• 제목/요약/키워드: Component Vibration Test

검색결과 168건 처리시간 0.027초

선내 탑재된 소음기 성능평가 방법에 관한 연구 (A Study on Silencer Performance Assessment under Onboard Condition)

  • 이도경;진봉만;이철원;김노성;최수현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.731-736
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    • 2004
  • The exhaust noise of auxiliary engine in ships is directly transmitted to bridge wing with only distance attenuation. It is not easy to find out practical treatment to be applied between exhaust pipe and bridge wing to reduce the transmission of the exhaust noise. In general, therefore, a silencer is fitted to reduce the exhaust noise and correspondingly noise of bridge wing. The silencer should be properly designed under the consideration of the frequency component of the exhaust noise and the required performance such as noise reduction or insertion loss. In general, the gas inside the exhaust pipe flows with high temperature and speed and thus onboard test condition is more adverse than the standard atmospheric condition. In this study, the test method to evaluate silencer performance using a probe microphone is introduced.

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터널 내 열차주행으로 인한 지반진동 현장측정시험 (Field Tests Investigating the Ground Borne Vibration Induced by Underground Railway Tunnel)

  • 안상권;방은석;이배
    • 한국철도학회논문집
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    • 제13권2호
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    • pp.208-213
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    • 2010
  • 최근 수도권광역급행철도(GTX)사업이 승인됨에 따라, 도심지 터널 내 열차주행에 따른 진동의 영향에 대한 관심이 커지고 있다. 본 논문은 암반층에 건설된 터널 내 열차주행으로 인한 지반진동을 측정하기 위해 실시된 현장측정시험의 과정 및 결과에 대해 기술한다. 약 200km/hr로 주행하는 KTX열차로 인해 발생된 지반의 진동이 터널 인근에 시공된 시추공에 삽입된 3축 시추공 진동 측정장치를 통해 측정되었다. 본 논문은 현재 상용화되어 있는 시추공 진동 측정장치의 한계에 대해서도 논의한다.

터빈 블레이드 진단을 위한 회전기계 마찰 진동에 관한 연구 (Study on Rub Vibration of Rotary Machine for Turbine Blade Diagnosis)

  • 유현탁;안병현;이종명;하정민;최병근
    • 한국소음진동공학회논문집
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    • 제26권6_spc호
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    • pp.714-720
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    • 2016
  • Rubbing and misalignment are the most usual faults that occurs in rotating machinery and with them severe effect on power plant availability. Especially blade rubbing is hard to detect on FFT spectrum using the vibration signal. In this paper, the possibility of feature analysis of vibration signal is confirmed under blade rubbing and misalignment condition. And the lab-scale rotor test device provides the blade rubbing and shaft misalignment modes. Feature selection based on GA (genetic algorithm) is processed by the extracted feature of the time domain. Then, classification of the features is analyzed by using SVM (support vector machine) which is one of the machine learning algorithm. The results of features selection based on GA compared with those based on PCA (principal component analysis). According to the results, the possibility of feature analysis is confirmed. Therefore, blade rubbing and shaft misalignment can be diagnosed by feature of vibration signal.

과학기술위성 반작용휠의 미소진동 측정 및 분석 (STSAT RWA Micro-Vibration Test and Analysis)

  • 오시환;남명용;박연묵;임조령;금정훈;이승우
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.695-698
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    • 2004
  • STSAT RWA (Reaction Wheel Assembly) micro-vibration is measured using KISTLER dynamic plate that can provide the time signals of three orthogonal forces and torques simultaneously up to 400Hz. In the post-processing, measured data are evaluated with respect to the wheel spin rate in both time and frequency domains, and the static/dynamic unbalances are evaluated from the extracted first harmonic component. Also the friction torque profile at each wheel speed is estimated from the measured data. Several higher order harmonic components are observed, that comes from its rotor shape as well as the wheel bearing characteristics. One of the most peculiar characteristics of this wheel is that the dynamic properties of two radial unbalance components are much different from each other as the RWA mounting configuration on a spacecraft is different from conventional RWA mounting configuration. Rocking mode is not appeared below 400Hz for all operating speed because the wheel size is very small. The post-processed results will be used for jitter analysis of STSAT due to RWA micro-vibration.

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Acoustic mode 를 고려한 공동주택 중량충격음 소음해석 (The numerical analysis of heavy-weight impact noise for an apartment houses considering acoustic mode)

  • 문대호;황재승;박홍근;홍건호;임주혁
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2009년도 춘계학술대회 논문집
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    • pp.394-402
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    • 2009
  • To investigate the heavy-weight impact noise of apartment houses, numerical analysis was performed. The analysis acoustic pressure consider acoustic mode by finite element method. The variables considered effecting on the acoustic pressure are the Acoustic mode, acoustic damping, and the impulse load. The heavy-weight impact noise is a changeable value in the room. Since the most part of the frequency component of heavy-weight impact noise has low frequency. The noise in low frequency is related to the vibration of structure, the reflection of acoustic wave caused by wall and the standing wave called by acoustic mode. The prediction by the numerical analysis was verified with test result of the heavy weight-impact noise at apartment houses.

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다축 제어용 가진기의 구동소프트웨어 개발 및 보정에 관한 연구 (A Study on Operational Software Development and Calibration of Multi-Axis Vibration Testing Device)

  • 정상화;김재열;류신호
    • 한국자동차공학회논문집
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    • 제9권2호
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    • pp.143-151
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    • 2001
  • In the recent day, fatigue life prediction techniques play a major role in the design of components in the ground vehicle industry. Full scale durability testing in the laboratory is an essential of any fatigue life evaluation of components or structure of the automotive vehicle. Component testing is particularly important in todey's highly competitive industries where the design to reduce weight and production costs must be balanced with the necessity to avoid expensive service failure. Generally, Multi-axis durability testing device is used to carry out the fatigue test. In this paper, The operation software for simultaneously driving Multi-axis vibration testing device is developed and the input and output data are displayed in windows of PC controller with real time. Moteover the characteristics of the displacement and the load of Multi-axis actuators are calibrated separately.

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Modeling and testing for hydraulic shock regarding a valve-less electro-hydraulic servo steering device for ships

  • Jian, Liao;Lin, He;Rongwu, Xu
    • International Journal of Fluid Machinery and Systems
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    • 제8권4호
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    • pp.318-326
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    • 2015
  • A valve-less electro-hydraulic servo steering device (short: VSSD) for ships was chosen as a study object, and its mathematic model of hydraulic shock was established on the basis of flow properties and force balance of each component. The influence of system structure parameters, changing rate of motor speed and external load on hydraulic shock strength was simulated by the method of numerical simulation. Experiment was designed to test the hydraulic shock mathematic model of VSSD. Experiment results verified the correctness of the model, and the model provided a correct theoretical method for the calculation and control of hydraulic shock of valve-less electro-hydraulic servo steering device.

다단 왕복동 공기압축기의 평형추 설계 (Counter Weight Design of Multi-stage Reciprocating Air Compressors)

  • 김영철;김병옥;신현익
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.656-661
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    • 2003
  • Modem reciprocating air compressors have tendency to a multi-stage W-type or V-type cylinder arrangement for the purpose of high outlet pressure, compactness and low vibration and noise. A valid counter weight calculation method using the complex expression is proposed for reducing the inertia forces of the compressor. Counter weight removes only 1st forward whirl component. Counter weight formulations are applied to the six various compressor structures which are (a) 1 cylinder single-throw crank shaft, (b) 2 cylinder single-throw crank shaft (c) 2 cylinder double-throw clank shaft, (d) 3 cylinder single-throw crank shaft, (e) 4 cylinder single-throw crank shaft and (f) 4 cylinder double-throw crank shaft. The improvement of performance is verified through available vibration test.

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고발사율 대공포 발사에 따른 체계자세 연구 (The System Position from High Firing Rate of Anti-Aircraft Gun system)

  • 황부일;이부환;김치환
    • 대한기계학회논문집A
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    • 제39권6호
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    • pp.611-615
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    • 2015
  • 비행기 방어용 대공포는 저고도 방어체계로 사용되고 있으며, 방어능력 극대화를 위해 대부분 고발사율 대공포를 두개 이상 탑재하여 교전 시 명중률을 높이고 있다. 고 발사율 대공포의 경우, 포열진동 및 탄의 불균형 분산은 정확한 조준사격 및 명중률에 아주 결정적인 영향을 미치게 된다. 따라서 사격 진동 및 충격량을 감소하는 구조는 대공포 체계에서는 주요 설계 대상이다. 본 연구에서는 차량의 현가장치 특성에 따라 고발사율 대공포 체계에서 발사시스템의 진동충격으로부터 차단하는 능력을 향상시키고, Recurdyn 과 Adams 를 이용한 동적 거동해석과 실 사격 시험결과를 비교하여 명중률에 영향을 미치는 현가 형태, 위치 및 수량에 따른 체계 자세 흔들림을 예측하였다. 본 연구를 통하여 대공포에 적합한 현가장치와 포 스프링 등과 같은 구성품을 선정할 수 있는 기초연구를 수행하였다.

실험에 의한 방진고무의 동특성에 관한 연구 (An Experimental Study on the Dynamic Characteristics of Rubber Isolator)

  • 김완두;김기세;권재도;우창수
    • Elastomers and Composites
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    • 제37권3호
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    • pp.183-191
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    • 2002
  • 우수한 신장성과 탄성복원 능력으로 여러 산업분야에 방진, 제진, 충격흡수 및 완충재료로 널리 사용되고 있는 고무재료에 대하여 주파수, 변형률 진폭 및 온도변화가 동특성에 미치는 영향을 실험을 통하여 검토하였다. 동특성 시험은 5종류의 경도에 대하여 인장.압축시험과 전단시험용의 천연고무 시험 편으로 비 공진법으로 수행하였다. 시험결과, 경도가 높을수록 동적 특성 값들이 크게 나타났으며 저장탄성계수와 손실계수는 주파수가 증가할수록 서서히 증가하였으며 변형률 진폭이 커질수록 감소하였다. 또한, 온도 특성을 $-50^{\circ}C$ 영역에서 저장탄성계수가 급격히 상승하며 손실계수가 최대로 나타나는 전이역임을 알 수 있었다.