A power system of an aircraft includes a hybrid energy storage system with at least two energy storage subsystems each having a different power-energy density. The power system also includes one or more electric motors operably coupled to the hybrid energy storage system and to an aircraft engine. The power system further includes a means for controlling one or more electric power flows of the hybrid energy storage system to/from the one or more electric motors based on a modeled electric power demand associated with an engine load of one or more spools of the aircraft engine.
HYBRID ENERGY STORAGE SYSTEM CONTROL FOR AN AIRCRAFT ENGINE
2020-01-30
Patent
Electronic Resource
English
Hybrid energy storage system control for an aircraft engine
European Patent Office | 2023
|HYBRID ENERGY STORAGE SYSTEM CONTROL FOR AN AIRCRAFT ENGINE
European Patent Office | 2020
|