Method of controlling a stand-alone electrical generator, in particular for aircraft
AssigneeDassault Aviation
InventorsChristophe Montret, Christian Marie Pierre Jacquet-Francillon
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AssigneeDassault Aviation
InventorsChristophe Montret, Christian Marie Pierre Jacquet-Francillon
Estimating the term…
The generator includes an asynchronous machine with a wound rotor driven mechanically and a stator connected to the network. The rotor is excited by a constant DC voltage source via an inverter controlled by a pulse width modulation control circuit. In accordance with the invention, the following are generated: a stator frequency set point, a rotor frequency set point which is a function of the stator frequency set point and the rotation speed of the machine, an rms stator voltage set point, an error signal which is a function of the difference between the rms stator voltage set point and the actual rms stator voltage. A rotor voltage set point is imposed on the control circuit which is a function of the error signal and the rotor frequency set point.
A method of controlling a stand-alone electrical generator including an asynchronous rotating machine whose wound rotor is driven mechanically at a particular voltage and with a particularly frequency, a stator and said rotor being excited by an inverter controlled by a pulse width modulation control circuit and supplied by a constant DC voltage source, said method comprising the steps of:
A method of controlling a stand-alone electrical generator including an asynchronous rotating machine whose wound rotor is driven mechanically at a particular voltage and with a particular frequency, a stator, and said rotor being excited by an inverter controlled by a first pulse width modulation control circuit and supplied by a constant DC voltage source, said method comprising the steps of:
Dependencies are inferred from the claim text.