Mechanische Architektur für Verteiltes Klappenbetätigungssystem

Details

Veröffentlichungs-Nr.

EP4617166

Aktenzeichen

EP25163315

Anmeldetag

12. März 2025

Veröffentlichung

29. Oktober 2025

Rechtsraum

EP

IPC

B64C9/16// B64D45/00

Abstract

A mechanical architecture is provided for aircraft distributed flap actuation and includes a shaft (310) and first and second actuation units (320, 330). The first actuation unit (320) includes a motor, a first actuator for translating and rotating a flap and being connected to a first side of the flap, a first gearbox to transfer and increase torque from the motor to the first actuator and a first brake configured to hold the flap in place. The second actuation unit (330) includes a second actuator that receives the torque from the first gearbox via the shaft (310) for translating and rotating the flap and being connected to a second side of the flap, a second gearbox that receives the torque from the first gearbox via the shaft (310) and reduces the torque and a second brake receptive of the torque from the second gearbox and configured to hold the flap in place through the second actuator.

Anmelder

Firma

Goodrich Actuation Systems Limited

Land

🇬🇧 Großbritannien

Fachgebiete