Einlassstruktur eines Flugzeugantriebssystems mit Einlassbereich mit Variabler Luftströmung

Details

Veröffentlichungs-Nr.

EP4011779

Aktenzeichen

EP21214183

Anmeldetag

13. Dezember 2021

Veröffentlichung

16. Juli 2025

Erteilung

16. Juli 2025

Rechtsraum

EP

IPC

B64D33/02F02C7/042

Abstract

An assembly is provided for an aircraft propulsion system. This aircraft propulsion system assembly includes a nacelle inlet structure (58). The nacelle inlet structure (58) includes an inner inlet opening (64), an outer inlet opening (66) and a rotating structure (72). The rotating structure (72) extends circumferentially about the inner inlet opening (64). The rotating structure (72) is configured to rotate about an axis (76) between a first position and a second position. The rotating structure (72) at least partially closes the outer inlet opening (66) in the first position. The rotating structure (72) at least partially opens the outer inlet opening (66) in the second position.

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete