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Page Title: Figure 1-20. Partial Schematic of Tach Converter.
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Figure   1-19.   Aircraft   Indicator   Check   Circuit   for   Null-Balanc   Indicators.
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TM-55-4920-401-13P Test Set Fuel Quantity Gage Capacity Type P/N 361 010 002 Manual
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Figure   1-21. %  RPM  Signal  Flow  Diagram.

TM   55-4920-401-13&P 1-17)   sets   the   temperature   to   which   heater   probes are   heated.   Eighteen   and   one-half   vac   from   a   sec- ondary   winding   of   transformer   T1   in   the   trimmer   is half-wave   rectified   by   CR12   on   the   probe   control and   function   switch   board.   This   rectified   voltage   is filtered   by   C11   and   C12   and   voltage   regulated   to   9 vdc  by  R27,  R28,  CR13,  and  CR14.  The  9  vdc  passes through   deck   3   of   the   FUNCTION   SELECT   switch when   it   is   in   HEATER   PROBE   position   and   excites the   PROBE   CONTROL   potentiometer.   Current from   the   PROBE   CONTROL   wiper   passes   through R19  and  R20  on  the  probe  control  circuit.  The  volt- age   developed   across   R20   represents   the   heater probe   set   temperature   and   is   applied   directly   to   the input   filter   of   the   temperature   indicator, (4)   %   RPM   Indicator.   The   following   is   a   de- scription  of  circuitry  that  is  unique  to  the  %  RPM indicator.   The   indicator   measures   the   rotational speed  (%  rpm)  of  the  low  pressure  (N1)  and  high pressure   (N2)   compressors.   The   selected   tachometer signal   is   applied   through   C17   and   R30   on   the   ta- chometer   board   to   the   inverting   input   of   amplifier A3.   Connected   to   the   noninverting   input   is   the   com- mon   signal   return.   Diodes   CR2   and   CR3   clamp   the input  signal  level  to  0.7  vdc.  The  output  of  A3  is  ad- justed   to   a   symmetrical   square   wave   by   R26.   Nega- tive   half-cycles   of   the   input   signal   cause   optical coupler  OC1  to  conduct  and  turn  on  Q13.  Plus  15  vdc from  Q13  turns  on  Q12  (fig.  1-20)  during  the  nega- tive   half-cycle.   During   the   positive   half-cycle,   Q13 turns   off   and   -15   vdc   through   R37   turns   on   Q11. When   Q12   turns   on,   C19   is   charged   by   +9   vdc through   two   precision   resistance   paths.   One   path contains   R47   and   the   other   path   contains   R48,   R49, and  R50.  When  Q12  turns  off  andQ11  turns  on,  C19 discharges   through   two   precision   resistance   paths. One  path  contains  R48  and  the  other  path  contains R47,  R49,  and  R50.  Since  resistors  R47  and  R48  are equal   (3.7K   ),   the   resistance   path   containing   R50 is   equal   for   both   charge   and   discharge   current.   Both the   charge   and   discharge   currents   develop   equal positive   pulses   across   resistor   R50.   These   pulses charge   filter   capacitors   C20   and   C21   at   the   input   of amplifier   A4.   The   gain   of   A4   is   adjusted   with   R44 and   R45   and   the   zero   calibration   point   is   adjusted with   R41   when   the   %   RPM   indicator   CAL   ADJ   pot is   set   to   the   center   of   its   range. Figure   1-20.   Partial   Schematic   of   Tach   Converter. 1-19

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