Antriebssystem für ein Flugzeug mit Offenem Rotor und Kühlkreislauf für ein Elektromaschinensystem

Details

Veröffentlichungs-Nr.

EP4775816

Anmeldetag

9. Januar 2026

Veröffentlichung

15. Juli 2026

Rechtsraum

EP

Abstract

An apparatus is provided for an aircraft that includes an open rotor propulsion system (20). The open rotor propulsion system (20) includes a turbine engine (32), a first electric machine (100A), a second electric machine (100B), a first controller (102A), a second controller (102B) and a first fluid circuit (134). The first controller (102A) is configured to control operation of the first electric machine (100A). The second controller (102B) is configured to control operation of the second electric machine (100B). The first fluid circuit (134) is configured to circulate a first liquid to cool and/or lubricate the first electric machine (100A), the first controller (102A), the second electric machine (100B) and the second controller (102B).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA