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IRF7484QPBF Datasheet, PDF (8/10 Pages) International Rectifier – AUTOMOTIVE MOSFET
IRF7484QPbF
100
Duty Cycle = Single Pulse
10
0.01
1
0.05
0.10
0.1
Allowed avalanche Current vs
avalanche pulsewidth, tav
assuming ∆ Tj = 25°C due to
avalanche losses
0.01
1.0E-06
1.0E-05
1.0E-04
1.0E-03
1.0E-02
1.0E-01
tav (sec)
1.0E+00
1.0E+01
Fig 19. Typical Avalanche Current Vs.Pulsewidth
1.0E+02
1.0E+03
Notes on Repetitive Avalanche Curves , Figures 15, 16:
250
225
TOP
Single Pulse
BOTTOM 10% Duty Cycle
(For further info, see AN-1005 at www.irf.com)
1. Avalanche failures assumption:
Purely a thermal phenomenon and failure occurs at a
200
ID = 14A
temperature far in excess of Tjmax. This is validated for
every part type.
175
2. Safe operation in Avalanche is allowed as long asTjmax is
150
not exceeded.
3. Equation below based on circuit and waveforms shown in
125
Figures 12a, 12b.
100
4. PD (ave) = Average power dissipation per single
avalanche pulse.
75
5. BV = Rated breakdown voltage (1.3 factor accounts for
voltage increase during avalanche).
50
25
0
25
50
75
100
125
Starting TJ , Junction Temperature (°C)
6. Iav = Allowable avalanche current.
7. ∆T = Allowable rise in junction temperature, not to exceed
Tjmax (assumed as 25°C in Figure 15, 16).
tav = Average time in avalanche.
150 D = Duty cycle in avalanche = tav ·f
ZthJC(D, tav) = Transient thermal resistance, see figure 11)
Fig 20. Maximum Avalanche Energy
Vs. Temperature
PD (ave) = 1/2 ( 1.3·BV·Iav) = DT/ ZthJC
Iav = 2DT/ [1.3·BV·Zth]
EAS (AR) = PD (ave)·tav
8
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