公开(公告)号：US20190128780A1

公开(公告)日：2019-05-02

申请号：US16225285

申请日：2018-12-19

Applicant: Airbus Operations SAS

Inventor： Antoine PILON ,  Natalino AGOSTINO ,  Adrien PIERREL

IPC: G01M15/14 ,  B64D45/00 ,  F02C9/00 ,  F02D41/22 ,  G05B23/02 ,  G07C5/08

Abstract: A monitoring method, the purpose of which is, when a loss of power is detected in an aircraft engine, to generate an alarm in the form of a single message displayed on a display screen in the cockpit, in order to indicate if the level of damage suffered by the engine is critical or not. The steps implemented are based on alarm signals transmitted by a central processing unit of the engine and also on alarm signals transmitted by a diagnostic device for the onboard systems of the aircraft, in order to take account of both the situation of the engine and also the situation of the systems surrounding the engine which can be affected by damage to an engine.