| 摘要 |
A structural component for an aircraft or spacecraft having an outer skin, comprising at least one former element for reinforcing the outer skin. The former element is arcuately curved in accordance with an inner contour of the outer skin 10, wherein the former element has a plurality of first cutouts for receiving longitudinal reinforcements and at least one second cutout, which is configured between adjacent first cutouts of one or more former elements. The invention furthermore relates to an aircraft or spacecraft with the structural component according to the invention.
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