An architecture for an electric distributed propulsion system (1000) includes one or more generators (1004a, 1004b) connected to a gearbox (1002), a first and a second plurality of motors (1008a-e, 1008f-j) connected to the one or more generators, each motor of the plurality of motors connected to a blade to provide thrust, a first and a second power bus electrically connected between the one or more generators and the first and the second plurality of motors, each power bus independent of the other power bus, a first and a second controller (1012a, 1012b) independently connected to each of the first and second plurality of motors, each of the first and second controllers serving as a primary and a backup controller to provide redundant control to both the first and the second plurality of motors, and dual channels in communication between pilot input sensors and the first and the second controllers, each channel of the dual channels independent of the other channels, and the dual channels including an additional channel to provide redundant communication to the first and second controllers.
ELECTRIC DISTRIBUTED ANTI-TORQUE ARCHITECTURE
ELEKTRISCH VERTEILTE ANTI-DREHMOMENT-ARCHITEKTUR
ARCHITECTURE ANTICOUPLE DISTRIBUÉE ÉLECTRIQUE
2023-06-07
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern |