• Journal of the Korean Society for Precision Engineering
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• v.9 no.3
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• pp.165-171
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• 1992

진동하는 구조물을 설계할 때에는 그 구조물 중의 Strain이나 응력이 최대가 되는 장소나 시각을 알 필요가 있다. 지금까지의 Strain 해석에는 Strain gauge 등과 같은 접촉법이 많이 이용되고 있다. 더우기, 접촉법으로 대변형 진동을 하는 물체의 Strain을 해석하는 것은 곤란하다. 최근에는 비접촉법으로 Strain 분포를 해석하기 위해 화상처리를 이용한 계측이 행하여지고 있다. 이들의 Strain 분포를 측정하는 광학적인 방법으로는 격자법, Moire법, 홀로 그랩픽 간섭법 등이 있다. 특히 대변형이나 대Strain을 해석하는 데에는 격자법이 많이 이용되고 있는데, 종래의 격자법은 Data를 처리하는 데에 많은 시간과 노력이 소요되고 작업도 매우 복잡하며, Data의 수도 제한이 되어서 구조물의 분포의 해석 정도에 큰 영향을 미치게 된다. 본 논문 에서는 스테레오법을 이용해서 2차원 격자를 붙인 시료표면의 각 점의 3차원 좌표를 계측하고, 또 Fourier 변환 격자법을 적용하여 촬영된 2차원 격자의 화상에서 위상치를 구한다. 그리고 물체의 변형 전후의 대응 관계의 화상에서 3차원 형상과 Strain 분포를 해석하는 방법을 제안한다. 이 방법을 이용하면 진동하는 구조 물의 3차원 변위분포, Strain 분포를 정도 좋게 해석할 수가 있다.

• Journal of Korean Association for Spatial Structures
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• v.7 no.3 s.25
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• pp.49-55
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• 2007

In this paper, always monitoring system of fiber Bragg Crating(FBG)Sensor is described and FBGs are well suited for measuring the movement in the part of the spatial structure(for example, cable, membrane and so on)under the pressure conditions. In order to measure the movement of long span structure, we need the measurable equipment that takes in many spots to measure. In the result of experiment, the fiber sensors showed good response to the pressure conditions. Therefore, We could calculate the movement of spatial structure and be possible health monitoring of the spatial structure.

• Journal of Korean Association for Spatial Structures
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• v.8 no.6
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• pp.95-100
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• 2008

The object of this paper is to verify possible to monitor the deformation of cable in the tensegrity structure. Also, always monitoring system of tensegrity structure using Fiber Bragg Grating Sensor is described. We carry out experiments with measuring deformation of cable in the tensegrity structure based on loading conditions. In the result of experiment, the Fiber Bragg Grating Sensors shows accurate response to the loading conditions. Therefore, we can make sure the possibility of Fiber Bragg Grating Sensor in health monitoring of the cable structure like tensegrity structure.

• Proceedings of the Optical Society of Korea Conference
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• 2003.02a
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• pp.324-325
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• 2003

광섬유 브래그 격자 센서(Fiber Brags Grating Sensor： FBG Sensor)는 여타 광섬유 센서와 같이 가볍고 저렴하며 주위의 전자기적 잡음에 무관한 장점과 더불어 측정대상이 반사광의 파장변화이므로, 광섬유 연결부나 실험장치들에 의해 생기는 광 손실이나 잡음에 대해서 강인한 측정을 할 수 있다. 그리고 파장변화가 변형률이나 온도변화에 선형적으로 나타나므로, 센서로서 많은 연구가 진행되고 있다. 특히, 구조물의 내부에 삽입하여 구조물 스스로 외부의 환경변화를 감지하여 필요한 동작을 수행하는 지능형 구조물(Smart Structure)에 적합한데, 이를 위해선 구조물의 여러 지점을 측정해야 하므로, 브래그 격자 여러개를 한 시스템에서 사용하는 다중화(Multiplexing)가 필수적이다. (중략)

• Proceedings of the Materials Research Society of Korea Conference
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• 2003.11a
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• pp.162-162
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• 2003

최근에 산화물 인공격자의 우수한 특성으로 인하여 활발한 연구가 진행되고 있다. 본 연구에서는 펄스레이저 증착방법을 이용하여 산소분압 100mTorr, $650^{\circ}C$에서 LSCO/MgO 기판위에 La-50mol% 첨가된 SrTiO$_3$ (SLTO)와 SrTiO$_3$ 를 적층시켜 산화물 인공격자를 만들어 결정구조에 대하여 연구하였다. SrTiO$_3$ (STO)는 상온에서 3.904$\AA$인 cubic perovskite 구조를 가지고 있다. 일반적으로 La$^{3+}$ (1.14$\AA$)은 Sr$^{2+}$(1.12$\AA$)과 이온반경이 거의 유사하기 때문에 ABO 페로브스카이트 구조의 A자리에 치환될 것으로 기대되며 또한 Sr$^{2+}$ 자리에 La$^{3+}$ 가 치환되므로써 발생하는 charge compensation은 Sr 자리에 Vacancy 생성으로 판단된다. 인공격자의 성장확인을 위하여 SLTO와 STO를 10층씩 증착하여 XRD분석을 통하여 평가하여 보았다. 확인된 결과를 바탕으로 산화물 인공격자의 적층 주기를 SLTO layer를 한층으로 고정시키고 STO를 한 층에서 다섯 층까지 다양하게 변화시켰다. 본 연구의 목적은 산화물 인공격자에서 결정결함을 제어하여 소자에 응용할 수 있는 전기적 물성을 평가하기 위함이다. X-ray diffraction 결과 SLTO/STO 인공격자는 (001) 방향으로 우선배향하였으며 적층주기에 따라 격자상수의 변화를 보였다. AES의 depth profile 분석을 통하여 La의 분포를 확인하였으며, HRTEM 분석을 통하여 미세구조분석을 실시하였다.

• Composites Research
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• v.30 no.6
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• pp.331-337
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• 2017

The composite lattice structures have advantages of high specific stiffness and strength and are mainly applied to the structures of launch vehicles that carry the compressive load. However, since these structures are manufactured by filament winding technology, there are some defects and voids found in the knots. For these reasons, the stiffness and strength of the lattice structures have to be compared with finite element model for predicting design load. But, the full scale test is difficult because time and space are limited and the shape of structure is complex, and hence the simple and reliable test methods for examination of stiffness are needed. In this paper, subelements of composite lattice structures were prepared and compressive and bending test were conducted for examination of stiffness of helical and hoop rib. Test methods for subelements of composite lattice structures that has curved and twisted shape were supposed and compared with finite element analysis results.

• Proceedings of the Korean Society For Composite Materials Conference
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• 1999.11a
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• pp.272-276
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• 1999

The present paper proposes design and manufacturing methods of the carbon/epoxy square grid structure with near zero-CTE in three geometrical principal directions. Bonding strength of the grid structure is examined for different bonding methods. Numerical examples show that maximum displacement of the composite grid structure is almost zero comparing with that of aluminum grid structure with same dimension under thermal loading.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.10
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• pp.979-987
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• 2008

In aerospace structural design, the position of lightening hole is often required to be optimized from the initial design in order to avoid an excessive stress concentration. To remodel the updated configuration in optimization procedure, re-meshing procedure is conventionally adopted. However, this approach is time-consuming, and has limitations especially in handling hexahedral or quadrilateral meshes, which are preferred because of their good numerical performances. To attenuate these disadvantages, new optimization scheme is proposed by combining the MLS(Moving Least Squares) based overset method and the genetic algorithm in this work. To test the validity of the proposed optimization scheme, optimizations of positions of lightening holes in 2D structures have been carried out.

• Journal of the Korea institute for structural maintenance and inspection
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• v.24 no.5
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• pp.143-149
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• 2020

The purpose of this study is to manufacture a variable density - hybrid lattice structure control by filling the pore of the metal addictive manufactured lattice structure with lightweight reactive acrylic compounds(RAC). To apply the variable density - hybrid lattice structure to the construction industry, the enhancing adhesion - reactive acrylic compounds(EA-RAC) which increased the adhesion strength was manufactured by adding ordinary portland cement to the RAC. Finally, the EA-RAC was filled into the lattice structure to test the specific density, water absorption, and adhesion strength of the variable density - hybrid lattice structure. The results were obtained with density controllable, water absorption less than 1.0%, and 1-day bonding strength of 1.78 MPa to 1.98 MPa.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.3
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• pp.32-38
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• 2005

FBG sensors have been studied more actively than any other fiber optic sensor because of good multiplexing capabilities among many fiber optic sensors. The demodulation method of FBG sensors is based on the detection of wavelength shift of their sensor peaks and properties such as strain and temperature can be measured by detecting them. However, the signal stability of FBG sensors can be influenced by the strain gradient induced by structural geometry or cracks on the surface when FBG sensors are embedded into or attached on the structure. In this study, the signal characteristics of reflected spectra of FBG sensors under strain gradient were verified and the relations between the grating length of FBG sensors and the amount of strain gradient were investigated. From the experimental results, the recommended working range of FBG sensors under strain gradients was shown quantitatively with respect to grating lengths of them.