• 제목/요약/키워드: torsion coupling

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Damage identification of isolators in base-isolated torsionally coupled buildings

  • Wang, Jer-Fu;Huang, Ming-Chih;Lin, Chi-Chang;Lin, Tzu-Kang
    • Smart Structures and Systems
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    • 제11권4호
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    • pp.387-410
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    • 2013
  • This paper deals with the damage assessment for isolators of base-isolated building systems considering the torsion-coupling (TC) effect by establishing damage indices. The damage indices can indicate the reduction in lateral stiffness of the isolator story as explicit formulas in terms of modal parameters. In addition, the damage location, expressed in terms of the estimated damage index and eccentricities before and after damage, is also presented. Numerical analysis shows that the proposed algorithms are applicable for general base-isolated multi-story TC buildings. A procedure from the analysis of seismic response to the implementation of damage indices is demonstrated by using a numerical case. A system identification technique is employed to extract modal parameters from seismic responses of a building. Results show that the proposed indices are capable of detecting the occurrence of damage and preliminarily estimating the location of damaged isolator.

Aeroelastic deformation and load reduction of bending-torsion coupled wind turbine blades

  • Shaojun, Du;Jingwei, Zhou;Fengming, Li
    • Wind and Structures
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    • 제35권5호
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    • pp.353-368
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    • 2022
  • Wind turbine blades are adjusted in real-time according to the wind conditions and blade deformations to improve power generation efficiency. It is necessary to predict and reduce the aeroelastic deformations of wind turbine blades. In this paper, the equivalent model of the blade is established by the finite element method (FEM), and the aerodynamic load of the blade is evaluated based on the blade element momentum (BEM) theory. The aeroelastic coupling model is established, in which the bending-torsion coupling effect of the blade is taken into account. The steady and dynamic aeroelastic deformations are calculated. The influences of the blade section's shear centre position and the blade's sweepback design on the deformations are analyzed. The novel approaches of reducing the twist angle of the blade by changing the shear centre position and sweepback of the blade are presented and proven to be feasible.

Transmission Characteristics of Long-Period Fiber Gratings Using Periodically Corroded Single-Mode Fibers

  • Lee, Jonghwan;Bang, Ngac An;Han, Young-Geun
    • Journal of the Optical Society of Korea
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    • 제19권4호
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    • pp.376-381
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    • 2015
  • Transmission characteristics of long-period fiber gratings (LPFGs) fabricated by periodically etching a conventional single-mode fiber (SMF) are investigated. After coating the SMF with photoresist, the cladding of the SMF is symmetrically and periodically removed by using a wet etching technique resulting in the formation of the LPFG. Tensile strain reinforces the coupling strength between the core and the cladding mode based on the photoelastic effect. The extinction ratio of the SMF-based LPFG at a wavelength of 1550.8 nm is measured to be -15.1 dB when the applied strain is $600{\mu}{\varepsilon}$. The ascent of ambient index shifts the resonant wavelength to shorter wavelength because of the increase of the effective refractive index of the cladding mode. The extinction ratio is diminished by increase in the ambient index because of the induction of the optical attenuation of the cladding mode. The transmission characteristics of the proposed LPFG with variations in torsion are also measured. The photoelastic effect based on torsion changes the extinction ratio and the resonant wavelength of the proposed SMF-based LPFG. The polarization-dependent loss of the LPFG is also increased by torsion because of the torsion-induced birefringence. The polarization-dependent loss of the LPFG at torsion of 8.5 rad/m is measured to be 3.9 dB.

비틀림전단시험에 의한 모래의 응력 -변형률 거동 (The Stress -Strain Behavior of Sand in Torsion Shear Tests)

  • 남정만;홍원표
    • 한국지반공학회지:지반
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    • 제9권4호
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    • pp.65-82
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    • 1993
  • 주응력회전시 모래의 응력-변형률 거동을 조사하기 위하여 Santa Monies해변의 모래에 대 한 비틀림전단시험이 여러가지 응력경로에 대해 실시되었다. 모래에 대한 비틀림전단시험에서는 점토에서와 달리 Torque의 작용방향을 시계방향과 반시계방향 모두에 대해 작용하였으며, 공시체의 측방변형량 측정도 내부압축실의 체적변형량으로부터 평균 변형량을 측정함으로 점토시 사용하였던 Clip gage를 제거하여 시험을 보다 편리하게 할 수 있었으며 어느 일부분에서 측정했던 측방변형을 대표값으로 사용하였던 단점을 보완하였다. 그리고 공시체의 제작은 모래를 공중낙하법에 의해 실시하여 밀도를 균등하게 만들었으며 공시체의 체적변형량은 COI 가스를 이용하여 체적변형량 측정을 보다 정확하게 할 수 있었다. 시험결과로부터 비틀림전단시험에 의한 모래의 응력 -변형률 거동이 조사되었으며 또한 주응력축 회전효과가 검토되었다. 그리고 연직응력이나 전단응력중 하나가 고정인 상태에서 다른 하중을 작용하였을시 선행하중에 의한 결합효과(coupling effect)에 의해 선행하중에 대한 전단변형률과 연직변형률이 계속 관찰되었다. 한편 축변형률에 대한 주응력비 o1/o3의 관계에서 파괴가 발생하는 축변형률의 위치는 축차주응력비 b(=(o2-o3)/(o1-o3))가 증가함에 따라 감소하는 것으로 나타났다.

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Magnetic Coupling in Oxoverdazyl-Benzene-Oxoverdazyl Diradical Systems: A DFT Study

  • Park, Young Geun;Ko, Kyoung Chul
    • EDISON SW 활용 경진대회 논문집
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    • 제2회(2013년)
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    • pp.25-35
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    • 2013
  • The intramolecular magnetic coupling constant (J) values of diradical-based magnet models (S1-S5) were studied using unrestricted density functional theory. The model systems were designed with series of oxoverdazyl radicals (o-Ver(N) and o-Ver(C)) linked through a benzene coupler. They were divided according to either connectivity of the radical (C or N) or geometrical topology (meta- and para-) of benzene coupler. Reasonable relationship was found between spin density distribution and sign of J value. With our results we determined ferromagnetic (positive J value) and antiferromagnetic (negative J value) interactions. J values were also calculated along the twisting movement by the scan of dihedral angles between the radical and the coupler. An overall trend was found as absolute value of J decreased over increasing torsion angles.

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유연체 로터-커플링-블레이드 시스템의 로터 축과 블레이드의 연성 진동에 관한 연구 (A Study on the Coupled Shaft-Torsional and Blade-Bending Vibrations in the Flexible Rotor-Coupling-Blade System)

  • 이선숙;오병영;윤형원;차석주;나성수
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 춘계학술대회논문집
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    • pp.221-226
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    • 2005
  • In this paper, a dynamic model for the rotor shaft-coupling-blade system is developed. The blades are attached to a disk and driven by an electric motor shaft which is flexible in torsion. We assumed that the shaft torsional flexibility is lumped in the flexible coupling which is usually adopted in rotor systems. The Lagrangian approach with the small deformation theory for both blade-bending and shaft-torsional deformations is employed for developing the equation of the motion. The assumed modes method is used for estimating the blade transverse deflection. The numerical results highlight the effects of both structural damping of the system and the torsional stiffness of the flexible coupling to the dynamic response of the blade. The results showed strong coupling between the blade bending and shaft torsional vibrations in the form of inertial nonlinearif, stiffness hardening and softening.

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유연체 로터-커플링-블레이드 시스템의 로터 축과 블레이드의 연성 진동에 관한 연구 (A Study on the Coupled Shaft-torsional and Blade-bending Vibrations in the Flexible Rotor-coupling-blade System)

  • 오병영;이선숙;윤형원;차석주;나성수
    • 한국소음진동공학회논문집
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    • 제15권9호
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    • pp.1023-1029
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    • 2005
  • In this paper, a dynamic model for the rotor shaft-coupling-blade system was developed. The blades are attached to a disk and driven by an electric motor shaft which is flexible in torsion. We assumed that the shaft torsional flexibility was lumped in the flexible coupling which is usually adopted in rotor systems. The Lagrangian approach with the small deformation theory for both blade-bending and shaft-torsional deformations was employed for developing the equation of the motion. The Assumed Modes Method was used for estimating the blade transverse deflection. The numerical results highlight the effects of both structural damping of the system and the torsional stiffness of the flexible coupling to the dynamic response of the blade. The results showed strong coupling between the blade bending and shaft torsional vibrations in the form of inertial nonlinearity, stiffness hardening and softening.

Thrust Characteristics of a Laser-Assisted Pulsed Plasma Thruster

  • Masatoshi Kawakami;Hideyuki Horisawa;Kim, Itsuro ura
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.294-299
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    • 2004
  • An assessment of a novel laser-electric hybrid propulsion system was conducted, in which a laser-induced plasma was induced through laser beam irradiation onto a solid target and accelerated by electrical means instead of direct acceleration only by using a laser beam. A fundamental study of newly developed rectangular laser-assisted pulsed-plasma thruster (PPT) was conducted. On discharge characteristics and thrust performances with increased peak current compared to our previous study to increase effects of electromagnetic forces on plasma acceleration. Maximum peak current increased for our early study by increasing electromagnetic effects in a laser assisted PPT. At 8.65 J discharge energy, the maximum current reached about 8000 A. Plasma behaviors emitted from a thruster in various cases were observed with an ICCD camera. It was shown that the plasma behaviors were almost identical between low and high voltage cases in initial several hundred nanoseconds, however, plasma emission with longer duration was observed in higher voltage cases. Canted current sheet structures were also observed in the higher voltage cases using a larger capacitor. With a newly developed torsion-balance type thrust stand, thrust performances of laser assisted PPT could be estimated. The impulse bit and specific impulse linearly increased. On the other hand, coupling coefficient and the thrust efficiency did not increase linearly. The coupling coefficient decreased with energy showing maximum value (20.8 ?Nsec/J) at 0 J, or in a pure laser ablation cases. Thrust efficiency first decreased with energy from 0 to 1.4 J and then increased linearly with energy from 1.4 J to 8.6 J. At 8.65 J operation, impulse bit of 38.1 ?Nsec, specific impulse of 3791 sec, thrust efficiency of 8 %, and coupling coefficient of 4.3 ?Nsec/J were obtained.

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Tuned mass dampers for torsionally coupled systems

  • Pansare, A.P.;Jangid, R.S.
    • Wind and Structures
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    • 제6권1호
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    • pp.23-40
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    • 2003
  • The steady state response of a torsionally coupled system with tuned mass dampers (TMDs) to external wind-induced harmonic excitation is presented. The torsionally coupled system is considered as one-way eccentric system. The eccentricity considered in the system is accidental eccentricity only. The performance of single tuned mass damper (TMD) optimally designed without considering the torsion is investigated for the torsionally coupled system and found that the effectiveness of a single TMD is significantly reduced due to torsion in the system. However, the design of TMD system without considering the torsion is only justified for torsionally stiff systems. Further, the optimum parameters of a single TMD considering the accidental eccentricity are obtained using numerical searching technique for different values of uncoupled torsional to lateral frequency ratio and aspect ratio of the system. The optimally designed single TMD system is found to be less effective for torsionally coupled system in comparison to uncoupled system. This is due to the fact that a torsionally coupled system has two natural frequencies of vibration, as a result, at least two TMDs are required which can control both lateral and torsional response of the system. The optimum damper parameters of different alternate arrangements such as (i) two identical TMDs placed at opposite corners, (ii) two independent TMDs and (iii) four TMDs are evaluated for minimum response of the system. The comparative performance of the above TMDs arrangements is also studied for both torsionally coupled and uncoupled systems. It is found that four TMDs arrangement is quite effective solution for vibration control of torsionally coupled system.

콘테이너선의 수평-비틂연성진동 해석 (Analysis of Coupled Horizontal-Torsional Vibrations of Container Ships)

  • 김극천;김상주
    • 대한조선학회지
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    • 제23권4호
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    • pp.1-10
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    • 1986
  • A container ship, due to wide hatch openings, has characteristics of poor torsional rigidity, strong coupling of horizontal-torsional modes and significant discontinuity in the longitudinal variation of hull sections. In the mathematical formulation of the problem the hull is modeled as a beam and the transfer matrix method is utilized. The cross decks between cargo hatch opening are separated from the main hull and regarded as equivalent springs restraining torsion of hull. The effect of shear deformation of ship-side plating on torsion is taken into account in addition to St. Venant's and bending torsional rigidities. Compatibility requirements at cross section discontinuity are approximately considered. Developing the practical calculation procedure and the computer programs for application to an actual ship, some parametric studies on modeling methods of the cross deck, the compatibility condition, added-mass center etc. are out for the purpose of comparison.

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