Betrieb eines Flugzeugantriebssystems Während eines Motorunoperativen Ereignisses

Details

Veröffentlichungs-Nr.

EP4722519

Anmeldetag

21. April 2023

Veröffentlichung

8. April 2026

Rechtsraum

EP

IPC

F02C9/42(DROLET MARTIN et al.)

Abstract

A method for operating an aircraft (22) having a first propulsion unit (28A) and a second propulsion unit (28B). During this method a propulsion unit-inoperative event is identified where the first propulsion unit (28A) is inoperative and the second propulsion unit (28B) is operative. A trimmed parameter for the second propulsion unit (28B) is converted to an actual parameter for the second propulsion unit (28B). The actual parameter is monitored over a period of time the second propulsion unit (28B) operates during the propulsion unit-inoperative event. An action is performed in response to determining that the second propulsion unit (28B) has operated for at least a time threshold with the actual parameter being equal to or greater than a parameter threshold.

Anmelder

Firma

Pratt & Whitney Canada Corp.

Land

🇨🇦 Kanada

Fachgebiete