GAS TURBINE ENGINE COMMUNICATION DATA MANAGEMENT FUNCTION

Examples described herein provide a method for assigning tasks to processors of a multi-core processor 241 associated with a gas turbine engine 104. The method includes assigning a first processing core 240a of the multi-core processor 241 to perform a first type of tasks having a first safety level...

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Bibliographische Detailangaben
Hauptverfasser:	SCHEID, Paul Raymond, POSNIAK, Jason E
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CALCULATING COMBUSTION ENGINES COMPUTING CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COUNTING ELECTRIC DIGITAL DATA PROCESSING GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PHYSICS WEAPONS
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Beschreibung
Zusammenfassung:	Examples described herein provide a method for assigning tasks to processors of a multi-core processor 241 associated with a gas turbine engine 104. The method includes assigning a first processing core 240a of the multi-core processor 241 to perform a first type of tasks having a first safety level. The method further includes assigning a second processing core 240c of the multi-core processor 241 to perform a second type of tasks having a second safety level, the second safety level being different than the first safety level. The method further includes executing a first core task of the first type of tasks on the first processing core 240a. The method further includes executing a second core task of the second type of tasks on the second processing core 240c.