Abstract:
A circuit in a power system for suppressing an AC ripple superimposed on a bus signal (70) on a bus (18a and 18b) includes a first circuit (60) for producing first and second signals (62a and 62b) having a frequency substantially equal to the AC ripple frequency wherein the second signal (62b) is a phase quadrature of the first signal (62a), a second circuit (64, 66, 76, 78, 84 and 86) for combining these signals with a signal representing the bus signal (70) having the AC ripple superimposed thereon so as to derive a control signal (88 and 90) having substantially the same frequency and phase as the AC ripple, and third circuit (92) responsive to this control signal (88 and 90) so as to substantially suppress the AC ripple on the bus (18a and 18b).
Abstract:
The present invention provides for detecting rotor speed through the use of sense coils (240) on the stator teeth. Voltage ripples caused by the rotor slots (SC-1) is detected by combining the signals of several sense coils so that the fundamental voltage signal is cancelled or rejected and only the ripple voltages remain which is a signal proportional to speed. Further, the present invention provides for using a generator (220) to control voltage to the induction motor (222) with a PWM inverter (226) to control frequency signals to the induction motor (222).
Abstract:
The problem of providing an engine starting system from any one of a plurality of input power sources is solved with an engine start control apparatus operating a generator (12) as a synchronous motor and employing input power limiting. The motor receives power from a main inverter (46) and a control unit which provides for input power limiting and also constant power characteristics in the field weakening range. The control unit includes a pulse width modulation (PWM) generator (22) which is responsive to a voltage command and a commutation command to develop switching signals for controlling the switches in the start inverter. The voltage command is used to vary the duty cycle of the PWM signals. The commutation angle command is used to control the timing of the PWM signals. In addition to commutation angle control, the start control system employs field weakening control to obtain constant power characteristics.
Abstract:
A motor generator system (120) in accordance with the invention includes a prime mover (21) for driving an output shaft (18), a main motor generator (105), having a rotor driven by the output shaft, for producing electrical power on at least one output winding (36a-36c) in response to the prime mover rotating the output shaft and for driving the output shaft in response to operation as a motor; an exciter (102) for applying excitation to a field winding (34) of the main motor generator during operation for producing electrical power on the at least one output winding and for applying current to the field winding of the main motor and generator to produce a magnetic field in the field winding during operation of the main motor generator as a motor; circuitry (122), responsive to current in a field winding (204) of the exciter, for producing an output signal representing a position of the rotor of the main motor generator driven by the output shaft; and a main inverter (114), responsive to the output signal, for commutating application of electrical current to the at least one output winding to control operation of the main motor generator during operation as a motor.
Abstract:
Systems and methods for starting a prime mover (21), such as a gas turbine engine of an aircraft auxiliary power unit (APU), are disclosed herein whereby an electromagnetic machine (10) is operated as a motor during operation in a self starting mode to bring the prime mover (21) up to selfsustaining speed. The same electromagnetic machine (10) is thereafter operated as a generator during operation in a generating mode.
Abstract:
The problem of excess size and weight resulting from the use of current sensors in a VSCF start system is solved by a motor control system (10) which utilizes a current estimator (68) to develop a current feedback value. The current estimator (68) is coupled to a rotor position detector (72) and an input power detector (78) to develop a signal representing the estimated current drawn by the motor (12).
Abstract:
Prior power generation systems generated output voltages having relatively large, undesirable over-voltage transients due to sudden load reduction. In order to overcome this disadvantage, a power generation system for generating a DC bus voltage on a DC bus (14) is provided with a switch (80) coupled across the DC bus (14) to suppress over-voltage transients. The power generation system includes a synchronous generator (24) that generates AC power and a rectifier (54) that rectifies the AC power to produce DC power and supply the DC power to the DC bus (14). A voltage regulator (62) controls the magnitude of the DC bus voltage by varying the amount of current provided to a field winding (46) associated with the synchronous generator (24). A switch (80) is coupled across the DC bus (14) and is repeatedly switched when the DC bus voltage reaches a predetermined magnitude.
Abstract:
The problem of maintaining precision control of a synchronous motor (12) is solved in a motor start control (10) which utilizes an estimate of the amplitude of the fundamental wave component as a feedback value. The motor (12) receives power from a main inverter (46) and an excitation inverter (48). The inverters (46, 48) are controlled by a control unit (22) which includes a pulse width modulation 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). At speeds above a preselected minimum speed, the voltage command (102) is developed in a closed loop manner responsive to a feedback signal (116) representing an estimate of the fundamental output of the main inverter (46).
Abstract:
The problem of reducing the effect of inaccuracies in rotor position detection for an engine starting system is solved in an engine start control apparatus (10) operating a generator (12) as a synchronous motor which employs acceleration control. The motor (12) receives power from a main inverter and an excitation inverter (48). The inverters (46, 48) are controlled by a control unit (22) which provides for acceleration control and closed loop reactive power control. The control unit (22) includes a pulse width modulation generator (100) which is responsive to a voltage command and a commutation command to develop switching signals for controlling the switches (S1-S6) in the main inverter (46). The voltage command is used to vary the duty cycle of the PWM signals. The commutation angle command is used to control the timing of the PWM signals. The commutation angle command is determined in accordance with an acceleration reference (112) and rotor position (70) feedback in a closed loop manner to maintain generally constant acceleration.
Abstract:
It has been recognized that the generator (12) in a generating system (10) can be used in a starting mode to provide motive power to the prime mover (14) to accelerate the latter up to self-sustaining speed. During operation in the starting mode, one or more malfunctions may occur which can cause damage to or destruction of system components. A system for detecting the failure of a prime mover (14) to ignite within a prime mover speed range in which the prime mover (14) is expected to achieve a self-sustaining condition continuously senses speed and acceleration of the prime mover (14) and determines the minimum prime mover acceleration encountered while operating within the speed range.