Flugzeugsteuerfläche mit Linearantrieb

Details

Veröffentlichungs-Nr.

EP4227213

Aktenzeichen

EP23156649

Anmeldetag

14. Februar 2023

Veröffentlichung

16. August 2023

Rechtsraum

EP

IPC

B64C9/02// B64C9/00

Abstract

An aircraft assembly (20) includes an aircraft control surface (24) having a first skin (50), a second skin (52) and a support structure laterally between and connected to the first skin (50) and the second skin (52). The support structure includes a spar (60C), a first stiffener and a second stiffener. The spar extends spanwise within the aircraft control surface (24). The first stiffener extends longitudinally within the aircraft control surface to the spar. The second stiffener extends longitudinally within the aircraft control surface (24) to the spar (60C). An actuator receptacle projects longitudinally into the aircraft control surface (24) from a base (42) of the aircraft control surface (24) to the spar. The actuator receptacle extends spanwise within the aircraft control surface (24) between the first stiffener and the second stiffener.

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete