| abstract |
The invention relates to a thrust reverser ( 9 ) for an aircraft nacelle ( 1 ), including: a front frame ( 11 ), a cowl ( 21 ) which can move between an operating position and an intermediate maintenance position downstream of the front frame ( 11 ), means ( 26 ) for moving the cowl ( 21 ) between closed and open positions, and an inner structure ( 23 ) which can move between an operating position and an intermediate maintenance position downstream of the front frame ( 11 ). In addition, the cowl ( 21 ) comprises two half-cowls ( 21 a, 21 b ) and the inner structure ( 23 ) comprises two structure halves ( 23 a, 23 b ), whereby said half-cowls ( 21 a, 21 b ) and said inner structure halves ( 23 a, 23 b ) can open outward when the cowl ( 21 ) and the inner structure ( 23 ) are in the intermediate maintenance position. |