A method of engine electrical load shed control includes receiving an accessory load indicator corresponding to an accessory load of an engine. A request for acceleration of the engine is detected. One or more electrical buses are depowered based on the accessory load indicator exceeding a shedding threshold and detection of the request for acceleration of the engine.
ENGINE ELECTRICAL LOAD SHED CONTROL
13.08.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Electrical Load Shed to Increase Available Aircraft Power
Europäisches Patentamt | 2020
|Electrical load shed to increase available aircraft power
Europäisches Patentamt | 2020
|