AIRCRAFT TURBOMOTOR MODULE STATOR, STATOR PART, AIRCRAFT TURBOMOTOR MODULE, AND, AIRCRAFT TURBOMOTOR

摘要

AIRCRAFT TURBOMOTOR MODULE STATOR, STATOR PART, AIRCRAFT TURBOMOTOR MODULE, E, AIRCRAFT TURBOMOTOR The invention relates to a ferrule (16) for aircraft turbo engine module stator provided with a plurality of openings bypass (22) each intended to receive a stator blade (4), each opening defining a skeleton (32) extending between a first end (25) designed to house the trailing edge (26) of the blade and a second end (27) designed to house the leading edge (28) of the blade. According to the invention, at least one of the openings (22) is associated with a mechanical discharge slit (36) through the ferrule and arranged facing and at a distance from the first opening end (25) according to the direction of the skeleton (32).