• 제목/요약/키워드: lever ratio

검색결과 32건 처리시간 0.022초

레버형 질량동조감쇠기에 의한 진동제어 (Vibration Control by Lever-type Tuned Mass Damper)

  • 심철권;은희창;김진봉
    • 대한건축학회논문집:구조계
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    • 제34권12호
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    • pp.27-34
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    • 2018
  • This paper considers the seismic performance of lever-type tuned mass damper(TMD). The lever-type TMD is designed utilizing the seismic-performance of TMD and the control force required for constraining story drift. The TMD is basically designed by tuning the frequency of primary structure. Thus, the TMD plays an important role to reduce the dynamic responses. The lever-type TMD has a merit to control more displacement responses than the existing TMD due to the control forces. It is shown that the optimum design of lever-type TMD is affected by the ratio of the TMD mass with respect to the mass of the primary structure, the damping ration of the primary structure, and the length ratio of the lever. A numerical example exhibits the effectiveness of the dynamic control by the lever-type TMD and its validity is illustrated in a three-story building structure subjected to earthquake.

레버형 반공진 진동 절연기의 진동 특성 연구 (Study on Performances of the Lever Type Anti-resonance Vibration Isolator)

  • 윤종환;김기우;이형일
    • 한국소음진동공학회논문집
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    • 제26권2호
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    • pp.187-194
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    • 2016
  • Parametric study on the lever type dynamic anti-resonance vibration isolator (DAVI) is executed to introduce the system in the path of vibration transmission for the vibratory response attenuation. The effects of inertia and location of the lever on the system performances are investigated using FEA. The effects of other parameters such as ratio of lever lengths, ratio of masses and the location of pivot are studied with analytical approach. According to the results, all the parameters except lever location affect the system response in their own ways. Consequently, the optimal lever type DAVI for translational or rotational system can be efficiently designed by selecting system parameters using the procedure introduced in this study.

정밀 스테이지에서 출력변위 확대를 위한 레버의 해석 (Theoretical Analysis of Levers in a Precision Stage for Large Displacement)

  • 황은주;민경석;송신형;최우천
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2004년도 추계학술대회 논문집
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    • pp.720-723
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    • 2004
  • Lever mechanisms are usually employed to enlarge output displacement in precision stages. In this study, theoretical analysis of a lever is presented including bending effect and relation between dimension parameters and an objective function. The objective function is chosen as multiplication of magnification ratio and forcedisplacement transmission. Through theoretical analysis, this study presents optimal values for the parameters and the analysis is verified by finite element method.

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지렛대 원리를 활용한 선분의 비에 관련된 도형 문제의 해결에 대한 연구 (A Study on Solving Geometry Problems related with the Ratio of Segments Using the Principle of the Lever)

  • 한인기;홍동화
    • 한국수학교육학회지시리즈E:수학교육논문집
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    • 제20권4호
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    • pp.621-634
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    • 2006
  • In this study we describe the characteristics of solving geometry problems related with the ratio of segments using the principle of the lever and the center of gravity, compare and analyze this problem solving method with the traditional Euclidean proof method and the analytic method.

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초정밀 나노 스테이지에서의 다중 변위 확대 기구 해석 (Analysis of Multiple Displacement Magnification Mechanism in Ultraprecision Nano Stage)

  • 민경석;최우천
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 춘계학술대회 논문집
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    • pp.1273-1276
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    • 2005
  • A displacement magnification mechanism is usually employed in a nano-positioning stage to achieve a large stage motion. A lever mechanism is the most widely used displacement magnifying mechanism. For more large stage motion, double or multiple lever mechanisms can be used. In this case, a more accurate analysis model is needed. This study proposes a more reasonable analysis model for a multiple lever mechanism based on the single lever mechanism model. This paper describes that the high equivalent stiffness of the lever is the most important factor reducing the magnification ratio of the lever mechanism through increasing the deflection of the link and including the axial displacement of the pivot.

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유연 힌지 구조의 스테이지 구동범위 확대를 위한 힌지의 목두께 해석 (Analysis of Flexure Hinge Neck Thickness of a Lever in Ultra Precision Stages of a Long Travel Range)

  • 황은주;민경석;송신형;최우천
    • 한국정밀공학회지
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    • 제22권5호
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    • pp.121-129
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    • 2005
  • Lever mechanisms are usually employed to enlarge output displacements in precision stages. In this study, theoretical analysis is done for a precision stage employing a lever and flexure hinges, including bending effect. This study presented relations between design parameters and magnification ratio. This study presents optimal values for the parameters to achieve a longer stage displacement. The analysis is verified by finite element analysis. It is found that adjusting stiffnesses can increase the travel range significantly.

Amplitude Modulation Response and Linearity Improvement of Directly Modulated Lasers Using Ultra-Strong Injection-Locked Gain-Lever Distributed Bragg Reflector Lasers

  • Sung, Hyuk-Kee;Wu, Ming C
    • Journal of the Optical Society of Korea
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    • 제12권4호
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    • pp.303-308
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    • 2008
  • Directly modulated fiber-optic links generally suffer higher link loss and larger signal distortion than externally modulated links. These result from the electron-photon conversion loss and laser modulation dynamics. As a method to overcome the drawbacks, we have experimentally demonstrated the RF performance of directly modulated, ultra-strong injection-locked gain-lever distributed Bragg reflector (DBR) lasers. The free-running DBR lasers exhibit an improved amplitude modulation efficiency of 12.4 dB under gain-lever modulation at the expense of linearity. By combining gain-lever modulation with ultra-strong optical injection locking, we can gain the benefits of both improved modulation efficiency from the gain-lever effect, plus improved linearity from injection locking. Using an injection ratio of R=11 dB, a 23.4-dB improvement in amplitude response and an 18-dB improvement in spurious-free dynamic range have been achieved.

아르키메데스 '방법'에 대한 새로운 해석 (The New Interpretation of Archimedes' 'method')

  • 박선용
    • 한국수학사학회지
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    • 제23권4호
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    • pp.47-58
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    • 2010
  • 이 연구에서는 고대 수학자 아르키메데스의 '방법'에 대한 새로운 해석을 제시한다. 이를 위해, 우선 그 '방법'의 해석과 관련된 핵심 쟁점을 살펴보고 논쟁의 중심에 불가분량과 지레의 원리가 있지만 그 사이의 관계가 규명되지 않았음을 확인한다. 그리고 아르키메데스의 신중한 불가분량 사용에 대해 수학사에 근거한 탐색적 추측활동을 수행함으로써, 아르키메데스 '방법'에 있어 지레의 원리의 핵심적 역할이 변화율의 통제라는 가설을 제안한다.

유연 힌지를 이용한 이중레버 시스템의 변위증폭 메카니즘에 관한 연구 (A Study on the Displacement Magnification Mechanism of Two-Lever System using Flexure Hinge)

  • 제원수;예상돈;민병현
    • 한국기계가공학회지
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    • 제7권2호
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    • pp.60-65
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    • 2008
  • The high-technology industries including a semi-conductor and an information communication need an ultra-precision technology from the technological points of view. Nano technology based on an ultra-precision technology is being studied to overcome the delicate technology that may occur in the semi-conductor fields. Then, the transferring equipment with high resolution and long displacement becomes an important technology. The goal of this study is to analyze the displacement magnification mechanism driven by piezoelectric actuator which has high resolution and fast response characteristics using flexure hinge with the merits of soft displacement, negligible back-lash and stick-slip, and no-lubrication. The analyses to reduce the magnification losses occurred during the magnification process are performed using ANSYS software based on FEM. The five design variables such as arm thickness, thickness of hinge, radius of hinge, length of input side at the 1st lever and magnification ratio of 1st lever are optimized to induce the maximum magnification ratio using Taguchi method.

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비행시험을 통한 엔진의 혼합기레버 위치 설정에 관한 연구 (A Study on Determination for Mixture Lever's Position by Flight Test)

  • 김진곤;김칠영;이정모;이정훈
    • 한국항공운항학회지
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    • 제3권1호
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    • pp.37-47
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    • 1995
  • It is very important to determine the performance and operating envelope of engine for aircraft's flight. The basic performance is provided by manufacturer, but installed engine's operating envelop is only determined by flight test. First, this study was measured cylinder head temperature(CHT), exhaust gas temperature(EGT) and oil temperature. At pre-determined altitude and power rate, these temperatures were measured by change of mixture ratio and mixture ratio condition for economic operation and max. power were found. And secondly, with the measured temperatures, possible positions of mixture lever were determined by flight test for stable flight Chang-91 and Lycoming IO-360-A series four cylinders engine with 200 hp was used for this study.

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