• 제목/요약/키워드: 샌드위치 코어

검색결과 62건 처리시간 0.015초

Size Effects in the Failure of Simple Supported Sandwich Slab Bridges (단순지지된 샌드위치 슬래브교량의 파괴시 치수효과)

  • Han, Bong-Koo;Kim, Duck-Hyun
    • Journal of the Korea institute for structural maintenance and inspection
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    • 제14권3호
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    • pp.83-90
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    • 2010
  • Composite materials can be used economically and efficiently in civil engineering applications when standards and procedure for analysis, design, construction and quality control are to be established. Bridge systems, including the girders and cross-beams, and concrete decks behave as the specially orthotropic plates. For such systems with sections, boundary conditions other than Navier solution types, it is very difficult to obtain its analytical solution. To design the bridge made by the composite materials, cross-section was used as the form-core shape for economical reason and finite difference method was used for output of the stress value. The Tsai-Wu failure criterion for stress space is used. In this paper, the rate of tensile strength reduction due to increased size was considered. And also numerical study is made for these cases.

Design and Analysis of Composite Reflector of High Stable Deployable Antenna for Satellite (위성용 전개형 고안정 반사판 안테나 복합재 주반사판 설계 및 해석)

  • Dong-Geon Kim;Kyung-Rae Koo;Hyun-Guk Kim;Sung-Chan Song;Seong-Cheol Kwon;Jae-Hyuk Lim;Young-Bae Kim
    • Composites Research
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    • 제36권3호
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    • pp.230-240
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    • 2023
  • The deployable reflector antenna consists of 24 unit main reflectors, and is mounted on a launch vehicle in a folded state. This satellite reaches the operating orbit and the antenna of satellite is deployed, and performs a mission. The deployable reflector antenna has the advantage of reduce the storage volume of payload of launch vehicle, allowing large space structures to be mounted in the limited storage space of the launch vehicle. In this paper, structural analysis was performed on the main reflector constituting the deployable reflector antenna, and through this, the initial conceptual design was performed. Lightweight composite main reflector was designed by applying a carbon fiber composite and honeycomb core. The laminate pattern and shape were selected as design variables and a design that satisfies the operation conditions was derived. Then, the performance of the lightweight composite reflector antenna was analyzed by performing detailed structural analysis on modal analysis, quasi-static, thermal gradient, and dynamic behavior.