Aero-engine gas path fault monitoring electrostatic simulation platform and method of use

The present invention discloses an aeroengine gas path fault monitoring electrostatic simulation platform and method of use, the test platform comprises a mounting platform, the analog channels the air, the air passage is mounted on the analog channel fault generating means and an electrostatic sensor, an electrostatic sensor connection the static data acquisition system; said fault comprises a fault generating means mimetic injection means, fuel injection means, leaves - Rubbing casing failure in generating one or more devices; blade - casing Rubbing touch fault generating means comprises Mount excitation shuttle Rub rotor and a control device. With the present invention the test platform and methods of use can be done at room temperature or elevated temperature for aeroengine blade - casing Rubbing fault, fault combustion chamber deposits, and the fault block member ablated foreign matter suction failure and the corresponding failure simulation data collected in the static mode, provides an effective platform for the study of experimentally and fault monitoring electrostatic simulation engine gas path.