• Title/Summary/Keyword: 실험적 모드해석

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Analysis and Design of Dimming Electronic Ballast for a Compact Fluorescent Lamps (컴팩트 형광램프용 조도제어형 전자식 안정기의 설계와 해석)

  • Kim, Jong-Kil;Son, Young-Dae
    • Proceedings of the KIEE Conference
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    • 1999.07f
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    • pp.2792-2794
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    • 1999
  • 본 논문에서는 컴팩트 형광램프용 조도제어형 전자식 안정기의 각 동작 모드별 해석과 설계 및 실험적 고찰을 제시한다. 부스트 컨버터와 해프브리지형 고주파 공진형 인버터를 결합한 일단계 인버터 안정기를 제안하고 그 기본동작 및 특성에 관해 검토한다. 역률을 높이기 위한 방법으로 부스트단에서는 전류불연속 모드로 동작하도록 하였다. 전력 손실을 줄이기 위해 직렬 공진형 인버터는 영전압 영전류 스위칭 방식을 적용하였다. 출력 전압을 조정할 수 있도록 설계하여 조도제어를 구현하였으며 다단계의 조도제어가 가능해진다. 전자식 안정기 시스템을 구성하기 위한 이론적인 근거를 마련하기 위하여 공진형 인버터를 동작 모드별로 해석하고 그 결과를 토대로 동작주파수 및 회로정수를 결정하며, 실제 전자식 안정기를 제작하여 시동특성과 조광특성을 비교 분석하였다. 36W 형광램프에 대한 실험 결과와 등가회로 모델에 의한 Pspice 시뮬레이션 결과를 토대로 제안한 전자식 안정기의 적용가능성을 입증하였다.

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Analysis of the Crankshaft Behavior on In-plane and Out-plane Mode at the Firing Stage (엔진 운전시 크랭크샤프트의 면내.외 모드의 거동 해석)

  • Abu Aminudin;Lee, Hae-Jin;Lee, Jung-Youn;Oh, Jae-Eung
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.16 no.4 s.109
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    • pp.319-328
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    • 2006
  • This paper presents a method for analysis of the mechanical behavior of a crankshaft in a four-cylinder internal combustion engine. The purpose of the analysis was to study the characteristics of the shaft in which the pin and arm parts were assumed to have a uniform section in order to simplify the modal analysis. The results of natural frequency transfer function and mode shape were compared with those obtained by experimental work. The results obtained from the comparison showed a good agreement with each other and consequently verified the analysis model. Furthermore, a prediction of crankshaft characteristics under the firing condition, by using the model, was performed. This study describes a new method for analyzing the dynamic behavior of crankshaft vibrations in the frequency domain based on the initial firing stages. The new method used RMS values to calculate the energy at each bearing journal and counter weight shape modification under the operating conditions.

A Hybrid Resonant Mode Identification using Non-decaying Mode Analysis in Dielectric Loaded Cylindrical Cavity Resonators (비소멸 모드 해석을 이용한 유전체 삽입 원통형 공동 공진기 하이브리드 공진 모드 구분)

  • Lee, Won-Hui;Hur, Jung
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.14 no.6
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    • pp.655-662
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    • 2003
  • A rigorous field analysis by the non-decaying mode and the contour graph method is presented for dielectric-rod loaded cylindrical cavity resonators. Resonant frequencies and the lowest order modes for this resonator are calculated. The mode charts are presented to design the resonators. TE mode(transverse electric or H mode, having no Ez), TM mode(transverse magnetic or I mode, having no ㎐) and HEM mode(hybrid electromagnetic mode, having non-zero Ez and ㎐) are analyzed in detail using non-decaying mode method. The mode charts are completed. The validity of the theory is confirmed by experiments. The results were on the whole satisfactory. Experimental measurements show excellent agrement with the numerical results. The average error of TE, TM, and HEM mode is about 0.20 %, 0.14 %, and 0.28 %, respectively.

A study on heading failure mode for underground excavation in cohesionless soils (비점착성 지반의 지하공간 굴착면 파괴모드에 대한 연구)

  • Shin, Jong-Ho;Kwon, Oh-Yeob;Cho, Jae-Wan;Choi, Min-Gu
    • Journal of Korean Tunnelling and Underground Space Association
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    • v.7 no.3
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    • pp.197-207
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    • 2005
  • Design analysis for underground spaces requires evaluating stability related to heading collapses. A failure mode is one of the critical factors in the conventional methods of stability evaluation. Identification of failure modes is, therefore, essential in securing safe construction. In this study failure modes at the tunnel heading in cohesionless soils are investigated using physical model tests for various tunnel depths and ground surface inclinations. Test results showed that the effect of depth and the inclination of ground surface on a failure mode are of significance. It is identified that, with an increase in depth, failure modes become localized in a region close to tunnel face. It is also known that an increase in the inclination of ground surface results in inclined an d wide failure modes. Numerical simulation of laboratory tests was performed, and shown that the numerical analysis is useful in identifying the heading failure modes, particularly for large underground spaces.

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Experimental and Analytical studies on Failure Behavior of Stud Shear Connectors in CFT Structures (CFT 구조에 적용된 스터드 전단연결재의 파괴 거동에 대한 실험 및 해석적 연구)

  • Lee, Sangyoon
    • Journal of the Society of Disaster Information
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    • v.9 no.4
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    • pp.400-412
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    • 2013
  • For the composite behavior of steel tube and inner concrete, the shear connectors should be applied to the CFT structures. However, the present design codes don't provide the design criteria that can be applied on shear connectors in the CFT structures typically filled with plain concrete. This study has been carried out to propose design criteria (shear strength and resistance factor) for the stud shear connectors in CFT structures. Experimental tests using the push-out specimens with the plain concrete blocks and finite element analysis were conducted for the purpose of verifying the main failure mode to propose the shear strength of studs in CFT structures. From the results of this study, the main failure mode of studs in CFT structures is splitting crack of concrete and this failure mode reduces shear strength of studs in CFT structures relatively to those embedded in RC blocks.

Damage Detection of a Steel Member Using Modal Testing (강부재의 손상발견을 위한 모달실험 기법)

  • Jang, Jeong Hwan;Lee, Jung Whee;Kim, Sung Kon;Chang, Sung Pil
    • Journal of Korean Society of Steel Construction
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    • v.9 no.4 s.33
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    • pp.467-477
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    • 1997
  • A series of experimental tests have been performed on a tube beam in which artificial damage is applied in order to address damage detectability using modal analysis. Modal parameters considered are frequency, displacement mode shape and strain mode shape CoMAC(Coordinate Modal Assurance Criterion) and Modal Vector Error have been adopted for presenting the change of displacement mode shape and strain mode shape. It is revealed strain mode shape is the most sensitive to damage.

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Transmission of Vibration Energy in Box-like Structures (격자형 구조물내의 진동에너지 전파)

  • 김현실;강현주;김재승
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1994.10a
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    • pp.126-131
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    • 1994
  • 본 연구에서는 굽힘파(bending wave)의 전달만 고려하였는데 실제로는 보 및 비틀림 모드도 존재하나 고주파수 대역에서는 굽힘모드가 지배적이며 소음의 발생도 굽힘모드에 의해 주로 발생하므로 보 및 비틀림모드의 생략이 큰 오차를 가져오지는 않는다. 테스트 모델에 대해 실험을 수행하여 결과를 비교하였다. 또한 구조물의 고주파수 진동소음 해석방법으로 널리 쓰이는 통계적 에너지 해석법(SEA)을 이용한 결과와 비교하였다.

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Modal Analysis of Wind Turbine Blade Using Optical-Fiber Bragg-Grating Sensors (광섬유 브레그격자 센서를 이용한 풍력발전기 날개의 모드 해석)

  • Kim, Chang-Hwan;Paek, In-Su;Yoo, Neung-Soo;Nam, Yoon-Su
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.5
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    • pp.513-516
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    • 2011
  • The dynamic behavior of a small wind-turbine blade was analyzed experimentally. Arrays of fiber Bragg-Grating (FBG) sensors attached along the blade were used to measure the strains of the blade surface. An impact test was performed to estimate the resonance frequencies of the fundamental and higher modes of the cantilever blade system developed for this study. The results were similar to the results for conventional strain gages. However, FBG sensors could sense modes that strain gauges could not sense. The strains obtained from the FBG sensor array were used to estimate displacement-mode shapes of the blade.

외부하중을 고려한 추진기관 연소관의 구조 해석

  • 구송회;이방업;조원만;이환규
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1995.11a
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    • pp.159-167
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    • 1995
  • 본 연구는 유도탄 비행시험시에 연소관의 스커트와 날개 장착용 브라켓에 작용하는 공력하중과 연소관에 내압이 동시에 작용하는 추진기관에 대하여 구조 해석하였다. 추진기관의 스커트부 및 브라켓부의 공력하중은 3차원적으로 작용하기 때문에 대칭성을 이용한 $180^{\circ}C$3차원 구조 해석을 수행하여 비행시험, 수압시험, 지상시험 모드에 대하여 응력 수준을 비교하였다. 해석 결과 3가지 모드의 최대 등가응력은 거의 같으며, 비행시험시 공력하중이 앞마개부에 미치는 영향은 최대 등 가응력의 6%이내로 상당히 작았다. 수압시험 모드와 지상시험 모드의 실험치와 해석치를 비교한 결과 정확한 해석을 위해서는 점화기를 모델링과 점화기와 연소관, 브라켓과 연소관에 접촉요소의 적용, 3차원 비선형 해석등 보다 상세한 해석이 필요함을 알 수 있었다.

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