door thrust reverser having at least one stationary structure in which at least one door is mounted hinging between a closed position in which it closes the reverser and creates an outer fairing and an open position in which it opens a passageway in the stationary structure and can at least partially block a flow of air generated by a turbojet engine to reorient it, and the turbojet engine nacelle

摘要

door thrust reverser having at least one stationary structure in which at least one door is mounted hinging between a closed position in which it closes the reverser and creates an outer fairing and an open position in which it opens a passageway in the stationary structure and can at least partially block an air flow generated by a turbojet engine in order to reorient it, and in the turbojet engine compartment the present invention relates to a thrust reverser (1) having reverse thrust doors which includes at least one stationary structure (3) on which at least one door (7) is mounted to pivot between closed position, wherein such door closes the reverser and constitutes a portion of an outer canopy, and an open position, in which such a door opens passageway in the stationary structure and is capable of at least partially blocking a flow of air generated by a jet engine in such a way as to reorient it, characterized by by the fact that the stationary structure also supports at least two sets of cascade paddles (10) which can be covered by the door when in the closed position, such sets of cascade paddles being laterally arranged on either side of the door.