System and method for detecting an uncommanded high thrust (UHT) event in an aircraft. The method comprises enabling a UHT function associated with an engine when an enabling condition has been met. When the UHT function is enabled, the UHT event is detected when a power lever of the aircraft is at a given position, a parameter indicative of engine speed or power is above a first threshold, and a rate of change of the engine speed is above a second threshold. In response to detecting the UHT event, an alert is output to trigger accommodations to the UHT event for the engine.
SYSTEM AND METHOD FOR DETECTING AN UNCOMMANDED OR UNCONTROLLABLE HIGH THRUST EVENT IN AN AIRCRAFT
SYSTEME ET PROCEDE DE DETECTION D`UN EVENEMENT PUISSANT NON SOLLICITE OU INCONTROLABLE DANS UN AERONEF
2020-11-13
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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