• Title/Summary/Keyword: 강성의 주기성

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Evaluation of Capacity Spectrum Methods for Estimating the Peak Inelastic Responses (최대 비탄성 변위 응답 예측을 위한 기존 능력스펙트럼법들의 유효성 평가 및 비교)

  • 김홍진;민경원;이상현;박민규
    • Journal of the Earthquake Engineering Society of Korea
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    • v.8 no.2
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    • pp.35-44
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    • 2004
  • In the capacity spectrum method(CSM) using a linear response spectrum, the peak response of an inelastic system under a given earthquake load is estimated transforming the system into the equivalent elastic one. The CSM for estimating the peak inelastic response is evaluated in this paper. The equivalent period and damping ratio are calculated using the ATC-40, G lkan, Kowalsky, and Iwan methods, and the performance points are obtained according to the procedure B of ATC-40. Analysis results indicate that the ATC-40 method generally underestimates the peak response resulting in the unsafe design, while the G lkan and Kowalsky methods overestimate the responses. The Iwan method produces the values between those by the ATC-40 method and the G lkan and Kowalsky methods, and estimates the responses relatively closer to the exact ones. Further, it is found that the Kowalsky method gives the negative equivalent damping ratios depending on the hardening ratios, and thereby can not be used to estimate the responses in some cases.

Seismic Performance Evaluation of Complex-Shaped Tall Buildings by Lateral Resisting Systems (횡력저항시스템에 따른 비정형 초고층건물 내진성능평가)

  • Youn, Wu-Seok;Lee, Dong-Hun;Cho, Chang-Hee;Kim, Eun-Seong;Lee, Dong-Chul;Kim, Jong-Ho
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.25 no.6
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    • pp.513-523
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    • 2012
  • The objective of this research is to examine how the lateral resisting system of selected prototypes are affected by seismic zone effect and shape irregularity on its seismic performance. The lateral resisting systems are divided into the three types, diagrid, braced tube, and outrigger system. The prototype models were assumed to be located in LA, a high-seismicity region, and in Boston, a low-seismicity region. The shape irregularity was classified with rotated angle of plane, $0^{\circ}$, $1^{\circ}$, $2^{\circ}$. This study performed two parts of analyses, Linear Response and Non-Linear Response History(NLRH) analysis. The Linear Response analysis was used to check the displacement at the top and natural period of models. NLRH analysis was conducted to invest base shear and story drift ratio of buildings. As results, the displacement of roof and natural period of three structural systems increase as the building stiffness reduces due to the changes in rotation angle of the plane. Also, the base shear is diminished by the same reason. The result of NLRH, the story drift ratio, that was subject to Maximum Considered Earthquake(MCE) satisfied 0.045, a recommended limit according to Tall Building Initiative(TBI).

A Comparative Study on the Economics of Reprocessing and Direct Disposal of Nuclear Spent Fuel (사용후 핵연료의 제처리와 직접 처분의 경제성 비교 연구)

  • Kang, Seong-Ku;Song, Jong-Soon
    • Journal of Radiation Protection and Research
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    • v.25 no.2
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    • pp.89-96
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    • 2000
  • Nuclear fuel cycle choices and costs are important in considering energy policies, fuel diversity, security of supply and associated social and environmental impacts. Particularly, the nuclear spent fuel is very important in view of high activity and the need of long term management. This study focuses on the comparison of reprocessing and direct disposal of nuclear spent fuel in terms of cost, safety and public acceptability. The results of the study show that the direct disposal is about 7% more economical than the reprocessing. In terms of safety, the results show that the risk of vitrified HLW (high-level radioactive waste) is less than directly disposed spent fuel. For the public acceptability, both of the methods are not well understood and therefore they are not accepted. In conclusion, it is necessary to guarantee the safety of the both spent fuel processing methods through continuous development of associated technology and to have a fuel cycle policy which should consider not only the economics but also social and environmental impacts.

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Design and Analysis of Pseudorandom Number Generators Based on Programmable Maximum Length CA (프로그램 가능 최대길이 CA기반 의사난수열 생성기의 설계와 분석)

  • Choi, Un-Sook;Cho, Sung-Jin;Kim, Han-Doo;Kang, Sung-Won
    • The Journal of the Korea institute of electronic communication sciences
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    • v.15 no.2
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    • pp.319-326
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    • 2020
  • PRNGs(Pseudorandom number generators) are essential for generating encryption keys for to secure online communication. A bitstream generated by the PRNG must be generated at high speed to encrypt the big data effectively in a symmetric key cryptosystem and should ensure the randomness of the level to pass through the several statistical tests. CA(Cellular Automata) based PRNGs are known to be easy to implement in hardware and to have better randomness than LFSR based PRNGs. In this paper, we design PRNGs based on PMLCA(Programable Maximum Length CA) that can generate effective key sequences in symmetric key cryptosystem. The proposed PRNGs generate bit streams through nonlinear control method. First, we design a PRNG based on an (m,n)-cell PMLCA ℙ with a single complement vector that produces linear sequences with the long period and analyze the period and the generating polynomial of ℙ. Next, we design an (m,n)-cell PC-MLCA based PRNG with two complement vectors that have the same period as ℙ and generate nonlinear sequences, and analyze the location of outputting the nonlinear sequence.

Non-linear Shimmy Analysis of a Nose Landing Gear with Free-play (유격을 고려한 노즈 랜딩기어의 비선형 쉬미 해석)

  • Yi, Mi-Seon;Hwang, Jae-Up;Bae, Jae-Sung;Hwang, Jae-Hyuk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.10
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    • pp.973-978
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    • 2010
  • In this paper, we studied the shimmy phenomena of an aircraft nose landing gear considering free-play. Shimmy is a self-excited vibration in lateral and torsional directions of a landing gear during either the take-off or landing. This phenomena is caused by a couple of conditions such as low torsional stiffness of the strut, friction and free-play in the gear, wheel imbalance, or worn parts, and it may make an aircraft unstable. Free-play non-linearity is linearized by the described function for a stability analysis in a frequency domain, and time marching is performed using the fourth-order Runge-Kutta method. We performed the numerical simulation of the nose landing gear shimmy and investigated its linear and nonlinear characteristics. From the numerical results, we found limit-cycle-oscillations at the speed under linear shimmy speed for the case considering free-play and it can be concluded that the shimmy stability can be decreased by free-play.

Parametric Design of Contact-Free Transportation System Using The Repulsive Electrodynamic Wheels (반발식 동전기 휠을 이용한 비접촉 반송 시스템의 변수 설계)

  • Jung, Kwang Suk
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.17 no.3
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    • pp.310-316
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    • 2016
  • We propose a novel contact-free transportation system in which an axial electrodynamic wheel is applied as an actuator. When the electrodynamic wheel is partially overlapped by a fixed conductive plate and rotates over it, three-axis magnetic forces are generated on the wheel. Among these forces, those in the gravitational direction and the lateral direction are inherently stable. Therefore, only the force in the longitudinal direction needs to be controlled to guarantee spatial stability of the wheel. The electrodynamic wheel consists of permanent magnets that are repeated and polarized periodically along the circumferential direction. The basic geometric configuration and the pole number of the wheel influence the stability margin of a transportation system, which would include several wheels. The overlap region between the wheel and the conductive plate is a dominant factor affecting the stiffness in the lateral direction. Therefore, sensitivity analysis for the major parameters of the wheel mechanism was performed using a finite element tool. The system was manufactured based on the obtained design values, and the passive stability of a moving object with the wheels was verified experimentally.

Hydroelastic Responses for a Very Large Floating Structure with a Breakwater (방파제를 고려한 초대형 부유식 해양구조물의 응답)

  • H.Y. Lee;H. Shin;C.G. Lim;O.H. Kim;J.M. Kang;M.C. Yoon
    • Journal of the Society of Naval Architects of Korea
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    • v.38 no.2
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    • pp.26-32
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    • 2001
  • In this paper, elastic responses of a floating structure in waves with a breakwater are presented. The method of source-dipole distribution is used to analyze the velocity potentials for the fluid region. The deflections of structure are expanded approximately in terms of natural mode functions of free-free beam. The model for present calculation is a floating plate with an length of 1000m and the hydroelastic responses for a floating structure with a straight breakwater are shown. The effects of distance between breakwater and structure, bending rigidity and relative length of regular waves are examined.

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Finite Element Vibration Analysis of Structures with Cyclic Symmetry using Discrete Fourier Transform (이산푸리에 변환을 이용한 순환대칭 구조물의 유한요소 진동 해석)

  • 김창부;김정락
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1995.10a
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    • pp.221-226
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    • 1995
  • 터빈 익렬, 펌프 익차, 원형 냉각탑, 치차 등과 같이 동일한 형상이 원주 방향으로 반복되어 있는 순환 대칭 구조물의 진동특성을 유한 요소법을 사용하여 해석하는 경우에 전체구조를 모델링하는 대신에 구조물을 동일한 형상의 부분구조로 분할하여 부분구조 한개만을 모델링하고 분할된 경계에서 적절한 경계조건을 부과하여 진동해석을 수행함으로서 컴퓨터 기억용량을 절감시키고 계산시간을 단축할 수 있는 방법이 널리 사용되고 있다. Orris and Petyt[1]는 부분구조의 양쪽 분할 경계면, 즉 연결 경계상에 있는 절점변위의 상관관계를 복소파동전파식을 이용해서 구하여 부분구조의 감소된 복소강성행렬 및 질량행렬을 만들고 실수부와 허수부를 분리하여 유한요소해석을 수행하는 방법을 제안하였다. 유한요소 프로그램 ANSYS[2]에서는 이와 같은 방법을 사용하고 있다. Thomas[3]는 순회 정규모드를 이용하였고, 참고문헌[4]에서는 순회행렬을 이용하였다. 또한 유한요소 프로그램 MSC/NASTRAN[5]에서는 푸리에 급수를 이용하고 유한요소 절점의 위치 및 변위를 원통 좌표계를 표현하여 순환대칭구조물의 유한요소해석을 수행할 수 있도록 되어있다. 본 논문에서는 순환 대칭구조물의 형상의 주기성과 순환성을 고려하여 이산퓨리에 변환을 이용함으로써 순환대칭구조물의 유한요소진동해석을 체계적으로 저용량의 컴퓨터에서 신속하고 정확하게 수행할 수 있는 방법을 제안하고자 한다.

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On the Vibration Control of Ship (선박진동 제어기술에 관한 소고)

  • 이호섭
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1996.04a
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    • pp.11-21
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    • 1996
  • 선박은 화물 및 여객을 수송하는 해상교통 수단으로써 여객 및 승무원의 안락성, 탑재장비, 기기의 성능 보전 상, 화물 및 구조부재의 안전성 차원에서 진동제어가 주요 해결 기술의 하나이다. 또한 최근 선박의 대형화, 고속화로 인해 엔진과 프로펠러의 기진력은 커지는데 반해 구조 강도계산 기술의 발달로 인해 선체구조 경량화가 촉진되어 선체의 유연성이 커질 뿐 아니라 전통적인 선체 구조와 기관, 축계 강성사이의 균형이 깨어짐으로 선박의 진동제어는 더욱 중요시 되고 있다. 선박의 경우 건조 후에 진동제어를 위한 조치를 취하는 일은 매우 제한적이고 많은 비용이 들기 때문에 설계단게에서 선박진동제어를 위한 사전 노력이 충분히 이루어지는 것이 중요하다. 따라서 선박의 주 기진원인 프로펠러, 주기관 등의 기진력 자체를 적정화하는 노력과 함께 그로 인한 응답을 극소화하기 위해 설계 단계부터 인도까지 단게별로 많은 노력을 기울이고 있다. 단계별 진동제어의 한 예를 Fig.1에서 보여주고 있다[1]. 선체와 같이 복잡한 대형구조물의 진동특성 및 응답을 계산함에 있어서 컴퓨터의 발달과 유한요소법과 같은 해석기술의 발달로 실제 구조와 매우 유사한 3차원 모델링이 가능하게 되어 해석의 정도를 높일 수 있게 되었다. 그러나 프로펠러 기진력, 유체와의 연성효과, 감쇠특성 등을 정도 높게 산정하는 데는 아직도 많은 어려움이 있다. 이와같은 문제는 진동응답의 계산정도를 저하시키는 주요 요인이 되어 설게단계에서 충분히 진동 제어가 이루어졌다 하더라도 건조 후 실제운항 시 진동문제가 발생되는 경우가 있다. 건조 후 진동문제 발생시 구조변경을 통한 해결은 한계가 있기 때문에 각종 진동제어 장치의 연구개발이 최근에 활발히 이루어지고 있다[2]. 본 고에서는 설계단계에서부터 건조 후까지의 선박진동제어 과정[1,2,5,6]을 단계별로 고찰하여, 점점 까다로워져 가는 선박 진동규제[3,4]에 대처하고 승무원의 안락성에 대한 욕구, 구조물의 안전성, 장비의 성능보존이 만족되는 저진동 선박의 건조를 위해 향후 해결해야할 과제들을 도출하여 선박진동분야이 연구개발 방향을 제시하고자 한다.

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Dynamic response of segment lining due to train-induced vibration (세그먼트 라이닝의 열차 진동하중에 대한 동적 응답특성)

  • Gyeong-Ju Yi;Ki-Il Song
    • Journal of Korean Tunnelling and Underground Space Association
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    • v.25 no.4
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    • pp.305-330
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    • 2023
  • Unlike NATM tunnels, Shield TBM tunnels have split linings. Therefore, the stress distribution of the lining is different even if the lining is under the same load. Representative methods for analyzing the stress generated in lining in Shield TBM tunnels include Non-joint Mode that does not consider connections and a 2-ring beam-spring model that considers ring-to-ring joints and segment connections. This study is an analysis method by Break-joint Mode. However, we do not consider the structural role of segment lining connections. The effectiveness of the modeling is verified by analyzing behavioral characteristics against vibration loads by modeling with segment connection interfaces to which vertical stiffness and shear stiffness, which are friction components, are applied. Unlike the Non-joint mode, where the greatest stress occurs on the crown for static loads such as earth pressure, the stress distribution caused by contact between segment lining and friction stiffness produced the smallest stress in the crown key segment where segment connections were concentrated. The stress distribution was clearly distinguished based on segment connections. The results of static analysis by earth pressure, etc., produced up to seven times the stress generated in Non-joint mode compared to the stress generated by Break-joint Mode. This result is consistent with the stress distribution pattern of the 2-ring beam-spring model. However, as for the stress value for the train vibration load, the stress of Break-joint Mode was greater than that of Non-joint mode. This is a different result from the static mechanics concept that a segment ring consisting of a combination of short members is integrated in the circumferential direction, resulting in a smaller stress than Non-joint mode with a relatively longer member length.