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Modeling and experimental research on zero-bias thermal stability of the torque motor for aviation electro-hydraulic servo valves

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Published online on

Abstract

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
A permanent magnet torque motor’s (PMTM) zero is very easily shifted under the dual thermal changes of structure and material in a high-temperature service environment. The aero-engine electro-hydraulic servo valve’s service performance is greatly ...