AIRCRAFT COMPRISING AT LEAST ONE ENGINE ASSEMBLY LINKED TO THE FUSELAGE OF THE AIRCRAFT BY TWO CONNECTING RODS POSITIONED AT LEAST PARTIALLY IN AN AIR INLET OF THE ENGINE ASSEMBLY

AIRCRAFT COMPRISING AT LEAST ONE ENGINE ASSEMBLY LINKED TO THE FUSELAGE OF THE AIRCRAFT BY TWO CONNECTING RODS POSITIONED AT LEAST PARTIALLY IN AN AIR INLET OF THE ENGINE ASSEMBLY

An aircraft which comprises a fuselage and at least one propulsion assembly linked to the fuselage by at least two connecting rods positioned at least partially in an inner zone of the air inlet of the nacelle of the propulsion assembly. Thus, the connecting rods do not interfere with the secondary...

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Bibliographische Detailangaben
Hauptverfasser: BOUCHET, Eric, COLMAGRO, Jérôme, GARCIA, Michel
Format: Patent
Sprache:eng
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 which comprises a fuselage and at least one propulsion assembly linked to the fuselage by at least two connecting rods positioned at least partially in an inner zone of the air inlet of the nacelle of the propulsion assembly. Thus, the connecting rods do not interfere with the secondary flow flowing inside the nacelle and do not affect the aerodynamic performance levels of the propulsion assembly.