An assembly is provided for a turbine engine with an axial centerline. This turbine engine assembly includes an outer nacelle and an inner nacelle with a bypass flowpath radially therebetween. The inner nacelle includes a nacelle wall and at least one access panel, which is adapted to at least partially cover an aperture in the nacelle wall. The outer nacelle axially overlaps the access panel.
Access panel(s) for an inner nacelle of a turbine engine
2017-10-24
Patent
Elektronische Ressource
Englisch
ACCESS PANEL(S) FOR AN INNER NACELLE OF A TURBINE ENGINE
Europäisches Patentamt | 2016
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