Hybride Elektrische Einzelmotorabstiegsmodusaktivierungslogik

Details

Veröffentlichungs-Nr.

EP4174299

Aktenzeichen

EP22204554

Anmeldetag

28. Oktober 2022

Veröffentlichung

2. Juli 2025

Erteilung

2. Juli 2025

Rechtsraum

EP

IPC

F02C9/42F02K5/00

Abstract

A computer-implemented method includes determining a thrust requirement to satisfy a desired glide slope and determining, based on the thrust requirement, whether thrust matching can be maintained while operating a first gas turbine engine in a fuel-burning mode and operating a second gas turbine engine in an electrically powered mode. The method further includes, responsive to determining that thrust matching cannot be maintained, commanding fuel flow to a combustor of the second engine to cause the second gas turbine engine to operate in the fuel-burning mode.

Anmelder

Firmen

RTX Corporation
Raytheon Technologies Corporation

Land

🇺🇸 USA

Fachgebiete