Hybrides Flugzeugantriebssystem

Details

Veröffentlichungs-Nr.

EP4779145

Anmeldetag

19. Januar 2026

Veröffentlichung

22. Juli 2026

Rechtsraum

EP

IPC

F02K3/06, F02K5/00

Abstract

An apparatus is provided for an aircraft that includes a turbine engine (24). The turbine engine (24) includes a compressor section (42), a combustor section (44), a turbine section (46), a support structure (110), a first rotor system (92) and a second rotor system (92). The support structure (110) extends axially along an axis (34). Each rotor system (92) may include an electric machine (96) and a bladed rotor (94). The electric machine (96) includes an electric machine stator (108) and an electric machine rotor (106). The electric machine stator (108) is mounted to the support structure (110). The electric machine rotor (106) circumscribes the electric machine stator (108) and is operatively coupled to the bladed rotor (94). The electric machine (96) is configured to generate an electromagnetic field with the electric machine stator (108) and the electric machine rotor (106). The bladed rotor (94) is configured to rotate about the axis (34).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete