Flugzeugmotorleistungsverwaltung für Grosse Generatorlasten

Details

Veröffentlichungs-Nr.

EP4786771

Anmeldetag

9. Januar 2026

Veröffentlichung

5. August 2026

Rechtsraum

EP

IPC

F02C9/28, F02C9/18, F02C9/20

Abstract

A method and system for managing increases in electrical loads in an aircraft engine has been developed. First, demand for an increased electrical load for an electrical generator of the aircraft engine is detected. Notification of the demand for the increased electrical load is transmitted to the aircraft engine full authority digital engine control system (FADEC). The FADEC calculates the necessary power management adjustments to maintain aircraft engine turbine temperature and adjustments to the compressor variable vane and surge bleed valve schedules. The FADEC then commands the adjustment in the aircraft engine power setting parameter, compressor variable vane position, and surge bleed valve position.

Anmelder

Firma

Honeywell International Inc.

Land

🇺🇸 USA

Fachgebiete