A Novel ZVS Full-Bridge Converter with Auxiliary Circuit Zhong Chen, Biao Ji, Feng Ji, and Lei Shi Aero-Power Sci-tech Center Nanjing University of Aeronautics & Astronautics Nanjing, 210016, China Email: chenz@nuaa.edu.cn Abstract—A novel full-bridge (FB) pulse-width-modulated (PWM) converter features zero-voltage-switching (ZVS) of all primary switches in the entire line and load range is described. In contrast to conventional full bridge converter, ZVS is achieved by utilizing energy stored in inductive components of the auxiliary circuit. The auxiliary inductors do not appear as series inductances in the power transfer path, so they do not cause severe voltage ringing across the output rectifier or duty cycle loss. The operation principle of the circuit is analyzed and design considerations of the converter are discussed. Finally, the experimental results from a 1-kW (54-V/20-A) prototype are presented to confirm the operation, validity, and features of the proposed converter. I. INTRODUCTION The full-bridge (FB) zero-voltage-switching (ZVS) pulsewidth-modulated (FB ZVS-PWM) converter, [1]-[11], is applied in medium to high power conversion due to high power density, ZVS operation, high efficiency, low electromagnetic interference (EMI) and moderate device stresses. In a conventional phase shifted full bridge (PSFB) converter, ZVS is achieved by inserting an inductor in series with the transformer [1]-[4]. However, full ZVS operation can only be achieved with a limited load and input-voltage range. The loss of ZVS will result in increased switching loss and electromagnetic interference. Intentionally by increasing the leakage inductance or by adding a large external inductance in series with the primary transformer can help extend the ZVS range of the lagging leg switches. But the larger series inductance has a detrimental effect on the performance of the converter since it results in increased loss of duty cycle, as well as severe voltage ringing across secondary-side rectifier diodes due to the resonance between the inductance and the junction capacitance of the rectifier. To suppress the ringing, a snubber circuit is required. If a conventional RC or RCD snubber is used, the conversion efficiency of the circuit may be significantly degraded [5]. And the large external inductance will cause large circulating current at full load which adversely affects the conversion 978-1-4244-4783-1/10/$25.00 ©2010 IEEE efficiency. As a nondissipative method, the secondary-side voltage oscillation in the FB ZVS converter is virtually eliminated by employing an active switch in the secondary side, but an added active switch increases the system complexity and causes additional switching loss [6]. For implementations with an external primary inductor, the ringing can also be effectively controlled by employing primary-side diodes. While the approaches in [7] offer practical solutions to the secondary-side ringing problem, they do not offer any improvement of the secondary-side duty-cycle loss. Using a saturable external inductor instead of a linear inductor, ZVS range can be increased without significantly losing the duty ratio [8]. However, a large-size core is required to eliminate the thermal problem. And at very light load current, ZVS operation can still be lost [8]-[9]. The energy stored in the magnetizing inductance can also be used to extend the ZVS range. In conventional PSFB converter, this results in significant increase in the rms switch current and the conduction loss [10]-[11]. In this paper, a novel full-bridge converter that achieves ZVS right down to no load without serious conduction loss penalty is proposed. This constant-frequency, FB ZVS converter employs an asymmetrical auxiliary circuit consisting of a few passive components. The proposed converter and its operating principle are described in Section II. Section III presents the optimal design considerations for the proposed converter. The experimental results are presented in Section IV to verify the validity of the proposed converter. II. OPERATION PRINCIPLE Fig. 1 shows the proposed ZVS full-bridge converter topology. The primary side of the converter consists of two bridges Q1-Q3 and Q2-Q4 connected through two capacitors Ca1 and Ca2 to the connection of the power transformer Tr and the auxiliary inductors La1 and La2. The two primary side capacitors are used to prevent the saturation of the power transformer and the auxiliary inductor cores by blocking the flow of any dc current through Tr, La1 and La2. The switching 1448 I1 I2 I3 Fig. 1. Proposed full bridge ZVS converter. transition of the switches in the Q2-Q4 leg of the bridge is delayed, phase-shifted, with respect to the switching transition of corresponding switches in the Q1-Q3 leg. Generally, these two auxiliary capacitors are selected large enough so that their voltages are approximately constant during a switching cycle. Because the average voltages of the auxiliary inductors and the power transformer during a switching cycle are zero and the pair of switches in each bridge leg operate with 50% duty cycle, the magnitude of voltage sources vca1 and vca2 are equal to 1/2Vin, i.e., vca1= vca2=1/2Vin. In addition, the auxiliary inductor stores energy which only be used to achieve ZVS, its size can be small. The output side of the converter is implemented with a full-wave rectifier with a tapped secondary. Also, any other implementation of the secondary side rectification stage is possible. In terms of power transfer from the input to load, the power circuit operates in exactly the same way as does a conventional phase-shifted full-bridge converter, and the auxiliary circuit hardly interferes with its power transfer. However, the auxiliary circuit removes the switching losses from all the switches. The key waveform of the ZVS PWM full-bridge converter is shown in Fig. 2. To perform the steady state analysis, the following assumptions are made. 1) All components and devices have ideal properties and characteristics. 2) C1= C3= Clead, C2= C4= Clag. 3) The output filter capacitor is large enough to be treated as a constant voltage source with a magnitude equal to Vo. 4) The turns ratios of the power transformer is the primary winding: the secondary winding=Np: Ns. (where Np: Ns=K) 5) The switching frequency fs is fixed and the inverse of the switching period Ts. Fig.3. shows the topological stages of the converter during a half period. The second half period is similar to the first half period. 1) Stage 1 [t0, t1] [Refer to Fig. 3(a)] In the last interval of the previous cycle, diagonal switches Q1 and Q4 are conducting, primary voltage is positive so that load current Io flows through DR1 and the upper secondary of transformer Tr. After switch Q1 is turned off at t=t0, current i1 starts charging output capacitance C1 of switch Q1 and discharging output capacitance C3 of switch Q3, where i1 is the sum of the current iLa1 and the primary current ip=Io/K. During this interval, the current of the inductor La1 keeps at ILa1 which can be calculated as (1). The voltage of Q1 rises slowly owing to C1. After the capacitor C3 is fully I La1 I La 2 Fig. 2. Key waveforms of proposed converter power stage. discharged, current i1 continues to flow through the antiparallel diode of switch Q3. The voltage across switch Q3 is given in (2) during this interval. Vin I La1 = (1) 8La1 ⋅ f s I o / K + I La1 (t − t 0 ) (2) 2Clead 2) Stage 2 [t1, t2] [Refer to Fig. 3(b)] Q3 can be turned on at zero voltage when D3 conducts. In this topological stage, the potential of point A becomes zero. Voltage across the power transformer also becomes zero since the transformer is shorted by the simultaneous conduction of the body diode of Q3 and switch Q4. The voltage applied across La2 is -Vin/2. Due to this voltage, the current iLa2 still decreases until t2. At t2, iLa2 reaches its minimum value -ILa2. And ILa2 can be expressed as (3). Vin I La 2 = (3) 8La 2 ⋅ f s And with real components, the primary current will decrease because of the forward voltage of power switch Vforward and parasitical impedance. The primary current can be expressed as V forward ⎤ − Lrk (t −t1 ) V forward ⎡ i p (t ) = ⎢i p (t1 ) + − (4) ⎥e r ⎦ r ⎣ where r is the equivalent series resistor for the circuit, Lk is the leakage inductance of power transformer . This interval is ended when the switch Q4 is turned off. 3) Stage 3 [t2, t3] [Refer to Fig. 3(c)] Q4 is turned off in ZVS at t2. Current i2 starts charging output capacitance C4 of switch Q4 and discharging output 1449 vc3 (t ) = Vin − Io + I La 2 ) cos ωr (t − t2 ) − I La 2 K I vc4 (t ) = ( I La 2 + o ) Z r sinωr (t − t2 ) K where Z r = Lk 2Clag , ωr = 1 2 Lk Clag i p (t ) = ( (5) (6) 4) Stage 4 [t3, t4] [Refer to Fig.3(d)] D2 conducts naturally when vc2 decays to zero, and Q2 can be turned on at zero voltage. At the same time, load current Io commutates from the upper secondary and rectifier DR1 into the lower secondary and corresponding rectifier DR2. The rate of change of the primary current is given by di p V = − in (7) dt Lk Since the leakage inductance of the power transformer is smaller, the duty-cycle loss in the converter is decreased. 5) Stage 5[t4, t5] [Refer to Fig.3(e)] The commutation of the load current from the upper to the lower secondary is completed at t=t4, the primary current commutation from the positive to negative direction is also finished so that the primary is ip=-Io/K. The input energy is transferred into the secondary side by power switches Q2 and Q3 and Tr. This stage ends at t5 when switch Q3 turns off. Then the second half of the switching period begins. In the second half of the switching period, the operation of the circuit is exactly the same as the operation in the first half of the switching period. (a) (b) (c) III. DESIGN CONSIDERATIONS Auxiliary inductors are required in the proposed converter to achieve ZVS. However, the auxiliary inductor current will result in additional conduction losses. This can be achieved by using an asymmetrical auxiliary arrangement. (d) (e) Fig. 3. Topological stages of proposed converter power stage. capacitance C2 of switch Q2. Since the potential of point B increases from zero toward Vin, while the potential of point A is constant at zero. The secondary windings are also shorted so that rectifiers DR1 and DR2 can conduct the load current simultaneously. vAB is fully applied to the Lk. Because the auxiliary inductor La2 is much larger than the leakage inductance Lk, it can be treated as a constant current source during the transition time. This stage finishes when vc4 rises to Vin and vc2 falls to zero at t3. The primary current and the voltage across Q4 are given by (5) and (6). A. ZVS Range for the Leading leg and the selection of La1 In order to achieve ZVS turned on, the output capacitance of the switch shall be completely discharged within the dead time period td(lead) under all operating conditions. Neglecting the capacitances of the transformer’s windings, the value of the current required to achieve ZVS of leading-leg switches Icharge is calculated as I (8) I ch arg e ⋅ td ( lead ) = La1 ⋅ td ( lead ) ≥ Clead ⋅Vin 2 Expressions (1) and (8) can be used to estimate the required value of the auxiliary inductance La1. From (1) and (8), we can get the following equation td ( lead ) La1 ≤ (9) 16 ⋅ Clead ⋅ f s Fig. 4 shows an example of the selection curves of the auxiliary inductor La1 as functions of td(lead) at different output capacitances. It is seen that with a fixed dead time, smaller La1 will achieve ZVS much more easily. When the output capacitance is decided, the dead time can be selected shorter with smaller La1. The dead time for the leading leg should be selected together with auxiliary inductor. 1450 vc 4 (V) La1 (μH) La 2 Clead 300pF 400pF 500pF 600pF 100μH 120μH 150μH 200μH I o (A) Fig. 6. Voltage across the parasitic capacitor of the lagging leg versus load current at different auxiliary inductances. (Vin=400V, Lk=6μH) td (lead ) (ns) Fig. 4. Example design curves for selecting the auxiliary inductors vs. dead time. so the primary current can be expressed as Io/K. Unlike the transition of leading leg, the transition of lagging leg switches can be divided into two cases according to the load current Io as shown in Fig. 5. Under most load current conditions, the transition may only go through stage I, as shown by Fig. 5(a). The primary current decreases as the voltage of C4 increases. When the voltage of C4 reaches Vin, D2 conducts, so Q2 can be turned on with ZVS. When the transition starts at t=t2, the voltage of C4 can be calculated as (6). Since the leakage inductance is much smaller compared with conventional full bridge converter, the resonant time is relatively shorter. So the load current may complete the commutation from the upper secondary to the lower secondary before the voltage of C4 reaches Vin. Then the converter will enter stage II, as shown by Fig. 5(b). The current through La2 will go on discharging C2 and charging C4. Simultaneously this current will compensate the output current Io. (a) stage I (b) stage II Fig. 5. Transition equivalent circuit of lagging leg. When the transition enters stage II, the voltage across Q4 can be expressed as (10). ⎛I ⎞ vc 4 (t ) = ⎜ o + I La 2 ⎟ Z r sin ωr (t2 ' − t2 ) ⎝K ⎠ ⎛ Io ⎞ ' ⎜ − K + I La 2 ⎟ ⋅ (t − t2 ) ⎠ +⎝ 2 ⋅ Clag (10) vc 4 (V) B. ZVS Range for the lagging leg and the selection of La2 Before analyzing the ZVS condition for the lagging leg, we suppose the dead time td(lag)= Tc/4, where Tc = 2π 2 ⋅ Lk ⋅ Clag . The output current ripple is neglected, Lk 7μH 6μH 5μH 4μH I o (A) Fig. 7. Voltage across the parasitic capacitor of the lagging leg versus load current at different leakage inductances.(Vin=400V, La2=100μH) ⎡ ⎛ −Io ⎞⎤ ⎢ ⎜ K + I La 2 ⎟ ⎥ ' where t = t2 + ⎢ arccos ⎜ ⎟ ⎥ ωr . t2 is the moment I o ⎢ ⎜⎜ + I La 2 ⎟⎟ ⎥ ⎝ K ⎠ ⎦⎥ ⎣⎢ when the load current completes commutation. According to (6) and (10), Fig. 6 and Fig. 7 can be plotted. Fig. 6 shows the voltage across Q4 versus load current Io with definite leakage inductance under different auxiliary inductances. Fig. 7 shows the voltage across Q4 in a function of load current Io with determined auxiliary inductance under different leakage inductances. From Fig. 6 and Fig. 7, we can know ZVS can only be achieved when the voltage across Q4 is higher than Vin. As the leakage inductor becomes smaller, the value of auxiliary inductance La2 should be made smaller. Smaller La2 will in turn result in larger ILa2. And this will increase conduction losses in the switches. If the leakage inductance is minimized, the load current will commutate fast, as shown in Fig. 5(b). And the current through auxiliary inductance should be made larger than the reflected load current. It results in increased conduction losses. So the leakage inductance should be optimally selected to simultaneously achieve the entire range ZVS operation and improve overall efficiency over the entire conversion range. ' 2 C. The selection of Ca1 and Ca2 The two capacitors are employed to establish dc voltages and block the flow of any dc current through the magnetic 1451 components. The permitted ripple voltage on these two capacitors is about 1% of the maximum voltage. D. Turns ratio of the transformer Finally, to achieve maximum efficiency improvement, the turns ratio of the transformer must be maximized. In fact, since the duty-cycle loss in the converter is negligible due to the smaller leakage inductance of the transformer, the converter can be designed with a larger turns ratio compared to the conventional PSFB converter. Moreover, the secondary–side ringing between the leakage inductance of the transformer and the junction capacitance of the rectifier is significantly reduced because of the smaller leakage inductance. Any residual parasitic ringing can be damped by a simple RCD-snubber circuit. IV. v DS(Q3 ) :[200V / div] v GS(Q3 ) :[20V / div] Time :[0.5μs / div] (a) the leading leg EXPERIMENTAL RESULTS In order to verify the operation principle of converter, a prototype converter was built in the lab with the following parameters. • Input voltage Vin : 300-400VDC; • Output voltage Vo : 54VDC; • Maximum output current Io : 20A; • Switching frequency fs : 100kHz; • Main switches Q1~Q4 : IRFP460 (International Rectifier), and its RDS(on)=0.3Ω; • Rectifier diodes (full-wave rectifier) : DSEI30-06A (IXYS); • Turns ratio K : 14:3:3; • Auxiliary inductor La1 : 250μH (core: PQ2020); • Auxiliary inductor La2 : 100μH (core: PQ2020); capacitors Ca1&Ca2: 2.2μF/250V • Auxiliary (polypropylene). The phase-shift control circuit was implemented using a UCC3895 controller. Fig. 8 shows the gate signals of PWM switches Q3 and Q2 along with their drain-to-source voltage waveforms at 5% load. As seen, the drain voltage reaches zero before the gate reaches its threshold demonstrating zero-voltage turn-on. Fig. 9 shows the currents flowing through the two auxiliary inductors with different peak value. The changing current can help realize ZVS for both legs from no load to full load. Fig. 10 shows the key waveforms of the proposed FB ZVS converter. As can be seen from the corresponding waveform in Fig. 10, the proposed converter has a very small duty cycle loss as well as a very much decreased parasitic ringing because of the smaller leakage of the power transformer. And we can see from the active state to the passive state the primary current has a downward step caused by the junction capacitance of output rectifier diodes discharging. Fig. 11 shows the measured efficiencies as functions of output current at Vin=400V. Generally, the efficiency improvement is more pronounced at light loads where the conventional FB ZVS converter operates with hard switching. Meanwhile, the ZVS operation is helpful to reduce EMI problem at very light load. By increasing the turns ratio of the transformer, both the conduction loss of the primary switches and the voltage stress on the components at the secondary side is decreased. v DS(Q2 ) :[200V / div] v GS(Q2 ) :[20V / div] Time :[0.5μs / div] (b) the lagging leg Fig. 8. Drive voltage and drain to source voltage of the leading lag and lagging leg at 5% load current. i La1 (1A / div) i La 2 (2A / div) Time :[2.5μs / div] Fig. 9. Current through auxiliary inductors at 5% load current. v AB (400V / div) ip (5A / div) v rect (50V / div) Time :[5μs / div] Fig. 10. Experimental waveforms of vAB and secondary voltage vrect at full load. 1452 REFERENCES [1] Io / A Fig. 11. Measured efficiency of proposed converter as a function of output current. V. 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