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R5973AD データシート(PDF) 27 Page - STMicroelectronics

部品番号 R5973AD
部品情報  Up to 1.5 A step-down switching regulator for aerospace applications
PDF  38 Pages
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メーカー  STMICROELECTRONICS [STMicroelectronics]
ホームページ  http://www.st.com
Logo STMICROELECTRONICS - STMicroelectronics

R5973AD データシート(HTML) 27 Page - STMicroelectronics

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R5973AD
Application information
38
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 15). 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 17 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 15. Short-circuit current VIN = 12 V
IL TOFF
VD Vout DCRL I
++

–
L
--------------------------------------------------------------- 3T
SW

VD Vout DCRL I
++

–
L
--------------------------------------------------------------- 6
s

=



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