• Title/Summary/Keyword: 알루미늄 보강판넬

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Collapse Analysis of Ultimate Strength for the Aluminium Stiffened Plate subjected to Compressive Load (알루미늄 보강판의 압축 최종강도 붕괴 해석)

  • Park, Joo-Shin;Ko, Jae-Yong;Kim, Yun-Young
    • Journal of Navigation and Port Research
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    • v.31 no.10
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    • pp.825-831
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    • 2007
  • The use of high-strength aluminum alloys for ship and offshore structure generally has many benefits compared to the structural steels. These materials are used widely in a variety of fields, especially in the hull and deck of high speed craft, box-girder of bridges, deck and side plates of offshore structure. The structural weight can be reduced using these aluminum structure, which can enable high speed The characteristics of stress-strain relationship of aluminum structure are fairly different from the steel one, because of the influence of Heat Affected Zone(HAZ) by the welding processing. The HAZ of aluminum is much wider than that of steel with its high heat conductivity. In this paper, the ultimate strength characteristics of aluminum stiffened panel subjected to axial loading, such as the relationship between extent of HAZ and the behavior of buckling/ultimate strength, are investigated through the Finite Element Analysis with varying its range.

Thermal Characteristics Investigation of 6U CubeSat's Deployable Solar Panel Employing Thermal Gap Pad (열전도 패드가 적용된 6U 큐브위성용 태양전지판의 열적 특성 분석)

  • Kim, Hye-In;Kim, Hong-Rae;Oh, Hyun-Ung
    • Journal of Aerospace System Engineering
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    • v.14 no.3
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    • pp.51-59
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    • 2020
  • In the case of cubesat, a PCB-based deployable solar panel advantageous in terms of weight reduction and electrical circuit design is widely used considering the limited weight and volume of satellites. However, because of the low thermal conductivity of PCB, there is a limit relative to heat dissipation. In this paper, the thermal gap pad is applied to the contact between the PCB-based solar panel and the aluminum stiffener mounted on the outside of the panel. Thus, the heat transfer from the solar cell to the rear side of the panel is facilitated. It maximizes the heat dissipation performance while maintaining the merits of PCB panel, and thus, it is possible to improve the power generation efficiency from reducing the temperature of the solar cell. The effectiveness of the thermal design of the 6U cubesat's deployable solar panel using the thermal gap pad has been verified through on-orbit thermal analysis based on the results, compared with the conventional PCB-based solar panel.