서지주요정보
다중화 기법에 의한 광섬유 브래그 격자 센서를 이용한 스마트 복합재 구조물의 변형률 모니터링에 관한 연구 = The strain monitoring of smart composite structures using fiber bragg grating sensors by multiplexing method
서명 / 저자 다중화 기법에 의한 광섬유 브래그 격자 센서를 이용한 스마트 복합재 구조물의 변형률 모니터링에 관한 연구 = The strain monitoring of smart composite structures using fiber bragg grating sensors by multiplexing method / 류치영.
발행사항 [대전 : 한국과학기술원, 2001].
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소장정보

등록번호

8012258

소장위치/청구기호

학술문화관(문화관) 보존서고

DAE 01001

휴대폰 전송

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초록정보

Fiber Bragg grating (FBG) sensors based on the wavelength division multiplexing technology are ideally suitable for structural health monitoring. In many applications, it is desirable to form several arrays of optical fiber sensors to monitor the response of structures. In this paper, I constructed an improved FBG sensor system using a wavelength-swept fiber laser which exhibits the high power of output for several sensor arrays. The fiber cavity etalon was also fabricated for the calibration of the nonlinear output wavelength of the laser and for taking the information of wavelength domain in the signal processing. In order to monitor the structural strain real-timely, the signal-processing program was constructed for storing and visualizing data from FBG sensors. To estimate the overall performance of the constructed FBG sensor system, quasi-static and dynamic test were executed. The signal characteristics of FBG sensor were also examined in various bonding and embedding condition. The constructed FBG sensor system with the fiber cavity etalon and a reference FBG (WSFLWI) was applied for the strain measurement of the laminated composites. In the 4-point bending test, internal strain of laminated composite was successfully measured. And buckling behavior of composite laminated panel under axial compressive loading was monitored. Finally, the behavior of composite wing box embedded 24 FBG sensors was real-timely monitored in the bending test. Experiments showed that the constructed FBG sensor system and the real-time signal-processing program could successfully monitor the behavior of composite wing box. This improved FBG sensor system could be useful for the large structures that require a large number of sensor arrays.

서지기타정보

서지기타정보
청구기호 {DAE 01001
형태사항 xii, 178 p. : 삽화 ; 26 cm
언어 한국어
일반주기 저자명의 영문표기 : Chi-Young Ryu
지도교수의 한글표기 : 홍창선
지도교수의 영문표기 : Chang-Sun Hong
학위논문 학위논문(박사) - 한국과학기술원 : 항공우주공학전공,
서지주기 참고문헌 : p. 72-77
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