| 摘要 |
Proposed is an attachment arrangement (1) for attaching a component to th e fuselage (3) of an aircraft, and an aircraft comprising such an attachment arrangement. The attachment arrangement (1) comprises an elongated stringer (5) that can be connected to the aircraft fuselage, and a fitting (11) that can be connected to the component. The stringer comprises a multitude of re cesses (9) that are formed one behind the other in the direction of longitud inal extension of the stringer. The fitting comprises at least one engagemen t element (13) that is adapted for positive-locking engagement in the recess es (9) of the stringer (5). The stringer and/or the fitting can comprise CFC . The fittings can also comprise various other plastics or metal. Weight sav ings are achieved while at the same time providing stable and variably-posit ionable attachment. Furthermore, a method for constructing a stringer for an attachment arrangement is proposed, in which method, by providing reinforce ment fibres adjacent to the recesses, a carbon scrim is locally reinforced a round the recesses.
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