Patent ID: 8951006
Filing Date: 2015-02-10
Classification: B64D,F02K,F05D,Y02T

Abstract:
1. A nacelle for a turbojet engine, of the type comprising a downstream structure comprising: an outer structure which defines, with a concentric inner structure surrounding a downstream part of the turbojet engine, an annular flow duct, wherein at least part of said inner structure is slidably mounted such that the inner structure moves translationally along a longitudinal axis of the nacelle, without pivoting, so that the inner structure can be moved between a working position in which the inner structure acts as a case for the downstream part of the turbojet engine and a maintenance position in which the inner structure uncovers said downstream part of the turbojet engine, wherein the inner structure moves translationally with respect to the nacelle by means of at least one pair of rails and slides, each rail cooperating with one slide having a curved portion.