• Title/Summary/Keyword: External Mounting Structure

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Structural Design of pod system for Helicopter Captive Flight Test (헬리콥터 탑재 비행 시험을 위한 파드 시스템 구조 설계)

  • Choi, Jang-Seob
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.6
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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.

Wind load analysis for designing a tracking solar generator (추적식 태양광 발전기 설계를 위한 풍하중 해석)

  • Kim, Young-Eun;Jeong, Kyu-Won;Lee, Jae-Jin
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.2
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    • pp.672-680
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    • 2017
  • A solar photovoltaic system is composed of a module mounting structure, supporting trunk, and a control unit that supplies generated electrical power to an external power grid or a load. The efficiency of the system depends on the incident solar light, so the mounting structure is installed to face the sun. However, because the sun always moves, systems that track the sun have better efficiency than fixed systems. The structure experiences wind pressure, snow load, seismic load, and structure weight. The wind pressure has the most serious effect on the structure. The pressure was obtained using finite element method for various gaps between modules and angles between the panel and the ground. The wind pressure is lowest when the gap is zero, and it increases with the inclination angle. Based on the results, a mounting structure module was designed.

Temperature Variation Corresponding to the Protection Method and Edge Distance in Near-Surface-Mounted FRP in Concrete with Fire Protection (콘크리트내 표면매립보강된 FRP의 내화단열방법과 연단거리에 따른 온도변화)

  • Lim, Jong-wook;Seo, Soo-yeon
    • Journal of the Architectural Institute of Korea Structure & Construction
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    • v.35 no.11
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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 $800^{\circ}C$.

Magnetic-Shielding Effectiveness Analysis of the Trigger Assembly of Small Arms (소구경 개인화기 격발신호 발생장치의 자기차폐효과 분석)

  • Lee, Kisu;Ahn, Joon Mo;Chae, Je-Wook
    • Journal of the Korea Institute of Military Science and Technology
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    • v.21 no.4
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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.

A Study on the Characteristic of Variable Impedance Line using DGS (DGS를 이용한 가변 임피던스 선로 특성에 관한 연구)

  • Kim Young-Ju;Joung Myoung-Sub;Park Jun-Seok;Cho Hong-Goo
    • The Transactions of the Korean Institute of Electrical Engineers C
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    • v.54 no.1
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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.

Design and Evaluations of Underwater Hydrophone with Self Noise Suppressing Structures -Part Ⅰ. Noise Transfer Characteristics & Effects of Structure Modifications - (저 잡음 수중 청음기의 설계 방안 연구 -Ⅰ. 잡음 전달 특성 및 구조 변경 영향 -)

  • Im, Jong-In;Roh, Young-Rae
    • The Journal of the Acoustical Society of Korea
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    • v.16 no.2
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    • pp.10-15
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    • 1997
  • The hydrophones is mounted in many applications on a vibrating surface and functions as an underwater acoustic signal receiver without sensing the vibrations from the mounting surface. However, their performance is usually degraded by the interference of exterior noises such as acoustic cavitation in water stream, host structural vibration in the hull, and propeller motions. This paper describes the design and evaluation of a self noise suppressing hydrophones which shows very poor sensitivity to the external noises, first, effects of the external noise on the its receiver performance is simulated with finite element method(FEM). Second, the geometrical variations are implemented on the original structure that include additional air pockets and acoustic walls which work as acoustic shied or scatter of the noises. The results show that the effect of the external noise is the most significant when it is applied near to the bottom of the side wall of the hydrophones. The transverse noise induced by the outside water flow is isolated most effectively when a thin compliant (damping) layer combined with two air pockets is inserted to the circumference of the nose. Noise level is reduced about fifty nine percent of that of the original structure.

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Design and Strength Analysis of a Mast and Mounting Part of Dummy Gun for Multi-Mission Unmanned Surface Vehicle (복합임무 무인수상정의 마스트 및 특수임무장비 장착부 설계 및 강도해석)

  • Son, Juwon;Kim, Donghee;Choi, Byungwoong;Lee, Youngjin
    • The Journal of Korean Institute of Information Technology
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    • v.16 no.11
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    • pp.51-59
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    • 2018
  • The Multi-Mission Unmanned Surface Vehicle(MMUSV), which is manufactured using glass Fiber Reinforced Plastic(FRP) material, is designed to perform a surveillance and reconnaissance on the sea. Various navigation sensors, such as RADAR, RIDAR, camera, are mounted on a mast to perform an autonomous navigation. And a dummy gun is mounted on the deck of the MMUSV for a target tracking and disposal. It is necessary to analyze a strength for structures mounted on the deck because the MMUSV performs missions under a severe sea state. In this paper, a strength analysis of the mast structure is performed on static loads and lateral external loads to verify an adequacy of the designed mast through a series of simulations. Based on the results of captive model tests, a strength analysis for a heave motion of the mast structure is conducted using a simulation tool. Also a simulation and fatigue test for a mounting part between the MMUSV and the dummy gun are performed using a specimen. The simulation and test results are represented that a structure of the mast and mounting part of the dummy gun are appropriately designed.he impact amount are performed through simulation and experiments.

Protection Design and Lightning Zone Analysis for Unmanned Aerial Vehicle with Composite Wings (복합재 주익 무인항공기의 낙뢰보호 설계와 피격영역 해석)

  • Hee-chae Woo;Yong-Tae Kim
    • Journal of the Korea Institute of Military Science and Technology
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    • v.26 no.3
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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.

A Development of Pivoting Composite Wing for Mounting Kit (키트용 접이식 복합재 날개 개발)

  • Joo, Young-Sik;Jun, Woo-Chul;Byun, Kwan-Hwa;Cho, Chang-Min
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.4
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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.

Review of SQUID Sensors for Measuring Magnetocardiography (심자도 측정을 위한 SQUID 센서 기술의 개발 현황)

  • Lee, Y.H.;Kim, J.M.;Yu, K.K.;Kim, K.;Kwon, H.
    • Progress in Superconductivity
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    • v.13 no.1
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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.