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february 2014 docid025611 rev 1 1/20 AN4414 application note anti-tampering ferrite less power supply for 3-phase energy meter harjeet singh introduction this power supply design is dedicated to ener gy meter applications and an other low power auxiliary supply for system s with galvanic isolation for a si ngle phase or 3- phase input mains supply. the smps can cater the super wide input voltage ranging 90 vac to 440 vac single phase or 3-phase / 4-wire configurations with low component counts. for energy meter applications, anti-tampering feature is a must nowadays which is governed by electricity board regulatory agencies. normally the smps are designed with ferrite core s, either a flyback transformer or a buck inductor, which saturates in an environment where strong magnetic fields are available. to avoid the same, some type of magnetic shielding are required, which adds a cost and complexity in manufacturing process of the magnetics. in case of tampering where smps are available in energy meters, commonly a strong magnetic field of about 0.5 tesla strength is applied, which interfaces with the ferr ite core and saturates it. due to saturation, sometimes the failure of power devices may al so take place, or the smps with integrated switches gets into the protection mode and lim iting the output voltage, consequently the meter stops which is a tempered condition. to overcome this situation, in the present case, an example to design the flyback converter without using any ferrites or a high permeability core for a re quired magnetizing inductance and so called an air core magnetic approach is described in this application note. if no ferrites are involved, no saturation phenomeno n can take place under the influence of an external strong magnetic field and this w ill comply the energy meter anti-tampering standard, which requires 0.5 tesla magnetic immunity. the only drawback could be the large number of turns and associated copper losses. since the required power is very low, the copper losses are acceptable up to a certain extent. the specification of overall input power to be within the limits as per energy meter power supply specifications needs to be complied. www.st.com
contents AN4414 2/20 docid025611 rev 1 contents 1 description of smps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 1.1 basic flyback equations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 1.2 anti-tampering requirement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 1.3 calculations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 2 reference . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 3 revision history . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
docid025611 rev 1 3/20 AN4414 description of smps 20 1 description of smps the front-end of the power supply comprise s of a surge suppressor, rectifiers and a mosfet as a series regulator. the 3-phas e, 4-wire bridge rectification scheme is adopted so as to run the system in case of neutral missing. the input side is protected against spikes using suitable varistors. then emi filter is connected across the dc using an undamped lc filter (l1, c8 and c11) for both the common mode and differential mode suppression. the purpose of the voltage clampi ng circuitry is to protect the flyback stage against overvoltages for a better reliability and it comprises of an n-channel 2 ? /600 v mosfet q1 and a self driven control circuit. the ntc limits the inru sh current. the zeners d5 and d6 regulate the dc bus to the input of the buck stage to about 345 - 350 vdc, while resistors r2, r5 and r7 provides enough of gate-source charge. the flyback converter is built using an integrated power device - the viper17, one of the devices from the viper ? plus family. some of the device features are listed below: ? 800 v avalanche rugged power section ? pwm operation with frequ ency jittering for low emi ? operating frequency: ? 60 khz for l type ? 115 khz for h type ? standby power < 50 mw at 265 vac ? limiting current with adjustable set point ? adjustable and accurate overvoltage protection ? onboard soft-start ? safe autorestart afte r a fault condition ? hysteretic thermal shutdown the device is available in dip-7 and so-16 narrow packages as shown in figure 1 . figure 1. dip-7 and so-16 narrow package table 1. typical power capability of viper17 part number 230 v ac 85 - 265 v ac adaptor (1) 1. typical continuous power in non ventilat ed enclosed adapter measured at 50 c ambient. open frame (2) 2. maximum practical continuous power in an open frame design at 50 c ambient, with adequate heat sinking. adaptor (1) open frame (2) viper17 9 w 12 w 5 w 7 w
description of smps AN4414 4/20 docid025611 rev 1 the dc output voltage from the clamp circuit is filtered using a 4.7 f capacitor c10 and supplied to the drain pin of the device. the vcc of the device is supplied through an auxiliary winding of the transf ormer (pins 1 - 2) and filter ed by the capacitor c9. a decoupling capacitor can also be connected to the vcc pin for noise suppression. on the primary side of the transformer rcd clamp is being used using the r3, c3 and d3 to keep the leakage spike as low as possible. the f eedback to the device is provided using the optocoupler u2 and tl431, u3 at the secondar y side of the transformer. the voltage divider network r11 and r12 provides 2.5 v reference to the pin1 of the tl431. the power supply is designed for 5 v at 100 ma. the transformer primary inductance is sized to limit the peak current through the device below the maximum le vel. the output dc is filtered using low esr capacitors c4 and c5. a post lc filter is also used to further scale down the ripple voltage to get ultimate 5 v output required for the microcontroller and other circuitry in the energy meter. some of the features of th e viper17 like ?br? and ?cont? are not used here as the objective is to analyze the viper17 application with the air core transformer. briefly these functions are explained below (refer to the viper17 datasheet for more information on br and cont features): ? br: the input voltage information is provided to the br pin by using the resistor divider network from rectified bus voltage and can dete ct the brownout threshold to turn off the device. the resistor divider network r15, r16, r17 and r18 are programmed to achieve brownout protection. ? cont: with the cont pin, one can impose a limit on the peak drain current (idlim can be programmed using the r14) and another feat ure is to have protection in case output overvoltage (outpu t ovp protection), which can be s ensed using the auxiliary winding which is used for vcc biasing. table 2. specification of smps parameters limits input voltage range 90 - 440 vac, 3-phase, 4-wire input supply frequency 50 hz input / output isolation yes output voltage/current 5 v/100 ma total output power 0.5 w application/load metering, auxiliary power supply output voltage ripple <100 mv (pk-pk) power factor correction no topology/ devices flyback viper17hn, std4nk60z
docid025611 rev 1 5/20 AN4414 description of smps 20 1.1 basic flyback equations generally the flyback design calculations are as below: equation 1 as we know: equation 2 rewriting as below: where: vdcmin = minimum dc input to flyback converter ipkp = peak primary current ton = turn-on time of primary s witch (viper in this case). equation 3 equation 4 where: dmax = maximum duty cycle fsw = operating switching frequency of converter. equation 5 equation 6 as we know, power = energy transferred x frequency. equation 7 where pin = input transformer power. vl di dt ---- - ? = vdcmin lp ipkp ton ----------- - ? = ton dmax ts ? = ton dmax fsw ---------------- = vdcmin lp ipkp fsw ? dmax --------------------------- - ? = ipkp vdcmin dmax ? lp f ? sw -------------------------------------------- = pin 1 2 -- - lp ipkp 2 fsw ? ? ? =
description of smps AN4414 6/20 docid025611 rev 1 the primary inductance is calculated as: equation 8 equation 9 where: ? = efficiency of flyback stage pout = output power required. equation 10 using equation 10 , we can rewrite equation 6 as: equation 11 reflected voltage is defined as: equation 12 rms primary current is: equation 13 turn ratio, n is defined as: equation 14 where: np = number of primary turns ns = number of secondary turns. lp 2pin ? ipkp 2 fsw ? ------------------------------ - = pin pout ? ------------ - = lp 2 pout ? ? ipkp 2 fsw ? ? ---------------------------------------- - = ipkp 2pout ? ? vinmin dmax ? ? ---------------------------------------------------- - = vr dmax 1dmax ? ?? ------------------------------ vdcmin ? = iprms ipkp dmax 3 ---------------- ? = n vr vout vf + --------------------------- np ns ------- - ==
docid025611 rev 1 7/20 AN4414 description of smps 20 1.2 anti-tampering requirement the e-meter smps requires a 0.5 t external magneti c immunity test and generally ferrites saturated with a 0.5 t external magn etic field. in order to comply this norm, a lot of attention is required in making proper shield transformers, which is very expensive and sometimes still difficult to comply the norms easily. the alternative to this is to adapt a ferrite less or air core transformer approach for such low power output requirement. considering the classical equat ions for a dcm (discontinuous conduction mode) flyback converter as described in section 1.1: basic flyback equations will result in a higher magnetizing inductance of primary of transformer. so using no ferrite material (we call this as ?air core?) to build the high frequency transformer would result in higher number of turns to achieve the required magnetizing inductance and with air core, the primary inductance in the range of 1 mh is itself difficult to ac hieve with reasonable number of primary turns. so the first most important crit erion to this approach is to select a low primary inductance value, lp, but the value must be greater than a threshold in order not to cause an excess peak drain current. the high voltage flyback switc her is specified with a finite peak current of mosfet, depending on its r ds_on and thermal dissipation. co nsidering the viper17 family devices, we have this current as: idlim = 0.4 a. so during the wide mains operation, the peak primary current should be well below this value to avoid any protection to activate in a nominal operation. the viper17 has a hiccup mode activation above this current level. as we know, the important parameters for a flyback design are: dmax = max duty cycle, vr = reflected voltage, lp = primary inductance, n = turn ratio, np/ns ipkp = peak primary current fsw = switching frequency equation 15 primary turns where: ae = cross-sectional area of core chosen as we know, selecting higher duty cycle will have below impact: equation 16 np lp ipkp ? bmax ae ? ----------------------------- - =
description of smps AN4414 8/20 docid025611 rev 1 this clearly states that selecting a higher duty cycle at a minimum input voltage will cause the peak primary current to decrease and require s a high magnetizing inductance. to attain the required inductance, we will require a larger number of turns and the transformer would be very bulky if no high permeability ferrite ma terial is used to r equire that inductance. moreover the dcr of windings will increase due to a long wi re length and copper losses will be more, impacting the efficiency and metering standard norms. for 3-phase metering, the power supply consumption shou ld be limited below 8 va. looking into the above challenges, we need to define a very low value of a maximum duty cycle and hence the peak primary (or drain curr ent) at somewhat higher value. on the other hand, this would require lesser turn ratio (n) and there would be a large number of secondary turns in comparison with a traditional flyback transformer. note: maximum primary peak (or a drain current of the device) < idlim (maximum specified value in the viper17 datasheet).
docid025611 rev 1 9/20 AN4414 description of smps 20 as we know from equation 10 : that is: equation 17 or so one can use a higher switching frequency of the operation to maintain a lower inductance and hence a lower number of primary turns. stmicroelectronics ? has the viper17h for 115 khz and the viper17l for 60 khz operation. select viper17h for this application. 1.3 calculations input voltage to conver ter: 80 v to 265 vac maximum withstanding volt age: 440 vac line-line. output voltage: vout = 5 v maximum output current: iout = 100 ma equation 18 pout = vout x iout the typical power stage to withstand this wi de mains operation is to clamp the dc bus voltage to the flyback stage at a lower level. this can be achieved by using a mosfet and a zener clamp circuit as a front-end stage as shown in the schematic in figure 9 on page 17 . this approach is a simple series pass regulator and well acceptable as we are dealing with a very low power output requirements. the dc input to the flyback stage doesn't exceed the voltage at which the zener clamp network starts conducting and any further increase in an input rectified voltage will drop across the series mosfet. since the current in the mosfet is very small, we can select a d 2 pak package in order to dissipate the heat on the copper area provided in the printed circuit board. minimum dc bus voltage at flyback input: equation 19 vdcmin ~ 100 vdc. lp 2 pout ? ? ipkp 2 fsw ? ? ---------------------------------------- - = lp ? 1 fsw --------- lp ? 1 bmax --------------- -
description of smps AN4414 10/20 docid025611 rev 1 maximum dc bus voltage at flyback input: equation 20 vdcmax ~ 360 vdc assuming efficiency, ? = 65 % (flyback stage): equation 21 fsw = 115 khz equation 22 equation 23 let vr = 10 v equation 24 equation 25 this gives dmax = 9.1% ton = dmax = 790 s which is greater than tonmin (= 400 ns), th e device minimum turn-on time as per the datasheet of the viper17hn. equation 26 where the max. drain current limitation threshold of the viper17 is 400 ma, so at minimum dc input voltage, the device will not enter into the hiccup mode. equation 27 ts 1 fsw --------- 8.69 ? s == vr dmax 1dmax ? ?? ------------------------------ vdcmin ? 10v == ipkp 2pout ? ? vinmin dmax ? ? ---------------------------------------------------- - 0.169a == lp 2 pout ? ? ipkp 2 fsw ? ? ---------------------------------------- - 540 ? h ? =
docid025611 rev 1 11/20 AN4414 description of smps 20 case 1 assuming lp = 400 h equation 28 as vr = 10 v, so equation 29 np is two times of ns . using a lesser diameter wire (dcr will obviously be high, but select in order to have it < 10 e in any case to avoid copper losses), a large number of turns can be accommodated in the available bobbin. here we can consider the ee19 bobbin. common practice to fix this type transformer specification is to wound primary turns as a selected awg wire on the bobbin till the required inductance ( lp ) is not achieved. freeze np at desired lp . select secondary turns, ns = np / n and auxiliary turns to maintain a minimum vcc bias voltage to the device. with lp = 400 h and pout = 0.5 w in table 3 are the test results: table 3. test results we can see that keeping the primary inductance as 400 h, the drain current reaches to its internal limit threshold level, which is not desirable as the device activates the hiccup mode of operation at this current level, so we need to increase the primary inductance in reasonable limits to avoid higher drain current. vmains (vac) ipkp (ma) tu rn-on time (ns) comments 80 175 700 - 120 210 ton > tonmin - 180 290 ton ~ tonmin = 400 - 230 350 ton ~ tonmin = 400 - 265 and above ~ 400 ton ~ tonmin = 400 device current reaches to idlim and enters into hiccup mode n vr vout vf + --------------------------- 2 == (ignoring vf)
description of smps AN4414 12/20 docid025611 rev 1 case 2 let's take lp = 680 h and increasing t he reflected voltage slightly: vr = 18 v. equation 30 so recalling the equation: equation 31 in our case v = voltage at flyback input, l = primary magnetizing inductance, lp and dt = turn-on time with 680 h as a primary inductance, let's analyze the flyback stage at different dc input conditions. at vdcmin ~ 100 vdc (which is corresponding to 80 vac), calculating the peak current through the device in a discontinuous conduction mode. equation 32 this gives: equation 33 dmax = 15.2% equation 34 ton = dmax x ts = 1.33 s equation 35 looking into waveforms in figure 2 and figure 3. , we have the same practical results. the waveforms are captured at different input voltage conditions. as long as the turn-on time of the flyback s witch is greater than its minimum turn-on time (internally fixed, 400 ns in the viper17), the device peak current is maintained as per the duty decided by the feedback loop. as input voltage increases and duty reduces in order ?tonmin? is achieved, there is no further decrea se in turn-on time with a further increase in input voltage and the device peak current will in crease as input voltag e increases and it can be calculated using equation 35 at fixed tonmin = 400 ns. si nce the mosfet clamp circuit ensures the maximum dc input to flyback as per the zener biasing and maintains maximum n vr vout vf + --------------------------- 3.2 considering vf 5v = ?? == vl di dt ---- - ? = vr dmax 1dmax ? ?? ------------------------------ vdcmin ? 18v == ipkp vdcmin ton ? lp -------------------------------------- - 196ma ==
docid025611 rev 1 13/20 AN4414 description of smps 20 input as 360 v till 440 vac input mains, henc e the peak curr ent through the device is limited. looking into the waveform in figure 8 , at maximum mains input of 440 vac (vdcmax ~ 360 vdc to flyback input), the peak current through the device is 211 ma. equation 36 we have: figure 2. ch1: fb signal, ch3: drain current , ch4: drain source voltage at 100 vdc ipkp vdcmax tonmin ?? lp ------------------------------------------------- - 360v 400ns ? 680 ? h ------------------------------------- 211ma ===
description of smps AN4414 14/20 docid025611 rev 1 figure 3. ch1: fb signal, ch3: drain current, ch4: drain source voltage at 100 vdc (expanded) figure 4. ch1: fb signal, ch3: drain current , ch4: drain source voltage at 200 vdc
docid025611 rev 1 15/20 AN4414 description of smps 20 figure 5. ch1: fb signal, ch3: drain current, ch4: drain source voltage at 200 vdc (expanded) figure 6. ch1: fb signal, ch3: drain current , ch4: drain source voltage at 300 vdc
description of smps AN4414 16/20 docid025611 rev 1 figure 7. ch1: fb signal, ch3: drain current, ch 4: drain source voltage at 300 vdc (expanded) figure 8. ch1: fb signal, ch3: drain current, ch4: drain source voltage at mains input vac = 440 ac
docid025611 rev 1 17/20 AN4414 description of smps 20 figure 9. schematic of smps 5 . 5 ( ' 677+5 5 10 5 10 ' 677+5 8 9,3(5+1 %5 'udlq *1' 9gg &217 'udlq )% & q)9 & x)9 5 10 1 8 3&% 5 . / p+ % 5 ( & x)9 5 (: ' 9: %5 ')6 & q) 3*1'b3 9 ' 677+5 5 ( & %5 ')6 < 8 7/ 3*1'b6 3*1'b3 / x+p$ 5 . 09 6.(9 & q) & q)9 5 ' 9: 5 . 5 (: $lufruh & q).9 < hdfk 1rwh%5dqg&217 ixqfwlrqvrighylfhduhqrwxvhg 5 (: & x)9 & x)9 9 75 5 . 5 10 & q) 3*1'b6 09 6.(9 5 . ' 9: & q) *1' 4 67'1.= & q) 09 6.(9 & 10 5 . 5 (: & x)9 $0
description of smps AN4414 18/20 docid025611 rev 1 note: proper mylar tapes are inserted between each windings for isolation. table 4. transformer specification parameters values max. output power 0.5 w input voltage range 80-440 vac, 50 hz primary inductance 680 h secondary inductance 133 h primary side leakage inductance < 5% at 1 khz peak primary current 0.4 a max. switching frequency 115 khz fixed bobbin size ee19 core type air core bobbin 8 pins vertical dielectric strength 2.75 kv table 5. winding details winding name start stop no. of turns wire gauge/dcr winding order np 4 3 345 0.2 mm / dcr = 6.5 ? bottom ns 5 8 107 0.2 mm / dcr = 2.2 ? above np naux 1 2 200 0.09 mm / dcr = 22 ? above ns table 6. bill of material part reference quantity part description u1 1 viper17hn u3 1 tl431 q1 1 mosfet std4nk60z d1, d3, d4 3 rectifier stth1r06
docid025611 rev 1 19/20 AN4414 reference 20 2 reference viper17 datasheet. 3 revision history table 7. document revision history date revision changes 21-feb-2014 1 initial release.
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