Gasturbinenbeschleunigungsgrenzwertvorspannung für Vorzeitig Asymmetrische Betriebsprogrammausgänge

Details

Veröffentlichungs-Nr.

EP4745382

Anmeldetag

14. November 2025

Veröffentlichung

20. Mai 2026

Rechtsraum

EP

IPC

F02C9/28, F02C9/42

Abstract

A method (200; 300) includes sending a first control signal (205; 305), wherein the first control signal causes a turbine engine of a plurality of turbine engines of an aircraft to initiate an entry into an asymmetric operating regime (210). The method further includes receiving a control input for an exit from the asymmetric operating regime (215; 310), determining a progression state of the turbine engine into the asymmetric operating regime (220a, 225a, 225b; 315), and sending a second control signal for accelerating the turbine engine to a high-power operating regime (227, 229; 320), wherein the second control signal specifies an acceleration rate based on the progression state of the turbine engine into the asymmetric operating regime.

Anmelder

Firma

Pratt & Whitney Canada Corp.

Land

🇨🇦 Kanada

Fachgebiete