is observed by the scanning acoustic microscope(SAM). When the impacted side is compressed, the residual fatigue bending strength of CF/PEEK specimen P is greater that that of CF/EPOXY SPECIMEN B. On the other hand, when the impacted side is in tension, the residual fatigue bending strength of CF/PEEK speicemen P is smaller than that of CF/EPOXY specimen B. In the case of impacted-side compression, fracture is proposed from the transverse crack generated near impact point. On the other hand, fracture is developed toward the impact point from the edge of interface-b delamination in the case of impacted-side tension.

굽힘 및 비틀림 연성 효과를 고려한 대형 풍력 터빈 블레이드의 강제 진동 및 하중 해석 (Forced Vibration and Loads Analysis of Large-scale Wind Turbine Blades Considering Blade Bending and Torsion Coupling)

  • 김경택;박종포;이종원
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.256-263
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    • 2008
  • The assumed modes method is developed to derive a set of linear differential equations describing the motion of a flexible wind turbine blade and to propose an approach to investigate the forced responses result from various wind excitations. In this work, we have adopted Euler beam theory and considered that the root of the blade is clamped at the rigid hub. And the aerodynamic parameters and forces are determined based on Blade Element Momentum (BEM) theory and quasi-steady airfoil aerodynamics. Numerical calculations show that this method gives good results and it can be used fur modeling and the forced vibration analysis including the coupling effect of wind-turbine blades, as well as turbo-machinery blades, aircraft propellers or helicopter rotor blades which may be considered as straight non-uniform beams with built-in pre-twist.

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위성체 유연 보 구조물의 열 안정성 해석 (Thermal Stability Analysis of a Flexible Beam Spacecraft Appendage)

  • 윤일성;송오섭
    • Composites Research
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    • 제15권3호
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    • pp.18-29
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    • 2002
  • 본 논문에서는 얇은 벽보로 모델링 한 위성체 구조물에 입사되는 열 하중에 의해 발생하는 굽힘 진동과 열적 플러터에 대하여 연구하였다. 복합재료 얇은 벽보는 회전관성과 1차, 2차 와핑, 전단변형의 비고전적 요소를 포함한다. CUS구조물로 모델링한 복합재료 얇은 벽보의 열 진동 특성은 적층 순서와 섬유강화복합재료의 방향특성인자로부터 기인된 종방향 굽힘과 횡방향 굽힘의 언성과 관련하여 연구되었다. 수치 해석적인 방법으로 열적 플러터의 안정성 영역의경계값을 구하였으며, 태양 열 플럭스의 입사각, 감쇠계수, 섬유각의 변화에 의한 보의 변위를 구하였다. 주 구조물에 압전소자를 부착하여, 감지기와 작동기로 사용하여 제어해석을 수행하였다.

증기발생기 전열관 감육부의 강도 및 손상평가 (Failure Assessment and Strength of Steam Generator Tubes with Wall Thinning)

  • 성기용;안석환;윤자문;남기우
    • 한국해양공학회지
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    • 제21권2호
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    • pp.50-59
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    • 2007
  • Steam generator tubes are degraded from wear, stress corrosion cracking, rupture and fatigue and so on. Therefore, the failure assessment of steam generator tube is very important for the integrity of energy plants. In the steam generator tubes, sometimes, the local wall thinning may result from severe degradations such as erosion-corrosion damage and wear due to vibration. In this paper, the elasto-plastic analysis was performed by FE code ANSYS on steam generator tubes with wall thinning. Also, the four-point bending tests were performed on the wall thinned specimens, and then it was compared with the analysis results. We evaluated the failure mode, fracture strength and fracture behavior from the experiment and FE analysis. Also, it was possible to predict the crack initiation point by estimating true fracture ductility under multi-axial stress conditions at the center of the thinned area from FE analysis.

굽힘하중을 받는 준 카고메 트러스 샌드위치 판재의 파손선도와 최적설계변수의 도출 (Failure Maps and Derivation of Optimal Design Parameters for a Quasi-Kagome Truss Sandwich Panel Subjected to Bending Moment)

  • 임채홍;전인수;강기주
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.96-101
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    • 2007
  • A new metallic sandwich panel with a quasi-Kagome truss core subjected to bending load has been analyzed. First, equations of the failure loads corresponding to the eight failure modes are presented. Then, non-dimensional forms of the equations are derived as functions of three geometric variables, one material parameter (yield strain), one load index and one weight index. Failure maps are presented for a given weight index. By using the dimensionless forms of equations as the design constraints, two kinds of optimization are performed. One is based on the weight, that is, the objective function, namely, the dimensionless load is to be maximized for a given weight. Another is based on the load, that is, the dimensionless weight is to be minimized for a given load. The results of the two optimization processes are found to agree each other. The optimized geometric variables are derived as a function of given weights or failure loads. The performance of the quasi-Kagome truss as the core of a sandwich panel is evaluated by comparison with those of honeycomb cored and octet truss cored panels

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스마트 스킨 샌드위치 시편의 압축거동 연구 (Compressive Behavior for Smart Skin of Sandwich Structure)

  • 김영성;김용범;박훈철;윤광준;이재화
    • 한국항공우주학회지
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    • 제30권8호
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    • pp.56-64
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    • 2002
  • 본 연구에서는 다중 적층 구조의 스마트 스킨에 대한 개념 설계, 제작을 하였으며, 압축 실험을 통해 스마트 스킨의 거동 특성을 확인하였다. 상용 유한요소 소프트웨어인 NASTRAN 을 이용한 선형 압축 해석을 통해 스마트 스킨의 층별 응력 분포를 예측하였으며, 최초 파괴층을 예측하였다. 압축 시험과 선형 비선형해석 결과를 비교하여 유한요소 모델의 신뢰도를 검증하였으며, 본 모델을 이용한 설계 인자 해석을 통해 스마트 스킨 설계 자료를 확보하였다. 하니컴 심재의 전단탄성계수가 굽힘 변형과 전단 변형이 동시에 발생하는 스마트 스킨의 좌굴 하중에 큰 영향을 미치는 것을 화인하였다.