Gasturbinenmotor mit Drittem Strom

Details

Veröffentlichungs-Nr.

EP4760077

Anmeldetag

10. Dezember 2025

Veröffentlichung

17. Juni 2026

Rechtsraum

EP

IPC

F02C3/107, F02K3/06, F02K3/02

Abstract

A gas turbine engine includes a turbomachine having a compressor section, a combustion section, and a turbine section arranged in serial flow order. The turbomachine defines an engine inlet to an inlet duct, a fan duct inlet to a fan duct, and a core inlet to a core duct. The primary fan is driven by the turbomachine, and a secondary fan is located downstream of the primary fan within the inlet duct. One or more actuation devices operably associated with the fan duct, the one or more actuation devices actuable to increase or decrease an exit area of the fan duct.

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA