A method (500) of modeling and integrating engine installation deltas includes receiving (502) flight data related to an aircraft that includes an engine installed therein. The flight data includes values of an engine parameter. The method also includes determining (504) values of a measured installation delta for the engine based, at least in part, on the flight data. The method also includes determining (506) values of a measured power parameter for the engine based, at least in part, on the flight data. The method also includes generating (510) a mathematical model of a plurality of installation deltas for the engine as a function of the engine parameter, where the plurality of installation deltas include the measured installation delta and an unmeasured installation delta. The method also includes validating (512) the mathematical model based, at least in part, on the values of the measured installation delta. The method also includes generating (516) a performance profile of the engine.
MODELING AND INTEGRATING AIRCRAFT ENGINE INSTALLATION DELTAS
MODELLIERUNG UND INTEGRATION VON FLUGTRIEBWERKINSTALLATIONSDELTAS
MODÉLISATION ET INTÉGRATION DE DELTAS D'INSTALLATION DE MOTEUR D'AÉRONEF
2022-06-01
Patent
Electronic Resource
English
IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Emerald Group Publishing | 1930
|SAE Technical Papers | 1930
|Engineering Index Backfile | 1930
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