Measurements on an injection pump actuator ("fly-by-wire")

Test stand

The photograph shows the actuator (on the right side) with a dual sensor for torque and position (on the left side). The actuator consists of an rotary magnet (limited angle torquer LAT, actuation angle: +/- 70°, by stops limited to +/- 62°). The angular position of the magnet is sensed by an integral potentiometer. The actuator is always acting against a spring pre-load, so in the case of loss of electric power the spring will shut down the engine safely.

By the magnitude of the motor current, acting in the actuator, the actuator can position against the spring pre-tension. The integral potentiometer closes the control loop. The actuator is connected by a MIL connector (shown in front of the test stand) to the supervising system.

The actuator is almost permanently acting (against the spring). So care must be taken with the self-heating, especially because the actuator is mounted directly on the hot engine block. So we made extensive tests to verify the thermal behaviour (parameter identification, simulations of various scenarios).

Test stand: Measurements on an injection pump actuator ("fly-by-wire")
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