GAS TURBINE ENGINE COMMUNICATION DATA MANAGEMENT FUNCTION COMMUNICATING VIA AIRCRAFT WIRELESS GATEWAY

GAS TURBINE ENGINE COMMUNICATION DATA MANAGEMENT FUNCTION COMMUNICATING VIA AIRCRAFT WIRELESS GATEWAY

Examples described herein provide a method that includes receiving engine data 208 from a sensor 206 associated with the engine 104. The method further includes associating a header with the engine data 208 to generate packaged engine data. The method further includes transmitting the packaged engin...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SCHEID, Paul Raymond, POSNIAK, Jason E
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
ELECTRIC COMMUNICATION TECHNIQUE
ELECTRICITY
TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHICCOMMUNICATION
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Beschreibung
Zusammenfassung:Examples described herein provide a method that includes receiving engine data 208 from a sensor 206 associated with the engine 104. The method further includes associating a header with the engine data 208 to generate packaged engine data. The method further includes transmitting the packaged engine data to an aircraft communication unit 102, wherein the header provides for the aircraft communication unit 102 to transmit the packaged engine data to a ground station communication unit 106 via a communication protocol.