NACELLE COWLING FOR TURBOJET AND NACELLE COMPRISING AT LEAST ONE SUCH COWLING

摘要

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.