Wing for aircraft, has absorption device arranged within flow outer contour with respect to depth direction of wing before fuel tank such that kinetic energy is converted into deformation energy during penetration of object via contour

摘要

The wing (10) has a supporting structure with a front spar (14) for retaining force acting on the wing. A flow outer contour (11) is provided in the supporting structure, and a fuel tank is arranged in an interior of the flow outer contour. An energy absorption device (18) is arranged within the flow outer contour with respect to depth direction of the wing before the fuel tank such that the kinetic energy is converted into deformation energy by the energy absorption device during penetration of the object through the flow outer contour.