Energy supply network, method and aircraft or spacecraft

The present invention provides an energy supply network, especially for an aircraft or spacecraft, comprising a first coupling device (2), the first coupling device (2) being configured to couple the energy supply network to an external energy source (9), a first high voltage direct current, HVDC, s...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	PRISSE, LUCIEN, MAVIER, JEROME, SCHROETER, TORBEN, JOHANNSEN, MARTIN, HINZE, MARTINA
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC,OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWERSUPPLY SYSTEMS CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONTROL OR REGULATION THEREOF CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUTPOWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY GENERATION SYSTEMS FOR STORING ELECTRIC ENERGY
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Beschreibung
Zusammenfassung:	The present invention provides an energy supply network, especially for an aircraft or spacecraft, comprising a first coupling device (2), the first coupling device (2) being configured to couple the energy supply network to an external energy source (9), a first high voltage direct current, HVDC, segment, the first HVDC segment (3) being coupled to the first coupling device (2) and a second HVDC segment (4), the second HVDC segment (4) being coupled to the first coupling device (2). The present invention furthermore provides a corresponding method and an aircraft or spacecraft.