Gehäusestruktur für ein Antriebssystem eines Luftfahrzeugs mit Offenem Rotor

Details

Veröffentlichungs-Nr.

EP4821822

Anmeldetag

13. April 2026

Veröffentlichung

14. Oktober 2026

Rechtsraum

EP

IPC

B64D27/12, B64D27/40

Abstract

An assembly for an aircraft propulsion system (20) includes a housing structure (54). The housing structure (54) includes an engine case assembly (106) and a nacelle (108). The nacelle (108) is disposed radially outboard of the engine case assembly (106). The nacelle (108) forms at least a portion of an exterior flow boundary (56) for the aircraft propulsion system (20) that borders an environment (22) external to the aircraft propulsion system (20). The nacelle (108) includes a nacelle interior skeletal structure (140) mounted to the engine case assembly (106) at a forward mount (146) and an aft mount (148).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete