• 제목/요약/키워드: Impact Location

검색결과 830건 처리시간 0.021초

충격위치와 심재적층각도에 따른 하니컴 샌드위치 패널의 저속충격 특성 연구 (A Study on Low-Velocity Impact Characterization of Honeycomb Sandwich Panels According to the Changes of Impact Location and Core Fabrication Angles)

  • 전광우;신광복;고희영;김대환
    • 대한기계학회논문집A
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    • 제33권1호
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    • pp.64-71
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    • 2009
  • In this paper, a study on low-velocity impact response of honeycomb sandwich panels was done for the changes of impact location and core fabrication angles. The test specimens were made of glass/epoxy laminate facesheet and aluminum honeycomb core. Square samples of 100mm and 100mm sides were subjected under low-velocity impact loading using instrumented testing machine at three energy levels. Impact parameters like maximum force, time to maximum force, deflection at maximum force and absorbed energy were evaluated and compared for the changes of impact location and core fabrication angle. The impact damage size were measured at facesheet surface by 3-Dimensional scanner. Also, sandwich specimens after impact test were cut to analyse the failure mode.

An Automatic Diagnosis Method for Impact Location Estimation

  • Kim, Jung-Soo;Joon Lyou
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1998년도 제13차 학술회의논문집
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    • pp.295-300
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    • 1998
  • In this paper, a real time diagnostic algorithm fur estimating the impact location by loose parts is proposed. It is composed of two modules such as the alarm discrimination module (ADM) and the impact-location estimation module(IEM). ADM decides whether the detected signal that triggers the alarm is the impact signal by loose parts or the noise signal. When the decision from ADM is concluded as the impact signal, the beginning time of burst-type signal, which the impact signal has usually such a form in time domain, provides the necessary data fur IEM. IEM by use of the arrival time method estimates the impact location of loose parts. The overall results of the estimated impact location are displayed on a computer monitor by the graphical mode and numerical data composed of the impact point, and thereby a plant operator can recognize easily the status of the impact event. This algorithm can perform the diagnosis process automatically and hence the operator's burden and the possible operator's error due to lack of expert knowledge of impact signals can be reduced remarkably. In order to validate the application of this method, the test experiment with a mock-up (flat board and reactor) system is performed. The experimental results show the efficiency of this algorithm even under high level noise and potential application to Loose Part Monitoring System (LPMS) for improving diagnosis capability in nuclear power plants.

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An Automatic Diagnosis Methods for Impact Location Estimation

  • 김정수;류준
    • 전기전자학회논문지
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    • 제3권1호
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    • pp.101-108
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    • 1999
  • 본 논문은 금속파편이 발생시 금속파편의 위치를 추정하기위한 위치 추정 알고리즘을 제안한다. 이 추정 알고리즘은 자동화된 알람 구별부와 위치 추정부로 구성된다. 알람 구별부는 충격 신호인지 거짓 충격 신호인지를 구별하는 기능을 수행하며, 위치 추정부는 충격신호로부터 충격신호의 시작점을 찾아내어 위치를 추정한다. 이 알고리즘의 타당성을 검증하기위해 원자로 Mock-up 상에서 실험한 결과 위치 추정값 과 실제 충격값이 약 10 % 이내의 오차율을 보였다.

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Impact force localization for civil infrastructure using augmented Kalman Filter optimization

  • Saleem, Muhammad M.;Jo, Hongki
    • Smart Structures and Systems
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    • 제23권2호
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    • pp.123-139
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    • 2019
  • Impact forces induced by external object collisions can cause serious damages to civil engineering structures. While accurate and prompt identification of such impact forces is a critical task in structural health monitoring, it is not readily feasible for civil structures because the force measurement is extremely challenging and the force location is unpredictable for full-scale field structures. This study proposes a novel approach for identification of impact force including its location and time history using a small number of multi-metric observations. The method combines an augmented Kalman filter (AKF) and Genetic algorithm for accurate identification of impact force. The location of impact force is statistically determined in the way to minimize the AKF response estimate error at measured locations and then time history of the impact force is accurately constructed by optimizing the error co-variances of AKF using Genetic algorithm. The efficacy of proposed approach is numerically demonstrated using a truss and a plate model considering the presence of modelling error and measurement noises.

재난 관련 위치 신뢰도 향상을 위한 소셜 미디어 활용 (Leveraging Social Media for Enriching Disaster related Location Trustiness)

  • 뉘엔반퀴엣;뉘엔양쯔엉;뉘엔신응억;김경백
    • 디지털콘텐츠학회 논문지
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    • 제18권3호
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    • pp.567-575
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    • 2017
  • 위치기반 서비스는 재난 경보 시스템 및 추천시스템 등의 다양한 응용에서 중요한 역할을 한다. 이들 응용들은 위치정보(위도, 경도 등) 뿐만 아니라 위치에 대한 사건(지진, 태풍 등)의 영향력을 필요로 한다. 최근 이러한 위치에 대한 사건의 영향력을 제공하기 위해, 다양한 형태의 정보(지진 정보와 센서 정보)를 이용한 위치 신뢰도 계산 방법이 연구 되었다. 이전의 연구에서는 사건의 영향을 선형으로 감소시키는 형태로 위치 신뢰도를 계산하였다. 이 논문에서는 소셜 미디어를 추가적으로 활용하여 사건의 위치에 대한 영향력, 즉 위치 신뢰도를 향상 시키는 만드는 방법을 제안하였다. 우선 지진정보와 소셜 미디어 데이터를 수집하는 시스템을 설계하였다. 두번째로, 지진정보에 기반한 위치 신뢰도 계산 방법을 소개하였다. 최종적으로 소셜 미디어에 기반하여 공간적으로 분산되는 형태로 신뢰도를 증강시키는 방법을 통해 위치 신뢰도 정보를 더욱 풍부하게 제공하는 방법을 제안하였다.

Experimental studies on impact damage location in composite aerospace structures using genetic algorithms and neural networks

  • Mahzan, Shahruddin;Staszewski, Wieslaw J.;Worden, Keith
    • Smart Structures and Systems
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    • 제6권2호
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    • pp.147-165
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    • 2010
  • Impact damage detection in composite structures has gained a considerable interest in many engineering areas. The capability to detect damage at the early stages reduces any risk of catastrophic failure. This paper compares two advanced signal processing methods for impact location in composite aircraft structures. The first method is based on a modified triangulation procedure and Genetic Algorithms whereas the second technique applies Artificial Neural Networks. A series of impacts is performed experimentally on a composite aircraft wing-box structure instrumented with low-profile, bonded piezoceramic sensors. The strain data are used for learning in the Neural Network approach. The triangulation procedure utilises the same data to establish impact velocities for various angles of strain wave propagation. The study demonstrates that both approaches are capable of good impact location estimates in this complex structure.

고해상도 상용카메라를 사용하는 영상변환을 이용한 탄착점 좌표획득 (Bomb Impact Point Location Acquisition by Image Transformation using High-Resolution Commercial Camera)

  • 박상재;하석운
    • 대한임베디드공학회논문지
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    • 제6권1호
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    • pp.1-7
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    • 2011
  • In the bomb impact test, to acquire the bomb impact point location the high-priced embedded equipments such as the Bomb Scoring System or the EOTS are needed. Recently, a high-resolution image processing could be possible since the resolution of the commercial camera is growing rapidly. In this paper we first propose an image transformation method for acquiring the real bomb impact image using a high-resolution commercial camera, and then present the process calculating the real bomb impact point location coordinate from the transformed image. Based on the experimental results we found the possibilities that the real bomb impact point information could be effectively earned just using the commercial camera.

용접열영향부 충격시험편 노치 위치에 따른 파괴거동 (Failure Behaviors Depending on the Notch Location of the Impact Test Specimens on the HAZ)

  • 장윤찬;홍재근;박지홍;김동욱;이영석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.706-711
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    • 2007
  • Numerical studies were performed to examine the effects of notch location of impact specimens on the failure behavior of HAZ (heat affected zone) when Charpy V-notch impact test were made at a low temperature ($1^{\circ}C$). Carbon steel plate (SA-516 Gr. 70) with thickness of 25mm for pressure vessel was welded by SMAW (shielded metal-arc welding) and specimens were fabricated from the welded plate. Charpy tests were then performed with specimens having different notch positions of specimens varying from the fusion line through HAZ to base metal. A series of finite element analysis which simulates the Charpy test and crack propagation initiating at the tip of V-notch was carried out as well. The finite element analysis takes into account the irregular fusion line and non-homogenous material properties due to the notch location of the specimen in HAZ. Results reveals that the energies absorbed during impact test depend significantly on the notch location and direction of specimen. Finite element analysis also demonstrates that the notch location of specimens, to a great extent, influences the reliability and consistency of the test.

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연속웨이브렛 변환을 이용한 충격음 위치 규명 (CWT-Based Method for Identifying the Location of the Impact Source in Buried Pipes)

  • 김의열;김민수;이상권;고재필
    • 대한기계학회논문집A
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    • 제34권11호
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    • pp.1555-1565
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    • 2010
  • 본 연구에서는 지하에 매설된 가스 파이프에 가해진 충격의 위치를 탐지하기 위한 개선된 방법을 제시하고 있다. 가스 파이프에서 가스 누출은 건설 기계 장비에 의한 기계적 충격에 의해 발생하며, 가스 이송산업계에 치명적인 재해을 발생시킬 수 있다. 이와 같은 문제를 초기에 발견하고 조치를 취하기 위해 기존에는 충격 위치 탐지를 위해 상관 관계 기법이 사용되어 왔다. 하지만, 외부 충격에 의해 파이프 따라 전파되는 음향파의 분산 특성은 양쪽 센서에 측정되는 도착 시간을 사용하여 센서 사이에 도착 시간 지연을 예측하는데 상당한 에러를 발생 시킬 수 있다. 그래서 이 논문에서는 분산파 대신 직접파의 도착 시간 지연을 측정하기 위해 웨이블렛 기법을 사용하였다. 제안된 방법은 지하에 매설된 실제 가스 파이프에서 측정된 음향 신호에 적용하여 기존의 상관 관계 기법에 비해 외부 충격 위치를 추정하는데 보다 효과적임을 확인하였다.

외팔 보를 이용한 Location Template Matching 방법을 적용함에 있어서 격자간격의 영향 분석 (Analysis of the Effect of the Grid Spacing on the Application of the Location Template Matching Method Using a Cantilever Beam)

  • 신기홍
    • 한국소음진동공학회논문집
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    • 제26권5호
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    • pp.609-615
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    • 2016
  • Measuring similarity between two signals is a key element of the location template matching (LTM) method which is one of impact source localization technique. As a measure of similarity, the correlation coefficient is most widely used, and the group delay based method is recently proposed to improve the accuracy of finding the impact source. In practice, the LTM method assumes that the similarity between two signals decreases as the distance between two corresponding impact points increases, where the distance between two neighboring impact points defines the grid spacing. In this paper, it is shown that this assumption is not always true but the correlation coefficients fluctuate forming a main robe and many side robes as the distance between two neighboring impact points increases. On the other hand, the standard deviation of group delay sharply increases with a small increase of the grid spacing. These are demonstrated by using a simple cantilever beam. Based on these findings, an optimal way of implementing the LTM method may be suggested by combining the correlation coefficient and the group delay based approaches.