Patent ID: 9577433
Date: 2017-02-21
CPC Classifications: B64D,H02J,Y02T

Claim:
1. An energy supply network for an aircraft or spacecraft, comprising: at least one energy generating device for generating electrical energy; at least two energy control devices, at least one of which is coupled directly to the at least one energy generating device and which are adapted each to provide a controlled supply voltage so as to supply electrical loads located in the aircraft with energy; and a high-voltage direct current transmission device which couples the at least two energy control devices to one another by means of high-voltage direct current transmission, wherein the at least two energy control devices each comprise an output power sensor and an input power sensor, which detect the power emitted and received respectively by such energy control device, the energy control devices compensating electrical energy between them via the high-voltage direct current transmission device as a function of at least one of the detected received power and the detected emitted power.