Flüssigkeitsschöpfer für ein Schubumkehrsystem

Details

Veröffentlichungs-Nr.

EP4039962

Aktenzeichen

EP22155980

Anmeldetag

9. Februar 2022

Veröffentlichung

13. November 2024

Erteilung

13. November 2024

Rechtsraum

EP

IPC

F02K1/72

Abstract

An assembly (72) is provided for an aircraft propulsion system (20). This aircraft propulsion system assembly (72) includes a thrust reverser system (38). The thrust reverser system (38) includes a cascade structure (68) and a scoop (94). The cascade structure (68) is configured with a plurality of flow passages (92). Each of the flow passages (92) extends through the cascade structure (68). The flow passages (92) include a first flow passage (92A). The scoop (94) is configured to direct fluid into at least the first flow passage (92A). The scoop (94) includes a serrated leading edge (102).

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete