• 제목/요약/키워드: Vibration Test & Analysis

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정지궤도위성 진동시험을 위한 가진 시스템 검증 (Verification of Vibration Test System for Geostationary Satellite)

  • 임종민;문상무;은희광;문남진;이동우;문귀원
    • 항공우주기술
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    • 제9권2호
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    • pp.143-152
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    • 2010
  • 우리나라 최초의 정지궤도위성 개발을 위하여 발사 시 발생하는 진동환경을 지상에서 구현하기 위한 전체 시스템 구축 및 검증이 요청되었다. 정지궤도위성은 기존 개발 위성대비 중량이 대폭 증가하여 수직 가진시스템의 경우, 신규 가진시스템 개발이 필요하였다. 수평 가진시스템은 고정용 치구와 슬립테이블의 열특성 차이에 따른 확인 및 수평방향 가진 시스템의 모멘트 성능 검증이 요청되었다. 또한 데이터 습득 요구 채널의 증가로 인하여 신규로 제어 및 습득 시스템을 구축하였다. 본 연구에서는 진동환경 시스템 전체에 대한 검증 과정 및 안정성 향상을 위해 적용한 여러 기법들을 소개하고자 한다.

복합재료 위성안테나의 진동시험을 위한 구조 동해석 (Dynamic Analysis of Composite Satellite Antenna Structure for Sine Vibration Test)

  • 송운형;권상룡;송광호;류시융;한재흥
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 춘계학술발표대회 논문집
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    • pp.119-122
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    • 2002
  • 인공위성 발사 시 안테나를 비롯한 탑재체는 극심한 진동을 경험하게 된다. 따라서 공진에 의한 구조물의 파손을 방지하기 위해 지상 인증시험을 수행하게 되며, 이를 위하여 구조 동해석을 통해 인증시험에 적용되는 적정 하중값을 결정하는 과정이 선행된다. 본 논문에서는 복합재료로 이루어진 Ka 대역 안테나 구조물의 동해석을 위하여 자유진동해석과 정현파 진동해석을 수행하고, 그 결과로서 진동시험 시 구조물의 인증시험에 요구되는 적정 하중값을 노칭기법을 이용하여 산출하였다.

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FIV 시험루프의 유동기인 진동 신호분석 (Flow-Induced Vibration Signal Analysis of the FIV Test Loop)

  • 이강희;강흥석;윤경호;송기남
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.601-606
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    • 2004
  • Vibration spectrums of the test loop according to flow conditions were analyzed in order to identify the sources of vibration at peak frequencies. While a flow condition of the sweep test was changed by varying pump rotational speed from 450 rpm to 1500 rpm by the step 150 rpm, midspan acceleration of the test section in width-direction and dynamic pressure perturbation in the test section were measured. Other sources of vibration due to the flow structure interactions, such as acoustic resonance, blade pulsing frequency and bellows wrinkles, were investigated. Pressure perturbation in the section and acoustic resonance due to branch pipe give major effects to the vibration of the test section in high frequency range of 1.5 kHz to 2.8 kHz.

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궤도진동에 대한 ISU 고압 시일 내구성능 개선 (Durability Improvement of High Pressure Seal for ISU under the Track Vibration)

  • 한인식
    • 한국자동차공학회논문집
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    • 제17권2호
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    • pp.112-117
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    • 2009
  • The new suspension, called ISU(In-arm suspension system) was developed for Infantry Fighting Vehicle. During vehicle field test, early failure of ISU's sealing system was occurred after driving the paved road. From the failure analysis, ISU's displacement data was obtained. In analysis of PSD data, track induced vibration which has high frequency and small amplitude characteristics, was dominant. Such track vibration would result in early seal failure because of friction increase and lack of lubrication. To simulate track vibration environment in laboratory, seals were tested under the condition of 20Hz, ${\pm}1$, ${\pm}2mm$ amplitude. The same type of seal failure occurred in vehicle test, was reproduced in the lab test under ${\pm}1mm$ amplitude. From the test results, the durability of improved seal was increased by 2.5 times compared with the previous one.

풍하중에 의한 타원형 구조물의 진동 제어 (Vibration Control of Tower Structure under Wind Load)

  • 황재승;김윤석;주석준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.427-430
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    • 2002
  • The present parer outlines the system identification and vibration control performance of air traffic control tower of Yangyang international airport with tuned mass damper(TMD). From the free vibration test, natural frequency, damping ratio and mode shape of tower are obtained and these values are compared with the values from numerical analysis. In the vibration control test to evaluate the vibration control performance, equivalent damping ratio increased by tuned mass damper are obtained in case the TMD is operated as passive mode. Damping ratio of tower evaluated from free vibration test is about $1.0{\%}$. It is very low value than damping ratio recommended in general code. Damping ratio of passive mode is about $5{\%}$. These equivalent damping ratio increased by TMD is enough to enhance the serviceability of tower structure under wind load.

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소형 위성 발사체의 정현파 진동 시험을 위한 가진 입력 결정 (Determination excitation spectrum for the sinusoidal vibration test of the small satellite launch vehicle)

  • 박순홍;윤세현;서상현;정호경;장영순
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 춘계학술대회논문집
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    • pp.193-196
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    • 2006
  • Vibration overtests have been common problems in aerospace industry. A test item can be overtested at its resonances when it is excited by the traditional spectrum enveloping peaks in the field acceleration spectrum. This paper introduces the method of modifying the excitation specification to alleviate the overtesting problem. A vibration analysis was performed to estimate interface forces and acceleration responses. A finite element model that was verified by an extensive modal test enabled us to shape the acceleration input accurately The produced notched input will be used in the sinusoidal vibration test of the small satellite launch vehicle.

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구조변경을 통한 선박용 Provision Crane의 진동저감 (Vibration reduction of provision crane in a ship by structural dynamic modification)

  • 김극수;조성재;최수현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 춘계학술대회논문집
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    • pp.433-437
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    • 2004
  • A provision crane is generally installed on the upper deck to the rear of the accommodation of the ship in order to load and unload engine part or something heavy. There are two types of provision cranes: one is jib-type and the other is monorail-type. So the natural frequency of the jib-type crane equipment is low, therefore, there are some possibility of resonance between crane structure and the main excitation sources of the ship in normal operating range. This study describe a vibration reduction technique for provision crane by applying a proper countermeasure through finite element analysis and modal test. In order to find out weak point in design of provision crane, a sensitive analysis has been performed.

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도로 노면 조건을 고려한 차량 엔진 주변 부품의 피로손상도 분석 (Analysis of Fatigue Damage of the parts around the vehicle engine with Respect to Road surface conditions)

  • 신성영;김찬중;이봉현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2014년도 추계학술대회 논문집
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    • pp.581-586
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    • 2014
  • In general vibration test considers both harmonic vibration and random vibration, When developing the vehicle component. But the effect of harmonic vibration is larger in the parts around the vehicle engine, sole testing the harmonic vibration is considered. In this study, the fatigue damage of the linear system fixed around the engine is analyzed when the effect of random vibration is higher, harsher than the normal road surface condition. In condition the vehicle speed and the engine RPM are similar, the higher the harshness of the road surface condition is, the larger the fatigue damage level is. Therefore both random vibration and harmonic vibration must be considered in vibration test of components around the engine. Proposing the sine on random(SOR) vibration test that can exam considering both of vibrations, harmonic and random.

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냉연코일강판 수송용 화차의 안전성 평가를 위한 차체하중시험과 진동시험 (A safety evaluation on the loading and vibration test for transport freight car of cold rolled coil sheet)

  • 김원경;정종덕;윤성철;홍용기
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2003년도 춘계학술대회 논문집
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    • pp.1499-1502
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    • 2003
  • This paper describes the result of carbody and vibration test for freight car. The purpose of the test is to evaluate an safety which carbody structure shall be considered fully sufficient rigidity so as to load a freight car under maximum load and operating condition on line track. The test carbody is constructed by RS korea co., LTD. in accordance with KNR specfication. The test cases of the carbody is tested the vertical load and compressive load to verify the strength and stillness. The vibration test is tested for analysis and evaluation of vibration, to allow for the fact that mechanical vibration in railway vehicles have specific characteristics.

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가진기의 동적 거동 해석 (Analysis on the Dynamic Behavior of Shaker)

  • 한상보;김윤환;송장규
    • 소음진동
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    • 제8권1호
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    • pp.75-80
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    • 1998
  • It is a well known fact that the shaker used in the vibration test interacts with the test structure and thus influences the test results. A two degree of freedom model of shaker is suggested and the vibration parameters of this model is experimentally extracted. According to this experimental results, the vibration parameters of the shaker can vary with respect to the test structure as well as the stinger used in the connecting mechanism. It is also found that the vibration parameters of the shaker provided by the manufacturer can not be accurate and these parameter values should be revaluated based on the test environments.

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