The present invention relates in general to drivers for gas discharge lamps. More specifically, the present invention relates to a driver for a metal halide lamp.
As is commonly known, a driver for a gas discharge lamp serves to feed the gas discharge lamp with the required amount of current, and receives itself its power from rectified AC mains. A well known conventional driver has a three-stage design. A first stage comprises an up-converter which receives the rectified AC mains input voltage and converts this input voltage to a higher DC output voltage. A second stage comprises a down converter which receives the DC output voltage from the up converter, and provides at its output a lower DC voltage (lamp voltage) and a required lamp current. This down converter has a current source characteristic, i.e. it controls the lamp current to a substantially constant value. A third stage comprises a commutator which regularly changes the direction of the lamp current, at a frequency typically in the order of about 100 Hz. In other words, although the lamp is operated at substantially constant current magnitude, the lamp current regularly changes its direction within a very brief time (commutating period).
Such three-stage electronic ballast design functions well, but has the disadvantage of being rather complicated and relatively costly. An alternative design, having the advantage of having less components and therefore reduced costs, has a two-stage design wherein the function of lamp current control and commutation are combined into one stage. Thus, such a two-stage electronic ballast comprises a first stage up converter for receiving the rectified AC mains input voltage and providing a higher DC output voltage. As a second stage, this two-stage electronic ballast comprises a half-bridge forward commutating stage (HBCF). In general, such HBCF comprises three branches. A first branch comprises two switches connected in series between the input terminals receiving the DC voltage from the first stage. A second branch comprises two capacitors connected in series between said two input terminals. A third branch, comprising the lamp, is connected between on the one hand the node between said two switches and on the other hand the node between said two capacitors.
There are situations where the above-described two-stage design is disadvantageous with respect to the above-described three-stage design. These situations occur mainly when the gas discharge lamp shows an asymmetric current behavior. This asymmetric current behavior may be an undesired property of the lamp itself. The chances on asymmetric current behavior are particularly substantial when a lamp approaches the end of its operational life.
Under normal circumstances, the current flowing in one direction during one half of the current period has exactly the same magnitude as the current flying in the opposite direction during the second half of the lamp period, while further the first half of the lamp period has exactly the same duration as the second half of the lamp period. In such circumstances the voltage at said node between said two capacitors will be half the input voltage. However, in the asymmetric situations described above, the voltage at said node will shift to the voltage of one of the input terminals, due to the fact that one of said capacitors needs to provide more current than the other capacitor.
A similar problem occurs in circumstances where it is desired to drive the lamp at a duty cycle differing from 50%. Normally, the duty cycle of the lamp current is exactly 50%, this duty cycle being defined as the duration of the one half of the lamp period divided by the overall lamp period. Again, if the current magnitude in the one half lamp period is equal to the current magnitude in the other half lamp period whereas the duration of the one half lamp period differs from the duration of the other half lamp period, one of said capacitors needs to provide more current than the other, and the voltage level at said node between said two capacitors shifts to the voltage level of one of the input terminals.
The above-mentioned problems do not occur in the conventional three-stage design, where such capacitors are absent. Further, driving a lamp with a duty cycle differing from 50% is relatively easy in such conventional three-stage design, simply by selecting an appropriate timing for the switching of the commutator switches.
Accordingly, it is an objective of the present invention to provide an electronic ballast for a gas discharge lamp wherein the advantages of the two-stage converter are combined with the advantages of the three-stage converter.
More particularly, it is an objective of the present invention to provide an electronic ballast for a gas discharge lamp having a two-stage design so that it involves a relatively small amount of components and therefore Relatively low costs, the electronic ballast comprising a half bridge commutating forward stage as second stage, the electronic ballast being capable of handling asymmetric currents, wherein the problem of voltage shift at the node between said two capacitors is eliminated.
According to an important aspect of the present invention, the electronic ballast comprises a double fly back converter as first stage, each fly back converter being coupled to a respective one of said capacitors, this double fly back converter circuit acting as power factor correction circuit charging each capacitor substantially independently from the other capacitor, such that the voltage shift during operation is avoided or limited to a relatively small and acceptable extent.
These and other aspects, features and advantages of the present invention will be further explained by the following description of preferred embodiments of the driver according to the present invention with reference to the drawings, in which same reference numerals indicate same or similar parts, and in which:
The electronic ballast 101 comprises a first stage up converter 110, a second stage down converter 120, and a third stage commutator 130. The input of the up converter stage 110 may be provided with a pre-conditioner and rectifier for filtering and rectifying the AC mains input voltage received at an input 102. Such pre-conditioner may comprise a first inductor 103 connected in series with one input terminal, a second inductor 104 connected to the other input terminal, and a capacitor 105 connected in parallel to output terminals of said inductors 103 and 104. The pre-conditioner may further comprise a rectifying unit 106, such as for instance a diode bridge. Thus, at its input, the up converter 110 receives rectified AC mains voltage.
The electronic ballast 101 has a common rail 107 connected to one input terminal of the up converter 110, this rail 107 being common to all three stages; the voltage level at this common rail 107 will be referred to as zero voltage. The up converter 110 comprises a series arrangement of an inductor 111 having one terminal coupled to one input terminal of the up converter 110, and a diode 112 having its anode connected to the inductor 111 and having his cathode coupled to the output of the up converter 110. A controllable switch (MOSFET) 113, controlled by a first control unit 115, is connected between the common rail 107 and the node between said inductor 111 and said diode 112. A buffer capacitor 114 is connected in parallel to the output of the up converter 110.
The up converter 110 provides at its output a DC voltage having a voltage level higher than the rectified AC mains voltage.
The down converter 120 comprises a series arrangement of an inductor 121 having one terminal connected to the output of the down converter 120, and a controllable switch 123, controlled by a second control unit 125, the controllable switch 123 being connected between said inductor 121 and said diode 112. The down converter 120 further comprises a diode 122 having its anode connected to the common rail 107 and having its cathode connected to the node between said inductor 121 and said controllable switch 123. A filter capacitor 124 is connected in parallel to the output of the down converter 120.
The down converter 120 substantially acts as a current source, providing at its output a substantially constant current at a reduced voltage level.
The commutator stage 130 comprises a first series arrangement of two controllable switches (MOSFET) 131 and 132, connected between the input of the commutator and the common rail 107, and a second series arrangement of two controllable switches 133 and 134, also connected between said input and said common rail 107. The commutator 130 further comprises a series arrangement of the gas discharge lamp 140 and an igniter coil 135, associated with an igniter circuit 136, said series arrangement of igniter coil 135 and lamp 140 being connected between, on the one hand, a node A between said switches 131 and 132 and, on the other hand, a node B between said switches 133 and 134. A filter capacitor 137 is connected in parallel to said series arrangement of igniter coil 135 and lamp 140.
The controllable switches 131, 132, 133, 134 are controlled by a third control unit 138. The three control units 115, 125 and 138 may be combined into one combined control unit.
The first control unit 115 of the up converter 110 controls the controllable switch 113 such that the output voltage of the up converter is substantially constant. To that end, the output voltage of the up converter 110, at the cathode of the diode 112, is measured and a measuring signal is provided to said control unit 115, but for sake of simplicity this is not shown in
The second control unit 125 of the down converter 120 controls the controllable switch 123 such that the output power level of the down converter 120 is substantially constant. To that end, a measuring signal representing the input current of the down converter 120 is provided to the control unit 125, but for sake of simplicity this is not shown in
The third control unit 138 of the commutator stage 130 controls the four controllable switches 131 to 134 such that the output current of the down converter 120 is applied to the lamp 140 in alternating directions. In one half lamp period, the switches 131 and 134 are closed (conductive) while the switches 132 and 133 are open (non-conductive), so that the output current from down converter 120 is applied to the lamp 140 in the direction from node A to node B. In the other half lamp period, the switches 131 and 134 are open (non-conductive) while the switches 132 and 133 are closed (conductive), so that the output current from the down converter 120 is applied to the lamp 140 in the opposite direction.
Conventionally, the third control unit 138 of the commutator stage 130 controls the four switches 131-134 with a duty cycle of 50%, so that the duration of the one half lamp period is exactly the same as the duration of the other half lamp period However, if it is desired to operate the lamp 140 with a duty cycle differing from 50%, this can easily be achieved by adequate control of the four switches 131 to 134, as will be clear to a person skilled in the art.
The second stage HBCF 250 comprises a series arrangement of two buffer capacitors, typically electrolytic capacitors, 251 and 252, connected between input (node 261) and common rail 107 (node 262). A node between these two capacitors 251 and 252 is indicated at A. The second stage HBCF 250 further comprises a series arrangement of two controllable switches 253 and 254, also connected between said input and said common rail 107. A node between said two switches is indicated at B. Said controllable switches are controlled by a control unit 255.
Between said two nodes A and B, a lamp branch is connected. This lamp branch comprises a series arrangement of a lamp 240, an igniter coil 235 associated with an igniter circuit 236, and a current limiting coil 256. A filter capacitor 237 is connected in parallel to the series arrangement of said igniter coil 235 and said lamp 240.
From a comparison between the circuit of the two stage electronic ballast 201 illustrated in
In operation, the control unit 255 controls the controllable switches 253 and 254 as follows. During a first half lamp period, the first switch 253 is open (non-conductive) while the second switch 254 is repeatedly opened and closed at a relatively high frequency. This causes a lamp current to flow from node A to node B, wherein the current limiting coil 256 in conjunction with the high frequency switching of second switch 254 effects a limitation of the lamp current. In the second half lamp period, the situation is reversed, in that the second switch 254 is open (non-conductive) and the first switch 253 is switched open and closed at a high frequency, causing a lamp current to flow in the direction from node B to node A.
In this process, the buffer capacitors 251 and 252 are charged. If the lamp 240 is operated with symmetric current, i.e. if the two half lamp periods have equal duration and equal current magnitude, and if the lamp 240 shows symmetric behavior, the voltage level at node A between said two capacitors 251 and 252 will, on average, take a value of half the input voltage (i.e. half the output voltage of the up converter 110).
However, if the lamp 240 behaves in an asymmetric way, or if the control unit 255 controls the switches 253 and 254 in an asymmetric way (duty cycle differing from acitor will always be consistently charged more than the other capacitor, so that the voltage level at node A will either rise to input voltage level or will drop to common rail voltage level.
A lamp 240 is connected between output terminals 263a, 263b of a lamp output 263, the first lamp output terminal 263a being coupled to the igniter coil 235, the second lamp output terminal 263b being coupled to the current limiting coil 256.
The first stage DC/DC converter 310 is, according to the basic principle of the present invention, implemented according to a double fly-back design, comprising an inductive energy storage buffer 320, at least one input circuit 330, and two output circuits 340 and 350, associated respectively to the first and second buffer capacitors 251 and 252 of the second stage HBCF 250. In the exemplary embodiment 301 illustrated in
The first end terminal 322 is connected to the positive output terminal of rectifier 106, and the central terminal 324 is connected to the negative output terminal of rectifier 106. Thus, an input circuit 330 is defined, which includes the first coil section 321A. In this input circuit 330, a controllable switch, preferably a MOSFET, 325 is included. In the example shown, this controllable switch 325 is arranged between the negative rectifier output and the central coil terminal 324. The controllable switch 325 is controlled by a control unit 326.
A first output circuit 340 is defined by the second coil section 321B being connected in parallel to the first buffer capacitor 251. More particularly, a first diode 341 has nnected to second coil end terminal 323 and has its cathode connected to an end terminal of first buffer capacitor 251 opposite node A, i.e. a first bridge input terminal 261. A second output circuit 350 is defined by the first coil section 321A being connected in parallel to the second buffer capacitor 252 of the HBCF 250. More particularly, a second diode 351 has its cathode connected to first end terminal 322 and has its anode connected to an end terminal of second buffer capacitor 252 opposite node A, i.e. a second bridge input terminal 262. The central coil terminal 324 is connected to node A by a common conductor 311, common to the first output circuit 340 and the second output circuit 350.
The operation of this double fly-back converter 310 is as follows. The control unit 326 controls the controllable switch 325 to switch repeatedly from its open (non-conductive) condition to its closed (conductive) condition. If the controllable switch 325 is closed, an input current flows through the first coil section 321A from its first end terminal 322 to its central terminal 324, as illustrated by arrow Iin in
The operation of the second stage HBCF 250 is as usual. The control unit 255 controls the switches 253 and 254 such as to effect a commutating lamp current. If the lamp shows asymmetric behavior, or if the control unit 255 receives a command signal Scomm, for instance from a user-controllable input device 257, ordering it to drive the switches 253 and 254 with a duty cycle differing from 50%, one of the buffer capacitors 251, 252 may discharge more than the other one. The buffer capacitor which is discharged faster will show a smaller voltage drop than the other one, as a result of which the corresponding output current charging this capacitor will have a higher current magnitude. As a result, the capacitor which is discharged faster is also charged faster.
The control unit 326 comprises a voltage sensor input 326a coupled to receive a measuring signal representing the output voltage of the flyback converter stage 310, and generates a switch actuating signal such that the third controllable switch 325 is switched open and closed at a predetermined operating frequency. In this case, such measuring signal may represent the voltage over the series arrangement of capacitors 251 and 252, i.e. the voltage between terminals 261 and 262. The control unit 326 is responsive to such measuring signal to adapt the duty cycle of said switch actuating signal in order to maintain the output voltage at a predetermined level.
The operation of the second embodiment 401 is identical to the operation of the first embodiment 301. A typical feature of this second embodiment 401 is that it may provide a galvanic separation between input winding 421 and output windings 424 and 425, as illustrated. If such galvanic separation is not necessary or not desired, the first end terminal 421a of input winding 421 may be connected to the first end terminal 425a of second output winding 425.
It should be clear to a person skilled in the art that the present invention is not limited to the exemplary embodiments discussed above, but that various variations and modifications are possible within the protective scope of the invention as defined in the appending claims. For instance, instead of the filter capacitor 237, a filter capacitor may be connected between second lamp output terminal 263b and the first bridge input terminal 261 and/or a filter capacitor connected between second lamp output terminal 263b and the second bridge input terminal 262.
Further, in the case of embodiment 401 of
Further, although in general the windings ratio of first output winding 321B; 424 and second output winding 321A; 425 will be equal to one, such is not essential, and it may in certain circumstances be useful to have a windings ratio differing from one.
Summarizing, the present invention provides a two-stage electronic ballast for driving a gas discharge lamp. As a first stage, the ballast comprises a half-bridge commutating forward (HBCF) stage comprising a series arrangement of a first buffer capacitor and a second buffer capacitor connected between two bridge input terminals. As a second stage, the ballast comprises a double flyback converter stage comprising an inductive energy storage buffer having at least one input circuit suitable for receiving a rectified AC mains input voltage, the buffer further having at least two output circuits, each output circuit being coupled to a respective buffer capacitor of said half-bridge commutating forward stage lly charging said buffer capacitors. Thus, the present invention succeeds in providing a two-stage electronic ballast which is capable of driving a gas discharge lamp with a commutating current having a variable duty cycle, as desired, differing from 50%, this duty cycle being capable of being set variably by a user such as to provide a lamp current with DC component, of which the level can be set by setting the duty cycle. This may be particularly useful in the case of a gas discharge lamp, particularly a metal halide lamp, of a type which has light generating properties depending on the DC current level in the lamp current.
Number | Date | Country | Kind |
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02078133.2 | Jul 2002 | EP | regional |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/IB03/03145 | 7/10/2003 | WO | 1/25/2005 |