Patent ID: 8424804
Filing Date: 2013-04-23
Classification: B29C,B64C,Y02T

Abstract:
1. An attachment arrangement for attaching a component to a fuselage of an aircraft comprising stringers and frame elements, wherein the attachment arrangement comprises: an elongated stringer configured to be a part of the aircraft fuselage; and a fitting configured to be connected to the component; wherein the stringer comprises one of glass-fiber-reinforced plastic and carbon-fiber-reinforced plastic; wherein the stringer comprises more than two recesses formed one behind the other in the direction of longitudinal extension of the stringer; wherein the fitting comprises at least one engagement element configured for positive-locking engagement in the recesses of the stringer, and wherein the recesses in the stringer are arranged between neighboring frame elements so as to be equidistant at a spacing s between adjacent recesses.