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AN4414 Datasheet(PDF) 12 Page - STMicroelectronics |
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AN4414 Datasheet(HTML) 12 Page - STMicroelectronics |
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12 / 20 page ![]() Description of SMPS AN4414 12/20 DocID025611 Rev 1 Case 2 Let's take Lp = 680 µH and increasing the 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 µH 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 µs 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 switch 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 decrease in turn-on time with a further increase in input voltage and the device peak current will increase as input voltage increases and it can be calculated using Equation 35 at fixed Tonmin = 400 ns. Since 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 == |
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