Device i.e. aircraft condition monitoring system, for monitoring engine of aircraft e.g. ARINC 429, has processing unit for triggering acquisition of values of parameters relating to transitory phenomenon of engine at relevant moments

摘要

The device i.e. aircraft condition monitoring system (ACMS) (5), has a monitoring unit (23) for monitoring parameters relating to a transitory phenomenon of an engine (3) of an aircraft. A processing unit (21) triggers the acquisition of values of the parameters at relevant moments depending on the evolution of one of the parameters and generates a report having the parameter values describing a sequence of the transitory phenomenon. An input interface receives data relating to physical parameters obtained from sensors (9a, 9b) located in the engine. An independent claim is also included for a method for monitoring an aircraft engine.