Integrated aircraft power conditioning unit

Integrated aircraft power conditioning unit

An integrated power conditioning unit includes a DC bus, a first terminal for connection to first AC equipment, a second terminal for connection to second AC equipment, a first inverter circuit providing bi-directional AC-DC conversion between a first AC power signal and a first DC power signal, and...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: WIEGMAN HERMAN LUCAS NORBERT, CARLSON WILLIAM EUGENE
Format: Patent
Sprache:eng
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:An integrated power conditioning unit includes a DC bus, a first terminal for connection to first AC equipment, a second terminal for connection to second AC equipment, a first inverter circuit providing bi-directional AC-DC conversion between a first AC power signal and a first DC power signal, and a converter assembly providing bi-directional AC-DC conversion between a second AC power signal and a second DC power signal. A control module controls the first inverter circuit such that the first DC power signal may flow from/to the DC bus and the first AC power signal may flow from/to the first terminal. The control module also controls the converter assembly such that the second AC signal power signal may flow from/to the second terminal and the second DC power signal may flow from/to the DC bus.