The invention belongs to the field of
aerospace sensors, and discloses an intelligent wide-range
pressure measurement system and method for an aero-engine. The
system comprises a pressure acquisition module which comprises at least two pressure sensors with different measuring ranges and overlapped measuring intervals, and an
electromagnetic valve group used for switching gas circuits of the pressure sensors; the
intelligent control module communicates with an engine
FADEC to obtain real-time working condition parameters, predicts the pressure change trend in combination with a pre-stored pneumatic model, switches gas circuits in advance before the pressure reaches a range critical point, triggers a special collection mode to lock an adaptive sensor under a transient working condition, and collects data at the highest sampling rate. The measurement method comprises the steps of working condition parameter acquisition, pressure
trend prediction, advanced range switching and self-diagnosis calibration, and through multi-sensor data comparison under environment pressure or stable working conditions, temperature drift errors are dynamically compensated, and faults of the sensors and transmission pipelines are accurately diagnosed. According to the scheme, the problems of switching
delay, data
distortion, sensor precision drift and difficulty in fault discovery of a traditional
system are effectively solved, high precision and stability of full-range
pressure measurement are guaranteed, and reliable support is provided for precise regulation and control and
flight safety of an aero-engine.