A system and method provide aircraft-specific customization of gas turbine engine operation. The system includes a gas turbine engine, a first processing unit, and an engine controller. The first processing unit is configured to selectively transmit an activation key. The engine controller is in operable communication with the first processing unit and the gas turbine engine. The engine controller is configured to receive the activation key transmitted by the first processing unit and is operable, upon receipt of the activation key, to: verify the received activation key is correct, enable operational parameters in the gas turbine engine and the engine controller when the received activation key is correct, and control the gas turbine engine using the enabled operational parameters.
SYSTEM AND METHOD FOR PROVIDING END-USE SPECIFIC CUSTOMIZATION OF GAS TURBINE ENGINE OPERATION
SYSTEM UND VERFAHREN ZUR BEREITSTELLUNG EINER ENDVERBRAUCHSSPEZIFISCHEN ANPASSUNG DES BETRIEBS VON GASTURBINENMOTOREN
SYSTÈME ET PROCÉDÉ POUR FOURNIR UNE PERSONNALISATION SPÉCIFIQUES À L'UTILISATION FINALE DU FONCTIONNEMENT D'UN MOTEUR DE TURBINE À GAZ
2023-08-02
Patent
Elektronische Ressource
Englisch
System and method for providing end-use specific customization of gas turbine engine operation
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