• 제목/요약/키워드: Vibration test

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자동차 배터리 지지 구조의 진동 피로 해석에 대한 연구 (Study on Vibration Fatigue Analysis of Automotive Battery Supporter)

  • 안상호
    • 자동차안전학회지
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    • 제11권4호
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    • pp.22-27
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    • 2019
  • In this paper, the vibration load and analysis results for automotive battery supporter were performed to provide efficient vibration tolerance performance prediction methods for single-product vibration tolerance testing, and the major influencing factors and considerations for setting up single-unit vibration tolerance tests were reviewed. A common applicable standard load was applied to efficiently predict the performance of single-unit vibrations through the frequency response analysis technique. The results similar to test results can be predicted by checking vulnerable parts of the vehicle components for vibration loads and applying scale factor to standard loads. In addition, it was confirmed that the test conditions with a frequency generating the same durability severity as the endurance test are needed for accurate prediction of the durability of the single-unit vibration tolerance test conditions, and the acceleration and frequency with the conditions that there is no significant nonlinear phenomena in the vibration system are established during the single-unit vibration tolerance test conditions.

테일홴 성능시험장치의 운용과 진동특성 (The Operation and Vibration Characteristics of Tail-fan Performance Test System)

  • 송근웅;김준호;강희정;이욱;심정욱
    • 한국소음진동공학회논문집
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    • 제15권4호
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    • pp.421-428
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    • 2005
  • This paper described operation and vibration characteristics of a 'tail-fan' anti-torque performance test system. KARI (Korea Aerospace Research Institute) developed a 'tail-fan' anti-torque system of a helicopter and a performance test-rig to test the performance of the tail-fan. The performance test-rig consists of driving, supporting and rotating parts. In the process of the performance test, firstly, operation test of the test-rig were carried out to verify design specifications. Secondly, natural frequencies of fan blade and test-rig were measured respectively. Lastly, to find the operation rotating speed for the performance test, vibration test were carried out using accelerometers on tail gear box. The performance test conditions of the tail-fan to avoid a resonance were found from the fan-plot and vibration test results. The tail-fan performance tests were well done safely.

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.

충격시험을 이용한 고정밀장비의 진동허용규제치 결정기법에 관한 연구 (A Study on the Determination of Vibration Criteria for Vibration Sensitive Equipments Using Impact Test)

  • 이홍기;박해동;김두훈;김사수
    • 소음진동
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    • 제7권2호
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    • pp.247-254
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    • 1997
  • In the case of a precision equipment, it requires a vibration free environment to provide its proper function. Especially, lithography and inspection devices, which have sub-nanometer class high accuracy and resolution, have come to necessity for producing more improved giga class semiconductor wafers. This high technology equipments require very strict environmental vibration standard in proportion to the accuracy of the manufacturing, inspecting devices. The vibration criteria are usually obtained either by the real vibration exciting test on the equipment or by the analytical calculation. This paper proposes a new method to solve this problem at a time. The permissible vibration level to a precision equipment can be easily obtained by analyzing a process of Frequency Response Function. This paper also demonstrates its effectiveness by applying the proposed method to finding the vibration criteria of a Computer Hard Disk Driver by Impact Test.

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Transfer Function Method를 이용한 자동차 연료탱크의 진동 피로 해석에 대한 연구 (Vibration Fatigue Analysis of Automotive Fuel Tank Using Transfer Function Method)

  • 안상호
    • 자동차안전학회지
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    • 제12권3호
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    • pp.27-33
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    • 2020
  • In this paper, the process of predicting efficient durability performance for vibration durability test of automobile parts using vibration test load on automobile fuel tank is presented. First of all, the common standard load that can be applied to the initial development process of the automobile was used for the fuel tank and the vulnerability of the fuel tank to the vibration fatigue load was identified through frequency response analysis. In addition, the vulnerability of the fuel tank was re-enacted through vibration durability test results, and the scale factor was applied to the standard load. In order to predict the vibration durability performance required for detailed design, vibration fatigue analysis was performed on the developed vehicle with the frequency of vibration severity equivalent to the durability test, and the vulnerability and life span of the fuel tank were identified through the process of applying weights to these selected standard loads, thereby reducing the test time of the development vehicle.

지구관측위성의 발사환경시험 요구조건 (Launch Environment Requirements for Earth Observation Satellite)

  • 김경원;김성훈;김진희;이주훈;황도순
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.747-750
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    • 2004
  • After launching, spacecraft is exposed to extreme environments. So spacecraft should be tested after design/manufacture to verify whether components can be operated functionally. Acceleration transferred from launch vehicle to spacecraft produces quasi-static load, sine vibration and random vibration. Random vibration is also induced by acoustic vibrations transferred by surface of spacecraft. And shock vibration is produced when spacecraft is separated from launch vehicle. To verify operation of spacecraft under these launch environments, separation shock test, sine vibration test, acoustic vibration test and random vibration test should be performed. This paper describes these launch environment test requirements.

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군용차량 주행 진동응답 분석 (Vibration Response Analysis of the Military Vehicle by Road Test)

  • 신동준;이종학;강영식;최지호;강동석
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2014년도 추계학술대회 논문집
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    • pp.262-266
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    • 2014
  • Military vehicle equipped with an antenna and a shelter for operating radar has a vibration exposure during driving time. This vibration would have influence on structure of military vehicle critically. In this paper, driving stability of the military vehicle is obtained through the vibration response analysis. And, vibration level of the military vehicle satisfied the military vibration specification through analysis and comparing the MIL-STD-810G. PSD and Grms data obtained by road test can be used for vibration test specification of cabinets and electronic equipment in shelter.

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에너지 활용 부품의 진동내구 평가기법 연구 (A study on the vibration durability test for the energy harvesting part of vehicle)

  • 주형준;김찬중;이기수
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2014년도 추계학술대회 논문집
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    • pp.587-588
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    • 2014
  • Studies that the vehicle exhaust system applied by the TEG(thermal electric generator) are actively in progress in order to improve the fuel efficiency of the vehicle. Vehicle exhaust system is on a poor vibration condition, it is susceptible to TEG. This paper is about the development of vibration durability test of TEG mounted on a vehicle exhaust system. Vehicle driving tests are performed to measure the vibration condition of the vehicle exhaust system. The vibration durability test mode of TEG is evaluated using equivalent vibration energy method. The vibration durability tests of TEG are performed using the multi-axial vibration simulation table.

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한국형 위성 발사체 성능 검증위성의 진동환경에 관한 연구 (A Study on the Vibrational Environment Test of KSLV-1 Demonstration Satellite)

  • 서현석;김홍배;우성현;채장수;오태식
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 춘계학술대회논문집
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    • pp.966-970
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    • 2005
  • On the basis of the development of KSLV-1, KoDSat was designed and manufactured to demonstrate the performance of KSLV-1. KoDSat is exposed to a severe vibrational environment at launch. The structural reliability of KoDSat has to be verified using vibrational test. The structural compatibility and verification of components between analysis and test can be proved using environmental vibration test. In this paper, we review the structural characteristic of thruster control unit for a space launch vehicle and design TCU housing using mathematical model. In order to verify the structural compatibility and reliability, half-sine shock, random and sing sweep vibration test was performed. Especially, sing sweep vibration test result is compared with analysis result and mathematical model is verified.

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고속 BLDC 전동기를 위한 시험설비의 구조적 동특성에 관한 연구 (A case study in the dynamic characteristic of a test rig for a high-speed motor)

  • 박철준;이성욱;박영수
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.641-645
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    • 2008
  • In this paper, vibration sources of the BLOC motor are identified and the motor vibrations are reduced by structural modification. For vibration characteristic identification, vibration signals measured by an accelerometer when the BLOC motor is moving. These signals are presented in a waterfall plot in order to find the dependency of frequency components on the motor speed. It is found that main vibration source is BLOC motor test rig. From finite element analyses and some experiments, it is also found that resonances occur because the natural frequencies of the test rig exist in usual driving speed rang. To shift the natural frequencies outside the driving rang, the test rig is modified increase stiffness. It is verified that considerable amount of vibration are reduced by the structural modification.

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