An assembly is provided for a turbine engine with an axial centerline. This turbine engine assembly includes an outer nacelle (50) and an inner nacelle (52) with a bypass flowpath (40) radially therebetween. The inner nacelle (52) includes a nacelle wall (70) and at least one access panel (68), which is adapted to at least partially cover an aperture (72) in the nacelle wall (70). The aperture (72) in the inner nacelle (52) is substantially axially aligned with an aperture in the outer nacelle (50) that extends axially between a fixed portion of the outer nacelle (50) and a thrust reverser door (58) in a deployed position.
ACCESS PANEL(S) FOR AN INNER NACELLE OF A TURBINE ENGINE
ZUGANGSPANEL(S) FÜR EINE INNERE GONDEL EINES TURBINENMOTORS
PANNEAU(X) D'ACCÈS POUR UNE NACELLE INTERNE DE TURBOMACHINE
2016-02-10
Patent
Elektronische Ressource
Englisch
Access panel(s) for an inner nacelle of a turbine engine
Europäisches Patentamt | 2017
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