A method for controlling power in an aircraft (10) includes monitoring an electric energy storage module (112) electrically connected to an electrical bus (110) for an exceedance of a first current limit and monitoring a generator module (108) connected to the electrical bus (110) for an exceedance of a second current limit. If the current limit of either of the electric energy storage module (112) or the generator module (108) is exceeded by a predetermined exceedance amount, the method includes reducing a power consumption for an electric machine (104) by a predetermined bias until the exceedance of the electrical energy storage module (112) and the exceedance of the generator module (108) are both less than or equal to zero.
NESTED CONTROL LOOP STRUCTURE FOR HYBRID PROPULSION SYSTEM
VERSCHACHTELTE REGELKREISSTRUKTUR FÜR HYBRIDANTRIEBSSYSTEM
STRUCTURE DE BOUCLE DE CONTRÔLE IMBRIQUÉE POUR SYSTÈME DE PROPULSION HYBRIDE
2023-02-22
Patent
Electronic Resource
English
IPC: | B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B60W CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION , Gemeinsame Steuerung oder Regelung von Fahrzeug-Unteraggregaten verschiedenen Typs oder verschiedener Funktion / B64U |
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 SYSTEMS
European Patent Office | 2023
|