AIRCRAFT COMPONENT WITH PANELS STIFFENED WITH STRINGERS

摘要

Aircraft component with panels (11) stiffened with stringers (15) configured with a web (17) and several feet (19) in which there are zones of potential intersection or interference of said stringers (15) with spars (25) and ribs (27), in which the configuration of the ends of the stringers (15) affected by said intersections or interferences include a first section (41) in which the height of the web (17) of the stringer (15) decreases until it disappears and the width of the feet (19) increases until a predetermined width A is reached and a second section (43) with several extended feet (23) of said predetermined width A and having no web (17), said first section (41) having the mechanical means (31) to join the end of the stringer (15) to the skin (13). The invention also relates to a method for manufacturing said panels (11).