• 제목/요약/키워드: Buckling pattern

검색결과 82건 처리시간 0.025초

750kW급 풍력발전기용 복합재 블레이드의 구조설계 (Structural Design of a 750kW Composite Wind Turbine Blade)

  • 정창규;박선호;한경섭
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2004년도 춘계학술발표대회 논문집
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    • pp.18-21
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    • 2004
  • A GFRP based composite blade was developed for a 750kW wind energy conversion system of type class I. The blade sectional geometry was designed to have a general shell-spar structure. The load cases specified in the IEC61400-1 international specification were considered. For withstanding all relevant extreme loads, the structural analysis for the complete blade was performed using a commercial FEM code. The static load carrying capacity, buckling stability, blade tip deflection and natural frequencies at various rotational speeds were evaluated to satisfy the strength requirements in accordance with the IEC61400-1 and GL Regulations. For designing a lightweight blade, the thickness and the lay-up pattern of the skin-foam sandwich structures were optimized iteratively using the DOT program T-bolts were used for joining the blade root and the hub, which were modeled using a 3D FE volume model. In order to confirm the safety of the root connection, the static stresses of the thick root laminate and the steel. bolts were predicted by taking account of the bolt pretension and the root bending moments. The calculated stresses were compared with the material strengths.

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Identification of failure mechanisms for CFRP-confined circular concrete-filled steel tubular columns through acoustic emission signals

  • Li, Dongsheng;Du, Fangzhu;Chen, Zhi;Wang, Yanlei
    • Smart Structures and Systems
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    • 제18권3호
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    • pp.525-540
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    • 2016
  • The CFRP-confined circular concrete-filled steel tubular column is composed of concrete, steel, and CFRP. Its failure mechanics are complex. The most important difficulties are lack of an available method to establish a relationship between a specific damage mechanism and its acoustic emission (AE) characteristic parameter. In this study, AE technique was used to monitor the evolution of damage in CFRP-confined circular concrete-filled steel tubular columns. A fuzzy c-means method was developed to determine the relationship between the AE signal and failure mechanisms. Cluster analysis results indicate that the main AE sources include five types: matrix cracking, debonding, fiber fracture, steel buckling, and concrete crushing. This technology can not only totally separate five types of damage sources, but also make it easier to judge the damage evolution process. Furthermore, typical damage waveforms were analyzed through wavelet analysis based on the cluster results, and the damage modes were determined according to the frequency distribution of AE signals.

Nonlinear numerical analysis and proposed equation for axial loading capacity of concrete filled steel tube column with initial imperfection

  • Ahmad, Haseeb;Fahad, Muhammad;Aslam, Muhammad
    • Structural Monitoring and Maintenance
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    • 제9권1호
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    • pp.81-105
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    • 2022
  • The use of concrete filled steel tube (CFST) column is widely accepted due to its property of high axial load carrying capacity, more ductility and more resistant to earthquake specially using in bridges and high-rise buildings. The initial imperfection (δ) that produces during casting or fixing causes the reduction in load carrying capacity, this is the reason, experimental capacity is always less then theoretical one. In this research, the effect of δ on load carrying capacity and behavior of concrete filled steel tube (CFST) column have been investigated by numerically simulation of large number of models with different δ and other geometric parameters that include length (L), width (B), steel tube thickness (t), f'c and fy. Finite element analysis software ANSYS v18 is used to develop model of SCFST column to evaluate strength capacity, buckling and failure pattern of member which is applied during experimental study under cyclic axial loading. After validation of results, 42 models with different parameters are evaluated to develop empirical equation predicting axial load carrying capacity for different value of δ. Results indicate that empirical equation shows the 0 to 9% error for finite element analysis Forty-two models in comparison with ANSYS results, respectively. Empirical equation can be used for predicting the axial capacity of early estimating the axial capacity of SCFT column including 𝛿.

자가 계측 유도 초음파의 통계적 패턴인식을 이용하는 배관 구조물의 복합 손상 진단 기법 (Multiple Damage Detection of Pipeline Structures Using Statistical Pattern Recognition of Self-sensed Guided Waves)

  • 박승희;김동진;이창길
    • 한국구조물진단유지관리공학회 논문집
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    • 제15권3호
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    • pp.134-141
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    • 2011
  • 최근 사회 기반 시설물에서 구조물의 안전성 및 적정 성능 수준을 확보하기 위하여 구조물의 결함 빛 노후화에 의한 성능 저하 등을 상시적으로 모니터링하기 위한 관심이 높아지고 있다. 이 중 배관 구조물은 국가 주요 자원의 수송을 책임지는 핵심 사회 기반 시설물임에도 불구하고 지중에 매립된다는 위치적 특성 상 상시적으로 구조물의 상태를 모니터링하기는 매우 어렵다. 또한 배관 구조물에서는 내부 미세 균열에서부터 국부 좌굴, 볼트 풀림, 피로 균열 등과 같이 다양한 형태의 손상이 복합적으로 발생 가능하다. 따라서 본 연구에서는 이러한 복합 손상을 효율적으로 진단하기 위하여 압전센서를 이용한 자가 계측 회로 기반의 유도 초음파 계측 시스템을 복합 손상 진단에 적용하였다. 유도 초음파 자가 계측으로부터 특정 중심 주파수에 해당하는 구조물의 웨이블렛 응답을 계측한다. 복합 손상을 유형별로 분류하기 위하여 유도 초음파 계측으로부터 추출한 특성을 이용하여 손상지수를 계산하고 이를 지도학습 기반 패턴인식 기법에 적용한다. 제안된 기법의 적용성 검토를 위하여 배관 구조물에 인위적으로 다중 손상을 생성시켜 시험을 수행하였다.

극저하중(極低荷重)사이클을 받는 강부재(鋼部材) 및 요소(要素)의 파괴거동(破壞擧動)에 관한 실험적(實驗的) 연구(硏究) (Experimental Study on Failure Behavior of Steel Members and Elements under Very Low Load-Cycles)

  • 박연수
    • 대한토목학회논문집
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    • 제14권2호
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    • pp.257-268
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    • 1994
  • 강진과 같은 큰 반복하중하에서 강부재 및 그들요소의 균열과 파단에 영향을 미치는 중요한 물리적 인자들을 찾아내어, 그 인자들간의 정량적인 관계를 규명하기 위해 실험적 연구를 수행하였다. 9개의 강판요소와 28개의 앵글 강부재를 시험체로서 사용하였으며, 비탄성 좌굴이 포함된 축방향의 반복하중을 5~20회 정도 받았다. 본 실험은 극저사이클 파괴거동에 있어서 제하이력과 파괴형태 및 단면형상의 영향평가에 특히 촛점을 두었다. 실험결과, 에너지 소산능력은 실험변수에 크게 의존하였으며, 균열의 발생 또는 파단과 에너지 소산능력 사이에 단순한 정량적 관계가 성립되지 않았다. 그러나, 실험변수에 관계없이 균열발생부에 있어서 잔류변형률의 최대치는 일정한 값을 보여주었다.

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다목적2호기 태양전지판의 전개시스템 개발: PART 1. 동적 모델링 (Development of Multi-Purpose Satellite 2 with Deployable Solar Arrays: Part 1. Dynamic Modeling)

  • 곽문규;허석
    • 한국항공우주학회지
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    • 제31권9호
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    • pp.38-45
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    • 2003
  • 본 논문은 Strain Energy Hinge(SEH)를 갖는 다목적 2호기의 태양전지판 전개에 대한 동적 모델링과 관련이 있다. 이 연구를 위해 SEH는 단순한 비틀림 스프링으로 치환되었으며 인공위성과 태양전지판은 강체로 가정하고 운동방정식을 유도하였다. 또한 모델링에 지상 실험에 가장 큰 영향을 주고 있는 것으로 관찰된 지지줄의 영향을 고려하였다. 무중력 상태에서의 전개와 지상 전개 결과를 비교한 결과 태양전지판의 전개는 유사하나 인공위성의 운동은 지지줄의 영향으로 인해 전혀 다른 것으로 나타났다. 결론적으로 지상 전개 실험 장치를 이용해 무중력 상태의 태양전지판 전개를 어느 정도 정확하게 묘사할 수 있다. 또한 지지줄의 영향을 조사한 결과 현재 실험실의 지지줄의 길이가 적합한 것으로 나타났다. 지상실험 결과와의 비교는 다음 논문에서 다룬다.

Seismic design of chevron braces cupled with MRF fail safe systems

  • Longo, Alessandra;Montuori, Rosario;Piluso, Vincenzo
    • Earthquakes and Structures
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    • 제8권5호
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    • pp.1215-1240
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    • 2015
  • In this paper, the Theory of Plastic Mechanism Control (TPMC) is applied to the seismic design of dual systems composed by moment-resisting frames and Chevron braced frames. The application of TPMC is aimed at the design of dual systems able to guarantee, under seismic horizontal forces, the development of a collapse mechanism of global type. This design goal is of primary importance in seismic design of structures, because partial failure modes and soft-storey mechanisms have to be absolutely prevented due to the worsening of the energy dissipation capacity of structures and the resulting increase of the probability of failure during severe ground motions. With reference to the examined structural typology, diagonal and beam sections are assumed to be known quantities, because they are, respectively, designed to withstand the whole seismic actions and to withstand vertical loads and the net downward force resulting from the unbalanced axial forces acting in the diagonals. Conversely column sections are designed to assure the yielding of all the beam ends of moment-frames and the yielding and the buckling of tensile and compressed diagonals of the V-Braced part, respectively. In this work, a detailed designed example dealing with the application of TPMC to moment frame-chevron brace dual systems is provided with reference to an eight storey scheme and the design procedure is validated by means of non-linear static analyses aimed to check the actual pattern of yielding. The results of push-over analyses are compared with those obtained for the dual system designed according to Eurocode 8 provisions.

피라미드형 내부구조재를 가지는 중공형 접합판재의 성형특성에 관한 연구 (A Study on the Forming Characteristic of Inner Pyramid Structure Bonded Sheet Metal)

  • 김지용;길해영;조기철;김종호;정완진
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2006년도 춘계학술대회 논문집
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    • pp.295-299
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    • 2006
  • The inner-structure bonded(ISB) sheet metal is defined as a composite sheet metal which has middle layer of truss-structure between two skin sheets. The characteristics such as ultra-light weight, high rigidity, high strength, etc are required especially for automobile parts. The characteristic of ISB sheet metal depends on inner-structure pattern or method of bonding. Pyramid type of crimped expanded metal is used for inner-structure and both of resistance welding and adhesive bonding are applied to make a specimen. As a result of compression test, it is appeared that forming limit is 10% reduction in thickness under a load of 8kgf per unit element(one inner-structure). In case of uniaxial tensile test the non-uniform surface integrity rather than the buckling of inner-structure happened at a load of 450kgf, which indicates elongation of 7.2% and thickness reduction of 13%. The eye-inspection method was applied to examine the defects occurring on the specimen during stretch forming. In case of biaxial stretch forming only the non-uniform deformation on the surface of a skin sheet could be observed. The forming limit in stretching of ISB sheet metal with the hemi-spherical punch of 150mm in diameter was 3mm in forming depth and 5% reduction in thickness.

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탄소섬유/에폭시 복합적층판의 저속 충격 및 잔류 압축강도에 관한 연구 (A Study on Low Velocity Impact and Residual Compressive Strength for Carbon/Epoxy Composite Laminate)

  • 이상연;박병준;김재훈;이영신;전제춘
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집A
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    • pp.250-255
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    • 2000
  • Damage induced by low velocity impact loading in aircraft composite laminates is the form of failure which is occurred frequently in aircraft. Low velocity impact can be caused either by maintenance accidents with tool drops or by in-flight impacts with debris. As the consequences of impact loading in composite laminates, matrix cracking, delamination and eventually fiber breakage for higher impact energies can be occurred. Even when no visible impact damage is observed, damage can exist inside of composite laminates and the carrying load of the composite laminates is considerably reduced. The reduction of strength and stiffness by impact loading occurs in compressive loading due to laminate buckling in the delaminated areas. The objective of this study is to determine inside damage of composite laminates by impact loading and to determine residual compressive strength and the damage growth mechanisms of impacted composite laminates. For this purpose a series of impact and compression after impact tests are carried out on composite laminates made of carbon fiber reinforced epoxy resin matrix with lay up pattern of $[({\pm}45)(0/90)_2]s$ and $[({\pm}45)(0)_3(90)(0)_3({\pm}45)]$. UT-C scan is used to determine impact damage characteristics and CAI(Compression After Impact) tests are carried out to evaluate quantitatively reduction of compressive strength by impact loading.

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Research on aerodynamic force and structural response of SLCT under wind-rain two-way coupling environment

  • Ke, Shitang;Yu, Wenlin;Ge, Yaojun
    • Wind and Structures
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    • 제29권4호
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    • pp.247-270
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    • 2019
  • Wind-resistant design of existing cooling tower structures overlooks the impacts of rainfall. However, rainstorm will influence aerodynamic force on the tower surface directly. Under this circumstance, the structural response of the super-large cooling tower (SLCT) will become more complicated, and then the stability and safety of SLCT will receive significant impact. In this paper, surrounding wind fields of the world highest (210 m) cooling tower in Northwest China underthree typical wind velocities were simulated based on the wind-rain two-way coupling algorithm. Next, wind-rain coupling synchronous iteration calculations were conducted under 9 different wind speed-rainfall intensity combinations by adding the discrete phase model (DPM). On this basis, the influencing laws of different wind speed-rainfall intensity combinations on wind-driving rain, adhesive force of rain drops and rain pressure coefficients were discussed. The acting mechanisms of speed line, turbulence energy strength as well as running speed and trajectory of rain drops on structural surface in the wind-rain coupling field were disclosed. Moreover, the fitting formula of wind-rain coupling equivalent pressure coefficient of the cooling tower was proposed. A systematic contrast analysis on its 3D distribution pattern was carried out. Finally, coupling model of SLCT under different working conditions was constructed by combining the finite element method. Structural response, buckling stability and local stability of SLCT under different wind velocities and wind speed-rainfall intensity combinations were compared and analyzed. Major research conclusions can provide references to determine loads of similar SLCT accurately under extremely complicated working conditions.