Abstract
Based on the electromagnetic induction Hall zero position sensor, a multi-stage reducer motor structure system with a brush DC motor is designed using an aviation fuel on–off valve. The output shaft of the motor structure can respond to commands, rotate double directions, and lock the brake shaft after reaching the designated position. After that, the current position and on/off situation of pipeline fuel can be derived accurately. The system has the advantages of light weight, small volume, fast response, high precision, high reliability, and integration.
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