Turbojet engine nacelle with lateral opening of covers

Details Turbojet engine nacelle with lateral opening of covers Turbojet engine nacelle with lateral opening of covers

B - Operations, Transporting

64

D

B64D 29/08 (2006.01)

Patent

CA 2642300

The present invention relates to a nacelle (1) of a turbojet engine (4),which nacelle is intended to be attached to a structure (2) of an aeroplane by a connecting pylon (3) and comprises at least one moving part (9', 9') above to be opened in order to provide access to the interior of the nacelle, characterized in that the said moving part is mounted to pivot about a pivot axis (25) directed along a line more or less perpendicular to the plane of the structure of the aeroplane to which the nacelle is attached.

La présente invention se rapporte à une nacelle (1 ) de turboréacteur (4) destinée à être rattachée à une structure (2) d'un avion par un mât (3) de liaison et comprenant au moins une partie mobile (9', 9") apte à être ouverte de manière à permettre un accès à l'intérieur de la nacelle, caractérisée en ce que ladite partie mobile est montée pivotante autour d'un axe (25) de pivotement orienté selon un axe sensiblement perpendiculaire au plan de la structure de l'avion à laquelle la nacelle est rattachée.

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