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Page Title: (b) Plus and Minus 15 VDC Supply.
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Figure    1-24.    Resistance    Check    Circuit    (Simplified    Schematic)
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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 1-25. Power Flow Block Diagram

TM    55-4920-401-13&P resistance   check   circuit   (fig.   1-24)   and   the   heater probe  power  relay  (fig.  FO-1). (b)   Plus   and   Minus   15   VDC   Supply.   O ne of   the   37   vac   secondaries   of   T1   (fig.   1-25)   is   full- wave   rectified   by   diodes   CR5-CR8   on   the   switch- power   board   to   forma   positive   and   negative   supply. The   positive   supply   is   regulated   to   +15   vdc   by   Q1, Q2,  and  A1  and  filtered  by  C3.  The  +  input  of  Al  is referenced   to   8.95   vdc   generated   by   CR15.   The negative   supply   is   regulated   to   -15   vdc   by   Q3,   Q4, and  A2  and  filtered  by  C4.  The  +  input  of  A2  is  ref- erenced  to  ground. (c)   Display   Lamp   Supply.   On   the   switch- power   board   diodes   CR1   and   CR2   full-wave   rectify and  C9  filters  the  14  vac  winding  to  provide  a  5  vdc supply   to   excite   the   display   diodes.   The   circuitry   of A3   and   the   DISPLAY   control   convert   the   supply   to an   adjustable   square   wave   by   controlling   the   on-off time  of  series  regulator  Q15.  At  the  50%  duty  cycle, the  square  wave  frequency  is  800  Hz  +  20%.  When the  DISPLAY  control  wiper  is  at  the  +15  vdc  end the  display  is  full  on,  and  when  the  wiper  is  at  the  - 15  vdc  end  the  display  is  full  off. (d)   Logic   Voltage   Supply.   The   18.5   vac winding  of  T1  is  full-wave  rectified  by  CR3  and  CR4 cm  the  switch-power  board,  filtered  by  C5,  and  regu- lated  to  +5  vdc  by  Q5.  Q5  is  controlled  by  a  differ- ential  amplifier  consisting  of  Q8  and  Q9  and  by transistors   Q6   and   Q7.   The   differential   amplifier maintains   its   base   voltages   at   ground   potential.   As- sume  an  increase  in  the  base  voltage  of  Q9.  Addi- tional   current   from   Q9   flows   through   R13,   de- creasing   the   bias   on   Q8.   The   bias   on   Q7   increases, causing  the  bias  on  Q6  to  decrease.  The  base  of  Q5 becomes   more   positive,   decreasing   the   current through   Q5. (e)  Nine  VDC  Supply.  This   supply   is   lo- cated   on   the   probe   control   and   function   switch board.  It  is  powered  by  one-half  of  a  37  vac  winding which  is  half-wave  rectified  by  CR12  and  filtered  by C11.  CR13  regulates  the  dc  voltage  to  18  vdc  and CR14  regulates  it  to  9  vdc.  The  9  vdc  is  switched  by the   FUNCTION   SELECT   switch   to   power   the   air- craft   indicator   check   circuit   (figs.   1-18   and   1-19), the  PROBE  CONTROL  and  probe  control  compen- sator   (MOD-1,   fig.   FO-1),   and   the   insulation   check circuit   (fig.   1-23). (f)   Plus   and   Minus   7   VDC   Supply.   T h is supply,   on   the   calibrator   board   provides   an   isolated source  of  power  to  drive  the  %  rpm  calibrator  circuit and  the  wave-shaping  circuitry  of  A3  on  the  ta- chometer   board. (11)   Logic   Circuitry. (a)  Definition  of  Logic  Levels.  Standard positive   logic   is   used.   Logic   0  is   a   low   voltage (= 0.4  vdc)  and  is  said  to  be  “false”.  Logic  1  is  a high   voltage   (= 2.4  vdc)  and  is  said  to  be  “true”. The  logic  circuitry  excitation  voltage  is  +5  vdc. 1-25

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