초록 ▼

The problem of providing aircraft engine starting is solved with an engine start control apparatus operating a generator (12) as a synchronous motor. The motor (12) receives power from a main inverter (46) and an excitation inverter (48) through an exciter (14) operating as a rotary transformer. The

The problem of providing aircraft engine starting is solved with an engine start control apparatus operating a generator (12) as a synchronous motor. The motor (12) receives power from a main inverter (46) and an excitation inverter (48) through an exciter (14) operating as a rotary transformer. These inverters (46, 48) are controlled by a control unit (22) which provides for constant power characteristics in the field weakening range. The control unit (22) includes a pulse width modulation (PWM) generator (100) which is responsive to a voltage command (102) and a commutation command (104) to develop switching signals (88) for controlling the switches (S1-S6) in the main inverter (46). The voltage command (102) is used to vary the duty cycle of the PWM signals. The commutation angle command (104) is used to control the timing of the PWM signals. The voltage command (102) and the commutation angle command (104) are controlled using closed loop current control.

대표청구항 ▼

A start control system for a brushless DC machine including a field coil and having a rotor and a stator having a stator coil which is controllably energized from a source of DC power defining a positive and a negative DC voltage for imparting rotation to the rotor, comprising: means for sensing the

A start control system for a brushless DC machine including a field coil and having a rotor and a stator having a stator coil which is controllably energized from a source of DC power defining a positive and a negative DC voltage for imparting rotation to the rotor, comprising: means for sensing the rotational position of the rotor; switching means coupled between the source of DC power and said stator coil for alternately applying the positive and negative voltage to the stator coil according to the rotational position of said rotor; means for developing a stator current reference signal representing a desired stator current level; means for generating an actual stator current signal representing actual current level through the stator coil; first control means for developing a duty cycle command for controlling the duty cycle of operation of said switching means; second control means coupled to said developing means, said generating means, said switching means and said first control means for modifying the rotational position at which the positive and negative voltages are applied to the stator coil according to a difference between said desired and actual stator current levels if the duty cycle command is above a select level; and means for sensing reactive power in the stator coil and means coupled to said sensing means for controllably energizing the field coil in accordance with said reactive power to maintain unity power factor operation.