The aspects of the present disclosure relate generally to gas discharge lamps and in particular to improved electronic ballasts for powering gas discharge lamps.
Gas discharge lamps belonging to a family of lighting devices, such as fluorescent lamps used in residential and industrial lighting and high intensity discharge lamps used in stadium lighting and automobile headlamps, have specialized power requirements. When starting or igniting a gas discharge lamp, a high voltage is used to ionize gases contained in the lamp tube and initiate an arc within the lamp. Once an arc has been established and the lamp has warmed to its desired operating temperature, the lamp enters a normal operating phase where it exhibits a negative resistance characteristic. Negative resistance is a condition where lamp current varies inversely with applied voltage and can create an unstable condition leading to excessive lamp current which may deteriorate or destroy the lamp. Thus, it is necessary to carefully control the lamp current to avoid damaging the lamp. When a lamp fails it is necessary to shut off power to the lamp to prevent overheating and possible fracturing of the lamp tube which could release the harmful chemicals contained in the lamp. It is also desirable to shut down the lamp current when a lamp is removed to avoid a shock hazard for maintenance workers who replace failed lamps.
A ballast is an electrical apparatus used to provide power to a load, such as a gas discharge lamp, and to regulate its current. When driving gas discharge lamps, the ballast is configured to provide a high voltage to ignite the lamp, regulate the current at safe operating levels during normal operation, and to shut down lamp power when a lamp fails or is removed. If the ignition voltage is applied for too long, the lamp may be overstressed or otherwise damaged. Under certain conditions, application of the ignition voltage may fail to ignite the lamp within a safe period of time. When this occurs, the ignition voltage must be removed to allow the lamp to cool before another ignition attempt is made. The process of applying an ignition voltage, checking for ignition, then waiting for a cooling period is referred to as an ignition cycle. The ballast is typically configured to apply several ignition cycles to the lamp in order to achieve reliable lamp starting under a wide range of environmental conditions and to enter a failure mode where lamp power is shut down if the lamp fails to start after predefined number of ignition cycles has been attempted.
Typical modern lamp ballasts include multiple power conversion stages. While various combinations of stages may be used, a common set of stages includes an AC to DC conversion stage, a power factor correction (PFC) stage, a power regulator stage, and a DC to AC inverter stage. Alternating current (AC) grid power is rectified and filtered to create rectified direct current (DC) power by the AC to DC conversion stage. The rectified power is passed through the PFC stage to keep the current drawn from the power grid in phase with the voltage of the power grid thereby maintaining a near unity power factor for efficient power usage. The PFC stage may be followed by a power regulator, typically configured as a buck regulator, which receives power factor corrected DC power from the PFC stage and produces a regulated DC power to control a power delivered to the lamp. A DC to AC inverter converts the regulated DC power into an AC power to drive the load.
Each stage in the ballast typically uses an operating voltage, such as a common collector voltage, Vcc, to operate control and logic circuits internal to each stage. These operating voltages are often provided from a secondary winding magnetically coupled to an energy storage inductor in the PFC stage. When a lamp fails or is removed from the ballast and between ignition cycles, lamp power is shut down resulting in a low-load or no-load condition in the ballast. During these low-load or no-load conditions there is insufficient current flowing through the PFC stage to provide sufficient Vcc power to operate control circuitry in each of the stages. To provide control voltage during periods of low-load or no-load, a linear power supply is typically included to maintain the control voltage. Linear supplies of this type dissipate significant amounts of power resulting in reduced ballast efficiency and the need for expensive and relatively large power components. Thus, there is a need for methods and apparatus to reduce power dissipations in lamp ballasts.
A typical AC to DC inverter stage as included in multi-stage ballasts, uses controllably conductive switching devices to chop a regulated DC power to produce an AC output power for the lamp. The inverter stage operates the switching device to alternately apply a forward current to the output power then apply a reverse current to the output power. The periods where current is changing direction, i.e. transitioning from forward current to reverse current and from reverse current to forward current, are referred to as transition periods, and when the inverter is reversing the direction of the current it is said to be in transition. Further, when an inverter begins reversing the current it is said to be entering transition. During these transition periods the power drawn by the load is significantly less than during normal operation and may be only about a third of the normal power. This reduced current requirement results in current spikes being transmitted to the lamp while the inverter is in transition for a ballast configured to have constant power output. When the ballast is driving an electrical discharge lamp, these current spikes can stress the lamp leading to reduced lamp performance and life.
Current crest factor (CCF) is a common measure of quality used to evaluate gas discharge lamp ballasts. The crest factor of a waveform is defined as the peak value divided by the root mean square (RMS) value. An ideal square wave has a crest value of one since its peak and RMS values are the same. Spikes of current, such as the spikes occurring during inverter transition, have large amplitude but contain little RMS power resulting in a high CCF value. A lamp ballast with a CCF close to unity will provide much better lamp life than a ballast with a large CCF, such as a CCF greater than about 2.
Accordingly, it would be desirable to provide ballast circuits that solve at least some of the problems identified above.
As described herein, the exemplary embodiments overcome one or more of the above or other disadvantages known in the art.
One aspect of the present disclosure relates to a multi-stage ballast for powering a gas discharge lamp. In one embodiment, the multi-stage ballast includes a power factor correction stage configured to receive an AC input power and produce a phase corrected DC power, a buck regulator stage coupled to the phase corrected DC power and configured to produce a regulated DC power. The buck regulator stage includes a buck switch. The ballast also includes a DC to AC inverter stage coupled to the regulated DC power and configured to produce an AC lamp power, and a microcontroller coupled to the inverter stage and to the buck switch. The microcontroller is configured to determine when the inverter enters transition and to shut off the buck switch for a predetermined period of time after the inverter enters transition.
Another aspect of the present disclosure relates to an electroluminescent device. In one embodiment, the electroluminescent device includes an AC to DC rectifier device configured to receive an AC input power and produce a rectified DC power, a power factor correction stage coupled to the rectified DC power and configured to produce a phase corrected DC power, and a buck regulator stage coupled to the phase corrected DC power and configured to produce a regulated DC power. The buck regulator stage includes a buck switch. The electroluminescent device also includes a DC to AC inverter stage coupled to the regulated DC power and configured to produce an AC lamp power, a microcontroller coupled to the inverter stage and to the buck switch, an internal power supply coupled to the rectified DC power and configured to produce a first operating voltage, and a gas discharge lamp coupled to the AC lamp power. The power factor correction stage, the buck regulator stage, and the inverter stage each include control circuitry coupled to the first operating voltage, and the microcontroller is configured to determine when the ballast is in a standby mode and to turn off the first operating voltage while the ballast is in standby mode.
These and other aspects and advantages of the exemplary embodiments will become apparent from the following detailed description considered in conjunction with the accompanying drawings. It is to be understood, however, that the drawings are designed solely for purposes of illustration and not as a definition of the limits of the invention, for which reference should be made to the appended claims. Additional aspects and advantages of the invention will be set forth in the description that follows, and in part will be obvious from the description, or may be learned by practice of the invention. Moreover, the aspects and advantages of the invention may be realized and obtained by means of the instrumentalities and combinations particularly pointed out in the appended claims.
In the drawings:
Reference will now be made in detail to the various embodiments, one or more examples of which are illustrated in the drawings. Each example is provided by way of explanation and is not meant as a limitation. For example, features illustrated or described as part of one embodiment can be used on or in conjunction with other embodiments to yield yet further embodiments. It is intended that the present disclosure includes such modifications and variations.
Referring now to
Multi-stage ballast 100 includes an operating voltage power supply 112 used to supply voltages to operate control circuitry within the ballast. Two sources are used to provide input power for the operating voltage power supply 112. During normal ballast operation a coupled power 118 is received from a secondary winding magnetically coupled to an energy storage inductor of the switched mode power converter 128. As will be discussed further below, during certain operating conditions, the coupled power 118 is insufficient, thus an alternate source of power or second power source 116 is provided to the operating voltage power supply 112 by coupling it directly to the rectifier stage 102. The operating voltage power supply 112 is used to provide a common collector voltage (VCC) known as an operating voltage 120 to low level control circuitry, 130, 134, 138 in each of the power stages 104, 106, 108, and also provides a low level voltage (VDD) 124 to operate the microcontroller 114. During periods when the ballast 100 is in a low-power or no-power condition, such as when the lamp 110 is drawing little or no power there is insufficient current flowing through the PFC stage to provide sufficient coupled power 118 to satisfy requirements of the operating voltage power supply 112. Low-load or no-load conditions occur during periods where the load lamp 110 is shut down such as during cool down periods between each ignition cycle or when a lamp has failed or has been removed. During these periods, the alternate source of input power 116 is drawn directly from the rectified input power 103.
The microcontroller 114 is coupled to the DC-AC inverter stage 108. Control signals 126 allow the microcontroller to determine various conditions within the DC-AC inverter stage 108 that may affect the PFC controller 104 and the power regulator stage 106. These conditions include low-load or no-load conditions that prevent the PFC controller 104 from supplying sufficient primary coupled power 118 to the operating voltage power supply 112, and transitions of the DC-AC inverter stage 108 which may induce harmful voltage spikes in the regulated DC power 107 produced by the power regulator stage 106.
The microcontroller unit 114 provides high level control and coordination functions to keep the PFC controller stage 104, power regulator stage 106, and DC-AC inverter stage 108, operating efficiently and to provide functionality such as for example lamp restarting and cool-down. The microcontroller 114 can comprise a small general purpose computer typically constructed on a single integrated circuit or small circuit board containing a processor, memory, and programmable input/output peripherals. In some embodiments the microcontroller unit 114 includes an analog-to-digital converter, digital-to-analog converter, and/or on board counters capable of providing control to the multi-stage ballast 100. The microcontroller unit 114 includes a processor capable of executing computer instructions as well as manipulating and moving data, and a memory capable of storing computer instructions and data.
During operation, the multi-stage ballast 100 needs to support several lamp operating modes. When the load or lamp 110 is lit the ballast 100 is in steady state and the ballast 100 operates under a normal load, i.e. the ballast 100 is providing a normal amount of current to the lamp 110. During ignition, the ballast 100 applies a high ignition voltage to the lamp 110 and is subjected to a light load. During cool-down periods, which are the periods between bursts of ignition voltage applied at startup, during lamp failure, or while a lamp is removed, the ballast 100 is in shutdown mode and is subjected to low-load or no-load in which no lamp current or very little lamp current is flowing.
A linear power supply, such as the linear supply 202, dissipates an amount of power proportional to the amount of current being supplied. A coupled supply such as the coupled supply 204 receives regulated power from a switching regulator such as the boost regulator in the PFC stage 104 and thus dissipates significantly less power. It is therefore desirable to use the coupled supply 204 as much as possible and only draw power from the linear supply 202 when the coupled supply 204 is not able to provide the required operating voltage 206. The coupled supply 204 uses magnetic coupling to draw power from an energy storage inductor in the PFC stage 104, which is typically a boost type switching regulator, and therefore can only supply power while current is flowing through the PFC stage's inductor. The design of the coupled supply 204 can support the power dissipation of VCC 120 and VDD 124 during light and normal loads. However, when the ballast 100 is in a low-load or no-load condition there is insufficient power produced by the coupled supply 204 and the power 206 must be supplied by the linear power supply 202. The operating voltage regulator 214 is configured to draw power from the coupled supply 204 whenever possible and to draw power from the linear supply 202 only when the coupled supply 204 is not providing sufficient power.
Typical ballast designs create the linear supply using power resistors which are reliable but waste significant amounts of power. Alternatively, switching supplies have been used to reduce the amount of wasted power but increase the cost of the ballast and adversely impact reliability. An alternative approach disclosed herein, is to include an operating voltage control switch 216 to control the operating voltage power regulator 214. Operating voltage control switch 216 is coupled to the microcontroller 114 allowing the microcontroller 114 to disconnect the operating voltage power regulator 214 from the linear power supply 202 during periods where it is not necessary to operate control circuitry in the power stages 104, 106, 108. For example, when the ballast 100 enters into a low-load or no-load condition, the switch 216 may be turned off. Since no lamp current is required during these periods, analog circuits and other control circuitry of the PFC controller stage 104, power regulator stage 106, and DC-AC inverter stage 108, does not need to operate so the ballast 100 may be put into a standby mode where the amount of operating voltage power dissipation is significantly reduced. Standby mode is where the ballast 100 is providing little or no current to the lamp 110 such as during cool-down periods, or when a lamp fails or is removed. In typical lamp ballasts, the control circuitry continues to receive power and continues to operate even though it is not providing any power to the load. By removing power from the control circuitry, a multi-stage ballast 100 that includes an operating voltage control switch 216 and a microcontroller 114 programmed to operate the switch 216, can significantly reduce power dissipated during standby mode.
For example, a typical multi-stage ballast 100 uses operating voltage 120 to provide a common collector voltage of about 15 volts at about 8 milliamps. VDD 124 requires a much lower power level of about 5 volts at less than 1 milliamp. Under these conditions a ballast using power resistors in the linear supply 202 will typically dissipate about 3.2 watts. This level of dissipation requires a pair of 2 watt power resistors or equivalent power transistor in the linear supply. Using the new solution where the operating voltage regulator 214 is switched off in standby mode, the power dissipation may be reduced to less than approximately 0.4 watts. In addition to improved energy efficiency, the reduced power dissipation of less than one half watt, allows the power resistors used in a traditional solution to be replaced with less costly surface mount resistors.
A microcontroller, such as the microcontroller 114 described above with reference to the multi-stage ballast 100, may be connected to VCC_CTR to operate the switching circuit 300. In a ballast such as the exemplary ballast 100, the microcontroller 114 can determine when the ballast is in a no-load condition. By including a low level supply architecture such as architecture 200 with an operating voltage control switch 216, the microcontroller 114 can be programmed to take advantage of knowledge of the ballast's operating mode and place the ballast in standby mode by opening the operating voltage control switch 216 to reduce the amount of power dissipated by the ballast.
The DC-AC inverter stage 108 is configured to receive the regulated DC power 107 and provide an AC inverter voltage, Vinv, to the load 410. The load 410 includes a lamp and may also include a resonant tank circuit and/or other current controlling components that help form a required lamp power from the inverter voltage, Vinv. The inverter includes an H-bridge power circuit 422 which is formed from four controllably conductive switching devices 412, 414, 416, 418, such as metal oxide semiconductor field effect transistors (MOSFETs), and receives its operating voltage 120 from a suitable power source and provides a set of external control signals 126 which allow the DC-AC inverter stage 108 to be controlled by an external device such as a microcontroller 114. In operation, the four switching devices 412, 414, 416, 418, are alternately turned on and off in pairs by control circuitry 420 to create a square wave inverter voltage Vinv to drive the load 410. First switching devices 412 and 418 are turned on, while switching devices 414 and 416 are turned off, to apply a forward polarity or positive inverter voltage Vinv to the load 410, then switching devices 414 and 416 are turned on, while switching devices 412 and 418 are turned off, to apply a reverse polarity inverter voltage Vinv to the load 410. When changing the polarity of the inverter voltage Vinv, all four switching devices 412, 414, 416, and 418, generally should be turned off for a brief amount of time to prevent potentially harmful shoot through currents, before turning on the alternate pair of switches. Once the alternate pair of switches is activated it takes a finite amount of time for the switching devices to begin conducting. The period of time during which the inverter voltage is changing polarity is referred to as the inverter transition period or just inverter transition.
During the inverter transition period the lamp 110 requires only about one third of the power required during normal operation. It is desirable in gas discharge lamps to operate the ballasts in a constant power mode, however due to the reduced lamp power requirements, this control scheme may lead to current spikes during inverter transitions.
In accordance with the novel embodiments disclosed herein, an additional control input 144 is included and is configured to stop pulse width modulation and turn the buck switch 404 off when the control signal 144 is activated. The exemplary ballast 100 described above includes a microcontroller 114 configured to operate the DC-AC inverter stage 108 through control signals 126. Thus, microcontroller 114 is able to determine when the DC-AC inverter stage 108 is in transition by examining the control signals 126 and activate the buck control signal 144. The microcontroller 114 is programmed to perform a CCF control method where the buck control signal 144, is activated for a predetermined period of time whenever the microcontroller determines that the inverter stage 108 enters transition. By activating the buck control signal 144, the buck switch 404 is turned off during the transition period thereby significantly reducing the current spikes and reducing the CCF of the ballast.
Thus, while there have been shown, described and pointed out, fundamental novel features of the invention as applied to the exemplary embodiments thereof, it will be understood that various omissions and substitutions and changes in the form and details of devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit and scope of the invention. Moreover, it is expressly intended that all combinations of those elements, which perform substantially the same function in substantially the same way to achieve the same results, are within the scope of the invention. Moreover, it should be recognized that structures and/or elements shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.
Number | Date | Country | Kind |
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201210267884.8 | Jul 2012 | CN | national |
Filing Document | Filing Date | Country | Kind |
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PCT/US2013/044917 | 6/10/2013 | WO | 00 |