Strukturanordnungen für Flugzeuge

Details

Veröffentlichungs-Nr.

EP4600140

Aktenzeichen

EP24275006

Anmeldetag

7. Februar 2024

Veröffentlichung

13. August 2025

Rechtsraum

EP

IPC

B64C1/06B64C1/08B64C1/12

Abstract

A structural assembly for an aircraft comprises: a frame structure comprising a plurality of structural members each having a longitudinal axis; at least one skin arranged on the frame structure; and at least one connecting element. The at least one connecting element comprises: a first portion configured to conformably interface with at least a portion of the at least one skin; and a second portion configured to rotationally receive at least a portion of one of said structural members, such that said connecting element is rotationally movable relative to said structural member about the longitudinal axis thereof. A method of manufacturing a structural component for an aircraft comprises providing said structural assembly; arranging the at least one connecting element on said structural member; rotationally adjusting the at least one connecting element relative to said structural member; arranging the at least one skin on the first portion of the at least one connecting element; attaching the at least one connecting element to said structural member; and attaching the at least one skin on the first portion of the at least one connecting element.

Anmelder

Firma

BAE SYSTEMS plc

Land

🇬🇧 Großbritannien

Fachgebiete