• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2008년도 추계학술대회 논문집
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• pp.61-62
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• 2008

• 한국산업융합학회 논문집
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• 제15권1호
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• pp.13-19
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• 2012

Due to a low stiffness of cranktrain and a failure experience from a history within short development time, a viscous torsional vibration damper was applied in order to reduce the torsional vibration and keep the high reliability for the durability of cranktrain system in the direct injection diesel engine. As an improvement of the crankshaft stiffness by increasing the diameter of main and pin journal, a rubber type damper could be considered. In this study, the control factors of rubber damper, the moment of inertia ring, stiffness of damper and damping coefficient of ring, were investigated by DFSS method through the analysis work and the measurement in the real engine condition.

• Steel and Composite Structures
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• 제2권3호
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• pp.209-222
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• 2002

This paper describes the buckling phenomenon of a tubular truss with unsupported length through a full-scale test and presents a practical computational method for the design of the trusses allowing for the contribution of torsional stiffness against buckling, of which the effect has never been considered previously by others. The current practice for the design of a planar truss has largely been based on the linear elastic approach which cannot allow for the contribution of torsional stiffness and tension members in a structural system against buckling. The over-simplified analytical technique is unable to provide a realistic and an economical design to a structure. In this paper the stability theory is applied to the second-order analysis and design of the structural form, with detailed allowance for the instability and second-order effects in compliance with design code requirements. Finally, the paper demonstrates the application of the proposed method to the stability design of a commonly adopted truss system used in support of glass panels in which lateral bracing members are highly undesirable for economical and aesthetic reasons.

• Earthquakes and Structures
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• 제8권2호
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• pp.379-399
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• 2015

Existing building structures can easily present material mechanical properties which can largely vary even within a single structure. The current European Technical Code, Eurocode 8, does not provide specific instructions to account for high variability in mechanical properties. As a consequence of the high strength variability, at the occurrence of seismic events, the structure may evidence unexpected phenomena, like torsional effects, with larger experienced deformations and, in turn, with reduced seismic performance. This work is focused on the torsional effects related to the irregular stiffness and strength distribution due to the concrete strength variability. The analysis has been performed on a case-study, i.e., a 3D RC framed 4 storey building. A Normal distribution, compatible to a large available database, has been taken to represent the concrete strength domain. Different plan layouts, representative of realistic stiffness distributions, have been considered, and a statistical analysis has been performed on the induced torsional effects. The obtained results have been compared to the standard analysis as provided by Eurocode 8 for existing buildings, showing that the Eurocode 8 provisions, despite not allowing explicitly for material strength variability, are conservative as regards the estimation of structural demand.

• 한국소음진동공학회논문집
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• 제12권2호
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• pp.116-123
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• 2002

Applying a general coupled lateral and torsional vibration finite element model of gear pair element, this paper intends to look into in detail the coupled lateral and torsional vibration characteristics of a turbo-chiller rotor bearing system, having a bull-pinion speed increasing gear. Investigations have been carried out systematically by comparing the uncoupled and coupled natural frequencies and their mode shapes upon varying the gear mesh stiffness with considerations on rotating speeds, and also by comparing the strain energies of lateral and torsional vibration modes. Results hale shown that some modes may hale the coupled lateral and torsional mode characteristics as the gear mesh stiffness Increases over a certain value, and moreover that their associated dominant modes may be different from their initial modes, j.e., a certain dominant mode may change from an initial torsional one to a lateral one or from an initial lateral one to a torsional one.

• Composites Research
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• 제32권4호
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• pp.191-198
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• 2019

헬리콥터의 주 로터 블레이드는 헬리콥터의 양력과 추력을 발생시키는 구조물로, 헬리콥터의 성능을 좌우하는 중요한 구조 구성품이다. 헬리콥터의 기계적 특성값은 헬리콥터 성능해석 단계에 활용되는 중요한 매개변수이나 대부분의 로터 블레이드는 복합재 등과 같은 여러가지 재료의 조합으로 제작되므로 기계적 특성값을 추정하는 것은 쉽지 않다. 본 논문에서는 유한요소해석과 실험적 방법을 통하여 무인 헬기 복합재 로터 블레이드의 단면별 휘임 및 비틀림 강성도를 취득하였다. 유한요소해석을 통해 요소 강성 행렬과 하중-변위 관계식을 이용하여 단면별 강성도를 계산하였으며, 스트레인 게이지를 이용한 휘임 및 비틀림 시험에서 구한 변형률 값을 이용하여 단면별 강성도를 계산하였다. 유한요소해석으로 계산한 단면별 강성도와 시험 결과를 이용하여 계산한 단면별 강성도가 잘 일치함을 확인하였다.

• 대한토목학회논문집
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• 제32권6A호
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• pp.347-354
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• 2012

본 연구에서는 Sine 파형 복부판을 갖는 I형 플레이트 거더의 비틂 상수와 �� 상수식을 제안한다. Sine 파형 복부판을 갖는 플레이트 거더는 일반적으로 기하학적 특성에 따라 높은 면외 방향 강성 및 전단강도, 비틂 강성을 갖는다. 특히, 플레이트 I형 거더의 횡-비틂 강도를 산정하는 데 있어서 부재 단면의 비틂 상수 및 �� 상수는 큰 영향을 미치는데, 종래의 수식으로는 Sine 파형 복부판의 이러한 단면상수를 합리적으로 산정하는 데 어려움이 있다. 따라서 본 연구에서는 Sine 파형 복부판의 기하학적 특성을 반영할 수 있는 새로운 제안식을 연구하였다. 쉘 요소를 사용한 I형 플레이트 거더의 순수 비틂 거동에 대한 유한요소해석결과를 통해 파형의 기하학적 특성에 따른 비틂 상수 변화를 분석하고 이를 회귀분석하여 수식을 제안하였다. 이후, 순수 비틂과 �� 비틂이 함께 존재하는 조건에서의 유한요소해석 결과를 통해 �� 상수 계산식을 제안하였다. 이 두 제안식은 단순 지지된 Sine 파형 복부판을 갖는 I형 플레이트 거더의 횡-비틂 좌굴해석 결과를 토대로 검증되었다. 본 연구에서 제안한 두 수식을 통해 Sine 파형 복부판을 갖는 I형 플레이트 거더의 중요한 두 단면 상수를 명확히 계산할 수 있고, 이를 통해 정확한 횡-비틂 좌굴 강도를 손쉽게 계산할 수 있다.

• 수산해양기술연구
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• 제40권3호
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• pp.232-243
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• 2004

After studying the composition about the torsional shafting of main engine for fishing vessel with Power Take Off (PTO) System, the authors made a computer program using the transfer stiffness coefficient method (TSCM) for analyzing torsional vibration about the shafting with PTO system and nonlinear elastic coupling. The torsional shafting of main engine was separated by 3 types according to the connecting. The torsional shafting of main engine was separated by 3 types according to the connecting condition of main engine with propeller or the PTO system or both of them. In this paper, the change of natural frequencies and natural modes according to connecting condition of torsional shafting and nonlinear elastic coupling were analyzed. The accuracy of the TSCM was confirmed by comparing with the computational results of the Finite Element Method.

• Wind and Structures
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• 제1권1호
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• pp.43-57
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• 1998

A three-degree-of-freedom base hinged assembly (BHA) for aeroelastic model tests of tall building was developed. The integral parts of a BHA, which consists of two perpendicular plane frames and a flexural pivot, enable this modeling technique to independently simulate building translational and torsional degree-of-freedom. A program of wind tunnel aeroelastic model tests of the CAARC standard tall building was conducted with emphasis on the effect of (a) torsional motion, (b) cross-wind/torsional frequency ratio and (c) the presence of an eccentricity between center of mass and center of stiffness on wind-induced response characteristics. The experimental results highlight the significant effect of coupled translational-torsional motion and the effect of eccentricity between center of mass and center of stiffness on the resultant rms acceleration responses in both along-wind and cross-wind directions especially at operating reduced wind velocities close to a critical value of 10. In addition, it was sound that the vortex shedding process remains the main excitation mechanism in cross-wind direction even in case of tall buildings with coupled translational-torsional motion and with eccentricity.

• Steel and Composite Structures
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• 제30권5호
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• pp.471-481
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• 2019

Beam-columns are structural members subjected to a combination of axial and bending forces. Lateral-torsional buckling is one of the main failure modes. Beam-columns that are bent about its strong axis may buckle out of the plane by deflecting laterally and twisting as the values of the applied loads reach a limiting state. Lateral-torsional buckling failure occurs suddenly in beam-column elements with a much greater in-plane bending stiffness than torsional or lateral bending stiffness. This study intends to establish a unique convenient closed-form equation that it can be used for calculating critical elastic lateral-torsional buckling load of beam-column in the presence of a known axial load. The presented equation includes first order bending distribution, the position of the loads acting transversely on the beam-column and mono-symmetry property of the section. Effects of axial loads, slenderness and load positions on lateral torsional buckling behavior of beam-columns are investigated. The proposed solutions are compared to finite element simulations where thin-walled shell elements including warping are used. Good agreement between the analytical and the numerical solutions is demonstrated. It is found out that the lateral-torsional buckling load of beam-columns with mono-symmetric sections can be determined by the presented equation and can be safely used in design procedures.