Gondel mit einem Verschiebbaren Einlass für ein Flugzeugantriebssystem

Details

Veröffentlichungs-Nr.

EP3747775

Aktenzeichen

EP19212413

Anmeldetag

29. November 2019

Veröffentlichung

26. Oktober 2022

Erteilung

26. Oktober 2022

Rechtsraum

EP

IPC

B64D29/06B64D33/02F02C7/042

Abstract

A nacelle assembly includes a fixed inlet segment (56) and a translating inlet segment (58). The translating inlet segment (58) includes a slider beam (86) laterally between a pair of tracks (68;70) of the fixed inlet segment (56). The slider beam (86) is mated with and slidable longitudinally along the pair of tracks (68;70). The translating inlet segment (58) is configured to translate longitudinally between a retracted position and an extended position. An aft end (78) of the translating inlet segment (58) is abutted against a forward end (60) of the fixed inlet segment (56) when the translating inlet segment (58) is in the retracted position. An airflow inlet (46) into an inlet passage of the nacelle assembly is opened longitudinally between the aft end (78) and the forward end (60) when the translating inlet segment (58) is in the extended position.

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete