INTERMEDIATE HOUSING OF A TURBOMACHINE WITH AN AERODYNAMIC PARAMETER MEASURING DEVICE, TURBINE MODULE COMPRISING SUCH AN INTERMEDIATE HOUSING AND A TURBOMACHINE EQUIPPED WITH SUCH A MODULE

摘要

The invention relates to an intermediate casing (17) of a turbomachine extending around a longitudinal axis X, the intermediate casing (17) comprising an internal ferrule (24) and an external ferrule (25) coaxial and between which an aerodynamic flow the turbomachine is intended to circulate, the intermediate casing comprising at least one arm (26) extending between the internal ferrule (24) and the external annular ferrule (25) along a radial axis R perpendicular to the longitudinal axis X, the arm (26) comprising a leading edge (27) upstream and a trailing edge (28) downstream along the longitudinal axis X. According to the invention, the intermediate casing (17) comprises a measuring device ( 35) of aerodynamic parameters of the aerodynamic flow, at least a portion of which forms part of the leading edge (27) of the arm (26).