F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/09 (2006.01) F02K 1/72 (2006.01)
Patent
CA 2705136
The invention relates to a nacelle for an aircraft engine that comprises a front cowling (13) and a rear cowling (1a), the rear cowling (1a) being mounted so as to slide between an upstream position defining a reduced nozzle (9) section and a downstream position defining an enlarged nozzle (9) section. The nacelle includes an intermediate member (25) arranged edge-to-edge with said front cowling (13), said member defining a housing (27) for receiving the upstream edge (11) of said rear cowling (1a) when the latter is in the upstream position.
Cette nacelle pour moteur d'avion comprend un capot avant (13) et un capot arrière (1a), ce capot arrière (1a) étant monté coulissant entre une position amont définissant une section de tuyère (9) réduite et une position aval définissant une section de tuyère (9) agrandie. Cette nacelle comprend un organe intermédiaire (25) disposé bord- à-bord avec ledit capot avant (13), cet organe définissant un logement (27) apte à recevoir le bord amont (11) dudit capot arrière (1a) lorsque ce capot se trouve dans sa position amont.
Aircelle
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
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