Stator guiding the inlet of air into a turbomachine and procedure for mounting a blade of this stator.

摘要

The present invention relates to a stator guiding the inlet of air into a turbo machine and to a procedure for mounting this stator. The object of the invention is to improve the fixing of the blades so that these better resist the impacts in the event of a foreign body being introduced into the turbine machine. This object is achieved with the aid of a stator comprising a plurality of blades (34) held radially by their internal pivots (42) and external pivots (40) between an inner collar (31) and an outer casing (32), characterised in that the inner collar (31) comprises at least one hole (60) intended to receive one of the said inner pivots (42) and in that the outer casing (32) comprises means (72, 80) for radially positioning and locking a blade (34) making it possible to hold the inner pivot (42) in the said hole (60). The invention relates more particularly to the stator of the high-pressure compressor of a turbojet engine.