A system and method for operating an aircraft. The system includes a health and usage monitoring system (HUMS) system for sensing health and usage data during flight of the aircraft, and a data transmission unit. The data transmission unit retrieves HUMS data from the HUMS system and generates a trigger signal when the retrieved HUMS data meets a selected criterion, the trigger signal being indicative of a condition of the aircraft. In response to the trigger signal, the data transmission unit transmits the retrieved HUMS data to a remote location.
Real time HUMS
29.12.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Tema Archiv | 1998
|British Library Conference Proceedings | 1995
|Israelischer Begleitpanzer HUMS
Kraftfahrwesen | 1984
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