| 摘要 |
The invention relates to a housing (16a) for a stator of a module of an aircraft turbine engine provided with a plurality of through-openings (22) respectively receiving a stator blade (4) and defining a skeleton (32) extending between a first end (25) for housing the trailing edge of the blade and a second end (27) for housing the leading edge (28) of the blade. According to the invention, a mechanical offloading slit formed through the housing is associated with one of the openings (22), facing, and at a distance from, the first end (25) of the opening according to the direction of the skeleton (32). |
