For aircraft taxiing, an aircraft is equipped with an electric machine installed in a propulsor gearbox (PGB), in parallel to the gas turbine, working in motor mode during taxi, and in generator mode during flight phases (such as take-off, climb, cruise, descent, approach and landing). Typical current systems which use an electric machine in the PGB do not use the electric machine in motor mode for taxi operations (i.e., it is only an additional generator). An optimized power supply providing a combination of a thermal engine such as an Auxiliary Power Unit (APU) and an electric energy storage system such as a battery provides power to the PGB electric machine even when the gas turbine is off.
Hybrid electric taxi system (HETS) or full electric taxi system (FETS)
2023-04-11
Patent
Electronic Resource
English
HYBRID ELECTRIC TAXI SYSTEM (HETS) OR FULL ELECTRIC TAXI SYSTEM (FETS)
European Patent Office | 2019
|Automotive engineering | 1976