AIRCRAFT POWERED BY HYBRID POWER

An aircraft with a hybrid power supply, the aircraft comprising: an external structure (12 to 20); electrical equipment (34); internal combustion propulsion means (40); and means for feeding energy to the propulsion means; the aircraft being characterized in that it further comprises: a plurality of...

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Bibliographische Detailangaben
Hauptverfasser:	ROUSSELIN, STEPHANE, FOUCAULT, ALAIN, JUCHAULD, ETIENNE, PIERROT, ARNAUD
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	An aircraft with a hybrid power supply, the aircraft comprising: an external structure (12 to 20); electrical equipment (34); internal combustion propulsion means (40); and means for feeding energy to the propulsion means; the aircraft being characterized in that it further comprises: a plurality of converters for directly converting light energy into electrical energy (24), which converters are disposed on at least a fraction of the outside surface of the external structure; means (32) for comparing the electrical energy produced by said converters with the instantaneous consumption of said electrical equipment (34); means (36) for recovering the excess electrical energy, if any; and means (38) for delivering to said propulsion means (40) additional energy taken from said excess electrical energy, if any.