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허선철(SunChul Huh),이광영(KwangYoung Lee),박원조(WonJo Park),김병화(ByungHwa Kim),정군석(GunSug Jung) 대한기계학회 2005 대한기계학회 춘추학술대회 Vol.2005 No.11
Wings for defense industry such as fighters, missiles, and rockets should have no deformation or damage on the structure, strength, and hardness safety of constituted pared and the structures near to the bodies. The structures of existing wings had holes for light weight and plates and frames were fixed with rivets or screws, thus, there were difficulties and limits in light weight. In this study, an improvement was made in current joint methods through EB welding and laser welding for light weight of wings and welding strength was measured through strength test. In addition, finite element analysis was performed for welding process so as to induce optimum welding condition.