Auslassleitschaufelanordnung für ein Turbofantriebwerk

Details

Veröffentlichungs-Nr.

EP4818508

Anmeldetag

23. März 2026

Veröffentlichung

7. Oktober 2026

Rechtsraum

EP

Abstract

A turbofan engine defining a circumferential direction is provided. The turbofan engine includes a turbomachine; an unducted rotor assembly drivingly coupled to the turbomachine, the unducted rotor assembly including a plurality of unducted rotor blades; and a plurality of outlet guide vanes positioned downstream of the plurality of unducted rotor blades, the plurality of outlet guide vanes each defining a span, the spans of the plurality of outlet guide vanes being nonuniform along the circumferential direction.

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA