The present disclosure provides methods and systems for determining a synthesized engine parameter of a gas turbine engine. An initial model parameter is obtained from an onboard model associated with the gas turbine engine. A correction factor for the onboard model is determined by modifying a difference between the onboard model and an aero-thermal model of the gas turbine engine using first and second engine parameters and first and second operating conditions, wherein the first and second engine parameters are independent from one another over an operating envelope of the gas turbine engine. The initial model parameter is scaled by applying the correction factor thereto to obtain a corrected model parameter. The corrected model parameter is output as the synthesized engine parameter.
METHODS AND SYSTEMS FOR DETERMINING A SYNTHESIZED ENGINE PARAMETER
METHODES ET SYSTEMES POUR DETERMINER UN PARAMETRE DE MOTEUR SYNTHETISE
2022-04-23
Patent
Electronic Resource
English
SYSTEMS AND METHODS FOR DETERMINING GAS TURBINE ENGINE OPERATING MARGINS
European Patent Office | 2024
|SYSTEMS AND METHODS FOR DETERMINING GAS TURBINE ENGINE OPERATING MARGINS
European Patent Office | 2024
|Parameter optimization for engine control systems
AIAA | 1978
|SYSTEMS AND METHODS FOR DETERMINING GAS TURBINE ENGINE OPERATING MARGINS
European Patent Office | 2024
|