AUXILIARY POWER SYSTEM

The present irwention relates to auxiliary power generator systems for an aircraft. More particular, the present invention relates to an auxiliary power system with a new architecture that include an essential auxiliary power unit (APU) with dual and fully redundant starter and electrical power gene...

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Bibliographische Detailangaben
Hauptverfasser:	ZAMARRO MARTIN, MARIA CRUZ, ANDREU FERNANDEZ, FRANCISCO MANUEL, CHIABRANDO, MARCOS JAVIER, DAVID, BENJAMIN, CASADO MONTERO, CARLOS
Format:	Patent
Sprache:	eng ; fre
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:	The present irwention relates to auxiliary power generator systems for an aircraft. More particular, the present invention relates to an auxiliary power system with a new architecture that include an essential auxiliary power unit (APU) with dual and fully redundant starter and electrical power generation systems that can connect independently to a normal electric network or an emergency electric network of an aircraft. in addition, the present invention also relates to an aircraft comprising said auxiliary power system and a method for supplying electric power to an aircraft by means of said system.