Verfahren und System zum Betrieb eines Hybriden Flugzeugmotors

Details

Veröffentlichungs-Nr.

EP4631857

Aktenzeichen

EP25169862

Anmeldetag

10. April 2025

Veröffentlichung

15. Oktober 2025

Rechtsraum

EP

IPC

B64D27/33B64D31/18B64D35/024B64D35/025

Abstract

The method can include operating the hybrid aircraft power plant (110) in a first mode of operation in which a plurality of controllable parameters including a fuel flow to the thermal engine (118) and an electric power to the electric motor (120) has a first set of values corresponding to a first power output; receiving a requested power output; determining a second set of values of the one or more of the controllable parameters to bring first power output to the requested power output; determining whether said second set of values poses a risk of undesired clutch behavior; and when the second set of values poses the risk, modulating the second set of values to avoid the risk and setting the plurality of controllable parameters to the modulated second set of values.

Anmelder

Firma

PRATT & WHITNEY CANADA CORP.

Land

🇨🇦 Kanada

Fachgebiete