Fahrwerkstürsystem für einen Fahrwerksraum

Details

Veröffentlichungs-Nr.

EP4026769

Aktenzeichen

EP21216356

Anmeldetag

21. Dezember 2021

Veröffentlichung

20. März 2024

Erteilung

20. März 2024

Rechtsraum

EP

IPC

B64C25/16

Abstract

A landing gear door system (20) for a landing gear compartment includes a door (22) pivotable about a pivot pin (44) configured for disposition in a longitudinal direction (21) on an airframe (10), and a mechanism (50) configured to rotate the door (22) about the pivot pin (44) between a closed position, in which an outer surface of the door panel (24) is configured to provide aerodynamic continuity with an outer aircraft skin of the airframe (10), and an open position, in which the door is rotated into the landing gear compartment and an opening is exposed. The door (22) has a door panel rigidly connected with an arm (30) such that the door panel (24) and arm (30) generally form a V-shape as viewed in the longitudinal direction (21).

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete