NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT

An aircraft may include a plurality of electrical power systems requiring electrical power, at least one hydraulic power system requiring hydraulic power, at least two main engines, and at least two non-propulsive utility power (NPUP) generation systems. The NPUP generation systems are configured to...

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Bibliographische Detailangaben
Hauptverfasser:	SEVERNS, Christopher M, KARIMI, Kamiar J, LIFFRING, Mark E, BAYLISS, Andrew J, ROE, George M, CURRIER, Thomas F, LESYNA, Mark W, JOHNSON, Andrew, KRUG, David S
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 may include a plurality of electrical power systems requiring electrical power, at least one hydraulic power system requiring hydraulic power, at least two main engines, and at least two non-propulsive utility power (NPUP) generation systems. The NPUP generation systems are configured to provide secondary power during operation of the aircraft. The NPUP generation systems are configured to provide at least a portion of the electrical power required by the electrical power system.