SELF-HEALING REMOTE DYNAMIC DATA RECORDING

A communication adapter (102) of a gas turbine engine (104) of an aircraft (108) includes a communication interface (216) configured to wirelessly communicate with an offboard system (106) and to communicate with an engine control (122) of the gas turbine engine (104). The communication adapter (216...

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Bibliographische Detailangaben
Hauptverfasser:	LIN, Calvin K, SCHEID, Paul Raymond
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ANTENNAS, i.e. RADIO AERIALS ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDEDFOR ELSEWHERE BASIC ELECTRIC ELEMENTS CHECKING-DEVICES CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING ELECTRICITY FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GENERATING RANDOM NUMBERS MEASURING MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGISTERING OR INDICATING THE WORKING OF MACHINES REGULATING SIGNALLING TARIFF METERING APPARATUS TESTING TIME OR ATTENDANCE REGISTERS TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILARSIGNALS VOTING OR LOTTERY APPARATUS
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Beschreibung
Zusammenfassung:	A communication adapter (102) of a gas turbine engine (104) of an aircraft (108) includes a communication interface (216) configured to wirelessly communicate with an offboard system (106) and to communicate with an engine control (122) of the gas turbine engine (104). The communication adapter (216) also includes a memory system (212) and processing circuitry (210) configured to check for a change of an identifier (211) associated with the engine control (122), check for a loss of a plurality of remote dynamic data recording parameters (300) from the engine control (122), and pass a request to update the remote dynamic data recording parameters from the offboard system (106) through the communication adapter (216) to the engine control (122) based on detecting the change of the identifier (211). The processing circuitry (210) is further configured to reload an existing configuration of the remote dynamic data recording parameters (300) at the engine control (122) based on determining that the loss of the remote dynamic data recording parameters (300) has occurred.