Metallic shell component for e.g. fuselage of aircraft, has coating area and/or base area of coating area provided with recess, such that thickness of coating area or base area is reduced within area of recess

摘要

The component (1) has a reinforcing unit (3) arranged at a coating area (2). The coating area and/or a base area (4) of the coating area are provided with a recess (5), such that thickness of the coating area (2) or the base area (4) is reduced within an area of the recess. The recess is arranged adjacent to the reinforcing unit. The recess is arranged such that the recess runs parallel to a connecting position of the coating area and the reinforcing unit, where the recess has a zigzag or wavelike shape.