An aircraft interface device (12) receives aircraft system data over an aircraft data bus structure (26) and remote data received via a wireless transceiver. The remote data originates from a computing device that is remote from the aircraft and/or aircraft system devices installed on the aircraft. The aircraft interface (12) device executes a conditional algorithm that includes a plurality of conditional expressions (40; 48A-48F) that are logically organized to define a trigger (42; 50) that initiates a triggered action (44; 52A-52C). The plurality of conditional expressions (40; 48A-48F) include a first conditional expression based upon the aircraft system data and a second conditional expression based upon the remote data. The aircraft interface device (12) executes the triggered action (44; 52A-52C) responsive to determining that the trigger (42; 50) is satisfied. The triggered action (44; 52A-52C) includes at least one of transmitting an alert, transmitting a report, and storing a report.
AIRCRAFT CONDITION MONITORING SYSTEM
FLUGZEUGZUSTANDSÜBERWACHUNGSSYSTEM
SYSTÈME DE SURVEILLANCE DE L'ÉTAT D'UN AÉRONEF
2023-08-23
Patent
Electronic Resource
English
AIRCRAFT TIRE CONDITION MONITORING SYSTEMS
SAE Technical Papers | 2009
Aircraft condition monitoring system (ACMS) for Airbus A330/A340
British Library Conference Proceedings | 1993
|Engine Condition Monitoring; Engine System and Aircraft Operational Effects
British Library Conference Proceedings | 1995
|Aircraft Airborne Condition Monitoring Experiences and Expectations
British Library Conference Proceedings | 2003
|