• 항공우주기술
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• 제13권1호
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• pp.20-26
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• 2014

본 논문에서는 충격하중과 잔류 에너지 등의 충격거동에 대한 영향을 확인하기 위하여 항복응력, 탄젠트 강성계수 및 파단 변형률을 변화시켰다. 그리고 섬유금속 적층판의 좌굴거동을 수치해석을 이용하여 수행하였다. 좌굴 성능을 비교하기 위하여 섬유금속 적층판과 알루미늄 판에 대해 인장 및 압축하중에 대한 여러 가지 경우의 해석을 수행하였다. 또한 정적 성능을 평가하기 위하여 박스 보 구조물의 정적해석을 수행하였다. 알루미늄 2024 박판과 유리섬유/에폭시 프리프레그로 만든 섬유금속 적층판에 대한 저속충격 해석을 수행하였다. 그리고 좌굴 및 정적해석 결과를 이용하여 섬유금속 적층판과 알루미늄의 성능을 비교하였다. 구조적 성능 비교를 위하여 동일한 무게의 알루미늄 2024 박판에 대한 해석을 수행하였다.

• Journal of Welding and Joining
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• 제8권3호
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• pp.24-30
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• 1990

2024 Aluminium was welded by domestic manufactured continuous type friction welder. The problems and optimum condition were studied in 2024 Al-2024 Al cases. Mechanical tests and microstructure analysis were studeid. Interfacial temperature of welding was predicted by FDM. The obtained results are as follows: 1) In case of Al-Al, the optimum condition range was wide. 2) At the boundary zone, fine recrystallized zone was not harmful to the mechanical property and no growth of precipitation was observed. 3) In case of Al-Al, temperature gradient can be predictedby FDM and heat input can be taken as weld parameter.

• 한국기계가공학회지
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• 제11권1호
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• pp.39-45
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• 2012

Currently, the aircraft industry, aircraft parts as well as airframe have been developed in producing, the aircraft parts and fuselages have been produced the product by cutting rather than forging and casting because of the residual stress and stress concentration. In this study, the aircraft is being used in many parts of aluminium alloy 2024 in wire-cut E.D.M. The selected experimental parameters are peak current, no-load voltage, off time and feed rate. It is found that cutting mountain part on surface roughness of the curve 0.3mm than 0.25mm diameter wire electrode is stable in many uniform distribution.

• 한국해양공학회지
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• 제17권5호
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• pp.76-81
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• 2003

Friction welding of GCD45 spheroidal graphite cast iron and 2024 aluminum alloy has been studied, especially in terms of the joint faces and strength of friction welding. For appropriate results of the friction welding of GCD45 graphite cast iron and 2024 aluminum alloy, an insert of A1050 pure aluminum metal was used. The joint strength of the A1050 pure aluminum insert approached the maximum strength of 165.7Mpa, compared to 128MPa for the joint between GCD45 graphite cast iron and A1050 pure aluminum without the insert metal. Maximum strength, 165.7Mpa, was possible for the following optimum conditions: 20MPa for the friction pressure, P1, 60MPa for the upsetting pressure, P2, 1 second for the friction time, t1, 3000rpm for the rotation, N, and 0.3 seconds for the brake time, tB.

• 한국생산제조학회지
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• 제20권6호
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• pp.714-719
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• 2011

The surface roughness depending on the machining method is very important because is produce a finished product through riveting, sealing, bonding, and special paint in order to curb the turbulence and air resistance which occur between the sheets. Aluminum alloy 2024 which is widely used for interior and exterior material of aircraft are tested. Jin-young JW-60C wire cutting machine was used in this experiment. In this paper, the experimental investigation has been performed to find out the influence of the surface roughness and surface shape characteristics on the wire-cut EDM of discharge energy in aluminium alloy 2024. The selected experimental parameters are peak current, no-load voltage, off time and feed rate. The experimental results give the guideline for selecting reasonable machining parameters. The high discharge energy on the idle time, almost no change in surface roughness can be seen.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
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• pp.117.1-117.1
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• 2005

• 월간포장계
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• 통권372호
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• pp.92-99
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• 2024

• 월간포장계
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• 통권372호
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• pp.100-103
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• 2024

• 월간포장계
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• 통권374호
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• pp.36-43
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• 2024

• 월간포장계
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• 통권371호
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• pp.48-51
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• 2024