• Composites Research
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• 제18권6호
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• pp.26-33
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• 2005

손상이 발생할 경우 복합재료의 기계적 물성치는 급격한 저하를 유발한다 특히, 조류충돌, 우박, 지상 이착륙 상황에서의 타이어 조각이나 돌조각 등과 같은 작은 질량에 의한 고속충격은 구조물과 서브시스템에 심각한 손상을 유발한다. 이런 복합재 적층판에서의 손상은 기존의 전통적인 방법으로 감지하기가 어려우며, 단일 감지 기술만을 이용하여 믿을 만한 손상평가 결과를 얻을 수 없다. 본 논문에서는 고분자 압전필름 센서를 이용하여 복합 적층판에서의 충격에 의한 손상의 개시 시점 및 확장을 탐지하였다. 획득한 센서신호는 시간-주파수 분석법인 웨이블릿 변환과 단시간 푸리에 변환을 적용하였으며, 초음파 C-scan과 전자현미경을 이용하여 시편에서의 손상 확장을 검사하였다 이 연구에서는 다양한 감지기술, 특히 고분자 압전 필름센서를 이용하여 복합재 적층판에서의 고속충격 손상 특성을 확인하였다.

• 대한기계학회논문집
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• 제19권7호
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• pp.1563-1572
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• 1995

The on-line cure monitoring during the cure process of fiber reinforced resin matrix composite material is important for the better quality and productivity. Among several cure monitoring methods, the dielectrometry that uses electrodes as its sensor is known to be the most promising method. In this study, the sensitivity of the dielectric sensor for the on-line cure monitoring was analyzed by finite element method and compared to the experimental results. Using the analytical results, the equation for the capacitance of the sensor was derived. Also, the optimal sensor design method was suggested after analyzing several different sensor shapes.

• 한국소음진동공학회논문집
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• 제11권6호
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• pp.169-174
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• 2001

Optimization of the collocated piezoceramic sensor/actuator placement is investigated numerically and verified experimentally for vibration control of laminated composite plates. The finite element method is used for the analysis of dynamic characteristics of the laminated composite plates with the piezoceramic sensor/actuator. The structural damping index(SDI) is defined from the modal damping(2$\omega$ζ) . It is chosen as the objective function for optimization. Weights for each vibrational mode are taken into account in the SDI calculation. The gradient method is used for the optimization. Optimum location of the piezoceramic sensor/actuator is determined by maximizing the SDI. Numerical simulation and experimental results show that the optimum location of the piezoceramic sensor/actuator is dependent upon the outer layer fiber orientations of the plate, and location and size of the piezoceramic sensor/actuator.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2016년도 제50회 동계 정기학술대회 초록집
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• pp.354.2-354.2
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• 2016

Mycosporine-like amino acids (MAAs) are small secondary metabolites produced by organisms that live in environments with high volumes of sunlight, is an important group of novel bioactive compounds having immense biotechnological poten-tials due to their UV screening properties and Polypyrrole (PPy) is a type of organic polymer formed by polymerization of pyrrole. A novel composite nanofilm (~60 nm) of mycosporine-like amino acid (MAA) and polypyrrole is synthesized by interfacial polymerization technique. This composite nanofilm is conductive and has strong photoresponse. A photoelectric UV sensor is fabricated by depositing the composite film onto a silicon chip. This UV sensor shows good sensitivity, selectivity and stability for UV detection.

• Composites Research
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• 제14권1호
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• pp.30-38
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• 2001

복합재료는 우수한 비강성, 비강도 특성 때문에 기존의 항공우주산업뿐만 아니라 로봇 팔. 공작기계 등에 널리 사용되고 있다. 복합재료 경화중의 온라인 모니터링기법은 생산성 향상 및 품질의 신뢰성 향상을 위하여 매우 중요한 연구분야로 대두되고 있다. 본 논문에서는 휘스톤 브리지식 유전회로를 설계하고 제작하였다. 또한 고온 경화 복합재료에 적용할 수 있는 고온 유전센서를 개발하여 그 성능을 평가하였다. 유한요소해석을 이용하여 유전 센서에 작용하는 열 잔류응력을 계산하였으며, 고온분위기 하에서 유전센서의 유전특성을 평가하였다. 이상에서 개발된 유전회로와 고온 유전센서를 이용하여 BMI(Blsmaleimlde) 수지의 경화모니터링을 수행하였다.

• Composites Research
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• 제17권2호
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• pp.28-33
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• 2004

광섬유 브래그 격자센서를 이용하여 인장하중을 받는 직교적출 복합해로 법에서 발생하는 파손신호를 계측하였다. 민감도와 주파수 대역성능을 향상시키기 위하여 수동 마흐_젠더 간섭계 방식의 복조기를 제안하였다. 제안한 FBG 센서시스템은 위상변조기와 같은 능동소자가 없기 때문에 구성이 간단하고 쉽게 구현할 수 있으며 충격이나 파손 신호와 같이 작은 진폭의 고주파 진동 측정이 가능하다. FBG 센서로 측정한 복합재료의 파손신호는 복합재료 시편의 90도 층에서 모재 균열이 진전하면서 발생하는 급격한 변형률 변이에 해당하는 초기 오프？ 값과 최대 수백 킬로헤르쯔에 이르는 주파수로 진동하고 었었다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.124-127
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• 2000

In this study, a technique for monitoring of fatigue damage of composite laminates by measuring the stiffness change using embedded intensity-based optical fiber sensors was investigated. Firstly, the underlying measurement principle and structure of intensity-based sensors and then a simple stiffness conversion process was explained. The monitoring technique was evaluated by fatigue tests of composite laminates with an embedded intensity-based sensor. From the test results, the response of the intensity-based sensor showed good correlation with that of surface mounted extensometer. Therefore, it can be concluded that the intensity-based sensors have good potential for the monitoring of fatigue damage of composite structures under fatigue loading. In addition, it could be confirmed that the intensity-based sensors have higher resistance to fatigue than the commercial electrical strain gauge.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1998년도 춘계학술대회논문집; 용평리조트 타워콘도, 21-22 May 1998
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• pp.684-688
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• 1998

Optimization of the collocated piezoceramic sensor/actuator placement is investigated numerically and verified experimentally for vibration control of laminated composite plates. The finite element method is used for the analysis of dynamic characteristics of the laminated composite plates with the piezoceramic sensor/actuator. The structural damping index(SDI) is defined from the modal damping. It is chosen as the objective function for optimization. Weights for each vibrational mode are taken into account in the SDI calculation. The gradient method is used for the optimization. Optimum location of the piezoceramic sensor/actuator is determined by maximizing tie SDI. Numerical simulation and experimental results show that the optimum location of the piezoceramic sensor/actuator is dependent upon the outer layer fiber orientations of the plate, and location and size of the piezoceramic sensor/actuator.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.215-218
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• 2005

In this research, design scheme of fiber Bragg grating(FBG) sensor system for aircraft application is suggested from the results and the know-how from the fon11er researches on structural health monitoring techniques using fiber optic sensors. Design factors to be taken into consideration were derived for both sensor parts including connection and system parts. For the stability of FBG sensor system, design requirements of temperature, vibration, humidity, electromagnetic interference were presented from U. S. military standards. The direction of software programming which increases stability and perfon11ance of the aircraft with the FBG sensor system was also examined.

• International Journal of Concrete Structures and Materials
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• 제3권1호
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• pp.33-37
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• 2009

Fiber Bragg grating (FBG) sensors already have been the focus for structural health monitoring (SHM) due to their distinguishing advantages. However, as bare optical fiber is very fragile, bare FBG strain sensor without encapsulation can not properly be applied in practical infrastructures. Therefore encapsulation techniques for making encapsulated FBG strain sensor show very important in pushing forward the application of FBG strain sensors in SHM. In this paper, a simplified approximate method to analyze the stress transferring rules for embedded FBG strain sensors in concrete monitoring is put forward according to mechanics of composite materials. Shear lag theory is applied to analyze the stress transferring rule of embedded FBG strain sensor in measured host material at the first time. The measured host objects (concrete) and the encapsulated FBG strain sensor are regarded as a composite, and then the stress transfer formula and stress transfer coefficient of encapsulated FBG strain sensor are obtained.