• 제목/요약/키워드: Ground Vibration Test

검색결과 225건 처리시간 0.041초

제주 남부지역의 시험발파에 의한 지반진동 특성 분석 (Analysis of Ground Vibration Characteristics by Test Blasting in Southern Region of Jeju)

  • 김승현;이동욱
    • 대한토목학회논문집
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    • 제39권3호
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    • pp.419-429
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    • 2019
  • 시험발파를 통해 제주 남부지역(현무암과 클링커 층상구조 지반)의 지반진동 특성을 분석하였다. 지반진동의 주요 성분을 파악하고 지반진동추정식을 도출함으로써 제주 남부지역의 지반진동의 전파 특성을 국내 설계지침과 비교하였다. 층상구조 지반에서의 지반진동은 근거리에서는 진동의 크기가 작으나 원거리로 갈수록 지반진동의 감쇠가 적어 진동에너지를 멀리까지 전달하는 것으로 나타났다. 그리고 주파수는 저주파수 대역으로 확인되었다. 이는 공극이 큰 클링커층이 고주파의 발파에너지 탄성파를 파형의 주기가 긴 저주파 형태로 바꿔 전달하기 때문으로 판단된다. 또한, 기반암이 다른 지역과의 지반진동을 비교하여 설계지침의 한계를 확인함으로써, 지역 특성이 반영된 설계 지반진동추정식 개발의 필요성을 제시하였다.

스마트 무인기 4자유도 지상시험치구 구조진동해석 (Structural Vibration Analysis of Smart UAV 4-Degree of Freedom Ground Test System)

  • 박강균;최현철;김동만;김동현;안오성
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2009년도 춘계학술대회 논문집
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    • pp.593-598
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    • 2009
  • In this study we present results for the design of ground test system for 4 degree of freedom(DOF) control test is one of the smart UAV ground test. This system is equipped with real smart UAV and Z direction DOF and 3 direction rotation DOF, Ensuring safe operation of the Smart UAV is a top priority. To this end, it is required to do structure analysis and test verification to confirm the design margin and safety. Based on the analysis, the ground test system has been redesigned to meet the structural conditions.

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항공기 구조물의 동적 거동 시험/해석 절차 (An Integrated Approach to the Dynamic Testing of Aerospace Structures)

  • 이상엽
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 춘계학술대회논문집
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    • pp.348-357
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    • 2006
  • Ground Vibration Tests (GVT) are needed on au new aircraft types and as part of certification. Its first objective is to verify models used for the calculation and prediction of the dynamic behavior of the structure. The main objectives of this paper are to introduce 'the integrated approach of dynamic testing for aerospace structure' in detail and 'The research projects in which LMS participated in aerospace structural dynamic area'

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지상진동시험결과를 이용한 KC-100 항공기의 플러터 해석모델 보정 (Flutter Analysis Model Tuning of KC-100 Aircraft with the Ground Vibration Test Results)

  • 백승길;최용준
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2011년도 추계학술대회 논문집
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    • pp.191-195
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    • 2011
  • The airframe ground vibration tests were conducted on the KC-100 aircraft according to the regulation requirement, KAS 23.629(a)(2) and the modal characteristics for the target modes were measured. To make FE model tuning, a design sensitivity approach with engineering judgment was implemented using MSC/Nastran and Attune, a genetic algorithm based parameter optimization software. Based on the comparison between initial prediction and test results, design variables such as beam cross-sectional properties and spring stiffnesses were devised. As the results, the correlation of the FE model to the GVT results was made appropriately, meeting the goal of matching the target frequencies within 5%.

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한국형 기동헬기 전기체 지상진동시험 (Ground Vibration Test for Korean Utility Helicopter)

  • 김세희;곽동일;정세운;최종호;김정훈
    • 한국항공우주학회지
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    • 제41권6호
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    • pp.495-501
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    • 2013
  • 한국형 기동헬기는 블레이드 가진주파수를 회피하고 지상 운용에서 로터와 기체의 동적 특성이 연계되어 나타나는 불안정성이 없도록 설계되었다. 이러한 설계 목적을 위해 진동 해석과 지상공진 해석을 수행하여 기체와 주로터의 동적 특성을 분석하였다. 이후 훨타워 시험을 통해 주로터의 동적특성을 확인하였으며 지상진동시험을 통해 기체의 동적 특성을 확인하였다. 지상진동시험은 지상 및 비행 운용 조건이 고려된 시험체 구성과 시험 조건을 적용하여 수행되었다. 본 논문에서는 한국형 기동헬기에 적용된 지상진동시험 방법 및 분석 기법을 보이고 해석 모델 보정기법과 보정된 해석 결과를 제시한다.

저진동 모래다짐말뚝(LVSCP)의 지반개량효과 분석 (Analysis of Ground Improvement Effect of Low Vibration Sand Compaction Pile Method)

  • 김종국;차준태;이재창;채영수
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2010년도 춘계 학술발표회
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    • pp.1234-1242
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    • 2010
  • In this study, the effect of noise and vibration, and influence of ground improvement are evaluated and its application is analyzed through the example of SCP designed at ground improvement in Song-Do international city. consequently, it showes even comfortable result that it is about 5.0m of inner space, when the LVSCP method is applied, rather than that it is about 30m of inner space when the existing SCP is applied in vibration control standards 2.0mm/sec. In the noise, now that the many differences according to environmental factors like other equipment noise, limited space and so on at the time of the construction by LVSCP method are coming out, so we think that appro itate measures are needed according to surroundings. By the way, when it comes to the estimation of the ground improvement work before and after an improvement of LVSCP method, its result shows that it is satisfacttion to all the standards of compaction control in dregded and reclaimed ground and sedimentary clay layer.

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항공기 지상실험에 의한 소음 저감 방안에 관한 연구 (A study of the noise suppression system at the aircraft ground run-up test room)

  • 김인수;고철수;김형근
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2003년도 추계학술대회논문집
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    • pp.718-723
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    • 2003
  • The number of jet aircraft is increasing. The aircraft noise making people near airports nervous have become a serious social problem. The aircraft noise can be classified into two groups; noise being generated at take-off or landing and noise form run-up test on the ground. In this paper, we consider the aircraft noise from run-up test on the pound and we suggest the noise suppression system.

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지하철 터널구간에서의 지반진동 상세해석 (Detailed Analysis of Ground Vibration in Subway Tunnel)

  • 이일화;황선근;조성호;고학송
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2005년도 춘계학술대회 논문집
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    • pp.722-725
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    • 2005
  • Recently, ground-borne noise and vibration generated by underground transit system has been recognized as an important environmental problem. This study reviews several of the improved procedures that have been used to predict ground-borne vibration. At first, ground stiffness profile is examined by SASW test which is the most reasonable surface wave test. It is very important to acquire the exact ground stiffness profile at ground response analysis. At second, the train loading to act roadbed is calculated by using the real measured phase angle data. In finite element analysis, averaged acceleration method, infinite element, Rayleigh damping and 2-dimensional wave propagation analysis is performed.

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다이너마이트와 미진동파쇄기 발파에 의한 지반진동속도 비교 (The Comparison of the Ground Vibration Velocity by Dynamite and Finecker Blasting)

  • 김일중
    • 터널과지하공간
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    • 제6권1호
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    • pp.39-47
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    • 1996
  • The results of the regression analysis and comparative study between 120 vibration events by dynamite blasting and 68 vibration events by finecker blasting which were monitored in the test blasting are as follows: The ground vibration velocity of dynamite blasting of 0.12 kg charge weight per delay at 7.4 m above the explosive is higher than that of finecker blasting of 0.96 kg charge weight per delay. In the case of 0.12 kg charge weight per delay, the ground vibration velocity of finecker blasting is equal to 5.5% of that of dynamite blasting at the 10 m distance from explosive. The decrement of ground vibration velocity of dynamite blasting of above 0.12 kg charge weight per delay is larger than that of finecker blasting of below 0.96 kg charge weight per delay. The rate of ground vibration velocity of the finecker blasting to that of dynamite blasting decreases with the distance from explosives, but increases with the decrease of charge weight per delay. The increment of ground vibration velocity of finecker blasting is less than that of dynamite blasting with the increase of charge weight per delay at the same distance from explosives. Under the condition of the constant critical ground vibration velocity or use the same charge weight per delay, the blasting working by finecker rather than by dynamite is able to be performed at the nearer place to structures.

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고체추진 로켓모터의 지상연소시험시 발생되는 진동현상에 관한 연구 (A Study on Vibration Phenomena occurred in Ground Firing Test of Solid Rocket Motors)

  • 김준엽;장성조;김도영
    • 대한기계학회논문집
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    • 제17권9호
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    • pp.2280-2285
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    • 1993
  • Many items, as internal pressure, thrust, temperature, strain, etc. are measured in Ground Firing Test (GFT) of rocket motors. But these items are influenced by various phenomena occurred during propellant combustion. In this study, natural frequencies of motor itself and system(motor+loadcell) on Stand were measured. Also motor responses were measured during burning and analyzed so that the vibration characteristics occurred during GFT and the causes and characteristics of vibration signal appearing on thrust curve were identified.