Verriegelungssystem für eine Schubumkehrvorrichtung eines Flugzeugs

Details

Veröffentlichungs-Nr.

EP4756208

Anmeldetag

31. Oktober 2025

Veröffentlichung

10. Juni 2026

Rechtsraum

EP

IPC

F02K1/72

Abstract

A locking system to secure a trans cowl to a frame of a thrust reverser on an engine of an aircraft. The locking system includes an arm that is connected to the trans cowl with the arm having a receptacle. A lock includes a body and a pin with the pin movable relative to the body and with the lock positionable between a locked position and an unlocked position. In the locked position, the pin is in an extended position relative to the body that extends into the receptacle to secure the trans cowl in a stowed position. In the unlocked position, the pin is in a retracted position relative to the body that is away from the arm to enable the trans cowl to move to a deployed position. (Fig. 1)

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA