Verbindungsanordnung zur Übertragung von Lasten zwischen Zwei Flügelelementen

Details

Veröffentlichungs-Nr.

EP3584155

Aktenzeichen

EP19180901

Anmeldetag

18. Juni 2019

Veröffentlichung

24. März 2021

Erteilung

24. März 2021

Rechtsraum

EP

IPC

B64C13/28B64C9/02B64C9/14B64C9/22B64C3/50

Abstract

Described and claimed is a C-shaped connection assembly for transmitting loads in a load plane between a first wing element and a second wing element. The connection assembly comprises a first and a second L-shaped load-bearing device. Each load-bearing device comprises a joint region and two legs extending parallel to the load plane and away from the joint region towards respective end regions. One leg of the first load-bearing device extends parallel to one leg of the second load bearing device. These legs are connected to one another. Two coupling portions for connecting the connection assembly to the second wing element are formed in the respective joint regions of the load-bearing devices. Two further coupling portions for connecting the connection assembly to the first wing element are formed in respective free end region of the load-bearing device and the joint region of the second load-bearing device. Further, a slat assembly for a main wing of an aircraft and an aircraft comprising a slat assembly are described and claimed.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete