Thrust reverser having a bypass vane-cascade and fitted with a stationary rear structure

摘要: A thrust reverser for a turbojet engine is provided with at least one displaceable assembly including cowling portion and flap. The the flap each subtend stationary upstream downstream portions such that forms of external covering reverse opening outer boundary gas flow in forward position. In position, uncovered, are displaced extends downstream, parallel to longitudinal axis above, without interference, portion. engages rolling contact plurality elements supported by an end pivots so as block duct redirect outward though vane-cascades.