F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/12 (2006.01) F02K 1/06 (2006.01) F02K 1/50 (2006.01) F02K 1/76 (2006.01)
Patent
CA 2536759
A turbofan nacelle (16) includes forward and aft cowls (58, 60) adjoining at a joint (62), and including an exhaust duct (36) having a main outlet (46) for discharging exhaust (32). A variable nozzle (38) surrounds the exhaust duct (36) and includes a secondary outlet (52) around the main outlet (46). A thrust reverser (64) bridges the forward and aft cowls (58, 60) upstream from the variable nozzle (38). The variable nozzle (38) is inductively powered and controlled across the closed joint (62), and is uncoupled inductively from the forward cowl (56) when the joint (62) is open.
La présente invention a trait à une nacelle de réacteur à double flux (16) comportant des capots avant et arrière (58, 60) adjacents à un joint (62), et comportant un conduit d'échappement (36) présentant un orifice de sortie principal (46) pour l'évacuation de gaz d'échappement (32). Une tuyère variable (38) entoure le conduit d'échappement (36) et comprend un orifice de sortie secondaire (52) autour de l'orifice de sortie principal (46). Un inverseur de poussée (64) relie les capots avant et arrière (58, 60) en amont à partir de la tuyère variable (38). La tuyère variable (38) est alimentée et commandée par induction à travers le joint fermé (62), et est découplée en induction du capot avant (56) lorsque le joint (62) est ouvert.
Lair Jean-Pierre
Wolters Gregory Thomas
Deeth Williams Wall Llp
The Nordam Group Inc.
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