A multi-engine power system is described that includes at least a first engine and a second engine configured to jointly provided mechanical power to the multi-engine power system. The multi-engine power system further includes a controller configured to estimate a deterioration factor of the first engine. The controller is further configured to adjust, based on the deterioration factor of the first engine, a first amount of mechanical power being provided by the first engine to increase a service time of the first engine, and adjust, based on the first amount of mechanical power being provided by the first engine, a second amount of mechanical power being provided by the second engine to compensate for the adjustment to the first amount of mechanical power.
ENGINE DEGREDATION MANAGEMENT VIA MULTI-ENGINE MECHANICAL POWER CONTROL
2017-11-09
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 |
ENGINE DEGRADATION MANAGEMENT VIA MULTI-ENGINE MECHANICAL POWER CONTROL
Europäisches Patentamt | 2020
|Engine degradation management via multi-engine mechanical power control
Europäisches Patentamt | 2019
|PVI Investigation on Airfoil with Ice Accretions and Resulting Performance Degredation
British Library Conference Proceedings | 2001
|