AIRCRAFT CAPABLE OF HOVERING

An aircraft (1) with a motor bay (8) is described; a motor system (6) with a discharge duct (17); a heat exchanger (20) arranged outside said motor system (6); a first air intake (25); a first duct (26) along which the heat exchanger (20) is arranged; a first converging nozzle (15) having a downstre...

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Bibliographische Detailangaben
Hauptverfasser:	BRAGHIROLI, Marco, CANTA, Enrico
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	An aircraft (1) with a motor bay (8) is described; a motor system (6) with a discharge duct (17); a heat exchanger (20) arranged outside said motor system (6); a first air intake (25); a first duct (26) along which the heat exchanger (20) is arranged; a first converging nozzle (15) having a downstream section (39) fluidically connected with the discharge duct (17) and with the first duct (26) so as to create a first flow rate of air adapted to cool the heat exchanger (20); and a second air intake (10) that is open in the motor bay (8) and distinct from the first air intake (25); a second converging nozzle (16) having a second downstream section (49) fluidically connected with the discharge duct (17) and with the motor bay (8), so as to create a second flow rate of cooling air of the motor bay (8) directed from the second air intake (10) towards the discharge duct (17) and by-passing the motor system (6).