The power system can include: a plurality of batteries, a plurality of electric propulsion units, flight computers, and power connections. The propulsion assemblies can include a motor, a propeller, and one or more inverters. The power system can optionally include a plurality of flight actuators. However, the power system can include any other suitable set of components. The power system functions to provide aircraft propulsion and/or aircraft control authority during flight.
ELECTRIC POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRCRAFT USING SAME
2021-11-04
Patent
Electronic Resource
English
VTOL ELECTRIC POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRCRAFT USING SAME
European Patent Office | 2024
|ELECTRIC POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRCRAFT USING SAME
European Patent Office | 2022
|ELECTRIC POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRCRAFT USING SAME
European Patent Office | 2020
|ELECTRIC POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRCRAFT USING SAME
European Patent Office | 2024
|ELECTRIC POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRCRAFT USING SAME
European Patent Office | 2023
|