This invention relates to aircraft propulsion systems, specifically to an online real-time
monitoring system and method for aircraft solenoid valves and self-locking valves. The
system provided by this invention comprises a host computer, valve
testing equipment, solenoid valves and / or self-locking valves, a
solenoid valve and / or self-locking
valve actuator, GNC monitoring equipment, cables, and network cables. The
solenoid valve and / or self-locking
valve actuator, GNC monitoring equipment, and solenoid valves and / or self-locking valves are connected to the valve
testing equipment via cables; the valve
testing equipment is connected to the host computer via a network cable. This connection method integrates the valve testing equipment with the
solenoid valve and / or self-locking valve control pathways, enabling long-term online real-time monitoring of the solenoid valve and / or self-locking valve's operational characteristics data, eliminating the need for offline, post-
processing interpretation. Furthermore, this invention offers advantages such as multiple parallel testing pathways, high time accuracy, long
operating time, strong versatility, high real-time performance, strong compatibility, and low latency.