• 대한기계학회논문집A
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• 제25권1호
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• pp.115-126
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• 2001

In this paper, through a series of comparative experiments, effects of two different cure processing methods, cocure and precure, on the mechanical properties of honeycomb core materials for aircraft applications are considered. Mass of moisture accumulated into the closed cells of the sandwich panel specimen from the measured mass of moisture diffused to the full saturation state into the elements(skin, adhesive layer, Nomex honeycomb), consisting the honeycomb sandwich specimen has been calculated. Water reservoir of 70$\^{C}$ was used to have specimens absorb moisture to see the influence of moisture absorbed into sandwich panel on its mechanical properties. For the repair condition holding for 2 hours at 177$\^{C}$(350℉) temperature, a pressure due to the vapor expansion in each cell of the sandwich panel, which may result in the local separation of the interface between laminated skin and the surface of the honeycomb, has been estimated by vapor pressure-temperature relation from the thermodynamic steam table and compared to the pressure from the ideal gas state equation. The bonding strengths of the laminated skins on the flat surface of the Nomex honeycomb have been compared by the flatwise tension test and climbing drum peel test performed at room temperature for dry, wet and wet-repair specimens, respectively.

• 대한기계학회논문집A
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• 제24권10호
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• pp.2520-2528
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• 2000

Mechanical and physical properties of composite materials make a great difference due to their cure process condition. In order to clarify the effect of cure process condition on the microscopic damage behavior and failure mechanism of Carbon/Epoxy composites, three point bend test has been performed. For this purpose, two kinds of specimens with single adhesive and multiple adhesive layers were prepared. For single adhesive layer, four different types of specimen were used, that is, non-sanding, sanding, cocured, laminated specimens. Three different types of specimen were also used for the multiple adhesive layer, non-sanding, sanding, cocured specimens. Acoustic emission technique has also been employed to monitor the damage progresses associated with each micro-failure mechanism. The characteristics of AE parameters associated with micro-failure mechanism of each specimen were discussed.

• 공업화학
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• 제7권4호
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• pp.691-697
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• 1996

천연고무 라텍스(NRL)와 각종 첨가제를 배합 숙성하여 NR 필름을 제조하였고, 클로로프렌고무 라텍스 (CRL)를 일정한 비율로 블렌드하여 NR/CR 필름을 제조하였다. 이들 필름의 전가류 시간에 따른 팽윤도와 기계적 성질의 변화를 측정한 결과, 팽윤도 80~85%, 전가류 시간 48~60hrs등에서 가장 우수하였고, CRL의 블렌드 비율이 증가함에 따라 인장강도는 감소하고 신장율은 증가하는 경향을 나타내었다. 제조공정을 달리하여 제조한 시편의 기계적특성을 비교한 결과, 1회 디핑법을 사용한 NR/CR 필름의 인장강도, 인열강도는 2회 디핑한 NR-d-CR 필름보다 더 우수하였다. 이들 시편의 표면을 SEM으로 관찰한 결과, CRL의 블렌드 비율이 증가할수록 필름 표면의 벌크한 집합체가 증가되는 것으로 보아 상분리가 일어났음을 관찰할 수 있었다.