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Showing posts with label Power Electronics. Show all posts
Showing posts with label Power Electronics. Show all posts

Thursday, 17 September 2015

SWITCHED RELUCTANCE DRIVES & ITS TYPES

SWITCHED RELUCTANCE DRIVES.

The Switched Reluctance motor is more than a high-speed stepper motor. It combines many of the desirable qualities of both induction-motor drives and d.c. commutator motor drives, as well as PM brushless d.c. systems. Its performance and inherently low manufacturing cost make it a vigorous challenger to these drives. Its particular advantages may be summarized as follows:
(1) The rotor is simple and requires relatively few manufacturing steps; it also tends to have a low inertia.
(2) The stator is simple to wind; the end-turns are short and robust and have no phase-phase crossovers.
(3) In most applications the bulk of the losses appear on the stator, which is relatively easy to cool.
(4) Because there are no magnets the maximum permissible rotor temperature may be higher than in PM motors.
(5) The torque is independent of the polarity of phase current; for certain applications this permits a reduction in the number of power semiconductor switches needed in the controller.
(6) Under fault conditions the open-circuit voltage and short-circuit current are zero or very small.
(7) Most converter circuits used with SR motors are immune from shoot-through faults, unlike the inverters used with a.c. and brushless d.c. drives.
(8) Starting torque can be very high, without the problem of excessive inrush currents, as for example the large starting current of induction motors at high slip.
(9) Extremely high speeds are possible.
(10) The torque/speed characteristic can be 'tailored' to the application requirements more easily than in the case of induction motors or PM motors
.
However, the absence of 'free' Permanent Magnet excitation imposes the burden of excitation on the stator windings and the controller, and increases the per-unit copper losses. Particularly in small motors this is a disadvantage that limits the efficiency and the torque per ampere.
Thst non-uniform, nature of the torque production which leads to torque ripple and may cone SR motor also has some clear disadvantages. The most important is the pulsed, or at leatribute to acoustic noise. Over a narrow speed range it is possible to reduce the torque ripple to less than 10 per cent r.m.s., which is comparable with the levels attainable in induction motors and other brushless d.c. drives, but it is practically impossible to maintain this level of smoothness over a wide speed range. Fortunately it is easier to achieve smooth torque at low speeds, where many loads are most sensitive to torque ripple effects. The acoustic noise can be severe in large machines where ultrasonic chopping frequencies are not practical. But even in small ones, when all steps have been taken to minimize chopper noise, there remains a characteristic sound similar to 'tick over' noise in internal combustion engines at light load; under heavy load this tends to become a 'growl' that may be difficult to eliminate. The noise level is sensitive to the size, being much less severe in small machines. It also depends on the mechanical construction and the precision of the firing angles.
The torque ripple is also sensitive to these factors. Although the construction is simple, electrical and mechanical precision are essential to keep it quiet and this tends to increase the cost.

SPEED, FREQUENCY, WINDING- SWITCHED RELUCTANCE DRIVES

 The 'classical' forms of switched reluctance motor are shown in Fig., with stator:rotor pole numbers of 6:4 and 8:6. Others are possible, including 4:2, 6:2,10:4,12:8, and variants with more than one tooth per pole such as 12:10.


Only the two shown in Fig. are considered here.
The relationship between speed and fundamental switching frequency follows from the fact that if the poles are wound oppositely in pairs to form the phases, then each phase produces a pulse of torque on each passing rotor pole; the fundamental switching frequency in one phase is therefore,
 where n is the speed in rev/s and Nr is the number of rotor poles. If there are q phases there are qNr steps per revolution and the 'step angle' or 'stroke' is,

The number of stator poles usually exceeds the number of rotor poles.

POLE ARCS-SWITCHED RELUCTANCE DRIVES

The pole arcs are determined by the essential torque-production mechanism, which is the tendency of the poles to align. If fringing is neglected there must be overlap between a pair of rotor poles and the poles of the excited stator phase; in this case torque can be produced through an angle β, which is the smaller of the stator and rotor pole arcs. To produce unidirectional torque through 360° it is obvious that β must not be smaller than the step angle, otherwise there will be 'gaps' where no torque is produced: thus,
In order to get the largest possible variation of phase inductance with rotor position, the interpolar arc of the rotor must exceed the stator pole arc. This leads to the condition,

which ensures that when the rotor is in the 'unaligned' position relative to the stator poles of one phase, there will be no overlap and therefore a very low inductance. The unaligned position is defined as the conjunction of any rotor interpolar axis with the axis of the stator poles of the phase in question.

In Fig. the phase on the vertical axis is 'unaligned' while the phase on the horizontal axis is 'aligned'.
A further constraint on the pole arcs is that usually the stator pole arc is made slightly smaller than the rotor pole arc. This permits slight increases in the slot area, the copper winding cross-section, and the aligned/unaligned inductance ratio.

The constraints on pole arcs can be expressed graphically as shown, in which the 'feasible triangles' define the range of combinations normally permissible. As might be expected, the variation in performance of machines defined by different points in these triangles is considerable.

 Figure shows, for a three-phase motor, the cross-sections corresponding to the vertices A, B, and C on graph. Design C is likely to have too high an unaligned inductance and too little winding area. Design B has more copper area but still the unaligned inductance will be high because of fringing. Design A has a large winding area and a high inductance ratio, leading to a high efficiency and power density, but its torque ripple is higher than in the others.
The 'optimum' tooth-width/tooth-pitch ratio used in stepper motor design is not applicable to the SR motor. It is of course possible to determine a combination of pole arcs that gives the highest inductance ratio and therefore the highest 'static torque per ampere'. But too many other factors have to be considered to make this the universal choice. Among them are the torque ripple, the starting torque, and the effects of saturation. Curvature effects are also more pronounced than in steppers because of the small number of poles. As in steppers, pole taper is likely to be of benefit in reducing core losses, the m.m.f. drop in the rotor and stator steel, and the adverse effects of saturation. Stator pole taper also reduces the unaligned inductance, but it slightly decreases the winding area.
Several other detailed modifications to the simple geometry of Fig. above are permissible and advantageous, such as the use of a hexagonal stator blank which increases the winding area and can produce a mechanically stiffer core, at the same time reducing the scrap from the punching process. By reducing the scrap, the total production cost can also be minimised. Pole overhangs can be used to control the local saturation during the initial overlap period. Welding the outside of the stator stack is permissible as in a.c. motors, but this cannot be used on the rotor, which requires mechanical means for compressing the lamination together. The rotor may be skewed slightly to reduce noise.

Monday, 14 September 2015

APPLICATIONS OF LINE COMMUTATED RECTIFIERS IN MACHINE DRIVES

APPLICATIONS OF LINE COMMUTATED RECTIFIERS IN MACHINE DRIVES

Important applications for line commutated three-phase controlled rectifiers, are found in machine drives. Figure shows a dc machine control implemented with a six-pulse rectifier.
 
Torque and speed are controlled through the armature current ID , and excitation current Iexc. The current ID is adjusted with VD , which is controlled by the firing angle α through equation below,
 
This dc drive can operate in two quadrants: positive and negative dc voltage. This two quadrant operation allows regenerative braking when α>90°,
and Iexc <0.
The converter shown can also be used to control synchronous machines, as shown in figure below. In this case, a second converter working in the inverting mode operates the machine as self-controlled synchronous motor. With this second converter, the synchronous motor behaves like a dc motor but has none of the disadvantages of mechanical commutation. This converter is not line-commutated, but machine-commutated.
 The nominal synchronous speed of the motor on a 50 or 60 Hz ac supply is now meaningless, and the upper speed limit is determined by the mechanical limitations of the rotor construction.
There is the disadvantage that the rotational emfs required for load commutation of the machine side converter are not available at standstill and low speeds. In such a case, auxiliary force commutated circuits must be used.
 The line-commutated rectifier through α controls the torque of the machine. This approach gives direct torque control of the commutator less motor and is analogous to the use of armature current control shown in previous figure for the converter-fed dc motor drive.  
The line-commutated rectifiers are also used for speed control of wound-rotor induction motors. Sub synchronous and super synchronous static converter cascades using a naturally commutated dc link converter can be implemented. The figure below shows a super synchronous cascade for a wound rotor induction motor, using a naturally commutated dc link converter.
 In the super synchronous cascade shown in figure, the right hand bridge operates at slip frequency as a rectifier or inverter, while the other operates at network frequency as an inverter or rectifier. Difficulty control is experienced near synchronism when the slip frequency emfs are insufficient for natural commutation, and special circuit configuration employing forced commutation or devices with a self-turn-off capability are necessary for the passage through
synchronism. This kind of super synchronous cascade works better with cycloconverters.

Saturday, 5 September 2015

CYCLOCONVERTERS

CYCLOCONVERTERS
The cycloconverter operates in all four quadrants during a period. A pause (dead time) at least as small as the time required by the switch-over logic occurs after the current reaches zero, i.e. between the transfer to operation in the quadrant corresponding to the other direction of current flow. 
If control signal value alters sinusoidally with the desired frequency, then the waveform depicted in figure a) consists of a single-phase voltage with a large harmonic current. If the load is inductive, the current will present less distortion than voltage as shown in figure b).


Three single-phase cycloconverters may be combined to build a three-phase cycloconverter. The three-phase cycloconverters find an application in low frequency, high power requirements.
Control speed of large synchronous motors in the low speed range is one of the most common applications of three-phase cycloconverters. The figure shows a diagram for this application. They are also used to control slip frequency in wound rotor induction machines, for supersynchronous cascade (Scherbius system).

DUAL CONVERTERS IN DC DRIVES


DUAL CONVERTERS IN DC DRIVES
In many variable-speed drives, the four-quadrant operation is required, and three-phase dual converters are extensively used in applications up to 2 MW level. Figure shows a three phase dual converter, where two converters are connected back-to-back.

In the dual converter, one rectifier provides the positive current to the load, and the other the negative current. Due to the instantaneous voltage differences between the output voltages of the converters, a circulating current flows through the bridges. The circulating current is normally limited by circulating reactor,

LD, as shown in figure. The two converters are controlled in such a way that if a+ is the delay angle of the positive current converter, the delay angle of the negative current converter is a- = 180° - a+.


The figure shows the instantaneous dc voltages of each converter, vD+ and vD-. Despite the average voltage VD is the same in both the converters, their instantaneous voltage differences given by the voltage vr, generates the circulating current ir, which is superimposed with the load currents iD+ and iD-.
To avoid the circulating current ir, it is possible to implement a “circulating current free” converter if a dead time of a few milliseconds is acceptable. The converter section not required to supply current remains fully blocked. When a current reversal is required, a logic switch-over system determines at first the instant at which the conducting converter’s current becomes zero.
This converter section is then blocked and the further supply of gating pulses to it prevented. After a short safety interval (dead time), the gating pulses for the other converter section are released.

DUAL GATE INVERTER OSCILLATOR

DUAL GATE INVERTER OSCILLATOR

The figure below shows DUAL GATE INVERTER OSCILLATOR.