There is provided an engine assembly for an aircraft, comprising a heat engine in driving engagement with an engine shaft having a first end coupled to a mechanical gearbox and a second end opposite the first end, an electric generator coupled to the second end to provide a generator output voltage, the electric generator separate from the mechanical gearbox, a power electronics module connected to the electric generator and configured to regulate the generator output voltage to provide a regulated output voltage that meets an electrical power demand of at least one aircraft accessory, and a voltage bus connected to the power electronics module and configured to supply the regulated output voltage to the at least one aircraft accessory.
ENGINE ASSEMBLY WITH A DEDICATED VOLTAGE BUS
2018-11-29
Patent
Electronic Resource
English
Transient control of a Dedicated EGR engine
Automotive engineering | 2016
|Dedicated Hybrid Engine — Natural Aspirated or Turbocharged?
TIBKAT | 2020
|