Power Electronics Powertrain Architectures for Hybrid and Solar Electric Airplanes with Distributed Propulsion

摘要

Distributed propulsion in aircraft has been shown to increase reliability and benefit aerodynamic performance. This paper discusses power electronic architectures and proposes control schemes suitable for distributed propulsion in hybrid and electric airplanes. Hybrid electric airplanes include permanent magnet synchronous generators driven by jet engines. The output of the generators is connected to the propulsion motors through back to back voltage source converters. Batteries, connected to the DC bus through buck-boost converters, are used to provide additional power to the propulsion motors during take off and climb. In the case of clectric airplanes, the jet engine-permanent magnet generator system is replaced by solar photovoltaic (PV) panels. The output of the solar PV system is controlled such that it operates at its maximum power point, and power is provided to batteries and propulsion motors. Simulation results on both hybrid and solar electric systems are presented.