The invention discloses a multi-channel
ion current detection circuit for an aero-engine pedestal. The multi-channel
ion current detection circuit comprises a
signal control box and a dual-channel real-time detection circuit, in each channel of the real-time detection circuit, the multi-gear
ion current display circuit is connected to an
ion current detection loop of the
signal control box, and the
ion current of the
ion current detection loop in the
signal control box is monitored in real time; in the threshold value display circuit and the multi-gear ion
current threshold selection circuit which are connected in series,
voltage division is realized through divider resistors which are connected in series at the front ends, adjustable resistors are connected in series on all
voltage division paths, and all the
voltage division paths which are connected in parallel and the adjustable resistors in the voltage division paths are connected to an ion
current threshold value adjusting circuit of the signal control box. The ion
current threshold value of the current threshold value adjusting circuit is set by adjusting the resistance value of the adjustable
resistor in each voltage dividing path, and the voltage display of each voltage dividing
resistor is realized through a
voltmeter V1 connected with each voltage dividing
resistor, so that the ion current threshold
value set in the corresponding voltage dividing path is reflected through the display of the
voltmeter V1. According to the technical scheme, the problems that an existing ionic current detection method cannot detect data of ionic current in an
afterburner of an engine in real time, and the
flame signal threshold value is difficult to adjust in the engine test run process are solved.