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Page Title: CABIN AIR/WATER SEPARATOR, CO- ALESCER CONE, AND COALESCER BAG
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Refrigeration  package  and  water  separator
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Aviation Structural Mechanic E1&C - How airplanes are built and how to maintain them
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Nonicing  and  low-limit  control  modulating  valve  schematic

icing.  (See  figure  4-8.)  Ice  forming  on  the  wire screen  at  the  water  separator  discharge  duct  is detected  by  two  pneumatic  pickups  located  just before  and  after  the  water  separator.  These pickups  sense  a  differential  pressure  across  the water separator. If differential pressure is sensed across  the  water  separator,  the  nonice  and  low- limit  control  valve  will  remain  open  until  the temperature  of  the  inlet  air  to  the  water  separator is high enough to melt collected ice. When the ice is  melted,  the  pressure  differential  returns  to normal.  In  addition,  the  refrigeration  pack  low- limit  control  electrically  signals  the  nonice  and low-limit  control  valve  when  separator  outflow drops  to  0°F. REFRIGERATION  PACK  LOW-LIMIT CONTROL.—  The  refrigeration  pack  low-limit control   (fig.   4-6)   is   located   in   the   ECS compartment.  It  is  mounted  downstream  from  the water   separator   in   a   6-inch   duct   of   cooled discharged  bleed  air. The refrigeration pack low-limit control uses 28-volt  dc  power  to  energize  its  circuitry.  A thermistor  senses  duct  air  temperature  and compares it with an internally generated reference. The difference is amplified to modulate a torque motor in the nonice and low-limit control valve. (See  figure  4-8.)  The  torque  valve  controls  the regulated air supply (3) with a flapper valve (1), which  controls  the  diaphragm  pressure  in  a butterfly actuating linkage (12). The nonice and low-limit  control  valve  can  be  returned  to  the differential pressure control mode by opening the cabin temperature high-limit thermostat (4). This causes the upper chamber (6) of the switcher valve (7) to be vented (17) and returned to its primary position. A check valve (5) is provided to prevent extraneous signals from affecting the nonice and low-limit  control  valve. REFRIGERATION  UNIT  CHECK  VALVE.— The refrigeration unit check valve (fig. 4-7, detail A) is an insert-type check valve with a split flapper spring-loaded  in  the  closed  position.  The  valve, which  is  installed  in  the  refrigeration  unit  to prevent hot bleed air from entering directly into the turbine, is located in a tee arrangement in the system  just  downstream  of  an  orifice. Icing  of  the  water  separator  will  occur  only at  low  altitudes  where  mass  airflow  and  tempera- ture are relatively high. Only a small amount of high-temperature   air   is   required   through   the orifice to melt such a deposit. However, at high altitude  where  the  mass  flow  and  bleed-air temperatures are low, the refrigeration pack low- limit control operates to open the nonice and low- limit  control  valve.  When  the  nonice  and  low-limit control  valve  is  open,  high  differential  pressure across the bleed-air orifice permits the refrigera- tion   unit   check   valve   to   open.   This   allows intermediate-temperature   air   to   bypass   the turbine,  and  thereby  maintain  water  separator temperature  above  0°F.  (See  figure  4-6.) CABIN   AIR/WATER   SEPARATOR,   CO- ALESCER CONE, AND COALESCER BAG.— The  water  separator  is  a  welded  cylindrical aluminum  container  installed  downstream  from the  turbine  and  fan  assembly.  Its  purpose  is  to remove   a   portion   of   the   moisture   condensed during  the  air-expansion  process  within  the expansion  turbine.  (See  figure  4-6.)  The  water separator container holds a coalescer bag, which collects   the   finely   dispersed   fog-like   moisture discharged  from  the  turbine.  The  wet  air  flows through the coalescer cone and through louvered swirl  vanes  to  cause  the  heavier  water  particles  to be  deposited  by  centrifugal  force  against  the  outer surface   of   the   collector   section.   Accumulated water is drained through the sump in the bottom of  the  collector  section.  The  partially  dried  air then leaves the water separator by way of the air outlet  duct.  The  coalescer  bag  may  be  removed for  cleaning  through  an  access  cover  secured  with a  quick-disconnect  band  coupling  to  the  water separator shell. WATER SEPARATOR ICE SCREEN.— An ice screen is located in the discharge end of the water  separator  to  collect  ice  when  moisturized airflow  temperature  is  below  the  dew  point temperature,  or  below  32°F.  The  condensed  ice crystals  gathered  across  the  ice  screen  cause  a pressure differential, which is sensed by the nonice and low-limit control valve. The nonice and low- limit  control  valve  then  increases  the  warm  air supply  through  the  mixing  muff,  the  coalescer bag,  and  to  the  ice  screen  to  melt  collected ice. WATER SEPARATOR BYPASS VALVE.— The bypass valve is a spring-loaded valve mounted in the water separator container. A failure of the nonice and low-limit control valve could cause ice particles   to   build   up   in   the   water   separator coalescer bag. This ice would block the cabin air system. To ensure that air is supplied to the cabin, the water separator bypass valve allows turbine air  to  bypass  the  coalescer  bag. 4-12

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