• Title/Summary/Keyword: 샌드위치 타입

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High efficiency flyback converter using coaxial cable transformer (동축권선 트랜스포머를 이용한 고효율 플라이백 컨버터)

  • Kim, Do-Hyun;Moon, Sol;Kim, Chan-In;Park, Joung-hu
    • Proceedings of the KIPE Conference
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    • 2011.11a
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    • pp.187-188
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    • 2011
  • 본 논문은 SMPS 및 가전기기와 휴대 전자기기 등에서 전원회로로 폭넓게 사용되고 있는 플라이백 컨버터의 트랜스포머를 기존의 샌드위치권선 방식이 아닌 동축권선 방식을 적용하여 기존의 샌드위치권선 방식보다 우수한 1,2차 커플링을 지니는 트랜스포머를 제안한다. 제안된 트랜스포머를 적용한 컨버터는 기존의 컨버터에 비하여 동일한 조건에서 보다 우수한 효율을 나타내고 있다. 제안된 컨버터용 트랜스포머의 구조 및 커플링을 설명하고 커플링계수를 비교 한 후 34[W]급 프로토 타입을 이용하여 검증하였다.

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Design of Dual Pressure Regulator (이중압력 조절기 설계)

  • Kim, Dong-Soo;Kim, Kang-Dae;Kim, Myoung-Sub
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.1226-1229
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    • 2008
  • In this paper, we designed sandwich type pressure regulator for air pressure control system. As a result of research, we obtained several important conclusions. First, we decided theory of poppet valve and relief valve which are used in sandwich type pressure regulator, and then designed prototype of pressure regulator. Second, we organized circuit diagram of dual pressure regulator of air pressure control system.

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Screen Printed Power Inductors for Miniaturized DC-DC Converter Applications (스크린 인쇄 기법을 이용한 초소형 DC-DC 컨버터용 파워인덕터)

  • Bang, Dong-H.;Park, Jae-Y.
    • Proceedings of the KIEE Conference
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    • 2008.07a
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    • pp.1395-1396
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    • 2008
  • 본 논문에서는 초소형 DC-DC 컨버터에 쓰이는 파워인덕터를 설계하였다. 제안된 인덕터는 Ni-Zn 페라이트와 Polyimide 혼합물질을 이용하여, 경화온도를 낮추어 유기기판(FR-4)에서도 적용될 수 있는 인덕터를 설계했다. 인덕터의 크기는 $5mm{\times}4.5mm{\times}0.5mm$ 이고, 도선의 물질은 구리(Cu)를 사용하였으며, 18${\mu}m$의 두께, 85${\mu}m$의 선폭, 85${\mu}m$의 선 간격으로 디자인 하였다. 그리고 구조는 2층 적층의 스파이럴 구조를 제안하여 소형화에 보다 유리하도록 설계를 하였다. 페라이트 혼합물질을 샌드위치 타입으로 EMI shielding한 인덕터의 경우 동작 주파수 5MHz에서 912nH의 인덕턴스, 29의 품질계수 특성을 나타냈으며, 그 결과 초소형 DC-DC 컨버터용 인덕터로서 소형화와 높은 효율을 만족하였다.

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Manufacture and Qualification of Composite Main Reflector of High Stable Deployable Antenna for Satellite (위성용 전개형 고안정 반사판 안테나 주반사판 제작 및 검증)

  • Dong-Geon Kim;Hyun-Guk Kim;Dong-Yeon Kim;Kyung-Rae Koo;Ji-min An;O-young Choi
    • Composites Research
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    • v.37 no.3
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    • pp.219-225
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    • 2024
  • It is essential to develop a light-weight, high-performance structure for the deployable reflector antenna, which is the payload of a reconnaissance satellite, considering launch and orbital operation performance. Among them, the composite main reflector is a key component that constitutes a deployable reflector antenna. In particular, the development of a high-performance main reflector is required to acquire high-quality satellite images after agile attitude control maneuvers during satellite missions. To develop main reflector, the initial design of the main reflector was confirmed considering the structural performance according to the laminate stacking design and material properties of the composite main reflector that constitutes the deployable reflector antenna. Based on the initial design, four types of composite main reflectors were manufactured with the variable for manufacturing process. As variables for manufacturing process, the curing process of the composite structure, the application of adhesive film between the carbon fiber composite sheet and the honeycomb core, and the venting path inside the sandwich composite were selected. After manufacture main reflector, weight measurement, non-destructive testing(NDT), surface error measurement, and modal test were performed on the four types of main reflectors produced. By selecting a manufacturing process that does not apply adhesive film and includes venting path, for a composite main reflector with light weight and structural performance, we developed and verified a main reflector that can be applied to the SAR(Synthetic Aperture Rader) satellite.

Study on Weight Reduction of Urban Transit Carbody Based on Material Changes and Structural Optimization (도시철도차량 차체의 경량화를 위한 소재 변경 및 구조체 최적화 연구)

  • Cho, Jeong Gil;Koo, Jeong Seo;Jung, Hyun Seung
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.9
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    • pp.1099-1107
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    • 2013
  • This study proposes a weight reduction design for urban transit, specifically, a Korean EMU carbody made of aluminum extrusion profiles, according to size optimization and useful material changes. First, the thickness of the under-frame, side-panels, and end-panels were optimized by the size optimization process, and then, the weight of the Korean EMU carbody could be reduced to approximately 14.8%. Second, the under-frame of the optimized carbody was substituted with a frame-type structure made of SMA 570, and then, the weight of the hybrid-type carbody was 3.8% lighter than that of the initial K-EMU. Finally, the under-frame and the roof-panel were substituted with a composite material sandwich to obtain an ultralight hybrid-type carbody. The weight of the ultralight hybrid-type carbody was 30% lighter than that of the initial K-EMU. All the resulting carbody models satisfied the design regulations of the domestic Performance Test Standard for Electrical Multiple Unit.

Survey on Chicken Housing Types in Different Farm Scale and Region (양계농가의 사육규모별, 지역별 계사 시설현황 분석)

  • Choi, H.C.;Kham, D.H.;Na, J.C.;Bang, H.T.;Yu, D.J.;Suh, O.S.;Song, J.I.;Jeon, B.S.;Jeon, J.H.;Yoo, Y.H.;Lee, S.C.;Kim, J.S.;Lee, D.H.
    • Journal of Animal Environmental Science
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    • v.15 no.3
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    • pp.189-198
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    • 2009
  • This survey was conducted to investigate the situation of housing type in poultry farms in Korea. The number surveyed among the farm size over 30,000 heads was 1,965 farms. Poultry housing types of windowless, open sided, vinyl house type were 19.0, 47.7, 19.8%, respectively. Waterers of nipple, bell, and 8 feet trough used in smaller than 50,000 heads of poultry farm were 40.6, 11.3 and 42.8%, respectively. But the bigger farm in the farm size of over 100,000 heads used more nipple waterer. Feeders of disk, hopper and chain used in poultry farm were 54.5, 16.3, 15.8%, respectively. Manure collecting system of scraper and belt was 29.4, 71.5 %, respectively. Ventilation systems of natural ventilation, natural + mechanical ventilation, mechanical ventilation were 40.5, 39.8, 20.7%, respectively.

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