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Patent 2167189 Summary

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(12) Patent Application: (11) CA 2167189
(54) English Title: LOW FREQUENCY SQUARE WAVE ELECTRONIC BALLAST FOR GAS DISCHARGE DEVICES
(54) French Title: BALLAST ELECTRONIQUE A ONDES RECTANGULAIRES DE BASSE FREQUENCE POUR DISPOSITIFS A GAZ LUMINEUX
Status: Dead
Bibliographic Data
(51) International Patent Classification (IPC):
  • H05B 41/16 (2006.01)
(72) Inventors :
  • VILA-MASOT, OSCAR (United States of America)
  • MELIS, JANOS (United States of America)
(73) Owners :
  • LED CORPORATION N.V. (Netherlands Antilles)
(71) Applicants :
(74) Agent: ARKIN, GARY
(74) Associate agent:
(45) Issued:
(86) PCT Filing Date: 1994-08-26
(87) Open to Public Inspection: 1996-02-27
Availability of licence: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): Yes
(86) PCT Filing Number: PCT/US1994/009467
(87) International Publication Number: WO1996/007130
(85) National Entry: 1996-01-12

(30) Application Priority Data: None

Abstracts

English Abstract




A low frequency square wave electronic ballast used for
a gas discharge device includes a high power factor pre-regulator
connected to a sinusoidal AC power supply and a power controlled
DC current source connected to the pre-regulator. A low frequency
square wave DC-to-AC inverter is connected to the DC current
source and an ignitor circuit is connected to the inverter. A
monitor circuit as well as a low power stabilized logic supply
voltage source are also employed. The entire circuit is
connected to a gas discharge device such that the instantaneous
power of this device is constant and controlled providing an
acoustic resonance free operation and an ideal ballast curve.


French Abstract

Un ballast électronique a ondes rectangulaires de basse fréquence utilisé pour un dispositif d'excitation à décharge de gaz comprend un pré-régulateur de facteur de puissance élevé (Unité 1) connecté à une alimentation à courant alternatif sinusoidal et une source de courant continue régulée (unité 2) connectée au pré-régulateur (Unité 1). Un onduleur c.c./c.a. à ondes carrées de basse fréquence (Unité 4) est connecté à l'onduleur (P.U. - 3). Un circuit de contrôle (Unité 6) ainsi qu'une source de tension d'alimentation stabilisée de faible puissance (Unité 5) sont également utilisés. Tout le circuit est connecté à un dispositif à gaz lumineux (lampe HID) de sorte que la puissance instantanée de ce dispositif est constante et commandée, son fonctionnement est exempt de résonance acoustique et sa courbe de ballast est idéale.

Claims

Note: Claims are shown in the official language in which they were submitted.





14

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:

1. A low frequency square wave electronic ballast for
a gas discharge comprising a high power factor preregulator
connected to a power supply, wherein said high power factor pre-
regulator is provided with a boost converter including an
inductor, a first MOSFET, a rectifier, and an output capacitor,
as well as a control unit provided with a shunt resistor, wherein
said shunt resistor is connected to the source of said first
MOSFET and to said output capacitor, and said inductor and said
rectifier are connected to said first MOSFET, and further
including a complementary MOSFET pair connected to said first
MOSFET and a driver MOSFET, first and second dual input NAND
gates each having outputs connected to the gates of said
complementary MOSFET pair implementing said driver MOSFET in
which each of the MOSFETs of said the complementary MOSFET pair
can be independently controlled.

2. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 1, wherein said
control unit is connected to said first and second NAND gates,
and further including a first and a second voltage comparator
connected to the inputs of said dual input NAND gates, a saw-
tooth generator controlled by a third dual input NAND gate,
wherein said first voltage comparator is connected to said shunt
resistor implementing zero current sensing and further wherein
the inverting input of said second voltage comparator is
connected to said saw-tooth generator, the first input of said
third NAND gate is connected to the delayed output of said second
voltage comparator and the second input of said third dual input
NAND gate is connected to the output of said first voltage
comparator input, and further including an error amplifier,
wherein the output of said error amplifier is connected to the
non-inverting input of said second voltage comparator, implement-
ing controlled ON-time technique in which the average current of
said inductor is sinusoidal.





3. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 1, comprising a
power controlled DC current source connected to said high power
preregulator, wherein said power controlled DC current source is
provided with a buck converter including a first MOSFET, an
inductor, a first rectifier connected between said first MOSFET
and said inductor, an output capacitor connected across said
first rectifier, a complementary MOSFET pair connected to said
first MOSFET, first and second dual input NAND gates connected
to said complementary MOSFET pair and a control circuit connected
directly to said first and said second dual input NAND gates
implementing floating control, and further wherein said control
circuit includes a zero inductor current sensing unit connected
to the first inputs of said first and second dual input NAND
gates, an inductor current control unit connected to the second
inputs of said first and second dual input NAND gates and an
output voltage inversion unit connected to said inductor current
control unit providing a power controlled DC current source.

4. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 3, wherein said
zero inductor current sensing unit includes a first voltage
comparator, a second rectifier and a Schottky rectifier, wherein
the cathode of said Schottky rectifier is connected to the
cathode of said first rectifier, the anode of said second
rectifier is connected to the anode of said first rectifier and
the anode of said Schottky rectifier is connected to the cathode
of said second rectifier, and further wherein the common point
of said Schottky and said second rectifiers is connected to said
first voltage comparator implementing the sensing of the zero
level of inductor current in the OFF state of said first MOSFET.

5. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 3, wherein said
inductor current control unit includes a second voltage compara-
tor, a second MOSFET having a source and drain, said second
MOSFET connected to the output of said first voltage comparator,




16

a first capacitor connected in parallel with the source and drain
of said second MOSFET, a third rectifier connected to said first
capacitor and a first resistor connected in series with said
third rectifier, and further wherein the common point of said
third rectifier and said first capacitor is connected to the non-
inverting input of said second voltage comparator, said first
rectifier being connected to the positive terminal of said output
capacitor and the source of said second MOSFET being connected
to the positive logic supply of said control circuit, providing
an analog modelling of the inductor current in the ON-state of
said first MOSFET.

6. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 3, wherein said
output voltage inversion unit includes a second capacitor, a
fourth rectifier, a voltage divider resistor pair connected to
said second capacitor, a first and a second Zener diode connected
in series with a second and a third resistor, respectively,
wherein the cathode of said fourth rectifier is connected to the
positive terminal of said output capacitor, the anode of said
fourth rectifier is connected to the first terminal of said
second capacitor, the second terminal of said second capacitor
and said second and third resistors are connected to the zero
level of said control circuit and said first and said second
Zener diodes are connected to the common point of said voltage
divider resistor pair, and further wherein the common point of
said voltage divider resistor pair is connected to the inverting
input of said second voltage comparator, implementing constant
output power in the range of a non-zero minimum and a maximum
output voltage and further including a third Zener diode
connected in series with a third resistor which are connected to
the logic supply of said control circuit, and a fifth rectifier
connected to the common point of said third Zener diode and said
third resistor wherein the cathode of said fifth rectifier is
connected to the inverting input of said second voltage compara-
tor implementing a constant output current in the range of the
zero and a non-zero minimum output voltage.




17

7. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 3, comprising a
low frequency square wave DC-to-AC inverter connected to said
power controlled DC current source wherein said low frequency
square wave DC-to-AC inverter includes first, second, third and
fourth MOSFETs, first, second, third and fourth complementary
MOSFET pairs, first and second logic optoisolators, a logic
signal driver unit and a frequency control unit, wherein said
first and said second complementary MOSFET pairs are connected
to said first and said second MOSFETs, said third and said fourth
complementary MOSFET pairs are connected to said third and said
fourth MOSFETs, said first and said second logic optoisolators
are connected to said third and said fourth complementary MOSFET
pairs, said first and said second complementary MOSFET pairs and
said first and said second logic optoisolators are connected to
said logic signal driver unit and said logic signal driver unit
is connected to said frequency control unit, implementing a time
programmed frequency control including DC operations of said low
frequency square wave DC-to-AC inverter.

8. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 7, wherein said
logic signal driver unit includes first, second, third and fourth
dual input NAND gates, first and second voltage comparators, an
RC circuit, a voltage divider resistor pair connected to the
logic supply of said logic signal driver unit, a logic control
input and an inhibition input, wherein said RC circuit is
connected to said logic control input and the zero voltage level
of said logic driver, the non-inverting input of said first
voltage comparator and the inverting input of said second voltage
comparators are connected to the common point of said RC circuit,
the inverting input of said first voltage comparator and the non-
inverting input of said second voltage comparator are connected
to the common point of said voltage divider resistor pair, the
output of said first voltage comparator is connected to the first
inputs of said first and said third dual input NAND gates, the
output of said second voltage comparator is connected to the

18

first inputs of said second and fourth dual input NAND gates, the
second input of said third dual input NAND gate is connected to
said logic control input, the second input of said fourth dual
input NAND gate is connected to the inverter logic control signal
and the second inputs of said first and said second dual input
NAND gates are connected to said inhibiting input and further
wherein the outputs of said first, second, third and fourth dual
input NAND gates are connected to said first complementary MOSFET
pair, said second complementary MOSFET pair, said first logic
optoisolator and said second logic optoisolator, implementing an
alternating switching or DC operation, or an inhibition of said
square wave inverter including deadtime control avoiding cross
conductions of said first, second, third and fourth MOSFETs.

9. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 7, wherein said
frequency control unit includes a third and a fourth voltage
comparator, a digital timer having a first and a second output,
an analog timer, a low frequency digital oscillator and a D flip-
flop wherein said third and said fourth voltage comparators are
controlled by the input voltage of said square wave inverter,
said digital timer is controlled by said third voltage compara-
tor, said analog timer is controlled by said fourth voltage
comparator, the output of said low frequency digital oscillator
is connected to the clock input of said D flip-flop, the output
of said analog timer is connected to the SET input of said D
flip-flop and the output of said D flip-flop is connected to the
logic control input of said logic driver providing a short term
time programmed DC operation and the transition to normal low
frequency operation of said square wave inverter under loaded
condition, and further wherein the first output of said digital
timer is connected to the inhibition input of said logic driver
implementing a long term time programmed inhibiting of said
square wave inverter under low load condition.

10. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 3, wherein said

19
frequency control unit further includes a high frequency digital
oscillator controlled by said analog timer and first and second
AND gates, wherein the output of said high frequency digital
oscillator and the first output of said digital timer is
connected to said first AND gate, the output of which is
connected to said logical signal unit and the output of said low
frequency digital oscillator, and the output of said high
frequency digital oscillator is connected to said second AND
gate, the output of which is connected to said D flip-flop
providing a short term time programmed high frequency current
pulse operation of said square wave inverter.

11. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 7, comprising an
ignitor circuit connected to said high power factor preregulator
and connected to said low frequency square wave DC-to-AC
inverter, wherein said ignitor circuit includes a pulse trans-
former having first and second windings, a resistor connected to
the output capacitor of said high power factor pre-regulator, a
capacitor connected to said resistor, a thyristor and an RC
circuit connected to the gate of said thyristor and second output
of said digital timer, wherein said second winding of said pulse
transformer is connected to said capacitor and said thyristor,
and further wherein said first winding of said pulse transformer
is connected in series with the output of said square wave
inverter and said gas discharge device, providing periodical high
voltage ignition pulses for said gas discharge device.

12. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 7 comprising a
low power stabilized logic supply voltage source connected to
said high power factor preregulator, also connected to said power
controlled DC current source and to said low frequency square
wave DC-to-AC inverter, wherein said low power stabilized logic
supply voltage source includes a bridge rectifier connected to
said power supply, a first capacitor connected to the DC output
of said bridge rectifier, a high frequency half-bridge square


wave oscillator connected to said first capacitor, and five
linear regulators connected to said high frequency half-bridge
square wave oscillator, and further wherein said high frequency
half-bridge square wave oscillator includes first and second
transistors, second and third capacitors operating as voltage
divider capacitors, a transformer having a primary winding
connected to the common points of said transistors and said
voltage divider capacitors, first and second feedback windings
and five secondary windings, said high frequency half-bridge
square wave oscillator further including a first RC circuit
connected to said first feedback winding and the base of said
first transistor, a second RC circuit connected to said second
feedback winding and the base of said second transistor, and a
self-switching off starter connected to the base of said first
transistor, providing five isolated nonstabilized high frequency
square wave voltage sources providing five isolated and stabi-
lized logic supply voltage sources.

13. A low frequency square wave electronic ballast for
a gas discharge device in accordance with claim 12, comprising
a monitor circuit connected to said low power stabilized logic
supply voltage source, wherein said monitor circuit includes a
first and a second voltage comparator controlled by the rectified
voltage of said power supply implementing a window comparator for
input voltage, a third voltage comparator, a photoresistor
controlling said third voltage comparator, a fourth voltage
comparator, a thermistor controlling said fourth voltage
comparator, and further wherein said high power factor pre-
regulator and said power controlled DC current source are
controlled by the outputs of said voltage comparators providing
a light controlled switch, an over temperature protection and a
logic supply voltage protection.

Description

Note: Descriptions are shown in the official language in which they were submitted.


2167189


LOW FREQUENCY SQUARE WAVE ~T~CTRONIC R~r~T~A~T
FOR GAS DISCHARGE DEVI OES
BACgGROUND OF 1~ INVENTION
1. Field of the Invention
The present invention relates to a low frequency power
converter and specifically to low frequency electronic ballasts
for gas discharge devices. More specifically, the present
invention relates to a low frequency square wave electronic
ballast for high pressure sodium lamps.

2. Prior Art
An important application for high frequency switchmode
power converters is supplying power to gas discharge devices,
especially high pressure sodium (HPS) lamps. In the case of high
frequency powering of gas discharge lamps, the high frequency
h~ t and the gas discharge lamp have a higher level of
interaction than that which exists between a conventional low
frequency ballast and gas discharge lamp. High frequency
ballasts suffer from acoustic resonance which can cause various
problems such as instability, high output fluctuation, or, in the
worst case, cracked arc tubes. Therefore, an optimum solution
to this problem is the use of a high frequency DC-to-DC switch-
mode as a controlled current source connected to a low frequency
DC-to-AC square wave inverter supplying the gas discharge lamp.
Due to its lessened weight, higher efficiency and the nonexis-
tence of acoustic resonances, this novel high frequency ballast
-~ with a low frequency output has significant advantages when
compared with either the conventional low frequency ballasts and
the usual high frequency electronic ballast. Additionally, a
new, high sophisticated electronic ballast generation can be
introduced to provide several special features, such as, for
example, automatic or controlled ~; mm; ng.
Therefore, the essential design targets for a highly
sophisticated, high efficiency, low frequency electronic ballast
supplying gas discharge lamps would be the following:
(a) very high efficiency (s 95%), energy saving
and low temperature rise of critical components;

2167189




(b) low frequency square wave lamp current (crest
factor is unit). Since the instantaneous lamp power is constant
(no flickering), no acoustic resonance can occur;
(c) high reliability and long life time (lower
power loss, no electrolytic capacitors);
(d) fully controlled lamp power, elimin~ting the
effects of line voltage fluctuation and lamp aging;
(e) programmed and/or controlled~immlngproviding
essential energy saving;
(f) automatic switching off when the lamp has
- reached the end of its life time (programmed in advance);
(g) automatic light switching and high temperature
protection; and
(h) power factor correction (PF 2 95%) and EMI
filtering.
The prior art is replete with many known circuits
providing high frequency ballast for gas discharge lamps. For
instance, high efficient electronic ballast which can be used
with HPS (HID) lamps are discussed in U.S. Patent No. 5,097,183
entitled "Master-Slave Half-bridge DC-to-AC Switchmode Power
Converter" and U.S. Patent Application Serial No. 883,762, filed
May 15, 1992, entitled "Self-Symmetrizing and Self-Oscillating
Half-Bridge Power Inverter" assigned to the assignee of the
present invention.

- 25 SUMMARY OF THE INVENTION
It is an object of the present invention to provide a
power controlled and current limited current source implementing
the ideal ballast curve for HPS (HID) lamps.
A second object of the present invention is to provide
a power controlled current source, wherein the power can be
selected and/or continuously changed.
A further object of the present invention is to provide
a high frequency DC-to-DC converter as a power controlled current
source, wherein no electrolytic capacitors are used.

21 671 89
.




Another object of the present invention is to provide
a high frequency buck converter configuration which has a
substantially improved efficiency, wherein the control circuit
is floating together with the main switching transistor.
A further object of the present invention is to provide
a circuit, especially for a buck converter configuration,
implementing the inversion of output voltage and zero current
sensing.
Another object of the present invention is to provide
a high efficiency square wave full-bridge inverter operation in
a very wide frequency range including DC operation.
A further object of the present invention is to provide
a logic control circuit controlling a square wave full-bridge
inverter implementing programmed transition between the high (or
zero) and the low frequency operations.
Another object of the present invention is to provide
a low power stabilized logic supply voltage source connected to
main voltage, wherein no electrolytic capacitors are used.
A further object of the present invention is to provide
a low power stabilized logic supply voltage source connected to
main voltage, wherein no electrolytic capacitors are used.

BRIEF DESCRIPTION OF Tn~ DRAWINGS

FIG. 1 illustrates a schematic diagram of the preferred
- electronic ballast for gas discharge devices including six basic
units;

FIG. 2A, 2B and 2C show the voltage and current
waveforms with respect to the schematic diagram of FIG. 1;

FIG. 3A illustrates the ballast curve as a diagram of
lamp power versus lamp voltage realized by the preferred
electronic ballast of the present invention;

FIG. 3B shows the diagram of lamp current versus lamp
voltage;

2 1 6 7 1 89




FIG. 4 shows the circuit diagram of a high power factor
preregulator designated as UNIT-1 in FIG. 1;

FIG. 5A shows the circuit diagram of a power control
converter designated as UNIT-2 in FIG. 1;

5FIG. 5B illustrates a diagram of the inductor current
with respect to UNIT-2;

FIG. 5C illustrates a diagram of the functional
relationship between output and control voltages;

FIG. 6A shows the circuit diagram of a controlled full-
bridge inverter and ignitor circuit designated as UNIT-3 and
UNIT-4 in FIG. 1;

FIG. 6B illustrates the four output control signals of
a logic drive unit designated as LD-3 in FIG. 1;

FIG. 6C illustrates a timing diagram with respect to
UNIT-3 under no load condition;

FIG. 6D illustrates a timing diagram with respect to
UNIT-3 under loaded condition; and

- FIG. 7 shows the circuit diagram of a logic supply and
a monitor unit designated as UNIT-5 and UNIT-6 in FIG. 1.

20DETATr.~n DESCRIPTION OF THE lNV~N'llON
FIG. 1 illustrates a schematic diagram of the preferred
electronic ballast for gas discharge devices including:
a high power factor preregulator designated as UNIT-1
including a boost converter (PU-1), a MOSFET driver (MD-1) and
a control unit (CU-1);
a power controlled DC current source designated as
UNIT-2 including a buck converter (PU-2), a MOSFET driver (MD-2)
and a control unit (CU-2);

2167189




a low-frequency square wave DC-to-AC converter
designated as UNIT-3 including a full-bridge square wave inverter
(PU-3), four MOSFET drivers (MD-3), a logic driver (LD-3) and a
frequency control unit (CU-3);
a high voltage ignitor circuit designated as UNIT-4;
a stabilized logic supply voltage source designated as
UNIT-5 including a low power half-bridge square wave inverter
(B) and five linear regulators (LR-1, LR-2, LR-3, LR-4 and LR-
5);
a monitor unit designated as UNIT-6 including an input
voltage, a temperature and a light sensing circuit; and
a gas discharge device, especially a high pressure
sodium lamp designated as HID lamp.
FIG. 2A, 2B and 2C show some characteristic voltage and
current waveforms of the preferred electronic ballast with
respect to schematic diagram of FIG. 1. Particularly, FIG. 2A
shows the nearly sinusoidal input current (Ii) of the high power
factor preregulator. Furthermore, FIG. 2B shows the input (V1)
and output (VO) voltages of the power controlled DC current
source. FIG. 2C shows the lamp voltage (VL = + VO) and lamp
current (IL) waveforms in the normal, low frequency mode. This
figure illustrates that an instantaneous lamp power can be
obtained.
FIG. 3A illustrates the ballast curve as a diagram of
the functional relationship between the lamp power (PL) and the
-~ lamp voltage (VL). Furthermore, FIG. 3B shows the diagram of
lamp current (IL) versus lamp voltage (VL). Three different
ranges can be distinguished, depending on the lamp voltage as it
is shown in FIG. 3A and 3B, namely;
a constant lamp current range in the warming up period
(05Vr.~VL(min) );
a constant lamp power range is a certain range of lamp
voltage (VL(~) <VL~VL(~) ); and
a forbidden range ( VL> Vr (~) ), if the lamp voltage
reaches V~ ) the ballast will automatically switch off.

2167189




Two different nom;n~l lamp power levels can be selected
by the preferred ballast, for instance 200W or 250W. Further-
more, the lamp power can be continuously changed providing
~lmm;ng capability which can be significant from an energy saving
viewpoint.
The six basic units of the present invention will now
be explained.
UNIT-1 includes an input filter F10 and is shown in
FIG. 4. The circuit is based on a st~n~rd boost converter
configuration including a bridge rectifier B10, an inductor L10,
a power MOSFET M10, a fast rectifier D10 and an output capacitor
C10. Controlled on-time and zero current switching on techniques
are applied. Therefore, the peak and average inductor current
is sinusoidal as is the input voltage. The MOSFET driver
designated as MD-1 in FIG. 1 is implemented by MOSFETs M11 and
M12, the inputs of which are connected to the outputs of dual
input NAND Schmitt-triggers IC10 and IC11, respectively.
The control unit designated as CU-1 in FIG. 1 includes:
an error amplifier IC15;
a saw-tooth generator implemented by a resistor R11,
a capacitor C11, a MOSFET M13 and a NAND Schmitt-trigger IC13;
a pulse width modulated (PWM) comparator IC14; and
a zero current sensing comparator IC12 connected to a
shunt resistor R10.
An essential difference between the preferred high
- power factor preregulator of the present invention and standard
regulators, is the position of the shunt resistor R10. In this
case, the voltage drop (which is proportional to the inductor
current) on R10 is positive when compared to the zero level of
the control unit providing sensitivity and less loss. This
m~;m~l on-time and the m~lm~l inductor current is limited by
Zener diode Z10. This solution is effective if the main switch
M10 is switched on at zero inductor current level as in the
preferred embodiment. A further difference between the preferred
high power factor preregulator and standard regulators, is the
utilization in the present invention, of a relatively small value
film capacitor C10 instead of employing a large value electro-


2 ~ 67l 89
-

lytic capacitor as the output capacitor. In the case, the
fluctuation (120Hz) of the output voltage V1 is large as can be
seen in FIG. 2B.
UNIT-2, which is connected to the output capacitor C10
of UNIT-1 is shown in FIG. 5A. The power unit designated as PU-2
in FIG. 1 is based upon a standard buck converter configuration
including a power MOSFET M20, a fast rectifier D20, an inductor
L20 and an output (film) capacitor C20. The MOSFET driver
designated as MD-2 in FIG. 1 is implemented by MOSFETs M21 and
M22 controlled by dual input NAND Schmitt-triggers IC20 and IC21.
The control unit designated as CU-2 in FIG. 1 is much different
from the standard control methods. This control circuit will be
described as follows:
a) Floating control: The control unit is connected
directly to the MOSFET-driver MD-2 (M21 and M22) and therefore
to the main switch M20.
b) Zero current sensing employing rectifiers: A fast
rectifier D21 connected in series with a Schottky-rectifier D22
are connected in parallel to the main rectifier D20. If the main
switch M20 is OFF, the main rectifier D20 is ON and an approxi-
mately 200mV voltage drop occurs across the Schottky-rectifier
D22. This voltage controls a voltage comparator IC22 connected
to the first inputs of NAND Schmitt-triggers IC20 and IC21, which
forces M20 OFF, implementing the only possibility of switching
on M20 at zero inductor current. FIG. 5B illustrates the diagram
- of inductor current iL(t).
c) Control of inductor current: Assuming the ON-state
of M20 and a discharged initial condition for capacitor C21, its
voltage Vc(t) can be calculated as follows:

V,--V
V ( t) = o t

where t is the time with respect to an ON time interval, R =
R20 + R21 (the effect of R22 and R23 are neglected), C = C21 and
Vi and VO are the input and output voltages. Since the inductor
current iL ( t) is also proportional to Vi-VO we obtain:

2167189
, j




iL(t) = RLCVC(t)

where L is the inductance of inductor L20. Using a voltage
compArator IC23 connected to the second inputs of dual input NAND
Schmitt-triggers IC20 and IC21, the peak inductor current can be
derived as follows:
IP= RL vr ( 1 )

where Ip is the peak inductor current and Vr=l2-Vf is a given
reference voltage as it is shown in FIG. 5A. Therefore the peak
inductor current as well as the average inductor current Ia=Ip/2
can be directly controlled by a reference voltage Vr. To achieve
the discharging of the capacitor C21, a low power P channel
MOSFET M23 is connected to the output of the voltage comparator
IC22, with c^apacitor C21 connected in parallel with the source
and drain of this MOSFET.
d) Control of output power: Assuming that the reference
voltage is proportional to the inverse value of output voltage
VO:

V~=12-V~= V ~ VO(min)SV~V(m~) (2)

O
.
and substituting (2) into (1) we obtain:
p IpVo RC
2 2L

where PA is the average output power.
Therefore, the control of a fixed output power is
solved in a certain range of output voltage, assuming an
electronic realization of equation ( 2) which will now be
described.

21 671 89




e) Electronic realization of the functional relation-
ship Vl=/VO: The output voltage VO is boosted to the floating
control level by employing a rectifier D23 and a smoothing
capacitor C22. This is essentially the flyback method especially
for a buck converter configuration without applying a secondary
winding on inductor L20. Applying voltage divider resistors R24
and R25 and Zener diodes Z20 and Z21 connected in series with
resistors R26 and R27 respectively, a sufficient (~1%) approxi-
mation of function Vr=/VO (in a certain range of output voltage)
can be achieved, as it is illustrated in FIG. 5C. If VO<Vo(~n),
Vr and therefore Ip (Ia) is limited to an appropriate value by a
zener diode z22 as it is also shown in FIG. 5A.
To achieve discharging capacitor C21, a low power P
channel MOSFET M23 is connected to the output of the voltage
comparator IC22, with capacitor C21 connected in parallel with
the source and drain of this MOSFET.
For HPS lamps assuming 100V nominal lamp voltage,
Vo(~)z80V, Vo(~z160V and I~ z3amperes. The output voltage
can be limited by applying a Zener diode Z23(Vz=160~ connected
in series with a current limiting resistor R28 and an optocoupler
OC20 (connected also to IC22) providing OFF-state for the main
switch M20. The output power can be changed by changing the
value of resistor R21. For instance if R=R20=R21, the output
power can be 250W and if R=R20 (R21 = 0), the output power is
'- 25 200W. Furthermore, a continuous ~lmmlng of the output power
- (lamp power) can be achieved by a continuous decrease of the
value of resistor R21, which can be advantageous from an energy
saving consideration.
UNIT-3, which is connected to the output capacitor of
UNIT-2 is shown in FIG. 6A. The power unit designated as PU-3
in FIG. 1 is based on a full-bridge configuration including
MOSFETs M31, M32, M33 and M34. The MOSFET drivers designated as
MD-3 in FIG. 1 are implemented by four complementary MOSFETs
CM31, CM32, CM33 and CM34. Furthermore, complementary MOSFETs
CM33 and CM34 are driven by optoisolators OC33 and OC34,
respectively, providing isolation from the control level. The

2167189
`

logic driver designated as LD-3 in FIG. 1 provides four logic
signals Q " Q2, Q3 and Q4 controlling the MOSFET driver MD-3.
The logic driver signal waveforms for Q " 72~ 73 and 74 are
shown in FIG. 6B. The logic driver signals contain appropriate
deadtimes avoiding cross conductions of the main switches. The
symmetrical input logic signal Q is shifted with ~tz5~s by a
dual comparator IC32/2 and IC32/1, and an RC circuit (R31, C31)
resulting in signals Qg and 75. The non-inverting input of
IC32/l and the inverting input of IC32/2 are connected to the
common point of the RC circuit containing R31 and C31. The
inverting input of IC32/1 and the non-inverting input of IC32/2
are connected to the common point of a voltage divider pair
including resistors R32 and R33. Using dual input NAND gates
IC31/l, IC31/2, IC31/3 and IC31/4, the four logic driver signals
15 can be derived from the upper MOSFET driver as:
73 = Q Ps~ Q4 =

and for the lower MOSFET drivers as:
Q1 = QgX, Q2 = QgX

where X is an inhibition signal (if X=O, the lower MOSFETs M31
and M32 are switched off).
The logic control unit designated as CU-3 in FIG. 1
20 implements a time programmed starting and restarting process
including the control of ignitor unit (UNIT-4), a low frequency
symmetrical logic signal (Q) to control the logic driver in the
normal operating (X=1), and an automatic switching off feature
under no load or lamp failure conditions or in the case of an old
25 lamp.
The control unit CU-3 including the following function-

al circuits:
a first voltage comparator (IC33/1) with a comparator
level V1, where V, is somewhat smaller than VO(~;

2167189
.

1 1
a second voltage comparator (IC33/2) with a comparator
level V2, where V2 is somewhat smaller than V1;
a first timer (IC34) having a timing period of tlzlOs;
a second timer including a digital counter IC35 and a
digital oscillator IC36 having a timing period of t2z120s;
a low frequency digital oscillator IC37 where thefrequency fiz25Hz and the duty cycle is arbitrary;
a high frequency digital oscillator IC38 having a
frequency f2z20kHz and the duty cycle being smaller than 0.5;
a T flip-flop implemented by a D flip-flop IC39 having
a clock input and a SET input providing the symmetrical signal
Q; and
two AND gates IC40/1 and IC40/2, as well as two
inverters whose functions are obvious from FIG. 6A.
FIG. 6C shows the timing diagram under no load
condition including the case of an unsuccessful ignition. FIG.
6D shows the timing diagram in the case of a successful ignition
(normal operation). The ignited lamp operating quickly in a
complicated plasma physical process (including the glow dis-
charge) achieves the state of arc discharge, assuming that a
sufficient high voltage and high current are provided. After
achieving arc discharge, an important task of the circuit of the
present invention is to stabilize the lamp in the arc discharge
state. Since the discharge tube is cold, any slow zero current
_ 25 crossing can cause an extinction of arc discharge.
Therefore, there are two different short term starting
methods for avoiding extinction as applying a high frequency
current pulse operation, or a DC operation.
The time period of short term starting operation is
implemented by the first timer (tlzlOs). After the short term
starting period, the discharge becomes a normal low frequency
(z50Hz) symmetrical square wave operation. The different
starting operations can be selected by a switch S as it is shown
in FIG. 6A, which switches between the high frequency (HF) or
direct current (DC) mode. In the case of DC starting operation,
the control circuit can be obviously simplified. For HPS lamps,

2 1 67 1 8~
12
the simpler DC starting method can be satisfactory. The square
wave full-bridge PU-3 can be completed with one of the standard
current limiting methods connected together with the control unit
which is not shown in FIG. 6A.
UNIT-4, which is connected to the output of UNIT-3 is
also shown in FIG. 6A. Additionally, resistor R42 is connected
to the output capacitor C10 of the preregulator unit. UNIT-4
implements an ignitor for HID lamps providing high voltage
(z3500~ ignition signals. The circuit is based on a pulse
transformer configuration including a pulse transformer L41, a
thyristor Th41, a capacitor C41 and an RC circuit (R41 and C42)
connected to the gate of thyristor Th41. The capacitor C41 is
charged by a resistor R42 connected to the output capacitor of
UNIT-1. The capacitor C41 is discharged periodically by
thyristor Th41 which is controlled by the digital counter of unit
CU-3 with a repetition frequency of 2Hz. The voltage of the
fully charged capacitor C41 (~450~ is increased by a transform-
er including windings N~ and N2 where Nl/N2=8. In normal
operation the thyristor Th41 is switched off and the pulse
transformer implemented by a gapped core lnductor acting as a
filter element. Furthermore, inductor L41 provides a continuous
current flow through the lamp when the unit PU-3 changes the
polarity of lamp voltage containing deadtimes.
UNIT-5, which is connected to the sinusoidal AC power
supply (more precisely to the common mode filter of UNIT-1) is
- shown in FIG. 7. UNIT-5, acting as a stabilized voltage source,
includes a low power half-bridge square wave inverter designated
as HB and five linear regulators designated as LR-1, LR-2, LR-3,
LR-4 and LR-5. The low power self-oscillating half-bridge
inverter (square wave oscillator) includes a rectifier bridge
B51, an energy storage (film) capacitor C51, connected to the DC
output of B51, two transistors T51 and T52 acting as controlled
switches, two voltage divider capacitors C52 and C53 and a
transformer L51 acting as a high frequency half-bridge square
wave oscillator.
The transformer has a primary winding N~, two feedback
windings Nf~ and Nf2, and five secondary windings Ns1, Ns2' Ns3~ Ns4

2167189

13
and Nss providing appropriate (non-stabilized) voltage sources
for the five linear regulators. The feedback windings, connected
in series with RC circuits (R51, C54 and R52, C55), are connected
to the bases of transistors T51 and T52, providing decreasing
base (diode) currents and therefore alternating switched ON or
OFF states for the transistors. The self-oscillating feature is
realized by the polarity change in the windings caused by the
switched off magnetizing current of transformer L51. Further-
more, the circuit includes a self-switching off starter circuit
implemented by a continuously charged capacitor C65, a DIAC S51
and a transistor T53 controlled by winding Nf1. The rectified
output voltages are essentially DC voltages from a high frequency
viewpoint. Therefore, only small value film capacitors can be
used as smoothing elements. Stabilized output voltages (1 2V) can
be obtained by the use of any standard linear regulation methods.
UNIT-6 operates as a monitor unit including four
Schmitt-triggers is also shown in FIG. 7. The Schmitt-triggers
ST-1, ST-2, ST-3 and ST-4 (see FIG. 1) are implemented by four
voltage comparators designated as IC61, IC62, IC63 and IC64. The
first Schmitt-trigger (IC61) is controlled by a photoresistor
(PH) implementing a light controlled switch. The second Schmitt-
trigger ( IC62) is controlled by a thermistor (TH) implementing
a temperature controlled switch. The third and fourth Schmitt-
trigger (IC63 and IC64) are controlled by a voltage Vx which is
proportional to the input voltage implementing a window compara-
- tor. Transistor T61 is controlled by the common outputs of
comparators (AND connection) resulting the monitor unit. The
output (M) of transistor T61 controls UNIT-1 and UNIT-2 imple-
menting ON or OFF states for them as M=0 or M=1 (-12~ .
Thus, while preferred embodiments of the present
invention have been shown and described in detail, it is to be
understood that such adaptations and modifications as occur to
those skilled in the art may be employed without departing from
the spirit and scope of the invention, as set forth in the
claims.

Representative Drawing
A single figure which represents the drawing illustrating the invention.
Administrative Status

For a clearer understanding of the status of the application/patent presented on this page, the site Disclaimer , as well as the definitions for Patent , Administrative Status , Maintenance Fee  and Payment History  should be consulted.

Administrative Status

Title Date
Forecasted Issue Date Unavailable
(86) PCT Filing Date 1994-08-26
(85) National Entry 1996-01-12
(87) PCT Publication Date 1996-02-27
Dead Application 1999-08-26

Abandonment History

Abandonment Date Reason Reinstatement Date
1998-08-26 FAILURE TO PAY APPLICATION MAINTENANCE FEE

Payment History

Fee Type Anniversary Year Due Date Amount Paid Paid Date
Application Fee $0.00 1994-08-26
Maintenance Fee - Application - New Act 2 1996-08-26 $50.00 1996-08-26
Registration of a document - section 124 $0.00 1996-11-07
Maintenance Fee - Application - New Act 3 1997-08-26 $50.00 1997-08-19
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
LED CORPORATION N.V.
Past Owners on Record
MELIS, JANOS
VILA-MASOT, OSCAR
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
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Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
International Preliminary Examination Report 1996-01-12 25 1,146
Office Letter 1996-03-07 1 19
Office Letter 1996-10-22 1 11
Office Letter 1996-08-02 1 36
Cover Page 1996-05-14 1 16
Drawings 1996-02-27 11 179
Claims 1996-02-27 7 409
Abstract 1996-02-27 1 21
Description 1996-02-27 13 637
Representative Drawing 1999-06-02 1 19
Fees 1997-08-19 1 44
Fees 1996-08-26 1 42