A system includes a low pressure machine (206), a high pressure machine (202), a motor controller device, a first set of switches configured to selectively couple the low pressure machine (206) to an inverter or a rectifier included in the motor controller device, based on a control signal, and a second set of switches configured to selectively couple the high pressure machine (202) to the inverter or the rectifier, based on the control signal.
MULTIPLEXED BI DIRECTIONAL CONVERTERS FOR HYBRID ELECTRIC AIRCRAFT PROPULSION
MULTIPLEXIERTE BIDIREKTIONALE WANDLER FÜR HYBRIDEN ELEKTRISCHEN FLUGZEUGANTRIEB
CONVERTISSEURS BIDIRECTIONNELS MULTIPLEXÉS POUR PROPULSION ÉLECTRIQUE HYBRIDE D'AÉRONEF
21.05.2025
Patent
Elektronische Ressource
Englisch
MULTIPLEXED BI DIRECTIONAL CONVERTERS FOR HYBRID ELECTRIC AIRCRAFT PROPULSION
Europäisches Patentamt | 2025
|Hybrid-Electric Propulsion for Aircraft
Online Contents | 2015
|