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R5972D датащи(PDF) 24 Page - STMicroelectronics

номер детали R5972D
подробное описание детали  Up to 1.5 A step-down switching regulator for aerospace applications
PDF  35 Pages
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производитель  STMICROELECTRONICS [STMicroelectronics]
домашняя страница  http://www.st.com
Logo STMICROELECTRONICS - STMicroelectronics

R5972D датащи(HTML) 24 Page - STMicroelectronics

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R5972D
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DocID026873 Rev 1
So Equation 28 and Equation 29 in overcurrent conditions can be simplified to:
Equation 30
considering TON that has been already reduced to its minimum.
Equation 31
considering that fSW has been already reduced to one third of the nominal.
In case a short-circuit at the output is applied and VIN = 12 V the inductor current is
controlled in most of the applications (see Figure 13). When the application must sustain the
short-circuit condition for an extended period, the external components (mainly the inductor
and diode) must be selected based on this value.
In case the VIN is very high, it could occur that the ripple current during TOFF (Equation 31)
does not compensate the current increase during TON (Equation 30). Figure 15 shows an
example of a power-up phase with VIN = VIN MAX = 36 V whereIL TON > IL TOFF, so the
current escalates and the balance between Equation 30 and Equation 31 occurs at a current
slightly higher than the current limit. This must be taken into account in particular to avoid
the risk of an abrupt inductor saturation.
Figure 13. Short-circuit current VIN = 12 V
IL TON
VIN DCRL RDSON
+
 I
–
L
---------------------------------------------------------------- TON MIN

VIN
L
--------- 250ns

=
IL TOFF
VD Vout DCRL I
++

–
L
--------------------------------------------------------------- 3T
SW

VD Vout DCRL I
++

–
L
--------------------------------------------------------------- 12
s

=



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