An aircraft hybrid electrical propulsion (HEP) system includes an electrical system configured to deliver power to a plurality of electrical loads, a propulsion system configured to generate thrust in response to an input power, and an HEP controller in signal communication with the electrical system and the propulsion system. The HEP controller is configured to monitor a load demand of at least one electrical load among the plurality of electrical loads and to actively control the input power to actively control the thrust in response to changes in the load demand.
AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATION
2024-09-12
Patent
Electronic Resource
English
AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATION
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