• 한국군사과학기술학회지
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• 제16권6호
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• pp.779-788
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• 2013

The load requirements should be known to design mechanical structure. This paper proposes a generation method of load requirements using U.S. military specification to design the external mounting structure of the helicopters of which the flight environments such as aerodynamic forces and inertia forces are unknown. In this study, the load requirements which were applied at the design of the pod structure for helicopter captive flight test could be computed by using this method. The validation of proposed method was confirmed from the test flight using developed pod system.

• 한국산학기술학회논문지
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• 제18권2호
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• pp.672-680
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• 2017

태양광 발전 시스템은 태양광 패널이 부착되어 있는 구조물, 이를 지지하는 부분과 발전된 전력을 계통 또는 부하측에 공급하는 장치로 구성된다. 태양광 패널의 발전효율은 태양빛의 입사량에 영향을 받기 때문에 패널이 태양빛을 가장 많이 받을 수 있는 방향으로 패널 구조물을 설치한다. 그러나 태양은 계속 이동하기 때문에 고정식 보다는 태양을 향하여 패널이 회전하는 방식이 더욱 효율이 좋다. 태양광 패널 구조물은 야외에 설치되므로 풍하중, 적설하중 지진하중 등이 작용한다. 본 논문에서는 태양광 패널 구조물에 가장 영향이 큰 풍하중을 유한요소법을 사용하여 구하고 이를 적용하여 태양 추적식 발전 장치의 구조물을 설계하였다. 특히 패널간의 간격에 따른 풍하중을 구하고, 패널 구조물이 지면과 이루는 각도에 따른 풍하중의 변화도 구하였다. 패널간의 간격은 간격이 없을 경우, 간격이 40 mm, 80 mm일 경우 등 3가지 경우에 대하여 해석을 하였으며, 지면과의 각도는 30도, 45도, 60도 등에 대하여 해석을 하였다. 해석결과 풍하중은 패널간의 간격이 없을 경우가 가장 적게 나타났고, 지면과의 경사각이 클수록 커지는 것을 알 수 있었다.

• 대한건축학회논문집:구조계
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• 제35권11호
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• pp.137-146
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• 2019

Recently, the Near-Surface-Mounting method using Fiber reinforced polymer (FRP) has been developed and applied to the reinforcement of many concrete structural members. However, as a part of the fire resistance design, there is a lack of research related to fire insulation for the areas reinforced with FRP. In case of NSM reinforcement, there is a difference in the transferred temperature from the external surface to the groove corresponding to the location of the groove where the FRP is embedded, and the effect of this should be reflected in the fireproof insulation design. Therefore, in this study, after forming grooves for surface embedding in concrete blocks, fireproof insulation reinforcement was performed using Calcium Silicate (CS) fireproof board and an experiment to evaluate the temperature transfer was performed. By observing the temperature at these groove positions, the reduction of temperature transfer according to fireproof insulation detail was studied. As a result, when the NSM-FRP is properly fire-insulated using the CS-based fireproof board, the epoxy inside the groove does not reach its glass transition temperature until the external temperature reaches $800^{\circ}C$.

• 한국군사과학기술학회지
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• 제21권4호
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• pp.456-463
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• 2018

With the development of weapon systems by mounting various sensors, it makes important to analyze the precise functioning of sensor to external environment. In the case of small arms with magnetic sensor, the malfunction of small arms might be caused by strong external magnetic fields. In this study, the effects of magnetic sensor on external magnetic fields were analyzed, and optimal magnetic shield and shield structure were designed through M&S. In addition, the magnetic-shielding effectiveness of magnetic sensor in small arms was verified with commercial shielding materials. As a result, it was demonstrated that the Fe-Cu-Si-Nd-B with the structure of multi-layer metallic shields was shown the magnetic-shielding effectiveness of 83 % for an external permanent magnet and 19 % for an alternating magnetic field of 180 dBpT at 60 Hz, respectively.

• 대한전기학회논문지:전기물성ㆍ응용부문C
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• 제54권1호
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• pp.35-40
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• 2005

In this paper, we designed and fabricated the variable impedance line by using the DGS(Defected Ground Structure) which is useful in mounting the external lumped elements. Also we used a varactor diode as Control device stuff at the proposed variable impedance line. We are able to change the impedance of transmission line as varied the capacitance of varactor diode by adjusting DC bias. The impedance variation of the proposed DGS line is about maximum 70 Ω. We will study about the application of DAM(Direct antenna modulation) in the future work.

• 한국음향학회지
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• 제16권2호
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• pp.10-15
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• 1997

수중 청음기는 진동하는 물체 위에 설치되어 다양한 외부 잡음 원이 유입되는 환경에 노출되어 있다. 외부 잡음 원으로는 수중 청음기가 설치된 구조물 자체의 진동, 프로펠러 잡음, 그리고 유동 유기 잡음들이 있고, 이들 외부 잡음원은 실제 강도가 상당히 높아서 센서의 정확한 작동에 장애가 되고 있다. 본 연구에서는 외부 잡음에 무관한 고 정밀도, 저 잡음 특성을 갖는 수중 청음기를 개발하기 위하여 유한 요소법(FEM)을 사용하여 잡음 전달 특성의 분석 및 air pocket과 음향 감쇠층의 다양한 조합으로 이루어진 개선된 구조의 수중 청음기를 설계하고, 내 잡음성 평가를 하였다. 그 결과 센서 측면 하단부에 잡음 원이 위치할 경우 가장 큰 잡음 신호로 작용하므로 구조를 변경한 결과 기존 수중 청음기에 비해 59% 이상 내 잡음성을 증진 시켰다.

• 한국정보기술학회논문지
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• 제16권11호
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• pp.51-59
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• 2018

본 논문에서는 해상에서 수상감시정찰 및 수중탐색임무를 수행할 수 있는 복합임무 무인수상정을 설계하였으며, 설계된 복합임무 무인수상정의 선체부는 유리섬유강화플라스틱을 이용하여 제작하였다. 수상감시정찰 및 자율운항 임무를 수행하기 위해 레이더, 라이다, 카메라 등과 같은 다양한 항법센서를 마스트에 장착하였으며, 특수임무를 수행하기 위한 더미건 장비를 선수부 갑판에 장착하였다. 악천후의 해상상태에서 주어진 임무를 성공적으로 수행하기 위해서는 갑판에 탑재된 구조물들에 대한 강성확보가 매우 중요하다. 따라서 본 논문에서는 정하중, 횡하중 및 수직방향 운동에 따른 마스트 구조물의 강도해석 및 더미건 장비의 충격량에 대한 선체부의 강도해석을 시뮬레이션 및 실험을 통해 수행하였다. 시뮬레이션 및 실험 결과에 따라 본 연구에서 설계된 마스트 구조물 및 더미건 장착부의 선체부는 충분한 강성을 확보하고 있음을 확인하였다.

• 한국군사과학기술학회지
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• 제26권3호
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• pp.302-312
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• 2023

This paper describes the analysis of lightning strike zoning, the indirect lightning data simulation and the protection design for lightning indirect effects of equipment by lightning strike for unmanned aircraft consisting of composite wings. Through the analysis of lightning strike zoning according to the external shape of unmanned aerial vehicles, the structure areas that should be protected during lightning strike is derived, and the protection requirements of lightning indirect effects for flight critical equipments and equipment that must be operated upon lightning strike was derived. Lightning protection levels according to the location of mounting equipment and surrounding structure materials for each equipment was derived, and the protection design of the unmanned aerial vehicle with composite structures was also proposed from direct effect of lightning. Later, the lightning protection technology will be verified by the ground test of lightning direct and indirect effects.

• 한국군사과학기술학회지
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• 제16권4호
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• pp.486-492
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• 2013

The pivoting composite wing is developed for the kit to be mounted on the external stores. The wing has a pivoting structure for the installation to an aircraft and high aspect ratio to increase lift drag ratio. The wing needs to be light and have sufficient strength and stiffness to satisfy structural design requirements. The wing is designed with carbon fiber composite and the structural parts are integrated to reduce cost to manufacture. In order to verify the structural performances, the design load analysis and flight load survey, the static analysis and test, the ground vibration test and flutter analysis are performed. It is shown that the wing has sufficient structural strength and stiffness to satisfy the structural design requirements.

• Progress in Superconductivity
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• 제13권1호
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• pp.1-6
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• 2011

Measurement of magnetic signals generated from electric activity of myocardium provides useful information for the functional diagnosis of heart diseases. Key technical component of the magnetocardiography (MCG) technology is SQUID. To measure MCG signals with high signal-to-noise ratio, sensitive SQUID magnetic field sensors are needed. Present magnetic field sensors based on Nb SQUIDs have field sensitivity good enough to measure most of MCG signals. However, for accurate measurement of fine signal pattern or detection of local atrial fibrillation signals, we may need higher field sensitivity. In addition to field sensitivity, economic aspect of the SQUID system is also important. To simplify the SQUID readout electronics, the output voltage or flux-to-voltage transfer of SQUID should be large enough so that direct measurement of SQUID output can be done using room-temperature preamplifiers. Double relaxation oscillation SQUID (DROS), having about 10 times larger flux-to-voltage transfers than those of DC-SQUIDs, was shown to be a good choice to make the electronics compact. For effective cancellation of external noise inside a thin economic shielded room, first-order axial gradiometer with high balance, simple structure and long-baseline is needed. We developed a technology to make the axial gradiometer compact using direct bonding of superconductive wires between pickup coil and input coil. Conventional insert has mechanical support to hold the gradiometer array, and the dewar neck has equal diameter with the dewar bottom. Boiling of the liquid He can generate mechanical vibrations in the gradiometer array due to mechanical connection structure. Elimination of the mechanical support, and direct mounting of the gradiometer array into the dewar bottom can reduce the dewar neck diameter, resulting in the reduction of liquid He consumption.