A method is provided for component management. During this method, a first output signal is received from a first aircraft system at a component management system. The first aircraft system includes a first engine and a first component installed in the first engine. The first output signal communicates identification data for the first engine and a first operating parameter for the first engine. A first component parameter for the first component is determined based on the identification data for the first engine and the first operating parameter for the first engine. A record for the first component is updated in the component management system using the first component parameter for the first component.
MANAGEMENT OF AIRCRAFT SYSTEM COMPONENTS ACROSS DIFFERENT AIRCRAFT ENGINES
2025-05-29
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
MANAGEMENT OF AIRCRAFT SYSTEM COMPONENTS ACROSS DIFFERENT AIRCRAFT ENGINES
European Patent Office | 2025
|Making Ceramic Components For Advanced Aircraft Engines
NTRS | 1994
|SLUB | 1948
|Engineering Index Backfile | 1940