A nacelle (12) for a gas turbine engine (10) that extends along an engine centerline (CO includes an inner portion (28), an outer portion (30), and a nacelle flow control system (26). The outer portion (30) surrounds the inner portion (28) and connects to the inner portion (28) at a leading edge (32). The nacelle flow control system (26) includes an internal flow control (38) for the inner portion (28) and an external flow control (40) for the outer portion (30).
NACELLE INTERNAL AND EXTERNAL FLOW CONTROL
INTERNE UND EXTERNE FLUSSSTEUERUNG EINER GONDEL
RÉGULATION DE L'ÉCOULEMENT INTERNE ET EXTERNE D'UNE NACELLE
16.11.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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