Hebeanordnung für eine Flugzeugtür

Details

Veröffentlichungs-Nr.

EP4403460

Aktenzeichen

EP24152937

Anmeldetag

19. Januar 2024

Veröffentlichung

4. März 2026

Erteilung

4. März 2026

Rechtsraum

EP

IPC

B64C1/14

Abstract

A door assembly (26) for an aircraft (20) includes a door (28), a door handle (34), a door hinge (32), a support assembly (50), and a lifting assembly (58). The door handle (34) is rotatable between an unlatched position and a latched position. The support assembly (50) rotatably mounts the door hinge (32) to the door (28). The lifting assembly (58) includes a latch cam (120), a lift track (123), and a latch idler (122). The latch cam (120) is mounted to the door handle (34), rotatable with the door handle (34) about the door handle rotational axis (124), and forms an eccentric roller path (126) extending about the door handle rotational axis (124). The latch idler (122) includes a first roller (146) and a second roller (148). The first roller (146) is disposed on a lift track (123) of the support assembly (50) and configured to roll along the lift track (123). The second roller (148) is disposed within the eccentric roller path (126). The latch idler (122) is configured to lift the door (28) as the door handle (34) rotates from the latched position to the unlatched position.

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete