Device for measuring at least one parameter of an aerodynamic flow of a turbine engine equipped with a vibratory damping means and turbine engine

摘要

Measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine, comprising data collection means 2, a body with a longitudinal axis L in the radial direction of the engine and carrying the data collection means, a connecting part at a first end 4 of the body 3 which connects to a radially outer wall of the turbine engine duct and a stud 21 which is located at the second end 5 of the body and which is at least partially rubber-like material and comes into contact with the radially inner wall of the turbine duct. The stud may be compressible and form a flexible connection with the turbine wall. The stud may have internal reinforcement. The stud may be glued to the body. The body may be hollow to allow a communication path for the data collection means out of the engine.