Thrust reverser for a turbofan engine nacelle

摘要: The invention relates to a thrust reverser for turbofan engine nacelle including stationary portion (15) downstream from which is mounted at least one cowl (9) movable between direct-jet position, in the aligned with (15), and thrust-reversal mobile spaced apart so as define an opening passage of secondary flow (F), means deflecting (16) (F) through opening, actuator (45) (24) guiding relative first second adjacent cascade vane (13), positioned angle (B) movement axis (A) (9), arranged opposite such that deflected partially passes vanes (13) order increase deflection said upstream direction, being (13). A covering wall (31) connects bypassing (24).