The invention provides a
temperature compensator testing
system and testing method for an aircraft. The
temperature compensator includes a push rod, and the
system includes a
temperature control module, a sensor group, a
data processing module and a pressure block, wherein the
temperature control module is set to have different temperatures , used to simulate the
working environment of the
temperature compensator in the aircraft engine
servo device; the sensor group is used to detect the temperature change of the
working environment, and detect the displacement of the push rod and the pressure change of the pressure block, and output sensor signals; the
data processing module Receive the sensor
signal, analyze and process the sensor
signal, and output the performance analysis result of the temperature compensator. By automatically simulating the
working environment of the temperature sensor, using the sensor as a
data acquisition device, performance analysis is performed based on the data output by the sensor, and finally a performance analysis structure is obtained to realize automatic detection of the performance of the temperature compensator, with simple operation and high detection efficiency.