In accordance with at least one aspect of the present disclosure, there is provided a method for controlling power in an aircraft. The method includes, monitoring an electric energy storage module electrically connected to an electrical bus for an exceedance of a first current limit and monitoring a generator module connected to the electrical bus for an exceedance of a second current limit. If the current limit of either of the electric energy storage module or the generator module is exceeded by a predetermined exceedance amount, the method includes reducing a power consumption for an electric machine by a predetermined bias until the exceedance of the electrical energy storage and the exceedance of the generator module are both less than or equal to zero.
NESTED CONTROL LOOP STRUCTURE FOR HYBRID PROPULSION SYSTEMS
STRUCTURE DE BOUCLE DE REGULATION NICHEE POUR DES SYSTEMES DE PROPULSION HYBRIDES
2023-02-17
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
NESTED CONTROL LOOP STRUCTURE FOR HYBRID PROPULSION SYSTEM
European Patent Office | 2023
|Nested control loop structure for hybrid propulsion system
European Patent Office | 2023
|NESTED CONTROL LOOP STRUCTURE FOR HYBRID PROPULSION SYSTEM
European Patent Office | 2023
|