Patent · US Active

Actuator arrangement for a wing assembly of an aircraft

US12286228B2 · kind B2 · utility

0Cited by

2References

19Claims

0Family size

Assignee

AIRBUS OPERATIONS LIMITED · DE

Inventors

Luc Andreani · Hamburg, DE
Florian Lorenz · Hamburg, DE

Key dates

Filing date	May 30, 2023
Grant date	Apr 29, 2025
Priority date	—
Expiry date	Jul 24, 2043

Classification

Technology area (CPC B)Performing Operations; Transporting
CPC primaryB64C9/16
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

A actuator arrangement is disclosed in which the high-lift device support that supports and guides movement of a high-lift device, such as a flap, is in axial alignment with a control actuator assembly that controls one or more control surfaces. This allows a single support fairing to be sufficient for covering both the track member and the control actuator assembly and allowing for reduced drag and weight.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.