Fail-safe regulator biasing circuit

Electricity: motive power systems – Induction motor systems – Primary circuit control

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Details

318798, 318140, 318147, 318153, 340650, H02P5/28

Patent

active

059031301

ABSTRACT:
A controller for a starter/generator used with an aircraft engine, includes means for monitoring field return current in a generator field winding; means for monitoring generator voltage; and microprocessor control means for adjusting generator field current as a function of the field current and voltage and field return current. The field return current and output voltage monitoring functions allow for open field, field integrity, over voltage, field weakening and torque limiting functions to be realized in an integrated programmable system configuration.

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