Wirbelerzeugungssystem, Zugehöriges Flugzeug und Verfahren zur Beurteilung Aerodynamischer Informationen

Details

Veröffentlichungs-Nr.

EP4725836

Anmeldetag

7. Oktober 2025

Veröffentlichung

15. April 2026

Rechtsraum

EP

IPC

B64C23/06

Abstract

This vortex generating system (18) comprises: - a vortex generator (16) comprising + a base (22), + a baffle (24), moveable in rotation around a rotation axis (R) relative to the base (22), and + an actuator (26), configured to move the baffle (24) in rotation around the rotation axis (R) relative to the base (22); and - a control unit (20), connected to the vortex generator (16) and comprising: + an acquisition module (36), configured for acquiring a target active position of the baffle (24), + a control module (34), configured for controlling the actuator (26) into an active configuration, in which the actuator (26) is applying a controlling torque to the baffle (24) depending on the acquired target active position, and + an evaluation module (40), configured for generating an inconsistency evaluation signal as a function of the controlling torque and of the target active position.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland