AIRCRAFT WITH A BLEED SUPPLY HYBRID ARCHITECTURE

AIRCRAFT WITH A BLEED SUPPLY HYBRID ARCHITECTURE

The invention refers to an aircraft comprising a bleed supply architecture (1), the aircraft having a nose section, a central section, and a rear section, and comprising a pneumatic system (2) for supplying compressed bleed air to the different aircraft systems, a bleed supply for providing bleed ai...

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Bibliographische Detailangaben
Hauptverfasser: SAÑUDO OBREGON, Cristina, RAMOS-PAUL LASTRA, Pedro, Felipe, JUAREZ BECERRIL, Alberto
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:The invention refers to an aircraft comprising a bleed supply architecture (1), the aircraft having a nose section, a central section, and a rear section, and comprising a pneumatic system (2) for supplying compressed bleed air to the different aircraft systems, a bleed supply for providing bleed air to the pneumatic system (2), and an auxiliary power unit (4). The aircraft additionally comprises an electric powered load compressor (5) coupled to the pneumatic system (2) for providing bleed air to said pneumatic system (2). The auxiliary power unit (4) is adapted for feeding electric power to the load compressor (5). The load compressor (5) and the pneumatic system (2) are installed at the same central section of the aircraft to reduce pressure losses.