Stützanordnung für einen Hochauftriebskörper, Hochauftriebskörperanordnung sowie Flügel und Flugzeug

Details

Veröffentlichungs-Nr.

EP4778830

Anmeldetag

2. Oktober 2025

Veröffentlichung

22. Juli 2026

Rechtsraum

EP

IPC

B64C9/18, B64C9/02, B64C9/24

Abstract

A support assembly (10) for a high lift body (8), in particular a leading-edge-slat, configured to be mounted to a spar (6) of a wing (3) of an aircraft (1), as well as a corresponding high lift body arrangement (4), a wing (3) and an aircraft (1) are provided, the support assembly (10) comprising at least two hinging organs (30) each providing at least one hinge point (G) configured for hinging the high lift body (8) at the spar (6) movably between a stowed position (S) and a deployed position (T) along a motion path (E) involving a translatory component (I, J, L) extending within a deployment plane (P) extending transversely with respect to a mounting plane (H) provided by the spar (6) for mounting the hinging organs (30) to the spar (6).

Anmelder

Firma

AIRBUS Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete