Verriegelungsanordnung für eine Flugzeugtür

Details

Veröffentlichungs-Nr.

EP4403461

Aktenzeichen

EP24152943

Anmeldetag

19. Januar 2024

Veröffentlichung

25. Februar 2026

Erteilung

25. Februar 2026

Rechtsraum

EP

IPC

B64C1/14

Abstract

An interlock assembly (52) for an aircraft door (28) includes a shaft (54), an interlock first portion (56), and an auto-disarm second portion (58). The shaft (54) is rotatable about a second rotational axis (60) between an armed position and a disarmed position. The shaft (54) includes an interlock cam (64) and an auto-disarm cam (66). In a first interlock position, the interlock first portion (56) permits rotation of the shaft (54) between the armed position and the disarmed position. In a second interlock position, the interlock first portion (56) prevents rotation of the shaft (54) from the disarmed position to the armed position. In a first auto-disarm position, the auto-disarm second portion (58) permits rotation of the shaft (54) between the armed position and the disarmed position. In a second auto-disarm position, the auto-disarm second portion (58) prevents rotation of the shaft (54) from the disarmed position to the armed position.

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete