Nacelle cowling for turbojet and nacelle comprising at least...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 29/08 (2006.01)

Patent

CA 2621216

The invention concerns a nacelle cowling (5) for turbojet, characterized in that it is provided with a fixed part (6) and a mobile part (7), the mobile part being adapted to slide along the fixed part, from a closed position wherein the mobile part extends in the extension of the fixed part, up to an open position wherein the mobile part is at least partly superimposed to the fixed part. For example, the fixed part is located in the upper part of the cowling, the mobile part being located in the lower part of said cowling.

L'invention concerne un capot (5) de nacelle pour turboréacteur, caractérisé en ce qu'il est muni d'une partie fixe (6) et d'une partie mobile (7), la partie mobile étant apte à coulisser le long de la partie fixe, depuis une position fermée dans laquelle la partie mobile s'étend dans le prolongement de la partie fixe, jusqu'à une position ouverte dans laquelle la partie mobile est au moins partiellement superposée à la partie fixe. Par exemple, la partie fixe est située en partie supérieure du capot, la partie mobile étant située en partie inférieure dudit capot.

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