A drive system for an aircraft has a first energy store for supplying electrical energy, a second energy store for supplying electrical energy, and an electric drive for supplying drive power for the aircraft. An energy distribution unit of the drive system is designed to transmit the supplied electrical energy of the first energy store and the supplied electrical energy of the second energy store to the electric drive. The energy distribution unit is also designed to charge the second energy store using a first portion of the energy supplied by the first energy store and at the same time to transmit a second portion of the energy supplied by the first energy store to the electric drive, in order to supply the drive power for the aircraft. An aircraft having a drive system and a method for supplying drive power for an aircraft are disclosed.
Drive System For An Aircraft And Method For Supplying Drive Power For An Aircraft
2019-08-08
Patent
Elektronische Ressource
Englisch
DRIVE SYSTEM FOR AN AIRCRAFT AND METHOD FOR SUPPLYING DRIVE POWER FOR AN AIRCRAFT
Europäisches Patentamt | 2020
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