Blockertüranordnung für eine Schubumkehrvorrichtung eines Flugzeugantriebssystems

Details

Veröffentlichungs-Nr.

EP4772734

Anmeldetag

7. Januar 2026

Veröffentlichung

8. Juli 2026

Rechtsraum

EP

IPC

F02K1/72

Abstract

A thrust reverser includes an outer fixed structure, an inner fixed structure, a translating sleeve (54), and a blocker door assembly (62). The outer fixed structure (56) and the inner fixed structure (58) extend circumferentially about an axis forming a thrust reverser duct (64). The translating sleeve further forms the thrust reverser duct. The blocker door assembly includes a blocker door (66), a drag link (68), and a clevis fitting (70). The blocker door is pivotably mounted to the translating sleeve. The drag link is pivotably mounted to the blocker door. The clevis fitting includes an articulating fitting member (78), a fixed fitting member (80), and a fixed plate (82). The articulating fitting member is pivotably mounted to the drag link about a first tangentially-extending rotational axis. The articulating fitting member is pivotably mounted to the fixed fitting member about a second axially-extending rotational axis. The fixed fitting member and the fixed plate are mounted to the inner fixed structure.

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete