Lamelle für einen Flugzeugflügel

Details

Veröffentlichungs-Nr.

EP3708487

Aktenzeichen

EP20157456

Anmeldetag

14. Februar 2020

Veröffentlichung

5. April 2023

Erteilung

5. April 2023

Rechtsraum

EP

IPC

B64C9/24B64C9/02

Abstract

A slat (108) for the leading edge of a swept aircraft wing includes slat tracks (114) that dictate the path of movement of the slat as it moves from a retracted positon (Figure 7) to a fully deployed position (Figure 15). Each slat track (114) has a shape that follows a helical path. The motion of the slat thus includes a component of rotation about a first axis, which may be perpendicular to the line of flight (120) and a component of translational movement parallel to the first axis. When viewed from above the slat may move predominantly in a direction parallel to the line of flight (120).

Anmelder

Firma

Airbus Operations Limited

Land

🇬🇧 Großbritannien

Fachgebiete