• 제목/요약/키워드: Design Ultimate Loads

검색결과 174건 처리시간 0.029초

풍력발전시스템의 블레이드에 작용하는 극한하중에 대한 난류의 영향 연구 (A Study on the Effects of Turbulence to Ultimate Loads Acting on the Blade of Wind Turbine)

  • 현승건;김건훈
    • 한국태양에너지학회 논문집
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    • 제33권1호
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    • pp.7-14
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    • 2013
  • This study has analysed the ultimate loads acting on a wind turbine which is operating in a high turbulent flow condition because the ultimate loads are critical factors on the safe design of wind turbine. Since wind flow on the most parts of Korean mountainous are strongly influenced by complex configurations of the topography, turbulence intensity on somewhere is so stronger than an international design standard. For this reason, the characteristics of turbulent wind data collected from actual sites were analyzed and used for the ultimate load evaluation of the wind turbine. With the 270 design load cases on the international standards, the differences of ultimate loads on the wind turbine operating in the standard or high turbulent wind condition are calculated and compared for the an enhanced knowledge of the safe design basis. As are result, it is revealed the specific ultimate loads are strongly affected by the high turbulent wind conditions, thus the characteristics of turbulent flow must be considered during the design of wind turbine.

Design and ultimate behavior of RC plates and shells: two case studies

  • Min, Chang-Shik
    • Structural Engineering and Mechanics
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    • 제14권2호
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    • pp.171-190
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    • 2002
  • Two cases of design are performed for the hyperbolic paraboloid saddle shell (Lin-Scordelis saddle shell) and the hyperbolic cooling tower (Grand Gulf cooling tower) to check the design strength against a consistent design load, therefore to verify the adequacy of the design algorithm. An iterative numerical computational algorithm is developed for combined membrane and flexural forces, which is based on equilibrium consideration for the limit state of reinforcement and cracked concrete. The design algorithm is implemented in a finite element analysis computer program developed by Mahmoud and Gupta. The amount of reinforcement is then determined at the center of each element by an elastic finite element analysis with the design ultimate load. Based on ultimate nonlinear analyses performed with designed saddle shell, the analytically calculated ultimate load exceeded the design ultimate load from 7% to 34% for analyses with various magnitude of tension stiffening. For the cooling tower problem the calculated ultimate load exceeded the design ultimate load from 26% to 63% with similar types of analyses. Since the effective tension stiffening would vary over the life of the shells due to environmental factors, a degree of uncertainty seems inevitable in calculating the actual failure load by means of numerical analysis. Even though the ultimate loads are strongly dependent on the tensile properties of concrete, the calculated ultimate loads are higher than the design ultimate loads for both design cases. For the cases designed, the design algorithm gives a lower bound on the design ultimate load with respect to the lower bound theorem. This shows the adequacy of the design algorithm developed, at least for the shells studied. The presented design algorithm for the combined membrane and flexural forces can be evolved as a general design method for reinforced concrete plates and shells through further studies involving the performance of multiple designs and the analyses of differing shell configurations.

풍력터빈 출력예측 및 극한하중평가에 관한 연구 (A Study on the Ultimate Load Assessment and the Performance Prediction of a Wind Turbine)

  • 김범석;음학진;김만응
    • 대한기계학회논문집B
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    • 제33권5호
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    • pp.326-333
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    • 2009
  • Design life-time of a wind turbine is required to be at least 20 years. In the meantime, the wind turbine will experience a lot of load cases such as extreme loads and fatigue loads which will include several typhoons per year and extreme gusts with 50 years recurrence period as well as endless turbulence flow. Therefore, IEC61400-1 specifies design load cases to be considered in the wind turbine design and requires the wind turbine to withstand the load cases in various operational situations. This paper investigates the ultimate loads which the wind turbine will experience for 20 years and their characteristics based on the IEC61400-1 using an aero-elastic software, GH-Bladed. And the performance characteristics of a wind turbine such as electrical power generation and annual energy yield are also investigated.

수평축 풍력터빈 출력예측 및 극한하중평가 (Ultimate Load Assessment and Performance Prediction of a Horizontal Axis Wind Turbine)

  • 김범석;김만응;음학진
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2880-2885
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    • 2008
  • Design lifttime of a wind turbine is required to be at least 20 years. In the meantime, the wind turbine will experience a lot of load cases such as extreme loads and fatigue loads which will include several typhoons per year and extreme gusts with 50 years recurrence period as well as endless turbulence flow. Therefore, IEC61400-1 specifies design load cases to be considered in the wind turbine design and requires the wind turbine to withstand the load cases in various operational situations. This paper investigates the ultimate loads which the wind turbine will experience for 20 years and their characteristics based on the IEC61400-1 using an aero-elastic software, GH-Blade. And the performance characteristics of a wind turbine such as electrical power generation and annual energy yield are also investigated.

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4인승 선미익 경항공기 전기체 정적 구조시험 (Full Scale Airframe Static Test of 4 Seater Canard Airplane)

  • 신정우;김성찬;김성준;채동철;이상욱;김태욱;심재열
    • 한국군사과학기술학회지
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    • 제9권4호
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    • pp.15-23
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    • 2006
  • In this paper, full-scale airframe static test of 4-seater canard airplane(the Firefly) was explained. From the results of the structural analysis, 5 design limit loads test conditions and 11 design ultimate loads test conditions were selected. Test loads analysis was performed and test fixtures and load control system(LCS) were prepared to realize the test loads. To protect the test article during the test, the overload protection system was prepared. Strain and deflection values were acquired through the data acquisition system(DAS) to verify the structural analysis results.

선체판부재의 최종강도에 대한 횡압력의 영향에 관한 연구 (A Study on the Lateral Pressure Effect for Ultimate Strength of Ship Platings)

  • 박주신;고재용;이준교;이경환
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2005년도 춘계 학술발표회 논문집
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    • pp.583-591
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    • 2005
  • The ship plating is generally subjected to combined in-plane load and lateral pressure loads. In-plane loads include axial load and edge shear, which are mainly induced by overall hull girder bending and torsion of the vessel. Lateral pressure is due to water pressure and cargo. These load components are not always applied simultaneously, but more than one can normally exist and interact. Hence, for more rational and safe design of ship structures, it is of crucial importance to bitter understand the interaction relationship of the buckling and ultimate strength for ship plating under combined loads. Actual ship plates are subjected to relatively small water pressure except for the impact load due to slamming and panting etc. The present paper describes an accurate and fast procedure for analyzing the elastic-plastic large deflection behavior up to the ultimate limit state of ship plates under combined loads. In this paper, the ultimate strength characteristics of plates under axial compressive loads and lateral pressure loads are investigated through ANSYS elastic-plastic large deflection finite element analysis with varying lateral pressure load level.

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Study on Applicability of Ultimate Strength Design Formula for Sandwich Panels - Application Cases of Double Hull Tanker Bottom Structures

  • Kim, Bong Ju
    • 한국해양공학회지
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    • 제34권2호
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    • pp.97-109
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    • 2020
  • In this study, ultimate strength characteristics of clamped sandwich panels with metal faces and an elastic isotropic core under combined in-plane compression and lateral pressure loads are investigated to verify the applicability of the ultimate strength design formula for ship structures. Alternative elastomer-cored steel sandwich panels are selected instead of the conventional bottom stiffened panels for a Suezmax-class tanker and then the ultimate strength characteristics of the selected sandwich panels are examined by using nonlinear finite element analysis. The change in the ultimate strength characteristics due to the change in the thickness of the face plate and core as well as the amplitude of lateral pressure are summarized and compared with the results obtained by using the ultimate strength design formula and nonlinear finite element analysis. The insights and conclusions developed in the present study will be useful for the design and development of applications for sandwich panels in double hull tanker structures.

최종강도 경험식을 이용한 복합재 원통구조의 최적적층 설계 (Optimal Lamination Design of Composite Cylinders using an Empirical Ultimate Pressure Load Formula)

  • 조윤식;백점기
    • 대한조선학회논문집
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    • 제56권4호
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    • pp.316-326
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    • 2019
  • In this paper, a methodology is presented for determining the optimal lamination of composite cylindrical structures subject to hydrostatic pressure. The strength criterion in association with the process of optimal design is the buckling collapse of composite cylinders under hydrostatic pressure loads. An empirical formula expressed in the form of the Merchant-Rankine equation is used to calculate the ultimate strength of filament-wound composite cylinders where genetic algorithm is applied for determining the optimized stacking sequences. It is shown that the optimized lamination provides improved collapse pressure loads. It is concluded that the developed method would be useful for the optimal lamination design of composite cylindrical structures.

기본훈련기 방향타 조종장치 정적하중 시험에 관한 연구 (A Study on the Static Test of Rudder Control System for a Basic Trainer)

  • 전찬원;이수용;강규섭
    • 한국항공우주학회지
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    • 제30권2호
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    • pp.115-121
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    • 2002
  • 본 논문은 KTX-1 기본훈련기 방향타 조종계통의 정적 하중 시험을 요약한 것이다. 방향타 콘트롤 시스템 정적 하중시험은 정하중 구조 시험용 KTX-1 #004호기에 장착 상태에서 실시하였으며 사용되는 모든 부품은 실제와 동일한 것으로 장착하고 정적하중 시험을 실시하였다. 시험하중 조건은 설계 제한하중(Design Limit Load)과 설계 극한하중(Design Ultimate Load)까지 시험을 수행하며, 전방석과 후방석 패달에 동시하중을 작용하는 경우 중복하중계수(Dual Factor)까지 고려하였다. 이 시험의 요구하중은 MIL-A-8855(USAF)의 요구조건에 따라 수행하였으며, 방향타 콘트롤 시스템 시험 결과는 미 군사규격 요구조건을 만족하였다.

선체곡판의 압축최종강도 설계식의 개발 (The Development of Ultimate Compressive Strength for Ship Curved Plates)

  • 박영일;권용우;백점기;이제명;고재용
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2004년도 가을 학술발표회 논문집
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    • pp.101-109
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    • 2004
  • Ship structures is thin-walled structures and she has lots of curved platings. In these days, lots different kinds of closed-formulas are development for ultimate strength of flat plate but for curved panels, there are not enough study or papers for this field. In this study, the ultimate strength characteristics for ship curved plates are studied. The ship plating is generally subjected to combined in-plane and lateral pressure loads. In-plane loads included biaxial compression/tension and edge shear. This is first report about the developing of ultimate compressive strength for ship curved plating. A closed-form formula for predicting the ultimate compressive strength of curved plates are empirically derived by curve fitting based on the computed results. The results and insights developed in the present study will be useful for damage tolerant design of curved plated structures.

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