Bypass jet engine comprising a thrust reverser

摘要

The engine has a thrust reverser (18) e.g. door type thrust reverser, including a deviation unit (20) to divert a part of a gas stream (12) near or downstream of a rear end (11) of a nacelle (10) in a thrust reverse position, such that the diverted gas stream contacting a gas stream (14) reduces speed of ejection towards a back of the stream (14) and generates a thrust reverse effect in the reverse position. The deviation unit is radially fixed inside a section (45) of an ejector shroud (44) at level of the rear end of the nacelle in the reverse position.